DOC AIRBUS | AMM A320FAIDS - ENGINE REPORTS - DESCRIPTION AND OPERATION
** ON A/C NOT FOR ALL
1. General
The AIDS Reports are results of the related AIDS monitored aircraft systems (refer to the list below for the list of reports which are available). The reports can be requested manually or are started automatically. The monitor functions have fixed trigger mechanisms, fixed data collection and output formatting. Collected monitored-aircraft-data is automatically supplied to the related systems during unusual aircraft operation. If a report is requested manually with the remote print button, it is generated immediately (independently of any other start logic). The manually or automatically generated reports (stored in the SSMM) can be transferred to the printer and/or the MDDU, and/or the ACARS and/or the DAR/SAR. Some parameters for customer requirements are re-programmable through the MCDU or by GSE (For more information refer to 31-36-00).
The following Engine AIDS Reports are available:
** ON A/C NOT FOR ALL The AIDS Reports are results of the related AIDS monitored aircraft systems (refer to the list below for the list of reports which are available). The reports can be requested manually or are started automatically. The monitor functions have fixed trigger mechanisms, fixed data collection and output formatting. Collected monitored-aircraft-data is automatically supplied to the related systems during unusual aircraft operation. If a report is requested manually with the remote print button, it is generated immediately (independently of any other start logic). The manually or automatically generated reports (stored in the SSMM) can be transferred to the printer and/or the MDDU, and/or the ACARS and/or the DAR/SAR. Some parameters for customer requirements are re-programmable through the MCDU or by GSE (For more information refer to 31-36-00).
The following Engine AIDS Reports are available:
- <01> Engine Cruise Report,
- <02> Cruise Performance Report,
- <04> Engine Take-Off Report,
- <05> Engine On-Request Report,
- <06> Engine Gas Path Advisory Report,
- <07> Engine Mechanical Advisory Report,
- <09> Engine Divergence Report,
- <10> Engine Start Report,
- <11> Engine Run Up Report.
2. Reports
A. Engine Cruise Report <01>
Engine Cruise Report <01> (Engine Type CFMI with Advanced EVMU)
Engine Cruise Report <01> (Engine Type CFMI with Advanced EVMU)
Engine Cruise Report <01> (Engine Type CFMI with Advanced EVMU) ** ON A/C NOT FOR ALL
Engine Cruise Report <01> (Engine Type CFMI with Advanced EVMU) ** ON A/C NOT FOR ALL
The engine cruise report is a collection of aircraft and engine information averaged over a period of time in which both the engine and the aircraft met the appropriate stability criteria. The engine cruise report is generated when one of the logic conditions 1000 to 7000 (for details see engine cruise report logic) is present.
Engine Cruise Report <01> (Engine Type CFMI with Advanced EVMU) Engine Cruise Report <01> (Engine Type CFMI with Advanced EVMU) Engine Cruise Report <01> (Engine Type CFMI with Advanced EVMU) ** ON A/C NOT FOR ALL Engine Cruise Report <01> (Engine Type CFMI with Advanced EVMU) ** ON A/C NOT FOR ALL NOTE: For the standard header definition of the report refer to (Ref. AMM D/O 31-36-00-00).
(1) Engine Cruise Report Data Field Description <01> (Engine Type CFMI with Advanced EVMU)
NOTE: Reports that are transmitted from the ACARS system do not have report lines without a line identifier.
| +---------------------------------------------------------------------+ |
| ! Value ! Content Description ! |
| !--------------!------------------------------------------------------! |
| ! ESN ! Engine Serial Number ! |
| ! 999999 ! (000000 to 999999) ! |
| ! ! Eng 1 param. 7C.1.046.01 digit 3, 2, 1 ! |
| ! ! 7C.1.047.01 digit 6, 5, 4 ! |
| ! ! Eng 2 param. 7C.2.046.01 digit 3, 2, 1 ! |
| ! ! 7C.2.047.01 digit 6, 5, 4 ! |
| !--------------!------------------------------------------------------! |
| ! EHRS ! Engine Flight Hours ! |
| ! 99999 ! (00000 to 99999 hours) ! |
| ! ! DMU Engine 1 and Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! ERT ! Engine Running Time ! |
| ! 99999 ! (00000 to 65536 hours) ! |
| ! ! Eng 1 param. 7C.1.050.01 ! |
| ! ! Eng 2 param. 7C.2.050.10 ! |
| !--------------!------------------------------------------------------! |
| ! ECYC ! Engine Cycle ! |
| ! 99999 ! (00000 to 99999) ! |
| !--------------!------------------------------------------------------! |
| ! AP ! Auto Pilot Status ! |
| ! 99 ! (00 to G8) ! |
| ! ! FMGC 1 and 2 (FGC part) for Auto Pilot AP1 and AP2 ! |
| ! ! ! |
| ! ! XX Auto Pilot Modes: ! |
| ! ! !! ! |
| ! ! !!__Lateral Modes: 0 = NO MODE ! |
| ! ! ! 1 = HEADING ! |
| ! ! ! 2 = TRACK ! |
| ! ! ! 3 = NAV ! |
| ! ! ! 4 = LOC CAPTURE ! |
| ! ! ! 5 = LOC TRACK ! |
| ! ! ! 6 = LAND TRACK ! |
| ! ! ! 7 = RUNWAY ! |
| ! ! ! 8 = ROLL GO AROUND ! |
| ! ! ! ! |
| ! ! !__Longitudinal Modes: 0 = NO MODE ! |
| ! ! 1 = PITCH G/A ! |
| ! ! 2 = PITCH T/O ! |
| ! ! 3 = G/S TRACK ! |
| ! ! 4 = G/S CAPTURE ! |
| ! ! 5 = V/S ! |
| ! ! 6 = FPA ! |
| ! ! 7 = ALT ! |
| ! ! 8 = ALT ACQ ! |
| ! ! 9 = OPEN CLB ! |
| ! ! A = OPEN DES ! |
| ! ! B = IM CLB ! |
| ! ! C = IM DES ! |
| ! ! D = CLB ! |
| ! ! E = DES ! |
| ! ! F = FINAL DES ! |
| ! ! G = EXPEDITE ! |
| ! ! ! |
| ! ! AP1 ! AP2 ! |
| ! ! Report Line EC: ! Report Line EE: !Difinition: ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! / ! / !No Mode Act. ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.11 = 1 ! 01.2.275.00.11 = 1!RUNWAY Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.12 = 1 ! 01.2.275.00.12 = 1!NAV Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.13 = 1 ! 01.2.275.00.13 = 1!LOC CAPTURE ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.14 = 1 ! 01.2.275.00.14 = 1!LOC TRACK ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.15 = 1 ! 01.2.275.00.15 = 1!Roll GO ! |
| ! ! ! !AROUND Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.16 = 1 ! 01.2.275.00.16 = 1!HEADING Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.17 = 1 ! 01.2.275.00.17 = 1!TRACK Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.15 = 1 ! 01.2.274.00.15 = 1!PITCH TO Mode! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.16 = 1 ! 01.2.274.00.16 = 1!PITCH GA Mode! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.17 = 1 ! 01.2.274.00.17 = 1!V/S Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.18 = 1 ! 01.2.274.00.18 = 1!FPA Mode ! |
| ! ! -------------------!-------------------!-------------! |
| ! ! 01.1.274.00.19 = 1 ! 01.2.274.00.19 = 1!ALT Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.20 = 1 ! 01.2.274.00.20 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.19 = 1 ! 01.2.274.00.19 = 1!ALT ACQ ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.21 = 1 ! 01.2.274.00.21 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.20 = 1 ! 01.2.274.00.20 = 1!G/S TRACK ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.22 = 1 ! 01.2.274.00.22 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.21 = 1 ! 01.2.274.00.21 = 1!G/S CAPTURE ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.22 = 1 ! 01.2.274.00.22 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.23 = 1 ! 01.2.274.00.23 = 1!FINAL DES ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.2.274.00.24 = 1 ! 01.2.274.00.24 = 1!EXPED. Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.146.00.14 = 1 ! 01.2.146.00.14 = 1!LAND TRACK ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!CLB Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.13 = 0 ! 01.2.274.00.13 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.14 = 0 ! 01.2.274.00.14 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.24 = 0 ! 01.2.274.00.24 = 0! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!DES Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.13 = 0 ! 01.2.274.00.13 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.14 = 0 ! 01.2.274.00.14 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.24 = 0 ! 01.2.274.00.24 = 0! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!IM. CLIMB ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.13 = 1 ! 01.2.274.00.13 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!IM. DES Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.13 = 1 ! 01.2.274.00.13 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!OPEN CLB ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.14 = 1 ! 01.2.274.00.14 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!OPEN DES ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.14 = 1 ! 01.2.274.00.14 = 1! ! |
| ! ! ---------------------------------------------------- ! |
| ! ! Auto Pilot Status DMU: ! |
| ! ! AP1 printed in report line EC ! |
| ! ! AP2 printed in report line EE ! |
| !--------------!------------------------------------------------------! |
| ! QE ! Engine Quality Number, Report Stability ! |
| ! 99 ! (00 to 99) ! |
| !--------------!------------------------------------------------------! |
| ! N1 ! Selected N1 Actual ! |
| ! 9999 ! (0 to 120.0 %rpm) ! |
| ! ! Eng 1 param. 7C.1.346.01 ! |
| ! ! Eng 2 param. 7C.2.346.10 ! |
| !--------------!------------------------------------------------------! |
| ! N1C ! N1 Command ! |
| ! 9999 ! (0 to 120.0 %rpm) ! |
| ! ! Eng 1 param. 7C.1.341.01 ! |
| ! ! Eng 2 param. 7C.2.341.10 ! |
| !--------------!------------------------------------------------------! |
| ! N2 ! Selected N2 Actual ! |
| ! 9999 ! (0 to 120.0 %rpm) ! |
| ! ! Eng 1 param. 7C.1.344.01 ! |
| ! ! Eng 2 param. 7C.2.344.10 ! |
| !--------------!------------------------------------------------------! |
| ! EGT ! Selected T494 (Exhaust Gas Temperature) ! |
| ! X999 ! (-55 to 999.9 C) ! |
| ! ! Eng 1 param. 7C.1.345.01 ! |
| ! ! Eng 2 param. 7C.2.345.10 ! |
| !--------------!------------------------------------------------------! |
| ! FF ! Engine Fuel Flow ! |
| ! 9999 ! ( 0 to 7000 kg/h) ! |
| ! ! Eng 1 param. 7C.1.244.01 ! |
| ! ! Eng 2 param. 7C.2.244.10 ! |
| !--------------!------------------------------------------------------! |
| ! PS13 ! PS13 Static Air Pressure at Position 1.3 ! |
| ! 99999 ! (0.0 to 30.000 psia) ! |
| ! ! Eng 1 param. 7C.1.127.01 ! |
| ! ! Eng 2 param. 7C.2.127.10 ! |
| !--------------!------------------------------------------------------! |
| ! P25 ! Total Air Pressure at Position 2.5 ! |
| ! 99999 ! (0.0 to 50.000 psia) ! |
| ! ! Eng 1 param. 7C.1.262.01 ! |
| ! ! Eng 2 param. 7C.2.262.10 ! |
| !--------------!------------------------------------------------------! |
| ! T25 ! Selected T25 ! |
| ! X999 ! (-55.0 to 120.0 C) ! |
| ! ! Eng 1 param. 7C.1.263.01 ! |
| ! ! Eng 2 param. 7C.2.263.10 ! |
| !--------------!------------------------------------------------------! |
| ! P3 ! Selected PS3 ! |
| ! 9999 ! (0.0 to 450.0 psia) ! |
| ! ! Eng 1 param. 7C.1.264.01 ! |
| ! ! Eng 2 param. 7C.2.264.10 ! |
| !--------------!------------------------------------------------------! |
| ! T3 ! Temperature at Position 3 ! |
| ! X999 ! (-55.0 to 850.0 C) ! |
| ! ! Eng 1 param. 7C.1.265.01 ! |
| ! ! Eng 2 param. 7C.2.265.10 ! |
| !--------------!------------------------------------------------------! |
| ! T5 ! Temperature at Position 5 ! |
| ! X999 ! (-55.0 to 850.0 C) ! |
| ! ! Eng 1 param. 7C.1.260.01 ! |
| ! ! Eng 2 param. 7C.2.260.10 ! |
| !--------------!------------------------------------------------------! |
| ! VSV ! Variable Statore Vane Position ! |
| ! X99 ! (-5.0 to 45.0 deg) ! |
| ! ! Eng 1 param. 7C.1.072.01 ! |
| ! ! Eng 2 param. 7C.2.072.10 ! |
| !--------------!------------------------------------------------------! |
| ! VBV ! Variable Bleed Valve Position ! |
| ! X99 ! (-9.9 to 40.0 deg) ! |
| ! ! Eng 1 param. 7C.1.071.01 ! |
| ! ! Eng 2 param. 7C.2.071.10 ! |
| !--------------!------------------------------------------------------! |
| ! HPT ! High-Pressure Turbine Clearance Position ! |
| ! X99 ! (-10 to 100 %) ! |
| ! ! Eng 1 param. 7C.1.306.01 ! |
| ! ! Eng 2 param. 7C.2.306.10 ! |
| !--------------!------------------------------------------------------! |
| ! LPT ! Selected LPTC Posiiton ! |
| ! X99 ! (-10 to 100 %) ! |
| ! ! Eng 1 param. 7C.1.307.01 ! |
| ! ! Eng 2 param. 7C.2.307.10 ! |
| !--------------!------------------------------------------------------! |
| ! GLE ! Engine Generator Load ! |
| ! 999 ! (0 to 100%) ! |
| ! ! Eng 1 param. 29.1.077.01 ! |
| ! ! 29.2.077.01 ! |
| ! ! Eng 2 param. 29.1.077.10 ! |
| ! ! 29.2.077.10 ! |
| !--------------!------------------------------------------------------! |
| ! PD ! Precooler Inlet Pressure ! |
| ! 99 ! (0 to 50 psi) ! |
| ! ! Eng 1 param. 06F.1.143.01 ! |
| ! ! 06F.1.143.10 ! |
| ! ! Eng 2 param. 06F.2.142.10 ! |
| ! ! 06F.2.142.01 ! |
| !--------------!------------------------------------------------------! |
| ! TN ! Nacelle Temperature ! |
| ! X99 ! (-55 to 300 C) ! |
| ! ! Eng 1 param. 26.1.322.01 ! |
| ! ! 26.2.322.01 ! |
| ! ! Eng 2 param. 26.1.322.10 ! |
| ! ! 26.2.322.10 ! |
| !--------------!------------------------------------------------------! |
| ! PT2 ! Total Air Pressure at Position 2 ! |
| ! 99999 ! (o.o to 25.000 psia) ! |
| ! ! Eng 1 param. 7C.1.131.01 ! |
| ! ! Eng 2 param. 7C.2.131.10 ! |
| !--------------!------------------------------------------------------! |
| ! OIQH ! Oil Consumption from the previous flight ! |
| ! X999 ! (-9.99 to 20.00 qts/h) ! |
| !--------------!------------------------------------------------------! |
| ! VN ! FAN Pick Up N1 Track Vibration ! |
| ! 99 ! (0.0 to 10.0) ! |
| ! ! Eng 1 param. 3D.1.227.01 ! |
| ! ! Eng 2 param. 3D.1.227.10 ! |
| !--------------!------------------------------------------------------! |
| ! VL ! TRF Pick Up N1 Vibration ! |
| ! 99 ! (0.0 to 10.0) ! |
| ! ! Eng 1 param. 3D.1.227.11 ! |
| ! ! Eng 2 param. 3D.1.227.00 ! |
| !--------------!------------------------------------------------------! |
| ! PHA ! FAN Pick Up Phase Angle ! |
| ! 999 ! (0 to 360 deg) ! |
| ! ! Eng 1 param. 3D.1.226.11 ! |
| ! ! Eng 2 param. 3D.1.226.00 ! |
| !--------------!------------------------------------------------------! |
| ! PHT ! TRF Pick Up Phase Angle ! |
| ! 999 ! (0 to 360 deg) ! |
| ! ! Eng 1 param. 3D.1.226.11 ! |
| ! ! Eng 2 param. 3D.1.226.00 ! |
| !--------------!------------------------------------------------------! |
| ! VC ! FAN Pick Up N2 Track Vibration ! |
| ! 99 ! (0.0 to 4.0) ! |
| ! ! Eng 1 param. 3D.1.230.01 ! |
| ! ! Eng 2 param. 3D.1.230.10 ! |
| !--------------!------------------------------------------------------! |
| ! VH ! TRF Pick Up N2 Track Vibration ! |
| ! 99 ! (0.0 to 4.0) ! |
| ! ! Eng 1 param. 3D.1.230.11 ! |
| ! ! Eng 2 param. 3D.1.230.00 ! |
| !--------------!------------------------------------------------------! |
| ! EVM ! Engine Vibration Status Word ! |
| ! XXXXX ! Eng 1 param. 3D.1.035.01 ! |
| ! ! Eng 2 param. 3D.1.035.10 ! |
| !--------------!------------------------------------------------------! |
| ! OIP ! Engine Oil Pressure ! |
| ! 999 ! (0 to 400 psia) ! |
| ! ! Eng 1 param. 26.1.317.01 ! |
| ! ! 26.2.317.01 ! |
| ! ! Eng 2 param. 26.1.317.10 ! |
| ! ! 26.2.317.10 ! |
| !--------------!------------------------------------------------------! |
| ! OIT ! Engine Oil Temperature ! |
| ! X99 ! (-60 to 250 C) ! |
| ! ! Eng 1 param. 26.1.316.01 ! |
| ! ! 26.2.316.01 ! |
| ! ! Eng 2 param. 26.1.316.10 ! |
| ! ! 26.2.316.10 ! |
| !--------------!------------------------------------------------------! |
| ! ECW1 ! Engine Control Word 1 ! |
| ! XXXXX ! Bit Label Parameter Description ! |
| ! ! 11 7C.X.272.XX.19 = 1 Auto Thrust Active ! |
| ! ! 12 7C.X.272.XX.20 = 1 VSV Position Fault ! |
| ! ! 13 SPARE ! |
| ! ! 14 SPARE ! |
| ! ! 15 7C.X.351.XX.29 = 1 Fuel Flow Measurement ! |
| ! ! Invalid ! |
| ! ! 16 7C.X.275.XX.15 = 1 N1/N2 Control ACtive ! |
| ! ! 17 7C.X.275.XX.26 = 1 Channel A Active ! |
| ! ! 18 7C.X.275.XX.27 = 1 Channel B Active ! |
| ! ! 19 SPARE ! |
| ! ! 20 SPARE ! |
| ! ! 21 SPARE ! |
| ! ! 22 SPARE ! |
| ! ! 23 SPARE ! |
| ! ! 24 SPARE ! |
| ! ! 25 SPARE ! |
| ! ! 26 SPARE ! |
| ! ! 27 SPARE ! |
| ! ! 28 SPARE ! |
| ! ! 29 SPARE ! |
| !--------------!------------------------------------------------------! |
| ! SSEL ! Engine Control Word 1 ! |
| ! XXXXXXX ! Status of different FADEC sensors ! |
| ! XXXXXXX ! XXXXXXXXXXXXXX Label: Selected: Bit 11 --> 15) ! |
| ! ! IIIIIIIIIIIIII__ 346 N1 actual ! |
| ! ! IIIIIIIIIIIII___ 345 EGT ! |
| ! ! IIIIIIIIIIII____ 344 N2 actual ! |
| ! ! IIIIIIIIIII_____ 263 T25 ! |
| ! ! IIIIIIIIII______ 264 PS3 ! |
| ! ! IIIIIIIII_______ 265 T3 ! |
| ! ! IIIIIIII________ 072 VSV Position ! |
| ! ! IIIIIII_________ 071 VBV Position ! |
| ! ! IIIIII__________ 306 HPTC Position ! |
| ! ! IIIII___________ 307 LPTC Position ! |
| ! ! IIII____________ 347 FMV Position ! |
| ! ! III_____________ 211 TAT ! |
| ! ! II______________ 114 P0 ! |
| ! ! I_______________ 133 TLA Position ! |
| ! ! (All labels Bit 11 --> 15) ! |
| ! ! Source: ECU, different labels ! |
| ! ! The indicated values shall be coded as follows: ! |
| ! ! Bit: 15 14 13 12 11 ! indicated value ! |
| ! ! --------------------!---------------- ! |
| ! ! 0 0 0 0 0 ! 0 ! |
| ! ! 0 0 0 0 1 ! 1 ! |
| ! ! 0 0 0 1 0 ! 2 ! |
| ! ! 0 0 0 1 1 ! 3 ! |
| ! ! 0 0 1 0 0 ! 4 ! |
| ! ! 0 0 1 0 1 ! 5 ! |
| ! ! 0 0 1 1 0 ! 6 ! |
| ! ! 0 0 1 1 1 ! 7 ! |
| ! ! 0 1 0 0 0 ! 8 ! |
| ! ! 0 1 0 0 1 ! 9 ! |
| ! ! 0 1 0 1 0 ! A ! |
| ! ! 0 1 0 1 1 ! B ! |
| ! ! 0 1 1 0 0 ! C ! |
| ! ! 0 1 1 0 1 ! D ! |
| ! ! 0 1 1 1 0 ! E ! |
| ! ! 0 1 1 1 1 ! F ! |
| ! ! 1 0 0 0 0 ! G ! |
| ! ! 1 0 0 0 1 ! H ! |
| ! ! 1 0 0 1 0 ! I ! |
| ! ! 1 0 0 1 1 ! J ! |
| ! ! 1 0 1 0 0 ! K ! |
| ! ! 1 0 1 0 1 ! L ! |
| ! ! 1 0 1 1 0 ! M ! |
| ! ! 1 0 1 1 1 ! N ! |
| ! ! 1 1 0 0 0 ! O ! |
| ! ! 1 1 0 0 1 ! P ! |
| ! ! 1 1 0 1 0 ! Q ! |
| ! ! 1 1 0 1 1 ! R ! |
| ! ! 1 1 1 0 0 ! S ! |
| ! ! 1 1 1 0 1 ! T ! |
| ! ! 1 1 1 1 0 ! U ! |
| ! ! 1 1 1 1 1 ! V ! |
| ! ! ! |
| +---------------------------------------------------------------------+ |
(2) Engine Cruise Report Data Field Description <01> (Engine Type CFMI with Advanced EVMU)
NOTE: Reports that are transmitted from the ACARS system do not have report lines without a line identifier.
| +---------------------------------------------------------------------+ |
| ! Value ! Content Description ! |
| !--------------!------------------------------------------------------! |
| ! ESN ! Engine Serial Number ! |
| ! 999999 ! (000000 to 999999) ! |
| ! ! ECU Engine 1 7C.1.046.01 digit 3, 2, 1 ! |
| ! ! 7C.1.047.01 digit 6, 5, 4 ! |
| ! ! Engine 2 7C.2.046.10 digit 3, 2, 1 ! |
| ! ! 7C.2.047.10 digit 6, 5, 4 ! |
| !--------------!------------------------------------------------------! |
| ! EHRS ! Engine Flight Hours ! |
| ! 99999 ! (00000 to 99999 hours) ! |
| ! ! DMU Engine 1 and Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! ERT ! Engine Running Time ! |
| ! 99999 ! (00000 to 65536 hours) ! |
| ! ! ECU 7C.1.050.01 Engine 1 ! |
| ! ! 7C.2.050.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! ECYC ! Engine Cycle ! |
| ! 99999 ! (00000 to 99999) ! |
| ! ! DMU Engine 1 ! |
| ! ! Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! AP ! Auto Pilot Status ! |
| ! 99 ! Number of respective status (00 to G8) ! |
| ! ! FMGC 1 and 2 (FGC part) for Auto Pilot AP1 and AP2 ! |
| ! ! ! |
| ! ! XX Auto Pilot Modes: ! |
| ! ! !! ! |
| ! ! !!__Lateral Modes: 0 = NO MODE ! |
| ! ! ! 1 = HEADING ! |
| ! ! ! 2 = TRACK ! |
| ! ! ! 3 = NAV ! |
| ! ! ! 4 = LOC CAPTURE ! |
| ! ! ! 5 = LOCK TRACK ! |
| ! ! ! 6 = LAND TRACK ! |
| ! ! ! 7 = RUNWAY ! |
| ! ! ! 8 = ROLL GO AROUND ! |
| ! ! ! ! |
| ! ! !__Longitudinal Modes: 0 = NO MODE ! |
| ! ! 1 = PITCH G/A ! |
| ! ! 2 = PITCH TO ! |
| ! ! 3 = G/S TRACK ! |
| ! ! 4 = G/S CAPTURE ! |
| ! ! 5 = V/S ! |
| ! ! 6 = FPA ! |
| ! ! 7 = ALT ! |
| ! ! 8 = ALT ACQ ! |
| ! ! 9 = OPEN CLB ! |
| ! ! A = OPEN DES ! |
| ! ! B = IM CLB ! |
| ! ! C = IM DES ! |
| ! ! D = CLB ! |
| ! ! E = DES ! |
| ! ! F = FINAL DES ! |
| ! ! G = EXPEDITE ! |
| ! ! ! |
| ! ! Parameter for AP1 ! Parameter for AP2 ! |
| ! ! Report Line EC: ! Report Line EE: !Definition: ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! / ! / !No Mode Act. ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.11 = 1 ! 01.2.275.00.11 = 1!RUNWAY Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.12 = 1 ! 01.2.275.00.12 = 1!NAV Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.13 = 1 ! 01.2.275.00.13 = 1!LOC CAPTURE ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.14 = 1 ! 01.2.275.00.14 = 1!LOC TRACK ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.15 = 1 ! 01.2.275.00.15 = 1!Roll GO ! |
| ! ! ! !AROUND Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.16 = 1 ! 01.2.275.00.16 = 1!HEADING Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.17 = 1 ! 01.2.275.00.17 = 1!TRACK Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.15 = 1 ! 01.2.274.00.15 = 1!PITCH T/O ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.16 = 1 ! 01.2.274.00.16 = 1!PITCH GA Mode! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.17 = 1 ! 01.2.274.00.17 = 1!V/S Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.18 = 1 ! 01.2.274.00.18 = 1!FPA Mode ! |
| ! ! -------------------!-------------------!-------------! |
| ! ! 01.1.274.00.19 = 1 ! 01.2.274.00.19 = 1!ALT Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.20 = 1 ! 01.2.274.00.20 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.19 = 1 ! 01.2.274.00.19 = 1!ALT ACQ ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.21 = 1 ! 01.2.274.00.21 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.20 = 1 ! 01.2.274.00.20 = 1!G/S TRACK ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.22 = 1 ! 01.2.274.00.22 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.21 = 1 ! 01.2.274.00.21 = 1!G/S CAPTURE ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.22 = 1 ! 01.2.274.00.22 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.23 = 1 ! 01.2.274.00.23 = 1!FINAL DES ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.24 = 1 ! 01.2.274.00.24 = 1!EXPED. Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.146.00.14 = 1 ! 01.2.146.00.14 = 1!LAND TRACK ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!CLB Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.13 = 0 ! 01.2.274.00.13 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.14 = 0 ! 01.2.274.00.14 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.24 = 0 ! 01.2.274.00.24 = 0! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!DES Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.13 = 0 ! 01.2.274.00.13 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.14 = 0 ! 01.2.274.00.14 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.24 = 0 ! 01.2.274.00.24 = 0! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!IM. CLIMB ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.13 = 1 ! 01.2.274.00.13 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!IM. DES Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.13 = 1 ! 01.2.274.00.13 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!OPEN CLB ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.14 = 1 ! 01.2.274.00.14 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!OPEN. DES ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.14 = 1 ! 01.2.274.00.14 = 1! ! |
| ! ! ---------------------------------------------------- ! |
| ! ! Auto Pilot Status DMU: ! |
| ! ! Auto Pilot AP1 printed in report line EC ! |
| ! ! Auto Pilot AP2 printed in report line EE ! |
| !--------------!------------------------------------------------------! |
| ! QE ! Engine Quality Number, Report Stability ! |
| ! 99 ! (00 to 99) ! |
| ! ! DMU ! |
| !--------------!------------------------------------------------------! |
| ! N1 ! Selected N1 Actual ! |
| ! 9999 ! (0 to 120.0 %rpm) ! |
| ! ! ECU 7C.1.346.01 Engine 1 ! |
| ! ! 7C.2.346.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! N1C ! N1 Command ! |
| ! 9999 ! (0 to 120.0 %rpm) ! |
| ! ! ECU 7C.1.341.01 Engine 1 ! |
| ! ! 7C.1.341.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! N2 ! Selected N2 Actual ! |
| ! 9999 ! (0 to 120.0 %rpm) ! |
| ! ! ECU 7C.1.344.01 Engine 1 ! |
| ! ! 7C.2.344.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! EGT ! Selected T495 (Exhaust Gas Temperature) ! |
| ! X999 ! (-55 to 999.9 [C) ! |
| ! ! NOTE: Negative values are shown with an N in the ! |
| ! ! first position. If there are no negative ! |
| ! ! values then the value starts at the first ! |
| ! ! position. ! |
| ! ! ECU 7C.1.345.01 Engine 1 ! |
| ! ! 7C.2.345.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! FF ! Engine Fuel Flow (0 to 15000 p/h) ! |
| ! 9999 ! 0 to 7000 kg/h (0 to 15000 p/h) ! |
| ! ! ECU 7C.1.244.01 Engine 1 ! |
| ! ! 7C.2.244.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! PS13 ! PS13 Static Air Pressure at Position 1.3 ! |
| ! 99999 ! (0.0 to 30.000 psia) ! |
| ! ! ECU 7C.1.127.01 Engine 1 ! |
| ! ! 7C.2.127.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! P25 ! P25 Total Air Pressure at Position 2.5 ! |
| ! 99999 ! (0.0 to 50.000 psia) ! |
| ! ! ECU 7C.1.262.01 Engine 1 ! |
| ! ! 7C.2.262.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! T25 ! Selected T25 ! |
| ! X999 ! (-55.0 to 120.0 [C) ! |
| ! ! NOTE: Negative values are shown with an N in the ! |
| ! ! first position. If there are no negative ! |
| ! ! values then the value starts at the first ! |
| ! ! position. ! |
| ! ! ECU 7C.1.263.01 Engine 1 ! |
| ! ! 7C.2.263.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! P3 ! Selected PS3 ! |
| ! 9999 ! (0.0 to 450.0 psia) ! |
| ! ! ECU 7C.1.264.01 Engine 1 ! |
| ! ! 7C.2.264.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! T3 ! Selected T3 ! |
| ! X999 ! (-55.0 to 850.0 [C) ! |
| ! ! NOTE: Negative values are shown with an N in the ! |
| ! ! first position. If there are no negative ! |
| ! ! values then the value starts at the first ! |
| ! ! position. ! |
| ! ! ECU 7C.1.265.01 Engine 1 ! |
| ! ! 7C.2.265.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! T5 ! Selected T5 ! |
| ! X999 ! (-55.0 to 850.0 [C) ! |
| ! ! NOTE: Negative values are shown with an N in the ! |
| ! ! first position. If there are no negative ! |
| ! ! values then the value starts at the first ! |
| ! ! position. ! |
| ! ! ECU 7C.1.260.01 Engine 1 ! |
| ! ! 7C.2.260.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! VSV ! Selected Variable Statore Vane Position ! |
| ! X99 ! (-5.0 to 45.0 deg) ! |
| ! ! NOTE: Negative values are shown with an N in the ! |
| ! ! first position. If there are no negative ! |
| ! ! values then the value starts at the first ! |
| ! ! position. ! |
| ! ! ECU 7C.1.072.01 Engine 1 ! |
| ! ! 7C.2.072.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! VBV ! Variable Bleed Valve Position ! |
| ! X99 ! (-9.9 to 40.0 deg) ! |
| ! ! NOTE: Negative values are shown with an N in the ! |
| ! ! first position. If there are no negative ! |
| ! ! values then the value starts at the first ! |
| ! ! position. ! |
| ! ! ECU 7C.1.071.01 Engine 1 ! |
| ! ! 7C.2.071.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! HPT ! Selected High-Pressure Turbine Clearance Position ! |
| ! X99 ! (-10 to 100 %) ! |
| ! ! ECU 7C.1.306.01 Engine 1 ! |
| ! ! 7C.2.306.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! LPT ! Selected LPTC Posiiton ! |
| ! X99 ! (-10 to 100 %) ! |
| ! ! ECU 7C.1.307.01 Engine 1 ! |
| ! ! 7C.2.307.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! GLE ! Engine Generator Load ! |
| ! 999 ! (0 to 100%) ! |
| ! ! SDAC 29.1.077.01 Engine 1 ! |
| ! ! 29.2.077.01 ! |
| ! ! 29.1.077.10 Engine 2 ! |
| ! ! 29.2.077.10 ! |
| !--------------!------------------------------------------------------! |
| ! PD ! Precooler Inlet Pressure ! |
| ! 99 ! (0 to 50 psi) ! |
| ! ! BMC 06F.1.143.01 Engine 1 ! |
| ! ! 06F.2.143.01 ! |
| ! ! 06F.1.142.01 Engine 2 ! |
| ! ! 06F.2.142.10 ! |
| !--------------!------------------------------------------------------! |
| ! TN ! Nacelle Temperature ! |
| ! X99 ! (-55 to 300 [C) ! |
| ! ! NOTE: Negative values are shown with an N in the ! |
| ! ! first position. If there are no negative ! |
| ! ! values then the value starts at the first ! |
| ! ! position. ! |
| ! ! FWC 26.1.322.01 Engine 1 ! |
| ! ! 26.2.322.01 ! |
| ! ! 26.1.322.10 Engine 2 ! |
| ! ! 26.2.322.10 ! |
| !--------------!------------------------------------------------------! |
| ! PT2 ! PT2 Total Air Pressure at Position 2 ! |
| ! 99999 ! (0.0 to 25.000 psia) ! |
| ! ! ECU 7C.1.131.01 Engine 1 ! |
| ! ! 7C.2.131.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! OIQH ! Oil Consumption from the previous flight ! |
| ! X999 ! (-9.99 to 20.00 qts/h) ! |
| ! ! DMU Engine 1 ! |
| ! ! Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! VN ! FAN Pick Up N1 Track Vibration ! |
| ! 99 ! (0.0 to 10.0) ! |
| ! ! EVM 3D.1.227.01 Engine 1 ! |
| ! ! 3D.1.227.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! VL ! TRF Pick Up N1 Vibration ! |
| ! 99 ! (0.0 to 10.0) If value is 10.0 then 99 is printed. ! |
| ! ! EVM 3D.1.227.11 Engine 1 ! |
| ! ! 3D.1.227.00 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! PHA ! FAN Pick Up Phase Angle ! |
| ! 999 ! (0 to 360 deg) ! |
| ! ! EVM 3D.1.226.01 Engine 1 ! |
| ! ! 3D.1.226.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! PHT ! TRF Pick Up Phase Angle ! |
| ! 999 ! (0 to 360 deg) ! |
| ! ! EVM 3D.1.226.11 Engine 1 ! |
| ! ! 3D.1.226.00 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! VC ! FAN Pick Up N2 Track Vibration ! |
| ! 99 ! (0.0 to 4.0) ! |
| ! ! EVM 3D.1.230.01 Engine 1 ! |
| ! ! 3D.1.230.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! VH ! TRF Pick Up N2 Track Vibration ! |
| ! 99 ! (0.0 to 4.0) ! |
| ! ! EVM 3D.1.230.11 Engine 1 ! |
| ! ! 3D.1.230.00 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! EVM ! Engine Vibration Status Word ! |
| ! XXXXX ! EVM 3D.1.035.01 Engine 1 ! |
| ! ! 3D.1.035.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! OIP ! Engine Oil Pressure ! |
| ! 999 ! (0 to 400 psia) ! |
| ! ! FWC 26.1.317.01 Engine 1 ! |
| ! ! 26.2.317.01 Engine 2 ! |
| ! ! 26.1.317.10 Engine 1 ! |
| ! ! 26.2.317.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! OIT ! Engine Oil Temperature ! |
| ! X99 ! (-60 to 250 C) ! |
| ! ! FWC 26.1.316.01 Engine 1 ! |
| ! ! 26.2.316.01 Engine 2 ! |
| ! ! 26.1.316.10 Engine 1 ! |
| ! ! 26.2.316.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! ECW1 ! Engine Control Word 1 ! |
| ! XXXXX ! Bit Label Parameter Description ! |
| ! ! 11 7C.X.272.XX.19 = 1 Auto Thrust Active ! |
| ! ! 12 7C.X.275.XX.20 = 1 VSV Position Fault ! |
| ! ! 13 SPARE ! |
| ! ! 14 SPARE ! |
| ! ! 15 7C.X.351.XX.29 = 1 Fuel Flow Measurement ! |
| ! ! Invalid ! |
| ! ! 16 7C.X.275.XX.15 = 1 N1/N2 Control Active ! |
| ! ! 17 7C.X.275.XX.26 = 1 Channel A Active ! |
| ! ! 18 7C.X.275.XX.27 = 1 Channel B Active ! |
| ! ! 19 SPARE ! |
| ! ! 20 SPARE ! |
| ! ! 21 SPARE ! |
| ! ! 22 SPARE ! |
| ! ! 23 SPARE ! |
| ! ! 24 SPARE ! |
| ! ! 25 SPARE ! |
| ! ! 26 SPARE ! |
| ! ! 27 SPARE ! |
| ! ! 28 SPARE ! |
| ! ! 29 SPARE ! |
| !--------------!------------------------------------------------------! |
| ! SSEL ! Engine Control Word 1 ! |
| ! XXXXXXX ! Status of different FADEC sensors ! |
| ! XXXXXXX ! XXXXXXXXXXXXXX Label: Selected: Bit 11 --> 15) ! |
| ! ! IIIIIIIIIIIIII__ 346 N1 actual ! |
| ! ! IIIIIIIIIIIII___ 345 EGT ! |
| ! ! IIIIIIIIIIII____ 344 N2 actual ! |
| ! ! IIIIIIIIIII_____ 263 T25 ! |
| ! ! IIIIIIIIII______ 264 PS3 ! |
| ! ! IIIIIIIII_______ 265 T3 ! |
| ! ! IIIIIIII________ 072 VSV Position ! |
| ! ! IIIIIII_________ 071 VBV Position ! |
| ! ! IIIIII__________ 306 HPTC Position ! |
| ! ! IIIII___________ 307 LPTH Position ! |
| ! ! IIII____________ 347 FMV Position ! |
| ! ! III_____________ 211 TAT ! |
| ! ! II______________ 114 P0 ! |
| ! ! I_______________ 133 TLA Position ! |
| ! ! (All labels Bit 11 --> 15) ! |
| ! ! Source: ECU, different labels ! |
| ! ! The indicated values shall be coded as follows: ! |
| ! ! Bit: 15 14 13 12 11 ! indicated value ! |
| ! ! --------------------!---------------- ! |
| ! ! 0 0 0 0 0 ! 0 ! |
| ! ! 0 0 0 0 1 ! 1 ! |
| ! ! 0 0 0 1 0 ! 2 ! |
| ! ! 0 0 0 1 1 ! 3 ! |
| ! ! 0 0 1 0 0 ! 4 ! |
| ! ! 0 0 1 0 1 ! 5 ! |
| ! ! 0 0 1 1 0 ! 6 ! |
| ! ! 0 0 1 1 1 ! 7 ! |
| ! ! 0 1 0 0 0 ! 8 ! |
| ! ! 0 1 0 0 1 ! 9 ! |
| ! ! 0 1 0 1 0 ! A ! |
| ! ! 0 1 0 1 1 ! B ! |
| ! ! 0 1 1 0 0 ! C ! |
| ! ! 0 1 1 0 1 ! D ! |
| ! ! 0 1 1 1 0 ! E ! |
| ! ! 0 1 1 1 1 ! F ! |
| ! ! 1 0 0 0 0 ! G ! |
| ! ! 1 0 0 0 1 ! H ! |
| ! ! 1 0 0 1 0 ! I ! |
| ! ! 1 0 0 1 1 ! J ! |
| ! ! 1 0 1 0 0 ! K ! |
| ! ! 1 0 1 0 1 ! L ! |
| ! ! 1 0 1 1 0 ! M ! |
| ! ! 1 0 1 1 1 ! N ! |
| ! ! 1 1 0 0 0 ! O ! |
| ! ! 1 1 0 0 1 ! P ! |
| ! ! 1 1 0 1 0 ! Q ! |
| ! ! 1 1 0 1 1 ! R ! |
| ! ! 1 1 1 0 0 ! S ! |
| ! ! 1 1 1 0 1 ! T ! |
| ! ! 1 1 1 1 0 ! U ! |
| ! ! 1 1 1 1 1 ! V ! |
| ! ! ! |
| +---------------------------------------------------------------------+ |
(3) Engine Cruise Report Data Field Description <01> (Engine Type CFMI with Advanced EVMU)
NOTE: Reports that are transmitted from the ACARS system do not have report lines without a line identifier.
| +---------------------------------------------------------------------+ |
| ! Value ! Content Description ! |
| !--------------!------------------------------------------------------! |
| ! ESN ! Engine Serial Number ! |
| ! 999999 ! (000000 to 999999) ! |
| ! ! ECU Engine 1 7C.1.046.01 digit 3, 2, 1 ! |
| ! ! 7C.1.047.01 digit 6, 5, 4 ! |
| ! ! Engine 2 7C.2.046.10 digit 3, 2, 1 ! |
| ! ! 7C.2.047.10 digit 6, 5, 4 ! |
| !--------------!------------------------------------------------------! |
| ! EHRS ! Engine Flight Hours ! |
| ! 99999 ! (00000 to 99999 hours) ! |
| ! ! DMU Engine 1 and Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! ERT ! Engine Running Time ! |
| ! 99999 ! (00000 to 65536 hours) ! |
| ! ! ECU 7C.1.050.01 Engine 1 ! |
| ! ! 7C.2.050.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! ECYC ! Engine Cycle ! |
| ! 99999 ! (00000 to 99999) ! |
| ! ! DMU Engine 1 ! |
| ! ! Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! AP ! Auto Pilot Status ! |
| ! 99 ! Number of respective status (00 to G8) ! |
| ! ! FMGC 1 and 2 (FGC part) for Auto Pilot AP1 and AP2 ! |
| ! ! ! |
| ! ! XX Auto Pilot Modes: ! |
| ! ! !! ! |
| ! ! !!__Lateral Modes: 0 = NO MODE ! |
| ! ! ! 1 = HEADING ! |
| ! ! ! 2 = TRACK ! |
| ! ! ! 3 = NAV ! |
| ! ! ! 4 = LOC CAPTURE ! |
| ! ! ! 5 = LOCK TRACK ! |
| ! ! ! 6 = LAND TRACK ! |
| ! ! ! 7 = RUNWAY ! |
| ! ! ! 8 = ROLL GO AROUND ! |
| ! ! ! ! |
| ! ! !__Longitudinal Modes: 0 = NO MODE ! |
| ! ! 1 = PITCH G/A ! |
| ! ! 2 = PITCH TO ! |
| ! ! 3 = G/S TRACK ! |
| ! ! 4 = G/S CAPTURE ! |
| ! ! 5 = V/S ! |
| ! ! 6 = FPA ! |
| ! ! 7 = ALT ! |
| ! ! 8 = ALT ACQ ! |
| ! ! 9 = OPEN CLB ! |
| ! ! A = OPEN DES ! |
| ! ! B = IM CLB ! |
| ! ! C = IM DES ! |
| ! ! D = CLB ! |
| ! ! E = DES ! |
| ! ! F = FINAL DES ! |
| ! ! G = EXPEDITE ! |
| ! ! ! |
| ! ! Parameter for AP1 ! Parameter for AP2 ! |
| ! ! Report Line EC: ! Report Line EE: !Definition: ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! / ! / !No Mode Act. ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.11 = 1 ! 01.2.275.00.11 = 1!RUNWAY Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.12 = 1 ! 01.2.275.00.12 = 1!NAV Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.13 = 1 ! 01.2.275.00.13 = 1!LOC CAPTURE ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.14 = 1 ! 01.2.275.00.14 = 1!LOC TRACK ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.15 = 1 ! 01.2.275.00.15 = 1!Roll GO ! |
| ! ! ! !AROUND Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.16 = 1 ! 01.2.275.00.16 = 1!HEADING Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.17 = 1 ! 01.2.275.00.17 = 1!TRACK Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.15 = 1 ! 01.2.274.00.15 = 1!PITCH T/O ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.16 = 1 ! 01.2.274.00.16 = 1!PITCH GA Mode! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.17 = 1 ! 01.2.274.00.17 = 1!V/S Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.18 = 1 ! 01.2.274.00.18 = 1!FPA Mode ! |
| ! ! -------------------!-------------------!-------------! |
| ! ! 01.1.274.00.19 = 1 ! 01.2.274.00.19 = 1!ALT Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.20 = 1 ! 01.2.274.00.20 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.19 = 1 ! 01.2.274.00.19 = 1!ALT ACQ ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.21 = 1 ! 01.2.274.00.21 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.20 = 1 ! 01.2.274.00.20 = 1!G/S TRACK ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.22 = 1 ! 01.2.274.00.22 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.21 = 1 ! 01.2.274.00.21 = 1!G/S CAPTURE ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.22 = 1 ! 01.2.274.00.22 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.23 = 1 ! 01.2.274.00.23 = 1!FINAL DES ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.24 = 1 ! 01.2.274.00.24 = 1!EXPED. Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.146.00.14 = 1 ! 01.2.146.00.14 = 1!LAND TRACK ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!CLB Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.13 = 0 ! 01.2.274.00.13 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.14 = 0 ! 01.2.274.00.14 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.24 = 0 ! 01.2.274.00.24 = 0! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!DES Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.13 = 0 ! 01.2.274.00.13 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.14 = 0 ! 01.2.274.00.14 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.24 = 0 ! 01.2.274.00.24 = 0! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!IM. CLIMB ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.13 = 1 ! 01.2.274.00.13 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!IM. DES Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.13 = 1 ! 01.2.274.00.13 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!OPEN CLB ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.14 = 1 ! 01.2.274.00.14 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!OPEN. DES ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.14 = 1 ! 01.2.274.00.14 = 1! ! |
| ! ! ---------------------------------------------------- ! |
| ! ! Auto Pilot Status DMU: ! |
| ! ! Auto Pilot AP1 printed in report line EC ! |
| ! ! Auto Pilot AP2 printed in report line EE ! |
| !--------------!------------------------------------------------------! |
| ! QE ! Engine Quality Number, Report Stability ! |
| ! 99 ! (00 to 99) ! |
| ! ! DMU ! |
| !--------------!------------------------------------------------------! |
| ! N1 ! Selected N1 Actual ! |
| ! 9999 ! (0 to 120.0 %rpm) ! |
| ! ! ECU 7C.1.346.01 Engine 1 ! |
| ! ! 7C.2.346.10 Engine 2 ! |
| ! ! NOTE: The values from the last stable descent are ! |
| ! ! printed in the report lines V3 and V4. ! |
| ! ! The values from the last stable climb are ! |
| ! ! printed in the report lines V5 and V6. ! |
| !--------------!------------------------------------------------------! |
| ! N1C ! N1 Command ! |
| ! 9999 ! (0 to 120.0 %rpm) ! |
| ! ! ECU 7C.1.341.01 Engine 1 ! |
| ! ! 7C.2.341.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! N2 ! Selected N2 Actual ! |
| ! 9999 ! (0 to 120.0 %rpm) ! |
| ! ! ECU 7C.1.344.01 Engine 1 ! |
| ! ! 7C.2.344.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! EGT ! Selected T495 (Exhaust Gas Temperature) ! |
| ! X999 ! (-55 to 999.9 [C) ! |
| ! ! NOTE: Negative values are shown with an '-' in the ! |
| ! ! first position. If there are no negative ! |
| ! ! values then the value starts at the first ! |
| ! ! position. ! |
| ! ! ECU 7C.1.345.01 Engine 1 ! |
| ! ! 7C.2.345.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! FF ! Engine Fuel Flow ! |
| ! 9999 ! 0 to 7000 kg/h (0 to 15000 p/h) ! |
| ! ! ECU 7C.1.244.01 Engine 1 ! |
| ! ! 7C.2.244.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! PS13 ! PS13 Static Air Pressure at Position 1.3 ! |
| ! 99999 ! (0.0 to 30.000 psia) ! |
| ! ! ECU 7C.1.127.01 Engine 1 ! |
| ! ! 7C.2.127.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! P25 ! P25 Total Air Pressure at Position 2.5 ! |
| ! 99999 ! (0.0 to 50.000 psia) ! |
| ! ! ECU 7C.1.262.01 Engine 1 ! |
| ! ! 7C.2.262.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! T25 ! Selected T25 ! |
| ! X999 ! (-55.0 to 120.0 [C) ! |
| ! ! NOTE: Negative values are shown with an '-' in the ! |
| ! ! first position. If there are no negative ! |
| ! ! values then the value starts at the first ! |
| ! ! position. ! |
| ! ! ECU 7C.1.263.01 Engine 1 ! |
| ! ! 7C.2.263.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! P3 ! Selected PS3 (Burner Pressure) ! |
| ! 9999 ! (0.0 to 550.0 psia) ! |
| ! ! ECU 7C.1.264.01 Engine 1 ! |
| ! ! 7C.2.264.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! T3 ! Selected T3 ! |
| ! X999 ! (-55.0 to 850.0 [C) ! |
| ! ! NOTE: Negative values are shown with an '-' in the ! |
| ! ! first position. If there are no negative ! |
| ! ! values then the value starts at the first ! |
| ! ! position. ! |
| ! ! ECU 7C.1.265.01 Engine 1 ! |
| ! ! 7C.2.265.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! T5 ! Selected T5 ! |
| ! X999 ! (-55.0 to 850.0 [C) ! |
| ! ! NOTE: Negative values are shown with an '-' in the ! |
| ! ! first position. If there are no negative ! |
| ! ! values then the value starts at the first ! |
| ! ! position. ! |
| ! ! ECU 7C.1.260.01 Engine 1 ! |
| ! ! 7C.2.260.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! VSV ! Selected Variable Statore Vane Position ! |
| ! X99 ! (-5.0 to 45.0 deg) ! |
| ! ! NOTE: Negative values are shown with an '-' in the ! |
| ! ! first position. If there are no negative ! |
| ! ! values then the value starts at the first ! |
| ! ! position. ! |
| ! ! ECU 7C.1.072.01 Engine 1 ! |
| ! ! 7C.2.072.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! VBV ! Variable Bleed Valve Position ! |
| ! X99 ! (-9.9 to 40.0 deg) ! |
| ! ! NOTE: Negative values are shown with an '-' in the ! |
| ! ! first position. If there are no negative ! |
| ! ! values then the value starts at the first ! |
| ! ! position. ! |
| ! ! ECU 7C.1.071.01 Engine 1 ! |
| ! ! 7C.2.071.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! HPT ! Selected High-Pressure Turbine Clearance Position ! |
| ! X99 ! (-10 to 100 %) ! |
| ! ! ECU 7C.1.306.01 Engine 1 ! |
| ! ! 7C.2.306.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! LPT ! Selected LPTC Posiiton ! |
| ! X99 ! (-10 to 100 %) ! |
| ! ! ECU 7C.1.307.01 Engine 1 ! |
| ! ! 7C.2.307.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! GLE ! Engine Generator Load ! |
| ! 999 ! (0 to 100%) ! |
| ! ! SDAC 29.1.077.01 Engine 1 ! |
| ! ! 29.2.077.01 ! |
| ! ! 29.1.077.10 Engine 2 ! |
| ! ! 29.2.077.10 ! |
| !--------------!------------------------------------------------------! |
| ! PD ! Precooler Inlet Pressure ! |
| ! 99 ! (0 to 50 psi) ! |
| ! ! BMC 06F.1.143.01 Engine 1 ! |
| ! ! 06F.2.143.10 ! |
| ! ! 06F.1.142.01 Engine 2 ! |
| ! ! 06F.2.142.10 ! |
| !--------------!------------------------------------------------------! |
| ! TN ! Nacelle Temperature ! |
| ! X99 ! (-55 to 300 [C) ! |
| ! ! NOTE: Negative values are shown with an '-' in the ! |
| ! ! first position. If there are no negative ! |
| ! ! values then the value starts at the first ! |
| ! ! position. ! |
| ! ! FWC 26.1.322.01 Engine 1 ! |
| ! ! 26.2.322.01 ! |
| ! ! 26.1.322.10 Engine 2 ! |
| ! ! 26.2.322.10 ! |
| !--------------!------------------------------------------------------! |
| ! PT2 ! PT2 Total Air Pressure at Position 2 ! |
| ! 99999 ! (0.0 to 25.000 psia) ! |
| ! ! ECU 7C.1.131.01 Engine 1 ! |
| ! ! 7C.2.131.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! OIQH ! Oil Consumption from the previous flight ! |
| ! X999 ! (-9.99 to 20.00 qts/h) ! |
| ! ! DMU Engine 1 ! |
| ! ! Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! VN ! FAN Pick Up N1 Track Vibration ! |
| ! 99 ! (0.0 to 10.0) If value is 10.0 then 99 is printed. ! |
| ! ! EVM 3D.1.227.01 Engine 1 ! |
| ! ! 3D.1.227.10 Engine 2 ! |
| ! ! NOTE: The values from the last stable descent are ! |
| ! ! printed in the report lines V3 and V4. ! |
| ! ! The values from the last stable climb are ! |
| ! ! printed in the report lines V5 and V6. ! |
| !--------------!------------------------------------------------------! |
| ! VL ! TRF Pick Up N1 Vibration ! |
| ! 99 ! (0.0 to 10.0) If value is 10.0 then 99 is printed. ! |
| ! ! EVM 3D.1.227.11 Engine 1 ! |
| ! ! 3D.1.227.00 Engine 2 ! |
| ! ! NOTE: The values from the last stable descent are ! |
| ! ! printed in the report lines V3 and V4. ! |
| ! ! The values from the last stable climb are ! |
| ! ! printed in the report lines V5 and V6. ! |
| !--------------!------------------------------------------------------! |
| ! PHA ! FAN Pick Up Phase Angle ! |
| ! 999 ! (0 to 360 deg) ! |
| ! ! EVM 3D.1.226.01 Engine 1 ! |
| ! ! 3D.1.226.10 Engine 2 ! |
| ! ! NOTE: The values from the last stable descent are ! |
| ! ! printed in the report lines V3 and V4. ! |
| ! ! The values from the last stable climb are ! |
| ! ! printed in the report lines V5 and V6. ! |
| !--------------!------------------------------------------------------! |
| ! PHT ! TRF Pick Up Phase Angle ! |
| ! 999 ! (0 to 360 deg) ! |
| ! ! EVM 3D.1.226.11 Engine 1 ! |
| ! ! 3D.1.226.00 Engine 2 ! |
| ! ! NOTE: The values from the last stable descent are ! |
| ! ! printed in the report lines V3 and V4. ! |
| ! ! The values from the last stable climb are ! |
| ! ! printed in the report lines V5 and V6. ! |
| !--------------!------------------------------------------------------! |
| ! VC ! FAN Pick Up N2 Track Vibration ! |
| ! 99 ! (0.0 to 4.0) ! |
| ! ! EVM 3D.1.230.01 Engine 1 ! |
| ! ! 3D.1.230.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! VH ! TRF Pick Up N2 Track Vibration ! |
| ! 99 ! (0.0 to 4.0) ! |
| ! ! EVM 3D.1.230.11 Engine 1 ! |
| ! ! 3D.1.230.00 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! EVM ! Engine Vibration Status Word ! |
| ! XXXXX ! EVM 3D.1.035.01 Engine 1 ! |
| ! ! 3D.1.035.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! OIP ! Engine Oil Pressure ! |
| ! 999 ! (0 to 400 psia) ! |
| ! ! FWC 26.1.317.01 Engine 1 ! |
| ! ! 26.2.317.01 ! |
| ! ! 26.1.317.10 Engine 2 ! |
| ! ! 26.2.317.10 ! |
| !--------------!------------------------------------------------------! |
| ! OIT ! Engine Oil Temperature ! |
| ! X99 ! (-60 to 250 C) ! |
| ! ! FWC 26.1.316.01 Engine 1 ! |
| ! ! 26.2.316.01 ! |
| ! ! 26.1.316.10 Engine 2 ! |
| ! ! 26.2.316.10 ! |
| !--------------!------------------------------------------------------! |
| ! ECW1 ! Engine Control Word 1 ! |
| ! XXXXX ! Bit Label Parameter Description ! |
| ! ! 11 7C.X.272.XX.19 = 1 Auto Thrust Active ! |
| ! ! 12 7C.X.275.XX.20 = 1 VSV Position Fault ! |
| ! ! 13 SPARE ! |
| ! ! 14 SPARE ! |
| ! ! 15 7C.X.351.XX.29 = 1 Fuel Flow Measurement ! |
| ! ! Invalid ! |
| ! ! 16 7C.X.275.XX.15 = 1 N1/N2 Control Active ! |
| ! ! 17 7C.X.275.XX.26 = 1 Channel A Active ! |
| ! ! 18 7C.X.275.XX.27 = 1 Channel B Active ! |
| ! ! 19 SPARE ! |
| ! ! 20 SPARE ! |
| ! ! 21 SPARE ! |
| ! ! 22 SPARE ! |
| ! ! 23 SPARE ! |
| ! ! 24 SPARE ! |
| ! ! 25 SPARE ! |
| ! ! 26 SPARE ! |
| ! ! 27 SPARE ! |
| ! ! 28 SPARE ! |
| ! ! 29 SPARE ! |
| !--------------!------------------------------------------------------! |
| ! SSEL ! Engine Control Word 1 ! |
| ! XXXXXXX ! Status of different FADEC sensors ! |
| ! XXXXXXX ! XXXXXXXXXXXXXX Label: Selected: Bit 11 --> 15) ! |
| ! ! IIIIIIIIIIIIII__ 346 N1 actual ! |
| ! ! IIIIIIIIIIIII___ 345 EGT ! |
| ! ! IIIIIIIIIIII____ 344 N2 actual ! |
| ! ! IIIIIIIIIII_____ 263 T25 ! |
| ! ! IIIIIIIIII______ 264 PS3 ! |
| ! ! IIIIIIIII_______ 265 T3 ! |
| ! ! IIIIIIII________ 072 VSV Position ! |
| ! ! IIIIIII_________ 071 VBV Position ! |
| ! ! IIIIII__________ 306 HPTC Position ! |
| ! ! IIIII___________ 307 LPTH Position ! |
| ! ! IIII____________ 347 FMV Position ! |
| ! ! III_____________ 211 TAT ! |
| ! ! II______________ 114 P0 ! |
| ! ! I_______________ 133 TLA Position ! |
| ! ! (All labels Bit 11 --> 15) ! |
| ! ! Source: ECU, different labels ! |
| ! ! The indicated values shall be coded as follows: ! |
| ! ! Bit: 15 14 13 12 11 ! indicated value ! |
| ! ! --------------------!---------------- ! |
| ! ! 0 0 0 0 0 ! 0 ! |
| ! ! 0 0 0 0 1 ! 1 ! |
| ! ! 0 0 0 1 0 ! 2 ! |
| ! ! 0 0 0 1 1 ! 3 ! |
| ! ! 0 0 1 0 0 ! 4 ! |
| ! ! 0 0 1 0 1 ! 5 ! |
| ! ! 0 0 1 1 0 ! 6 ! |
| ! ! 0 0 1 1 1 ! 7 ! |
| ! ! 0 1 0 0 0 ! 8 ! |
| ! ! 0 1 0 0 1 ! 9 ! |
| ! ! 0 1 0 1 0 ! A ! |
| ! ! 0 1 0 1 1 ! B ! |
| ! ! 0 1 1 0 0 ! C ! |
| ! ! 0 1 1 0 1 ! D ! |
| ! ! 0 1 1 1 0 ! E ! |
| ! ! 0 1 1 1 1 ! F ! |
| ! ! 1 0 0 0 0 ! G ! |
| ! ! 1 0 0 0 1 ! H ! |
| ! ! 1 0 0 1 0 ! I ! |
| ! ! 1 0 0 1 1 ! J ! |
| ! ! 1 0 1 0 0 ! K ! |
| ! ! 1 0 1 0 1 ! L ! |
| ! ! 1 0 1 1 0 ! M ! |
| ! ! 1 0 1 1 1 ! N ! |
| ! ! 1 1 0 0 0 ! O ! |
| ! ! 1 1 0 0 1 ! P ! |
| ! ! 1 1 0 1 0 ! Q ! |
| ! ! 1 1 0 1 1 ! R ! |
| ! ! 1 1 1 0 0 ! S ! |
| ! ! 1 1 1 0 1 ! T ! |
| ! ! 1 1 1 1 0 ! U ! |
| ! ! 1 1 1 1 1 ! V ! |
| ! ! ! |
| +---------------------------------------------------------------------+ |
(4) Engine Cruise Report Data Field Description <01> (Engine Type CFMI with Advanced EVMU)
NOTE: Reports that are transmitted from the ACARS system do not have report lines without a line identifier.
| +---------------------------------------------------------------------+ |
| ! Value ! Content Description ! |
| !--------------!------------------------------------------------------! |
| ! ESN ! Engine Serial Number ! |
| ! 999999 ! (000000 to 999999) ! |
| ! ! ECU Engine 1 7C.1.046.01 digit 3, 2, 1 ! |
| ! ! 7C.1.047.01 digit 6, 5, 4 ! |
| ! ! Engine 2 7C.2.046.10 digit 3, 2, 1 ! |
| ! ! 7C.2.047.10 digit 6, 5, 4 ! |
| !--------------!------------------------------------------------------! |
| ! EHRS ! Engine Flight Hours ! |
| ! 99999 ! (00000 to 99999 hours) ! |
| ! ! DMU Engine 1 ! |
| ! ! Engine 2 ! |
| ! ! Remark: Time between "Main (LH and RH) Landing Gear! |
| ! ! Decompressed" and "Main (LH and RH) Landing! |
| ! ! Gear Compressed". The EHRS shall be set to ! |
| ! ! zero if a new ESN is recognized by the DMU.! |
| ! ! It shall be possible to set the EHRS via ! |
| ! ! the MCDU, e.g. if the DMU is changed on the! |
| ! ! a/c. ! |
| !--------------!------------------------------------------------------! |
| ! ERT ! Engine Running Time ! |
| ! 99999 ! (00000 to 65536 hours) ! |
| ! ! ECU 7C.1.050.01 Engine 1 ! |
| ! ! 7C.2.050.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! ECYC ! Engine Cycle ! |
| ! 99999 ! (00000 to 99999) ! |
| ! ! DMU Engine 1 ! |
| ! ! Engine 2 ! |
| ! ! Remark: Each time when flight phase 5 (climb) is ! |
| ! ! reached, the counter shall be incremented ! |
| ! ! by one. The ECYC is set to zero if a new ! |
| ! ! ESN is recognized by the DMU. It shall be ! |
| ! ! possible to set ECYC via the MCDU, if the ! |
| ! ! DMU is changed on the a/c. ! |
| !--------------!------------------------------------------------------! |
| ! AP ! Auto Pilot Status ! |
| ! 99 ! Number of respective status (00 to G8) ! |
| ! ! FMGC 1 and 2 (FGC part) for Auto Pilot AP1 and AP2 ! |
| ! ! ! |
| ! ! Parameter for AP1 ! Parameter for AP2 ! ! |
| ! ! Report Line EC: ! Report Line EE: !Definition: ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! / ! / !No Mode ! |
| ! ! ! !Active ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.11 = 1 ! 01.2.275.00.11 = 1!RUNWAY Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.12 = 1 ! 01.2.275.00.12 = 1!NAV Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.13 = 1 ! 01.2.275.00.13 = 1!LOC CAPTURE ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.14 = 1 ! 01.2.275.00.14 = 1!LOC TRACK ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.15 = 1 ! 01.2.275.00.15 = 1!Roll GO ! |
| ! ! ! !AROUND Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.16 = 1 ! 01.2.275.00.16 = 1!HEADING Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.17 = 1 ! 01.2.275.00.17 = 1!TRACK Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.15 = 1 ! 01.2.274.00.15 = 1!PITCH T/O ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.16 = 1 ! 01.2.274.00.16 = 1!PITCH GA Mode! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.17 = 1 ! 01.2.274.00.17 = 1!V/S Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.18 = 1 ! 01.2.274.00.18 = 1!FPA Mode ! |
| ! ! -------------------!-------------------!-------------! |
| ! ! 01.1.274.00.19 = 1 ! 01.2.274.00.19 = 1!ALT Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.20 = 1 ! 01.2.274.00.20 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.19 = 1 ! 01.2.274.00.19 = 1!ALT ACQ ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.21 = 1 ! 01.2.274.00.21 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.20 = 1 ! 01.2.274.00.20 = 1!G/S TRACK ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.22 = 1 ! 01.2.274.00.22 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.21 = 1 ! 01.2.274.00.21 = 1!G/S CAPTURE ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.22 = 1 ! 01.2.274.00.22 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.23 = 1 ! 01.2.274.00.23 = 1!FINAL DES ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.24 = 1 ! 01.2.274.00.24 = 1!EXPED. Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.146.00.14 = 1 ! 01.2.146.00.14 = 1!LAND TRACK ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!CLB Mode ! |
| ! ! AND ! AND ! ! |
| ! ! ! ! ! ! ! |
| ! ! -------------- ! -------------- ! ! |
| ! ! 01.1.274.00.13 = 0 ! 01.2.274.00.13 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.14 = 0 ! 01.2.274.00.14 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.24 = 0 ! 01.2.274.00.24 = 0! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!DES Mode ! |
| ! ! AND ! AND ! ! |
| ! ! ! ! ! ! ! |
| ! ! -------------- ! -------------- ! ! |
| ! ! 01.1.274.00.13 = 0 ! 01.2.274.00.13 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.14 = 0 ! 01.2.274.00.14 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.24 = 0 ! 01.2.274.00.24 = 0! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!IM. CLIMB ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.13 = 1 ! 01.2.274.00.13 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!IM. DES Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.13 = 1 ! 01.2.274.00.13 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!OPEN CLB ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.14 = 1 ! 01.2.274.00.14 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!OPEN. DES ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.14 = 1 ! 01.2.274.00.14 = 1! ! |
| ! ! ---------------------------------------------------- ! |
| ! ! Auto Pilot Status DMU: ! |
| ! ! Auto Pilot AP1 printed in report line EC ! |
| ! ! Auto Pilot AP2 printed in report line EE ! |
| ! ! Combined Auto Pilot Modes ! |
| ! ! The longitudinal auto pilot mode (1 to G) shall ! |
| ! ! appear on the left position for the AP1 and AP2 print! |
| ! ! format. ! |
| ! ! The lateral auto pilot mode (1 to 8) shall appear on ! |
| ! ! the right position for the AP1 and AP2 print format. ! |
| ! ! In case of a combined auto pilot mode e.g. DES mode ! |
| ! ! and NAV mode are engaged simultaneously, the 'E3' ! |
| ! ! shall appear below AP1 and AP2. ! |
| ! ! XX Auto Pilot Modes: ! |
| ! ! !! ! |
| ! ! !!__Lateral Modes: 0 = NO MODE ! |
| ! ! ! 1 = HEADING ! |
| ! ! ! 2 = TRACK ! |
| ! ! ! 3 = NAV ! |
| ! ! ! 4 = LOC CAPTURE ! |
| ! ! ! 5 = LOCK TRACK ! |
| ! ! ! 6 = LAND TRACK ! |
| ! ! ! 7 = RUNWAY ! |
| ! ! ! 8 = ROLL GO AROUND ! |
| ! ! ! ! |
| ! ! !__Longitudinal Modes: 0 = NO MODE ! |
| ! ! 1 = PITCH G/A ! |
| ! ! 2 = PITCH TO ! |
| ! ! 3 = G/S TRACK ! |
| ! ! 4 = G/S CAPTURE ! |
| ! ! 5 = V/S ! |
| ! ! 6 = FPA ! |
| ! ! 7 = ALT ! |
| ! ! 8 = ALT ACQ ! |
| ! ! 9 = OPEN CLB ! |
| ! ! A = OPEN DES ! |
| ! ! B = IM CLB ! |
| ! ! C = IM DES ! |
| ! ! D = CLB ! |
| ! ! E = DES ! |
| ! ! F = FINAL DES ! |
| ! ! G = EXPEDITE ! |
| !--------------!------------------------------------------------------! |
| ! QE ! Engine Quality Number, Report Stability ! |
| ! 99 ! (00 to 99) ! |
| ! ! DMU ! |
| ! ! Remark: 99=worst stable frame, ! |
| ! ! 00=best stable frame. ! |
| ! ! ! |
| ! ! i=1 VARe(i) ! |
| ! ! QE= SIGMA(We(i)*--------------- ! |
| ! ! N TOLe(i)*TOLe(i) ! |
| ! !QE= Engine quality number ! |
| ! !We(i)= Individual weighting factors for the individual! |
| ! ! quality parameters for the Cruise Report. ! |
| ! !VARe(i)= parameter variances ! |
| ! !TOLe(i)= Variation values for the individual quality ! |
| ! ! parameters for the cruise report. ! |
| !--------------!------------------------------------------------------! |
| ! N1 ! Selected N1 Actual ! |
| ! 9999 ! (0 to 120.0 %rpm) ! |
| ! ! ECU 7C.1.346.01 Engine 1 ! |
| ! ! 7C.2.346.10 Engine 2 ! |
| ! ! Remark: In the report line V3 and V4 the values ! |
| ! ! from the last stable descent shall be ! |
| ! ! printed. ! |
| ! ! In the report line V5 and V6 the values ! |
| ! ! from the last stable climb shall be ! |
| ! ! printed. ! |
| !--------------!------------------------------------------------------! |
| ! N1C ! N1 Command ! |
| ! 9999 ! (0 to 120.0 %rpm) ! |
| ! ! ECU 7C.1.341.01 Engine 1 ! |
| ! ! 7C.2.341.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! N2 ! Selected N2 Actual ! |
| ! 9999 ! (0 to 120.0 %rpm) ! |
| ! ! ECU 7C.1.344.01 Engine 1 ! |
| ! ! 7C.2.344.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! EGT ! Selected T495 (Exhaust Gas Temperature) ! |
| ! X999 ! (-55 to 999.9 [C) ! |
| ! ! Negative values shall be indicated by '-' on the ! |
| ! ! first position. Otherwise the first position shall ! |
| ! ! be used for the value. ! |
| ! ! ECU 7C.1.345.01 Engine 1 ! |
| ! ! 7C.2.345.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! FF ! Engine Fuel Flow ! |
| ! 9999 ! 0 to 7000 kg/h (0 to 15000 p/h) ! |
| ! ! ECU 7C.1.244.01 Engine 1 ! |
| ! ! 7C.2.244.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! PS13 ! PS13 Static Air Pressure at Position 1.3 ! |
| ! 99999 ! (0.0 to 30.000 psia) ! |
| ! ! ECU 7C.1.127.01 Engine 1 ! |
| ! ! 7C.2.127.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! P25 ! P25 Total Air Pressure at Position 2.5 ! |
| ! 99999 ! (0.0 to 50.000 psia) ! |
| ! ! ECU 7C.1.262.01 Engine 1 ! |
| ! ! 7C.2.262.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! T25 ! Selected T25 ! |
| ! X999 ! (-55.0 to 120.0 [C) ! |
| ! ! Negative values shall be indicated by '-' on the ! |
| ! ! first position. Otherwise the first position shall ! |
| ! ! be used for the value. ! |
| ! ! ECU 7C.1.263.01 Engine 1 ! |
| ! ! 7C.2.263.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! P3 ! Selected PS3 (Burner Pressure) ! |
| ! 9999 ! (0.0 to 450.0 psia) ! |
| ! ! ECU 7C.1.264.01 Engine 1 ! |
| ! ! 7C.2.264.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! T3 ! Selected T3 ! |
| ! X999 ! (-55.0 to 850.0 deg C) ! |
| ! ! Negative values shall be indicated by '-' on the ! |
| ! ! first position. Otherwise the first position shall ! |
| ! ! be used for the value. ! |
| ! ! ECU 7C.1.265.01 Engine 1 ! |
| ! ! 7C.2.265.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! T5 ! T5 Temperature at position T5 ! |
| ! X999 ! (-55.0 to 850.0 [C) ! |
| ! ! Negative values shal be indicated by '-' on the ! |
| ! ! first position. Otherwise the firt position shall ! |
| ! ! be used for the value. ! |
| ! ! ECU 7C.1.260.01 Engine 1 ! |
| ! ! 7C.2.260.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! VSV ! Selected Variable Stator Vane Position ! |
| ! X99 ! (-5.0 to 45.0 deg) ! |
| ! ! Negative values shall be indicated by '-' on the ! |
| ! ! first position. Otherwise the first position shall ! |
| ! ! be used for the value. ! |
| ! ! ECU 7C.1.072.01 Engine 1 ! |
| ! ! 7C.2.072.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! VBV ! Variable Bleed Valve Position ! |
| ! X99 ! (-9.9 to 40.0 deg) ! |
| ! ! Negative values shall be indicated by '-' on the ! |
| ! ! first position. Otherwise the first position shall ! |
| ! ! be used for the value. ! |
| ! ! ECU 7C.1.071.01 Engine 1 ! |
| ! ! 7C.2.071.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! HPT ! Selected High-Pressure Turbine Clearance Position ! |
| ! X99 ! (-10 to 100 %) ! |
| ! ! ECU 7C.1.306.01 Engine 1 ! |
| ! ! 7C.2.306.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! LPT ! Selected LPTC Posiiton ! |
| ! X99 ! (-10 to 100 %) ! |
| ! ! ECU 7C.1.307.01 Engine 1 ! |
| ! ! 7C.2.307.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! GLE ! Engine Generator Load ! |
| ! 999 ! (0 to 100%) ! |
| ! ! SDAC 29.1.077.01 Engine 1 ! |
| ! ! 29.2.077.01 ! |
| ! ! 29.1.077.10 Engine 2 ! |
| ! ! 29.2.077.10 ! |
| !--------------!------------------------------------------------------! |
| ! PD ! Precooler Inlet Pressure ! |
| ! 99 ! (0 to 50 psi) ! |
| ! ! BMC 06F.1.143.01 Engine 1 ! |
| ! ! 06F.2.143.10 ! |
| ! ! 06F.1.142.01 Engine 2 ! |
| ! ! 06F.2.142.10 ! |
| !--------------!------------------------------------------------------! |
| ! TN ! Nacelle Temperature ! |
| ! X99 ! (-55 to 300 [C) ! |
| ! ! Negative values shall be indicated by '-' on the ! |
| ! ! first position. Otherwise the first position shall ! |
| ! ! be used for the value. ! |
| ! ! FWC 26.1.322.01 Engine 1 ! |
| ! ! 26.2.322.01 ! |
| ! ! 26.1.322.10 Engine 2 ! |
| ! ! 26.2.322.10 ! |
| !--------------!------------------------------------------------------! |
| ! PT2 ! PT2 Total Air Pressure at Position 2 ! |
| ! 99999 ! (0.0 to 25.000 psia) ! |
| ! ! ECU 7C.1.131.01 Engine 1 ! |
| ! ! 7C.2.131.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! OIQH ! Oil Consumption from the previous flight ! |
| ! X999 ! (-9.99 to 20.00 qts/h) ! |
| ! ! DMU Engine 1 ! |
| ! ! Engine 2 ! |
| ! ! Remark: Following formula shall be used. ! |
| ! ! OIKa-OIKb ! |
| ! ! OIQH=---------(qts/h) ! |
| ! ! UTCb-UTCa ! |
| ! ! OIK=oil quantity corrected ! |
| ! ! suffix a denotes taxi out condition ! |
| ! ! suffix b denotes taxi in condition ! |
| ! ! The calculation shall be done 'Y01.5' seconds ! |
| ! ! before the flight phase changes from 2 to 3 and ! |
| ! ! 'Y01.4' seconds after beginning of flight phase 9. ! |
| ! ! OIKa=OIQa*(A*OITa+B) ! |
| ! ! OIKb=OIQb*(A*OITb+B) ! |
| ! ! OIQ= measured oil quantity 29.1.073.11 Engine 1 ! |
| ! ! 29.2.073.11 ! |
| ! ! 29.1.073.00 Engine 2 ! |
| ! ! 29.2.073.00 ! |
| ! ! OIQ= measured oil quantity 29.1.316.11 Engine 1 ! |
| ! ! 29.2.316.11 ! |
| ! ! 29.1.316.00 Engine 2 ! |
| ! ! 29.2.316.00 ! |
| ! ! OIT= oil temperature 26.1.316.01 Engine 1 ! |
| ! ! 26.2.316.01 ! |
| ! ! ! |
| ! ! 26.2.316.10 Engine 1 ! |
| ! ! 26.2.316.10 ! |
| ! ! A=6.4*1/10000 ! |
| ! ! B=1.013 ! |
| !--------------!------------------------------------------------------! |
| ! VN ! FAN Pick Up N1 Track Vibration ! |
| ! 99 ! (0.0 to 10.0) ! |
| ! ! If value is 10.0 then 99 shall be printed. ! |
| ! ! EVM 3D.1.227.01 Engine 1 ! |
| ! ! 3D.1.227.10 Engine 2 ! |
| ! ! Remark: In report line V3 and V4 the values from ! |
| ! ! the last stable descent shall be ! |
| ! ! printed. ! |
| ! ! In report line V5 and V6 the values from ! |
| ! ! the last stable climb shall be printed. ! |
| !--------------!------------------------------------------------------! |
| ! VL ! TRF Pick Up N1 Vibration ! |
| ! 99 ! (0.0 to 10.0) ! |
| ! ! If value is 10.0 then 99 shall be printed. ! |
| ! ! EVM 3D.1.227.11 Engine 1 ! |
| ! ! 3D.1.227.00 Engine 2 ! |
| ! ! Remark: In report line V3 and V4 the values from ! |
| ! ! the last stable descent shall be ! |
| ! ! printed. ! |
| ! ! In report line V5 and V6 the values from ! |
| ! ! the last stable climb shall be printed. ! |
| !--------------!------------------------------------------------------! |
| ! PHA ! FAN Pick Up Phase Angle ! |
| ! 999 ! (0 to 360 deg) ! |
| ! ! EVM 3D.1.226.01 Engine 1 ! |
| ! ! 3D.1.226.10 Engine 2 ! |
| ! ! Remark: In report line V3 and V4 the values from ! |
| ! ! the last stable descent shall be ! |
| ! ! printed. ! |
| ! ! In report line V5 and V6 the values from ! |
| ! ! the last stable climb shall be printed. ! |
| !--------------!------------------------------------------------------! |
| ! PHT ! TRF Pick Up Phase Angle ! |
| ! 999 ! (0 to 360 deg) ! |
| ! ! EVM 3D.1.226.11 Engine 1 ! |
| ! ! 3D.1.226.00 Engine 2 ! |
| ! ! Remark: In report line V3 and V4 the values from ! |
| ! ! the last stable descent shall be ! |
| ! ! printed. ! |
| ! ! In report line V5 and V6 the values from ! |
| ! ! the last stable climb shall be printed. ! |
| !--------------!------------------------------------------------------! |
| ! VC ! FAN Pick Up N2 Track Vibration ! |
| ! 99 ! (0.0 to 4.0) ! |
| ! ! EVM 3D.1.230.01 Engine 1 ! |
| ! ! 3D.1.230.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! VH ! TRF Pick Up N2 Track Vibration ! |
| ! 99 ! (0.0 to 4.0) ! |
| ! ! EVM 3D.1.230.11 Engine 1 ! |
| ! ! 3D.1.230.00 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! EVM ! Engine Vibration Status Word ! |
| ! XXXXX ! EVM 3D.1.035.01 Engine 1 ! |
| ! ! 3D.1.035.10 Engine 2 ! |
| ! ! XXXXX Bits HEX ! |
| ! ! !!!!!________14, 13, 12, 11 0..F ! |
| ! ! !!!!_________18, 17, 16, 15 0..F ! |
| ! ! !!!__________22, 21, 20, 19 0..F ! |
| ! ! !!___________26, 25, 24, 23 0..F ! |
| ! ! !____________ 29, 28, 27 0..F ! |
| !--------------!------------------------------------------------------! |
| ! OIP ! Engine Oil Pressure ! |
| ! 999 ! (0 to 400 psia) ! |
| ! ! FWC 26.1.317.01 Engine 1 ! |
| ! ! 26.2.317.01 ! |
| ! ! 26.1.317.10 Engine 2 ! |
| ! ! 26.2.317.10 ! |
| !--------------!------------------------------------------------------! |
| ! OIT ! Engine Oil Temperature ! |
| ! X99 ! (-60 to 250 C) ! |
| ! ! Negative values shal be indicated by '-' on the ! |
| ! ! first position. Otherwise the firt position shall ! |
| ! ! be used for the value. ! |
| ! ! FWC 26.1.316.01 Engine 1 ! |
| ! ! 26.2.316.01 ! |
| ! ! 26.1.316.10 Engine 2 ! |
| ! ! 26.2.316.10 ! |
| !--------------!------------------------------------------------------! |
| ! ECW1 ! Engine Control Word 1 ! |
| ! XXXXX ! XXXXX Bits HEX ! |
| ! ! !!!!!________14, 13, 12, 11 0..F ! |
| ! ! !!!!_________18, 17, 16, 15 0..F ! |
| ! ! !!!__________22, 21, 20, 19 0..F ! |
| ! ! !!___________26, 25, 24, 23 0..F ! |
| ! ! !____________ 29, 28, 27 0..F ! |
| ! ! Bit Label Parameter Description ! |
| ! ! 11 7C.X.272.XX.19 = 1 Auto Thrust Active ! |
| ! ! 12 7C.X.275.XX.20 = 1 VSV Position Fault ! |
| ! ! 13 SPARE ! |
| ! ! 14 SPARE ! |
| ! ! 15 7C.X.351.XX.29 = 1 Fuel Flow Measurement ! |
| ! ! Invalid ! |
| ! ! 16 7C.X.275.XX.15 = 1 N1/N2 Control Active ! |
| ! ! 17 7C.X.275.XX.26 = 1 Channel A Active ! |
| ! ! 18 7C.X.275.XX.27 = 1 Channel B Active ! |
| ! ! 19 SPARE ! |
| ! ! 20 SPARE ! |
| ! ! 21 SPARE ! |
| ! ! 22 SPARE ! |
| ! ! 23 SPARE ! |
| ! ! 24 SPARE ! |
| ! ! 25 SPARE ! |
| ! ! 26 SPARE ! |
| ! ! 27 SPARE ! |
| ! ! 28 SPARE ! |
| ! ! 29 SPARE ! |
| ! ! The 'X' for the System and SDI definition of the ! |
| ! ! engine parameters shall be as follows: ! |
| ! ! System SDI ! |
| ! ! Engine 1 1 01 ! |
| ! ! Engine 2 2 10 ! |
| !--------------!------------------------------------------------------! |
| ! SSEL ! Engine Control Word 1 ! |
| ! XXXXXXX ! Status of different FADEC sensors ! |
| ! XXXXXXX ! XXXXXXXXXXXXXX Label: Selected: ! |
| ! ! !!!!!!!!!!!!!!_ 346 N1 actual (Bit 11 -> 15)! |
| ! ! !!!!!!!!!!!!!__ 345 EGT (Bit 11 -> 15)! |
| ! ! !!!!!!!!!!!!___ 344 N2 actual (Bit 11 -> 15)! |
| ! ! !!!!!!!!!!!____ 263 T25 (Bit 11 -> 15)! |
| ! ! !!!!!!!!!!_____ 264 PS3 (Bit 11 -> 15)! |
| ! ! !!!!!!!!!______ 265 T3 (Bit 11 -> 15)! |
| ! ! !!!!!!!!_______ 072 VSV Position (Bit 11 -> 15)! |
| ! ! !!!!!!!________ 071 VBV Position (Bit 11 -> 15)! |
| ! ! !!!!!!_________ 306 HPTC Position (Bit 11 -> 15)! |
| ! ! !!!!!__________ 307 LPTH Position (Bit 11 -> 15)! |
| ! ! !!!!___________ 347 FMV Position (Bit 11 -> 15)! |
| ! ! !!!____________ 211 TAT (Bit 11 -> 15)! |
| ! ! !!_____________ 114 P0 (Bit 11 -> 15)! |
| ! ! !______________ 133 TLA Position (Bit 11 -> 15)! |
| ! ! Source: ECU, different labels ! |
| ! ! The indicated values shall be coded as follows: ! |
| ! ! Bit: 15 14 13 12 11 ! indicated value ! |
| ! ! --------------------!---------------- ! |
| ! ! 0 0 0 0 0 ! 0 ! |
| ! ! 0 0 0 0 1 ! 1 ! |
| ! ! 0 0 0 1 0 ! 2 ! |
| ! ! 0 0 0 1 1 ! 3 ! |
| ! ! 0 0 1 0 0 ! 4 ! |
| ! ! 0 0 1 0 1 ! 5 ! |
| ! ! 0 0 1 1 0 ! 6 ! |
| ! ! 0 0 1 1 1 ! 7 ! |
| ! ! 0 1 0 0 0 ! 8 ! |
| ! ! 0 1 0 0 1 ! 9 ! |
| ! ! 0 1 0 1 0 ! A ! |
| ! ! 0 1 0 1 1 ! B ! |
| ! ! 0 1 1 0 0 ! C ! |
| ! ! 0 1 1 0 1 ! D ! |
| ! ! 0 1 1 1 0 ! E ! |
| ! ! 0 1 1 1 1 ! F ! |
| ! ! 1 0 0 0 0 ! G ! |
| ! ! 1 0 0 0 1 ! H ! |
| ! ! 1 0 0 1 0 ! I ! |
| ! ! 1 0 0 1 1 ! J ! |
| ! ! 1 0 1 0 0 ! K ! |
| ! ! 1 0 1 0 1 ! L ! |
| ! ! 1 0 1 1 0 ! M ! |
| ! ! 1 0 1 1 1 ! N ! |
| ! ! 1 1 0 0 0 ! O ! |
| ! ! 1 1 0 0 1 ! P ! |
| ! ! 1 1 0 1 0 ! Q ! |
| ! ! 1 1 0 1 1 ! R ! |
| ! ! 1 1 1 0 0 ! S ! |
| ! ! 1 1 1 0 1 ! T ! |
| ! ! 1 1 1 1 0 ! U ! |
| ! ! 1 1 1 1 1 ! V ! |
| ! ! ! |
| +---------------------------------------------------------------------+ |
(5) Engine Cruise Report Data Field Description <01> (Engine Type CFMI with Advanced EVMU)
NOTE: Reports that are transmitted from the ACARS system do not have report lines without a line identifier.
| +---------------------------------------------------------------------+ |
| ! Value ! Content Description ! |
| !--------------!------------------------------------------------------! |
| ! ESN ! Engine Serial Number ! |
| ! 999999 ! (000000 to 999999) ! |
| ! ! ECU Engine 1 7C.1.046.01 digit 3, 2, 1 ! |
| ! ! 7C.1.047.01 digit 6, 5, 4 ! |
| ! ! Engine 2 7C.2.046.10 digit 3, 2, 1 ! |
| ! ! 7C.2.047.10 digit 6, 5, 4 ! |
| !--------------!------------------------------------------------------! |
| ! EHRS ! Engine Flight Hours ! |
| ! 99999 ! (00000 to 99999 hours) ! |
| ! ! DMU Engine 1 ! |
| ! ! Engine 2 ! |
| ! ! Remark: Time between "Main (LH and RH) Landing Gear! |
| ! ! Decompressed" and "Main (LH and RH) Landing! |
| ! ! Gear Compressed". The EHRS is set to zero ! |
| ! ! if a new ESN is recognized by the DMU. ! |
| ! ! It is possible to set the EHRS through ! |
| ! ! the MCDU, e.g. if the DMU is changed on the! |
| ! ! a/c. ! |
| !--------------!------------------------------------------------------! |
| ! ERT ! Engine Running Time ! |
| ! 99999 ! (00000 to 65536 hours) ! |
| ! ! ECU 7C.1.050.01 Engine 1 ! |
| ! ! 7C.2.050.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! ECYC ! Engine Cycle ! |
| ! 99999 ! (00000 to 99999) ! |
| ! ! DMU Engine 1 ! |
| ! ! Engine 2 ! |
| ! ! Remark: Each time when flight phase 5 (climb) is ! |
| ! ! reached, the counter is incremented by one.! |
| ! ! The ECYC is set to zero if a new ! |
| ! ! ESN is recognized by the DMU. ! |
| ! ! It is possible to set ECYC through the ! |
| ! ! MCDU, if the DMU is changed on the a/c. ! |
| !--------------!------------------------------------------------------! |
| ! AP ! Auto Pilot Status ! |
| ! 99 ! Number of respective status (00 to G8) ! |
| ! ! FMGC 1 and 2 (FGC part) for Auto Pilot AP1 and AP2 ! |
| ! ! ! |
| ! ! Parameter for AP1 ! Parameter for AP2 ! ! |
| ! ! Report Line EC: ! Report Line EE: !Definition: ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! / ! / !No Mode ! |
| ! ! ! !Active ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.11 = 1 ! 01.2.275.00.11 = 1!RUNWAY Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.12 = 1 ! 01.2.275.00.12 = 1!NAV Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.13 = 1 ! 01.2.275.00.13 = 1!LOC CAPTURE ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.14 = 1 ! 01.2.275.00.14 = 1!LOC TRACK ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.15 = 1 ! 01.2.275.00.15 = 1!Roll GO ! |
| ! ! ! !AROUND Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.16 = 1 ! 01.2.275.00.16 = 1!HEADING Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.17 = 1 ! 01.2.275.00.17 = 1!TRACK Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.15 = 1 ! 01.2.274.00.15 = 1!PITCH T/O ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.16 = 1 ! 01.2.274.00.16 = 1!PITCH GA Mode! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.17 = 1 ! 01.2.274.00.17 = 1!V/S Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.18 = 1 ! 01.2.274.00.18 = 1!FPA Mode ! |
| ! ! -------------------!-------------------!-------------! |
| ! ! 01.1.274.00.19 = 1 ! 01.2.274.00.19 = 1!ALT Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.20 = 1 ! 01.2.274.00.20 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.19 = 1 ! 01.2.274.00.19 = 1!ALT ACQ ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.21 = 1 ! 01.2.274.00.21 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.20 = 1 ! 01.2.274.00.20 = 1!G/S TRACK ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.22 = 1 ! 01.2.274.00.22 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.21 = 1 ! 01.2.274.00.21 = 1!G/S CAPTURE ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.22 = 1 ! 01.2.274.00.22 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.23 = 1 ! 01.2.274.00.23 = 1!FINAL DES ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.24 = 1 ! 01.2.274.00.24 = 1!EXPED. Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.146.00.14 = 1 ! 01.2.146.00.14 = 1!LAND TRACK ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!CLB Mode ! |
| ! ! AND ! AND ! ! |
| ! ! ! ! ! ! ! |
| ! ! -------------- ! -------------- ! ! |
| ! ! 01.1.274.00.13 = 0 ! 01.2.274.00.13 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.14 = 0 ! 01.2.274.00.14 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.24 = 0 ! 01.2.274.00.24 = 0! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!DES Mode ! |
| ! ! AND ! AND ! ! |
| ! ! ! ! ! ! ! |
| ! ! -------------- ! -------------- ! ! |
| ! ! 01.1.274.00.13 = 0 ! 01.2.274.00.13 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.14 = 0 ! 01.2.274.00.14 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.24 = 0 ! 01.2.274.00.24 = 0! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!IM. CLIMB ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.13 = 1 ! 01.2.274.00.13 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!IM. DES Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.13 = 1 ! 01.2.274.00.13 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!OPEN CLB ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.14 = 1 ! 01.2.274.00.14 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!OPEN. DES ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.14 = 1 ! 01.2.274.00.14 = 1! ! |
| ! ! ---------------------------------------------------- ! |
| ! ! Auto Pilot Status DMU: ! |
| ! ! Auto Pilot AP1 printed in report line EC ! |
| ! ! Auto Pilot AP2 printed in report line EE ! |
| ! ! Combined Auto Pilot Modes ! |
| ! ! The longitudinal auto pilot mode (1 to G) will ! |
| ! ! appear on the left position for the AP1 and AP2 print! |
| ! ! format. ! |
| ! ! The lateral auto pilot mode (1 to 8) will appear on ! |
| ! ! the right position for the AP1 and AP2 print format. ! |
| ! ! In case of a combined auto pilot mode e.g. DES mode ! |
| ! ! and NAV mode are engaged simultaneously, the 'E3' ! |
| ! ! will appear below AP1 and AP2. ! |
| ! ! XX Auto Pilot Modes: ! |
| ! ! !! ! |
| ! ! !!__Lateral Modes: 0 = NO MODE ! |
| ! ! ! 1 = HEADING ! |
| ! ! ! 2 = TRACK ! |
| ! ! ! 3 = NAV ! |
| ! ! ! 4 = LOC CAPTURE ! |
| ! ! ! 5 = LOCK TRACK ! |
| ! ! ! 6 = LAND TRACK ! |
| ! ! ! 7 = RUNWAY ! |
| ! ! ! 8 = ROLL GO AROUND ! |
| ! ! ! ! |
| ! ! !__Longitudinal Modes: 0 = NO MODE ! |
| ! ! 1 = PITCH G/A ! |
| ! ! 2 = PITCH TO ! |
| ! ! 3 = G/S TRACK ! |
| ! ! 4 = G/S CAPTURE ! |
| ! ! 5 = V/S ! |
| ! ! 6 = FPA ! |
| ! ! 7 = ALT ! |
| ! ! 8 = ALT ACQ ! |
| ! ! 9 = OPEN CLB ! |
| ! ! A = OPEN DES ! |
| ! ! B = IM CLB ! |
| ! ! C = IM DES ! |
| ! ! D = CLB ! |
| ! ! E = DES ! |
| ! ! F = FINAL DES ! |
| ! ! G = EXPEDITE ! |
| !--------------!------------------------------------------------------! |
| ! QE ! Engine Quality Number, Report Stability ! |
| ! 99 ! (00 to 99) ! |
| ! ! DMU ! |
| ! ! Remark: 99=worst stable frame, ! |
| ! ! 00=best stable frame. ! |
| ! ! ! |
| ! ! i=1 VARe(i) ! |
| ! ! QE= SIGMA(We(i)*--------------- ! |
| ! ! N TOLe(i)*TOLe(i) ! |
| ! !QE= Engine quality number ! |
| ! !We(i)= Individual weighting factors for the individual! |
| ! ! quality parameters for the Cruise Report. ! |
| ! !VARe(i)= parameter variances ! |
| ! !TOLe(i)= Variation values for the individual quality ! |
| ! ! parameters for the cruise report. ! |
| !--------------!------------------------------------------------------! |
| ! N1 ! Selected N1 Actual ! |
| ! 9999 ! (0 to 120.0 %rpm) ! |
| ! ! ECU 7C.1.346.01 Engine 1 ! |
| ! ! 7C.2.346.10 Engine 2 ! |
| ! ! Remark: In the report line V3 and V4 the values ! |
| ! ! from the last stable descent are printed. ! |
| ! ! In the report line V5 and V6 the values ! |
| ! ! from the last stable climb are printed. ! |
| !--------------!------------------------------------------------------! |
| ! N1C ! N1 Command ! |
| ! 9999 ! (0 to 120.0 %rpm) ! |
| ! ! ECU 7C.1.341.01 Engine 1 ! |
| ! ! 7C.2.341.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! N2 ! Selected N2 Actual ! |
| ! 9999 ! (0 to 120.0 %rpm) ! |
| ! ! ECU 7C.1.344.01 Engine 1 ! |
| ! ! 7C.2.344.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! EGT ! Select T495 (Exhaust Gas Temperature) ! |
| ! X999 ! (-55 to 999.9 deg C) ! |
| ! ! Negative values shall be indicated by 'N' on the ! |
| ! ! first position. Otherwise the first position can ! |
| ! ! be used for the value. ! |
| ! ! ECU 7C.1.345.01 Engine 1 ! |
| ! ! 7C.2.345.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! FF ! Engine Fuel Flow ! |
| ! 9999 ! 0 to 7000 kg/h (0 to 15000 p/h) ! |
| ! ! ECU 7C.1.244.01 Engine 1 ! |
| ! ! 7C.2.244.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! PS13 ! PS13 Static Air Pressure at Position 1.3 ! |
| ! 99999 ! (0.0 to 30.000 psia) ! |
| ! ! ECU 7C.1.127.01 Engine 1 ! |
| ! ! 7C.2.127.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! P25 ! P25 Total Air Pressure at Position 2.5 ! |
| ! 99999 ! (0.0 to 50.000 psia) ! |
| ! ! ECU 7C.1.262.01 Engine 1 ! |
| ! ! 7C.2.262.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! T25 ! Selected T25 ! |
| ! X999 ! (-55.0 to 120.0 deg C) ! |
| ! ! Negative values are indicated by 'N' on the first ! |
| ! ! position. Otherwise the first position is used for ! |
| ! ! the value. ! |
| ! ! ECU 7C.1.263.01 Engine 1 ! |
| ! ! 7C.2.263.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! P3 ! Selected PS3 (Burner Pressure) ! |
| ! 9999 ! (0.0 to 450.0 psia) ! |
| ! ! ECU 7C.1.264.01 Engine 1 ! |
| ! ! 7C.2.264.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! T3 ! Selected T3 ! |
| ! X999 ! (-55.0 to 850.0 deg C) ! |
| ! ! Negative values are indicated by 'N' on the first ! |
| ! ! position. Otherwise the first position is used for ! |
| ! ! the value. ! |
| ! ! ECU 7C.1.265.01 Engine 1 ! |
| ! ! 7C.2.265.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! T5 ! T5 Temperature at position T5 ! |
| ! X999 ! (-55.0 to 850.0 deg C) ! |
| ! ! Negative values are indicated by 'N' on the first ! |
| ! ! position. Otherwise the firt position is used for ! |
| ! ! the value. ! |
| ! ! ECU 7C.1.260.01 Engine 1 ! |
| ! ! 7C.2.260.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! VSV ! Selected Variable Stator Vane Position ! |
| ! X99 ! (-5.0 to 45.0 deg) ! |
| ! ! Negative values are indicated by 'N' on the first ! |
| ! ! position. Otherwise the first position is used for ! |
| ! ! the value. ! |
| ! ! ECU 7C.1.072.01 Engine 1 ! |
| ! ! 7C.2.072.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! VBV ! Variable Bleed Valve Position ! |
| ! X99 ! (-9.9 to 40.0 deg) ! |
| ! ! Negative values are indicated by 'N' on the first ! |
| ! ! position. Otherwise the first position is used for ! |
| ! ! the value. ! |
| ! ! ECU 7C.1.071.01 Engine 1 ! |
| ! ! 7C.2.071.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! HPT ! Selected High-Pressure Turbine Clearance Position ! |
| ! X99 ! (-10 to 100 %) ! |
| ! ! ECU 7C.1.306.01 Engine 1 ! |
| ! ! 7C.2.306.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! LPT ! Selected LPTC Position ! |
| ! X99 ! (-10 to 100 %) ! |
| ! ! ECU 7C.1.307.01 Engine 1 ! |
| ! ! 7C.2.307.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! GLE ! Engine Generator Load ! |
| ! 999 ! (0 to 100%) ! |
| ! ! SDAC 29.1.077.01 Engine 1 ! |
| ! ! 29.2.077.01 ! |
| ! ! 29.1.077.10 Engine 2 ! |
| ! ! 29.2.077.10 ! |
| !--------------!------------------------------------------------------! |
| ! PD ! Precooler Inlet Pressure ! |
| ! 99 ! (0 to 50 psi) ! |
| ! ! BMC 06F.1.143.01 Engine 1 ! |
| ! ! 06F.2.143.10 ! |
| ! ! 06F.1.142.01 Engine 2 ! |
| ! ! 06F.2.142.10 ! |
| !--------------!------------------------------------------------------! |
| ! TN ! Nacelle Temperature ! |
| ! X99 ! (-55 to 300 deg C) ! |
| ! ! Negative values are indicated by 'N' on the first ! |
| ! ! position. Otherwise the first position is used for ! |
| ! ! the value. ! |
| ! ! FWC 26.1.322.01 Engine 1 ! |
| ! ! 26.2.322.01 ! |
| ! ! 26.1.322.10 Engine 2 ! |
| ! ! 26.2.322.10 ! |
| !--------------!------------------------------------------------------! |
| ! PT2 ! PT2 Total Air Pressure at Position 2 ! |
| ! 99999 ! (0.0 to 25.000 psia) ! |
| ! ! ECU 7C.1.131.01 Engine 1 ! |
| ! ! 7C.2.131.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! OIQH ! Oil Consumption from the previous flight ! |
| ! X999 ! (-9.99 to 20.00 qts/h) ! |
| ! ! DMU Engine 1 ! |
| ! ! Engine 2 ! |
| ! ! Remark: Following formula is used. ! |
| ! ! OIKa-OIKb ! |
| ! ! OIQH=---------(qts/h) ! |
| ! ! UTCb-UTCa ! |
| ! ! OIK=oil quantity corrected ! |
| ! ! UTC=universal time coordinated (BNR) 17.1.150.00 ! |
| ! ! (attention to the date) ! |
| ! ! suffix a denotes taxi out condition ! |
| ! ! suffix b denotes taxi in condition ! |
| ! ! The calculation is done 'Y01.5' seconds before ! |
| ! ! the flight phase changes from 2 to 3 and 'Y01.4' ! |
| ! ! seconds after start of flight phase 9. ! |
| ! ! OIKa=OIQa*(A*OITa+B) ! |
| ! ! OIKb=OIQb*(A*OITb+B) ! |
| ! ! OIQ= measured oil quantity 26.1.073.01 Engine 1 ! |
| ! ! 26.2.073.01 ! |
| ! ! 26.1.073.10 Engine 2 ! |
| ! ! 26.2.073.10 ! |
| ! ! OIQ= oil temperature 26.1.316.01 Engine 1 ! |
| ! ! 26.2.316.01 ! |
| ! ! 26.1.316.10 Engine 2 ! |
| ! ! 26.2.316.10 ! |
| ! ! A=6.4*1/10000 ! |
| ! ! B=1.013 ! |
| !--------------!------------------------------------------------------! |
| ! VN ! FAN Pick Up N1 Track Vibration ! |
| ! 99 ! (0.0 to 10.0) ! |
| ! ! If value is 10.0 then 99 shall be printed. ! |
| ! ! EVM 3D.1.227.01 Engine 1 ! |
| ! ! 3D.1.227.10 Engine 2 ! |
| ! ! Remark: In report line V3 and V4 the values from ! |
| ! ! the last stable descent are printed. ! |
| ! ! In report line V5 and V6 the values from ! |
| ! ! the last stable climb are printed. ! |
| !--------------!------------------------------------------------------! |
| ! VL ! TRF Pick Up N1 Track Vibration ! |
| ! 99 ! (0.0 to 10.0) ! |
| ! ! If value is 10.0 then 99 is printed. ! |
| ! ! EVM 3D.1.227.11 Engine 1 ! |
| ! ! 3D.1.227.00 Engine 2 ! |
| ! ! Remark: In report line V3 and V4 the values from ! |
| ! ! the last stable descent shall be ! |
| ! ! printed. ! |
| ! ! In report line V5 and V6 the values from ! |
| ! ! the last stable climb shall be printed. ! |
| !--------------!------------------------------------------------------! |
| ! PHA ! FAN Pick Up Phase Angle ! |
| ! 999 ! (0 to 360 deg) ! |
| ! ! EVM 3D.1.226.01 Engine 1 ! |
| ! ! 3D.1.226.10 Engine 2 ! |
| ! ! Remark: In report line V3 and V4 the values from ! |
| ! ! the last stable descent are printed. ! |
| ! ! In report line V5 and V6 the values from ! |
| ! ! the last stable climb are printed. ! |
| !--------------!------------------------------------------------------! |
| ! PHT ! TRF Pick Up Phase Angle ! |
| ! 999 ! (0 to 360 deg) ! |
| ! ! EVM 3D.1.226.11 Engine 1 ! |
| ! ! 3D.1.226.00 Engine 2 ! |
| ! ! Remark: In report line V3 and V4 the values from ! |
| ! ! the last stable descent are printed. ! |
| ! ! In report line V5 and V6 the values from ! |
| ! ! the last stable climb are printed. ! |
| !--------------!------------------------------------------------------! |
| ! VC ! FAN Pick Up N2 Track Vibration ! |
| ! 99 ! (0.0 to 4.0) ! |
| ! ! EVM 3D.1.230.01 Engine 1 ! |
| ! ! 3D.1.230.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! VH ! TRF Pick Up N2 Track Vibration ! |
| ! 99 ! (0.0 to 4.0) ! |
| ! ! EVM 3D.1.230.11 Engine 1 ! |
| ! ! 3D.1.230.00 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! EVM ! Engine Vibration Status Word ! |
| ! XXXXX ! (Each 'X' represents 4 bits in hexadecimal of a ! |
| ! ! defined ARINC 429 word) ! |
| ! ! EVM 3D.1.035.01 Engine 1 ! |
| ! ! 3D.1.035.10 Engine 2 ! |
| ! ! XXXXX Bits HEX ! |
| ! ! !!!!!________14, 13, 12, 11 0..F ! |
| ! ! !!!!_________18, 17, 16, 15 0..F ! |
| ! ! !!!__________22, 21, 20, 19 0..F ! |
| ! ! !!___________26, 25, 24, 23 0..F ! |
| ! ! !____________ 29, 28, 27 0..7 ! |
| ! ! Bit Function ! |
| ! ! 11 N1 vib above advisory ! |
| ! ! 12 N2 vib above advisory ! |
| ! ! 13 Accelerometer reconfiguration ! |
| ! ! 14 Spare always at 1 ! |
| ! ! 15 Frequency analysis performed ! |
| ! ! 16 #1 brg accel channel fault ! |
| ! ! 17 TRF accel channel fault ! |
| ! ! 18 N1 speed channel fault ! |
| ! ! 19 N2 speed channel fault ! |
| ! ! 20 Unbalance fault ! |
| ! ! 21 Frequency fault ! |
| ! ! 22 NVM fault ! |
| ! ! 23 BB above threshold ! |
| ! ! 24 Spare ! |
| ! ! 25 Spare ! |
| ! ! 26 Spare ! |
| ! ! 27 adv on sel. acc. in flight or other acc. ! |
| ! ! in FP6 ! |
| ! ! 28 EVM SYST CLASS II FAULT ! |
| ! ! 29 EVMU CLASS I FAULT ! |
| !--------------!------------------------------------------------------! |
| ! OIP ! Engine Oil Pressure ! |
| ! 999 ! (0 to 400 psia) ! |
| ! ! FWC 26.1.317.01 Engine 1 ! |
| ! ! 26.2.317.01 ! |
| ! ! 26.1.317.10 Engine 2 ! |
| ! ! 26.2.317.10 ! |
| !--------------!------------------------------------------------------! |
| ! OIT ! Engine Oil Temperature ! |
| ! X99 ! (-60 to 250 deg C) ! |
| ! ! Negative values are indicated by 'N' on the first ! |
| ! ! position. Otherwise the firt position is used for ! |
| ! ! the value. ! |
| ! ! FWC 26.1.316.01 Engine 1 ! |
| ! ! 26.2.316.01 ! |
| ! ! 26.1.316.10 Engine 2 ! |
| ! ! 26.2.316.10 ! |
| !--------------!------------------------------------------------------! |
| ! ECW1 ! Engine Control Word 1 ! |
| ! XXXX ! (Each 'X' represents 4 bits in hexadecimal of a ! |
| ! ! defined ARINC 429 word) ! |
| ! ! XXXXX Bits HEX ! |
| ! ! !!!!!________14, 13, 12, 11 0..F ! |
| ! ! !!!!_________18, 17, 16, 15 0..F ! |
| ! ! !!!__________22, 21, 20, 19 0..F ! |
| ! ! !!___________26, 25, 24, 23 0..F ! |
| ! ! !____________ 29, 28, 27 0..7 ! |
| ! ! Bit Label Parameter Description ! |
| ! ! 11 7C.X.272.XX.19 = 1 Auto Thrust Active ! |
| ! ! 12 7C.X.275.XX.20 = 1 VSV Position Fault ! |
| ! ! 13 SPARE ! |
| ! ! 14 SPARE ! |
| ! ! 15 7C.X.351.XX.29 = 1 Fuel Flow Measurement ! |
| ! ! Invalid ! |
| ! ! 16 7C.X.275.XX.15 = 1 N1/N2 Control Active ! |
| ! ! 17 7C.X.275.XX.26 = 1 Channel A Active ! |
| ! ! 18 7C.X.275.XX.27 = 1 Channel B Active ! |
| ! ! 19 SPARE ! |
| ! ! 20 SPARE ! |
| ! ! 21 SPARE ! |
| ! ! 22 SPARE ! |
| ! ! 23 SPARE ! |
| ! ! 24 SPARE ! |
| ! ! 25 SPARE ! |
| ! ! 26 SPARE ! |
| ! ! 27 SPARE ! |
| ! ! 28 SPARE ! |
| ! ! 29 SPARE ! |
| ! ! The 'X' for the System and SDI definition of the ! |
| ! ! engine parameters are as follows: ! |
| ! ! System SDI ! |
| ! ! Engine 1 1 01 ! |
| ! ! Engine 2 2 10 ! |
| !--------------!------------------------------------------------------! |
| ! SSEL ! Status of different FADEC sensors ! |
| ! XXXXXXX ! ! |
| ! XXXXXXX ! XXXXXXXXXXXXXX Label: Selected: ! |
| ! ! !!!!!!!!!!!!!!_ 133 TLA Position (Bit 11 -> 15)! |
| ! ! !!!!!!!!!!!!!__ 114 PO (Bit 11 -> 15)! |
| ! ! !!!!!!!!!!!!___ 211 TAT (Bit 11 -> 15)! |
| ! ! !!!!!!!!!!!____ 347 FMV Position (Bit 11 -> 15)! |
| ! ! !!!!!!!!!!_____ 307 LPTH Position (Bit 11 -> 15)! |
| ! ! !!!!!!!!!______ 306 HPTC Position (Bit 11 -> 15)! |
| ! ! !!!!!!!!_______ 071 VBV Position (Bit 11 -> 15)! |
| ! ! !!!!!!!________ 072 VSV Position (Bit 11 -> 15)! |
| ! ! !!!!!!_________ 265 T3 (Bit 11 -> 15)! |
| ! ! !!!!!__________ 264 PS3 (Bit 11 -> 15)! |
| ! ! !!!!___________ 263 T 25 (Bit 11 -> 15)! |
| ! ! !!!____________ 344 N2 actual (Bit 11 -> 15)! |
| ! ! !!_____________ 345 EGT (Bit 11 -> 15)! |
| ! ! !______________ 346 N1 actual (Bit 11 -> 15)! |
| ! ! Source: ECU, different labels ! |
| ! ! The indicated values are coded as follows: ! |
| ! ! Bit: 15 14 13 12 11 ! indicated value ! |
| ! ! --------------------!---------------- ! |
| ! ! 0 0 0 0 0 ! 0 ! |
| ! ! 0 0 0 0 1 ! 1 ! |
| ! ! 0 0 0 1 0 ! 2 ! |
| ! ! 0 0 0 1 1 ! 3 ! |
| ! ! 0 0 1 0 0 ! 4 ! |
| ! ! 0 0 1 0 1 ! 5 ! |
| ! ! 0 0 1 1 0 ! 6 ! |
| ! ! 0 0 1 1 1 ! 7 ! |
| ! ! 0 1 0 0 0 ! 8 ! |
| ! ! 0 1 0 0 1 ! 9 ! |
| ! ! 0 1 0 1 0 ! A ! |
| ! ! 0 1 0 1 1 ! B ! |
| ! ! 0 1 1 0 0 ! C ! |
| ! ! 0 1 1 0 1 ! D ! |
| ! ! 0 1 1 1 0 ! E ! |
| ! ! 0 1 1 1 1 ! F ! |
| ! ! 1 0 0 0 0 ! G ! |
| ! ! 1 0 0 0 1 ! H ! |
| ! ! 1 0 0 1 0 ! I ! |
| ! ! 1 0 0 1 1 ! J ! |
| ! ! 1 0 1 0 0 ! K ! |
| ! ! 1 0 1 0 1 ! L ! |
| ! ! 1 0 1 1 0 ! M ! |
| ! ! 1 0 1 1 1 ! N ! |
| ! ! 1 1 0 0 0 ! O ! |
| ! ! 1 1 0 0 1 ! P ! |
| ! ! 1 1 0 1 0 ! Q ! |
| ! ! 1 1 0 1 1 ! R ! |
| ! ! 1 1 1 0 0 ! S ! |
| ! ! 1 1 1 0 1 ! T ! |
| ! ! 1 1 1 1 0 ! U ! |
| ! ! 1 1 1 1 1 ! V ! |
| ! ! ! |
| +---------------------------------------------------------------------+ |
(6) Engine Cruise Report Data Field Description <01> (Engine Type CFMI with Advanced EVMU)
NOTE: Reports that are transmitted from the ACARS system do not have report lines without a line identifier.
| +---------------------------------------------------------------------+ |
| ! Value ! Content Description ! |
| !--------------!------------------------------------------------------! |
| ! ESN ! Engine Serial Number ! |
| ! 999999 ! (000000 to 999999) ! |
| ! ! ECU Engine 1 7C.1.046.01 digit 3, 2, 1 ! |
| ! ! 7C.1.047.01 digit 6, 5, 4 ! |
| ! ! Engine 2 7C.2.046.10 digit 3, 2, 1 ! |
| ! ! 7C.2.047.10 digit 6, 5, 4 ! |
| !--------------!------------------------------------------------------! |
| ! EHRS ! Engine Flight Hours ! |
| ! 99999 ! (00000 to 99999 hours) ! |
| ! ! DMU Engine 1 ! |
| ! ! Engine 2 ! |
| ! ! Remark: Time between "Main (LH and RH) Landing Gear! |
| ! ! Decompressed" and "Main (LH and RH) Landing Gear ! |
| ! ! Compressed". The EHRS is set to zero if a new ESN ! |
| ! ! is recognized by the DMU. It is possible to set the! |
| ! ! EHRS through the MCDU, e.g. if the DMU is changed ! |
| ! ! on the a/c. ! |
| !--------------!------------------------------------------------------! |
| ! ERT ! Engine Running Time ! |
| ! 99999 ! (00000 to 65536 hours) ! |
| ! ! ECU 7C.1.050.01 Engine 1 ! |
| ! ! 7C.2.050.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! ECYC ! Engine Cycle ! |
| ! 99999 ! (00000 to 99999) ! |
| ! ! DMU Engine 1 ! |
| ! ! Engine 2 ! |
| ! ! Remark: Each time when flight phase 5 (climb) is ! |
| ! ! reached, the counter is incremented by one. The ! |
| ! ! ECYC is set to zero if a new ESN is recognized by ! |
| ! ! the DMU. It is possible to set ECYC through the ! |
| ! ! MCDU, if the DMU is changed on the a/c. ! |
| !--------------!------------------------------------------------------! |
| ! AP ! Auto Pilot Status ! |
| ! 99 ! Number of respective status (00 to G8) ! |
| ! ! FMGC 1 and 2 (FGC part) for Auto Pilot AP1 and AP2 ! |
| ! ! ! |
| ! ! Parameter for AP1 ! Parameter for AP2 ! ! |
| ! ! Report Line EC: ! Report Line EE: !Definition: ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! / ! / !No Mode ! |
| ! ! ! !Active ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.11 = 1 ! 01.2.275.00.11 = 1!RUNWAY Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.12 = 1 ! 01.2.275.00.12 = 1!NAV Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.13 = 1 ! 01.2.275.00.13 = 1!LOC CAPTURE ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.14 = 1 ! 01.2.275.00.14 = 1!LOC TRACK ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.15 = 1 ! 01.2.275.00.15 = 1!Roll GO ! |
| ! ! ! !AROUND Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.16 = 1 ! 01.2.275.00.16 = 1!HEADING Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.17 = 1 ! 01.2.275.00.17 = 1!TRACK Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.15 = 1 ! 01.2.274.00.15 = 1!PITCH T/O ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.16 = 1 ! 01.2.274.00.16 = 1!PITCH GA Mode! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.17 = 1 ! 01.2.274.00.17 = 1!V/S Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.18 = 1 ! 01.2.274.00.18 = 1!FPA Mode ! |
| ! ! -------------------!-------------------!-------------! |
| ! ! 01.1.274.00.19 = 1 ! 01.2.274.00.19 = 1!ALT Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.20 = 1 ! 01.2.274.00.20 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.19 = 1 ! 01.2.274.00.19 = 1!ALT ACQ ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.21 = 1 ! 01.2.274.00.21 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.20 = 1 ! 01.2.274.00.20 = 1!G/S TRACK ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.22 = 1 ! 01.2.274.00.22 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.21 = 1 ! 01.2.274.00.21 = 1!G/S CAPTURE ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.22 = 1 ! 01.2.274.00.22 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.23 = 1 ! 01.2.274.00.23 = 1!FINAL DES ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.24 = 1 ! 01.2.274.00.24 = 1!EXPED. Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.146.00.14 = 1 ! 01.2.146.00.14 = 1!LAND TRACK ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!CLB Mode ! |
| ! ! AND ! AND ! ! |
| ! ! ! ! ! ! ! |
| ! ! -------------- ! -------------- ! ! |
| ! ! 01.1.274.00.13 = 0 ! 01.2.274.00.13 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.14 = 0 ! 01.2.274.00.14 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.24 = 0 ! 01.2.274.00.24 = 0! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!DES Mode ! |
| ! ! AND ! AND ! ! |
| ! ! ! ! ! ! ! |
| ! ! -------------- ! -------------- ! ! |
| ! ! 01.1.274.00.13 = 0 ! 01.2.274.00.13 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.14 = 0 ! 01.2.274.00.14 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.24 = 0 ! 01.2.274.00.24 = 0! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!IM. CLIMB ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.13 = 1 ! 01.2.274.00.13 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!IM. DES Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.13 = 1 ! 01.2.274.00.13 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!OPEN CLB ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.14 = 1 ! 01.2.274.00.14 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!OPEN. DES ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.14 = 1 ! 01.2.274.00.14 = 1! ! |
| ! ! ---------------------------------------------------- ! |
| ! ! Auto Pilot Status DMU: ! |
| ! ! Auto Pilot AP1 printed in report line EC ! |
| ! ! Auto Pilot AP2 printed in report line EE ! |
| ! ! Combined Auto Pilot Modes ! |
| ! ! The longitudinal auto pilot mode (1 to G) appears ! |
| ! ! on the left position for the AP1 and AP2 print ! |
| ! ! format. ! |
| ! ! The lateral auto pilot mode (1 to 8) appears on the ! |
| ! ! right position for the AP1 and AP2 print format. ! |
| ! ! In case of a combined auto pilot mode e.g. DES mode ! |
| ! ! and NAV mode are engaged simultaneously, the 'E3' ! |
| ! ! appears below AP1 and AP2. ! |
| ! ! XX Auto Pilot Modes: ! |
| ! ! !! ! |
| ! ! !!__Lateral Modes: 0 = NO MODE ! |
| ! ! ! 1 = HEADING ! |
| ! ! ! 2 = TRACK ! |
| ! ! ! 3 = NAV ! |
| ! ! ! 4 = LOC CAPTURE ! |
| ! ! ! 5 = LOCK TRACK ! |
| ! ! ! 6 = LAND TRACK ! |
| ! ! ! 7 = RUNWAY ! |
| ! ! ! 8 = ROLL GO AROUND ! |
| ! ! ! ! |
| ! ! !__Longitudinal Modes: 0 = NO MODE ! |
| ! ! 1 = PITCH G/A ! |
| ! ! 2 = PITCH TO ! |
| ! ! 3 = G/S TRACK ! |
| ! ! 4 = G/S CAPTURE ! |
| ! ! 5 = V/S ! |
| ! ! 6 = FPA ! |
| ! ! 7 = ALT ! |
| ! ! 8 = ALT ACQ ! |
| ! ! 9 = OPEN CLB ! |
| ! ! A = OPEN DES ! |
| ! ! B = IM CLB ! |
| ! ! C = IM DES ! |
| ! ! D = CLB ! |
| ! ! E = DES ! |
| ! ! F = FINAL DES ! |
| ! ! G = EXPEDITE ! |
| !--------------!------------------------------------------------------! |
| ! QE ! Engine Quality Number, Report-Stability ! |
| ! 99 ! (00 to 99) ! |
| ! ! DMU ! |
| ! ! Remark: 99=worst stable frame, ! |
| ! ! 00=best stable frame. ! |
| ! ! The quality number is represented in mathematical ! |
| ! ! form bellow: ! |
| ! ! i=1 VARe(i) ! |
| ! ! QE= SIGMA(We(i)*--------------- ! |
| ! ! N TOLe(i)*TOLe(i) ! |
| ! !QE= Engine quality number ! |
| ! !We(i)= Individual weighting factors for the individual! |
| ! ! quality parameters for the cruise report. ! |
| ! !VARe(i)= Parameter variances ! |
| ! !TOLe(i)= Variation values for the individual quality ! |
| ! ! parameters for the cruise report. ! |
| !--------------!------------------------------------------------------! |
| ! N1 ! Selected N1 Actual ! |
| ! 9999 ! (0 to 120.0 %rpm) ! |
| ! ! ECU 7C.1.346.01 Engine 1 ! |
| ! ! 7C.2.346.10 Engine 2 ! |
| ! ! Remark: In the report line V3 and V4 the values ! |
| ! ! from the last stable descent are printed. ! |
| ! ! In the report line V5 and V6 the values from the ! |
| ! ! last stable climb are printed. ! |
| !--------------!------------------------------------------------------! |
| ! N1C ! N1 Command ! |
| ! 9999 ! (0 to 120.0 %rpm) ! |
| ! ! ECU 7C.1.341.01 Engine 1 ! |
| ! ! 7C.2.341.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! N2 ! Selected N2 Actual ! |
| ! 9999 ! (0 to 120.0 %rpm) ! |
| ! ! ECU 7C.1.344.01 Engine 1 ! |
| ! ! 7C.2.344.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! EGT ! Select T495 (Exhaust Gas Temperature) ! |
| ! X999 ! (-55 to 999.9 deg C) ! |
| ! ! Negative values are shown with '-' on the first ! |
| ! ! position. Otherwise the first position is used for ! |
| ! ! for the value. ! |
| ! ! ECU 7C.1.345.01 Engine 1 ! |
| ! ! 7C.2.345.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! FF ! Engine Fuel Flow ! |
| ! 9999 ! 0 to 7000 kg/h (0 to 15000 p/h) ! |
| ! ! ECU 7C.1.244.01 Engine 1 ! |
| ! ! 7C.2.244.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! PS13 ! PS13 Static Air Pressure at Position 1.3 ! |
| ! 99999 ! (0.0 to 30.000 psia) ! |
| ! ! ECU 7C.1.127.01 Engine 1 ! |
| ! ! 7C.2.127.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! P25 ! P25 Total Air Pressure at Position 2.5 ! |
| ! 99999 ! (0.0 to 50.000 psia) ! |
| ! ! ECU 7C.1.262.01 Engine 1 ! |
| ! ! 7C.2.262.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! T25 ! Selected T25 ! |
| ! X999 ! (-55.0 to 120.0 [C) ! |
| ! ! Negative values are shown with '-' on the first ! |
| ! ! position. Otherwise the first position is used for ! |
| ! ! the value. ! |
| ! ! ECU 7C.1.263.01 Engine 1 ! |
| ! ! 7C.2.263.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! P3 ! Selected PS3 ! |
| ! 9999 ! (0.0 to 450.0 psia) ! |
| ! ! ECU 7C.1.264.01 Engine 1 ! |
| ! ! 7C.2.264.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! T3 ! Selected T3 ! |
| ! X999 ! (-55.0 to 850.0 deg C) ! |
| ! ! Negative values are shown with '-' on the first ! |
| ! ! position. Otherwise the first position is used for ! |
| ! ! the value. ! |
| ! ! ECU 7C.1.265.01 Engine 1 ! |
| ! ! 7C.2.265.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! T5 ! T5 Temperature at position 5 ! |
| ! X999 ! (-55.0 to 850.0 deg C) ! |
| ! ! Negative values are shown with '-' on the first ! |
| ! ! position. Otherwise the firt position is used for ! |
| ! ! the value. ! |
| ! ! ECU 7C.1.260.01 Engine 1 ! |
| ! ! 7C.2.260.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! VSV ! Selected Variable Stator Vane Position ! |
| ! X99 ! (-5.0 to 45.0 deg) ! |
| ! ! Negative values are shown with '-' on the first ! |
| ! ! position. Otherwise the first position is used for ! |
| ! ! the value. ! |
| ! ! ECU 7C.1.072.01 Engine 1 ! |
| ! ! 7C.2.072.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! VBV ! Variable Bleed Valve Position ! |
| ! X99 ! (-9.9 to 40.0 deg) ! |
| ! ! Negative values are shown with '-' on the first ! |
| ! ! position. Otherwise the first position is used for ! |
| ! ! the value. ! |
| ! ! ECU 7C.1.071.01 Engine 1 ! |
| ! ! 7C.2.071.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! HPT ! Selected HPTC Position ! |
| ! X99 ! (-10 to 100 %) ! |
| ! ! ECU 7C.1.306.01 Engine 1 ! |
| ! ! 7C.2.306.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! LPT ! Selected LPTC Position ! |
| ! X99 ! (-10 to 100 %) ! |
| ! ! ECU 7C.1.307.01 Engine 1 ! |
| ! ! 7C.2.307.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! GLE ! Engine Generator Load ! |
| ! 999 ! (0 to 100%) ! |
| ! ! SDAC 29.1.077.01 Engine 1 ! |
| ! ! 29.2.077.01# ! |
| ! ! 29.1.077.10 Engine 2 ! |
| ! ! 29.2.077.10# ! |
| !--------------!------------------------------------------------------! |
| ! PD ! Precooler Inlet Pressure ! |
| ! 99 ! (0 to 50 psi) ! |
| ! ! BMC 06F.1.143.01 Engine 1 ! |
| ! ! 06F.2.143.10# ! |
| ! ! 06F.1.142.01 Engine 2 ! |
| ! ! 06F.2.142.10# ! |
| !--------------!------------------------------------------------------! |
| ! TN ! Nacelle Temperature ! |
| ! X99 ! (-55 to 300 deg C) ! |
| ! ! Negative values are shown with '-' on the first ! |
| ! ! position. Otherwise the first position is used for ! |
| ! ! the value. ! |
| ! ! FWC 26.1.322.01 Engine 1 ! |
| ! ! 26.2.322.01# ! |
| ! ! 26.1.322.10 Engine 2 ! |
| ! ! 26.2.322.10# ! |
| !--------------!------------------------------------------------------! |
| ! PT2 ! PT2 Total Air Pressure at Position 2 ! |
| ! 99999 ! (0.0 to 25.000 psia) ! |
| ! ! ECU 7C.1.131.01 Engine 1 ! |
| ! ! 7C.2.131.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! OIQH ! Oil Consumption from the previous flight ! |
| ! X999 ! (-9.99 to 20.00 qts/h) ! |
| ! ! DMU Engine 1 ! |
| ! ! Engine 2 ! |
| ! ! Remark: Following formula is used: ! |
| ! ! OIKa-OIKb ! |
| ! ! OIQH=---------(qts/h) ! |
| ! ! UTCb-UTCa ! |
| ! ! OIK=oil quantity corrected ! |
| ! ! suffix a denotes taxi out condition ! |
| ! ! suffix b denotes taxi in condition ! |
| ! ! The calculation is done 'Y01.5' seconds before ! |
| ! ! the flight phase changes from 2 to 3 and 'Y01.4' ! |
| ! ! seconds after beginning of flight phase 9. ! |
| ! ! OIKa=OIQa*(A*OITa+B) ! |
| ! ! OIKb=OIQb*(A*OITb+B) ! |
| ! ! OIQ= measured oil quantity 29.1.073.01 Engine 1 ! |
| ! ! 29.2.073.01# ! |
| ! ! 29.1.073.10 Engine 2 ! |
| ! ! 29.2.073.10# ! |
| ! ! OIT= oil temperature 29.1.316.01 Engine 1 ! |
| ! ! 29.2.316.01# ! |
| ! ! 29.1.316.10 Engine 2 ! |
| ! ! 29.2.316.10# ! |
| ! ! A=6.4*1/10000 ! |
| ! ! B=1.013 ! |
| !--------------!------------------------------------------------------! |
| ! VN ! FAN Pick Up N1 Track Vibration ! |
| ! 99 ! (0.0 to 10.0) ! |
| ! ! If value is 10.0 then 99 is printed. ! |
| ! ! EVM 3D.1.227.01 Engine 1 ! |
| ! ! 3D.1.227.10 Engine 2 ! |
| ! ! Remark: In report line V3 and V4 the values from ! |
| ! ! the last stable descent are printed. ! |
| ! ! In report line V5 and V6 the values from ! |
| ! ! the last stable climb are printed. ! |
| !--------------!------------------------------------------------------! |
| ! VL ! TRF Pick Up N1 track vibration ! |
| ! 99 ! (0.0 to 10.0) ! |
| ! ! If value is 10.0 then 99 is printed. ! |
| ! ! EVM 3D.1.227.11 Engine 1 ! |
| ! ! 3D.1.227.00 Engine 2 ! |
| ! ! Remark: In report line V3 and V4 the values from ! |
| ! ! the last stable descent are printed. ! |
| ! ! In report line V5 and V6 the values from the last ! |
| ! ! stable climb are printed. ! |
| !--------------!------------------------------------------------------! |
| ! PHA ! FAN Pick Up Phase Angle ! |
| ! 999 ! (0 to 360 deg) ! |
| ! ! EVM 3D.1.226.01 Engine 1 ! |
| ! ! 3D.1.226.10 Engine 2 ! |
| ! ! Remark: In report line V3 and V4 the values from ! |
| ! ! the last stable descent are printed. ! |
| ! ! In report line V5 and V6 the values from the last ! |
| ! ! stable climb are printed. ! |
| !--------------!------------------------------------------------------! |
| ! PHT ! TRF Pick Up Phase Angle ! |
| ! 999 ! (0 to 360 deg) ! |
| ! ! EVM 3D.1.226.11 Engine 1 ! |
| ! ! 3D.1.226.00 Engine 2 ! |
| ! ! Remark: In report line V3 and V4 the values from ! |
| ! ! the last stable descent are printed. ! |
| ! ! In report line V5 and V6 the values from the last ! |
| ! ! stable climb are printed. ! |
| !--------------!------------------------------------------------------! |
| ! VC ! FAN Pick Up N2 track vibration ! |
| ! 99 ! (0.0 to 4.0) ! |
| ! ! EVM 3D.1.230.01 Engine 1 ! |
| ! ! 3D.1.230.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! VH ! TRF Pick Up N2 track vibration ! |
| ! 99 ! (0.0 to 4.0) ! |
| ! ! EVM 3D.1.230.11 Engine 1 ! |
| ! ! 3D.1.230.00 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! EVM ! Engine Vibration Status Word ! |
| ! XXXXX ! EVM 3D.1.035.01 Engine 1 ! |
| ! ! 3D.1.035.10 Engine 2 ! |
| ! ! XXXXX Bits HEX ! |
| ! ! !!!!!________14, 13, 12, 11 0..F ! |
| ! ! !!!!_________18, 17, 16, 15 0..F ! |
| ! ! !!!__________22, 21, 20, 19 0..F ! |
| ! ! !!___________26, 25, 24, 23 0..F ! |
| ! ! !____________ 29, 28, 27 0..F ! |
| !--------------!------------------------------------------------------! |
| ! OIP ! Engine Oil Pressure ! |
| ! 999 ! (0 to 400 psia) ! |
| ! ! FWC 26.1.317.01 Engine 1 ! |
| ! ! 26.2.317.01# ! |
| ! ! 26.1.317.10 Engine 2 ! |
| ! ! 26.2.317.10# ! |
| !--------------!------------------------------------------------------! |
| ! OIT ! Engine Oil Temperature ! |
| ! X99 ! (-60 to 250 deg C) ! |
| ! ! Negative values are shown with '-' on the first ! |
| ! ! position. Otherwise the firt position is used ! |
| ! ! for the value. ! |
| ! ! FWC 26.1.316.01 Engine 1 ! |
| ! ! 26.2.316.01# ! |
| ! ! 26.1.316.10 Engine 2 ! |
| ! ! 26.2.316.10# ! |
| !--------------!------------------------------------------------------! |
| ! ECW1 ! Engine Control Word 1 ! |
| ! XXXXX ! XXXXX Bits HEX ! |
| ! ! !!!!!________14, 13, 12, 11 0..F ! |
| ! ! !!!!_________18, 17, 16, 15 0..F ! |
| ! ! !!!__________22, 21, 20, 19 0..F ! |
| ! ! !!___________26, 25, 24, 23 0..F ! |
| ! ! !____________ 29, 28, 27 0..F ! |
| ! ! Bit Label Parameter Description ! |
| ! ! 11 7C.X.272.XX.19 = 1 Auto Thrust Active ! |
| ! ! 12 7C.X.275.XX.20 = 1 VSV Position Fault ! |
| ! ! 13 SPARE ! |
| ! ! 14 SPARE ! |
| ! ! 15 7C.X.351.XX.29 = 1 Fuel Flow Measurement ! |
| ! ! Invalid ! |
| ! ! 16 7C.X.275.XX.15 = 1 N1/N2 Control Active ! |
| ! ! 17 7C.X.275.XX.26 = 1 Channel A Active ! |
| ! ! 18 7C.X.275.XX.27 = 1 Channel B Active ! |
| ! ! 19 SPARE ! |
| ! ! 20 SPARE ! |
| ! ! 21 SPARE ! |
| ! ! 22 SPARE ! |
| ! ! 23 SPARE ! |
| ! ! 24 SPARE ! |
| ! ! 25 SPARE ! |
| ! ! 26 SPARE ! |
| ! ! 27 SPARE ! |
| ! ! 28 SPARE ! |
| ! ! 29 SPARE ! |
| ! ! The 'X' for the System and SDI definition of the ! |
| ! ! engine parameters is as follows: ! |
| ! ! System SDI ! |
| ! ! Engine 1 1 01 ! |
| ! ! Engine 2 2 10 ! |
| !--------------!------------------------------------------------------! |
| ! SSEL ! Engine Control Word 1 ! |
| ! XXXXXXX ! Status of different FADEC sensors ! |
| ! XXXXXXX ! XXXXXXXXXXXXXX Label: Selected: ! |
| ! ! !!!!!!!!!!!!!!_ 346 N1 actual (Bit 11 -> 15)! |
| ! ! !!!!!!!!!!!!!__ 345 EGT (Bit 11 -> 15)! |
| ! ! !!!!!!!!!!!!___ 344 N2 actual (Bit 11 -> 15)! |
| ! ! !!!!!!!!!!!____ 263 T25 (Bit 11 -> 15)! |
| ! ! !!!!!!!!!!_____ 264 PS3 (Bit 11 -> 15)! |
| ! ! !!!!!!!!!______ 265 T3 (Bit 11 -> 15)! |
| ! ! !!!!!!!!_______ 072 VSV Position (Bit 11 -> 15)! |
| ! ! !!!!!!!________ 071 VBV Position (Bit 11 -> 15)! |
| ! ! !!!!!!_________ 306 HPTC Position (Bit 11 -> 15)! |
| ! ! !!!!!__________ 307 LPTH Position (Bit 11 -> 15)! |
| ! ! !!!!___________ 347 FMV Position (Bit 11 -> 15)! |
| ! ! !!!____________ 211 TAT (Bit 11 -> 15)! |
| ! ! !!_____________ 114 P0 (Bit 11 -> 15)! |
| ! ! !______________ 133 TLA Position (Bit 11 -> 15)! |
| ! ! Source: ECU, different labels ! |
| ! ! The indicated values are coded as follows: ! |
| ! ! Bit: 15 14 13 12 11 ! indicated value ! |
| ! ! --------------------!---------------- ! |
| ! ! 0 0 0 0 0 ! 0 ! |
| ! ! 0 0 0 0 1 ! 1 ! |
| ! ! 0 0 0 1 0 ! 2 ! |
| ! ! 0 0 0 1 1 ! 3 ! |
| ! ! 0 0 1 0 0 ! 4 ! |
| ! ! 0 0 1 0 1 ! 5 ! |
| ! ! 0 0 1 1 0 ! 6 ! |
| ! ! 0 0 1 1 1 ! 7 ! |
| ! ! 0 1 0 0 0 ! 8 ! |
| ! ! 0 1 0 0 1 ! 9 ! |
| ! ! 0 1 0 1 0 ! A ! |
| ! ! 0 1 0 1 1 ! B ! |
| ! ! 0 1 1 0 0 ! C ! |
| ! ! 0 1 1 0 1 ! D ! |
| ! ! 0 1 1 1 0 ! E ! |
| ! ! 0 1 1 1 1 ! F ! |
| ! ! 1 0 0 0 0 ! G ! |
| ! ! 1 0 0 0 1 ! H ! |
| ! ! 1 0 0 1 0 ! I ! |
| ! ! 1 0 0 1 1 ! J ! |
| ! ! 1 0 1 0 0 ! K ! |
| ! ! 1 0 1 0 1 ! L ! |
| ! ! 1 0 1 1 0 ! M ! |
| ! ! 1 0 1 1 1 ! N ! |
| ! ! 1 1 0 0 0 ! O ! |
| ! ! 1 1 0 0 1 ! P ! |
| ! ! 1 1 0 1 0 ! Q ! |
| ! ! 1 1 0 1 1 ! R ! |
| ! ! 1 1 1 0 0 ! S ! |
| ! ! 1 1 1 0 1 ! T ! |
| ! ! 1 1 1 1 0 ! U ! |
| ! ! 1 1 1 1 1 ! V ! |
| ! ! ! |
| +---------------------------------------------------------------------+ |
(7) Parameter Logic
| +---------------------------------------------------------------------+ |
| ! Param. ! Print Value (Standard Progr.) ! |
| !--------------!------------------------------------------------------! |
| ! ESN ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! EHRS ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! ERT ! Value at moment of trigger ! |
| !--------------! -----------------------------------------------------! |
| ! ECYC ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! AP ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! QE ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! N1 * ! Arithmetic average for F01*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! N1C ! Arithmetic average for F01*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! N2 ! Arithmetic average for F01*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! EGT ! Arithmetic average for F01*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! FF ! Arithmetic average for F01*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! PS13 ! Arithmetic average for F01*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! P25 ! Arithmetic average for F01*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! T25 ! Arithmetic average for F01*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! P3 ! Arithmetic average for F01*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! T3 ! Arithmetic average for F01*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! T5 ! Arithmetic average for F01*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! VSV ! Arithmetic average for F01*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! VBV ! Arithmetic average for F01*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! HPT ! Arithmetic average for F01*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! LPT ! Arithmetic average for F01*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! GLE ! Arithmetic average for F01*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! PD ! Arithmetic average for F01*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! TN ! Arithmetic average for F01*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! PT2 ! Arithmetic average for F01*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! OIQH ! Value from the last calculation ! |
| !--------------!------------------------------------------------------! |
| ! VN * ! Arithmetic average for F01*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! VL * ! Arithmetic average for F01*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! PHA * ! Arithmetic average for F01*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! PHT * ! Arithmetic average for F01*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! VC ! Arithmetic average for F01*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! VH ! Arithmetic average for F01*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! EVM ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! OIP ! Arithmetic average for F01*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! OIT ! Arithmetic average for F01*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! ECW1 ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! SSEL ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! * Remark: Special logic for print values for the parameters in ! |
| ! report line V3, V4, V5 and V6 refer Report Logic ! |
| ! description item 9 and 10. ! |
| +---------------------------------------------------------------------+ |
(8) Parameter Logic
| +---------------------------------------------------------------------+ |
| ! Param. ! Print Value (Standard Progr.) ! |
| !--------------!------------------------------------------------------! |
| ! ESN ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! EHRS ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! ERT ! Value at moment of trigger ! |
| !--------------! -----------------------------------------------------! |
| ! ECYC ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! AP ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! QE ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! N1 *1 ! Arithmetic average for F01*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! N1C ! Arithmetic average for F01*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! N2 ! Arithmetic average for F01*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! EGT ! Arithmetic average for F01*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! FF ! Arithmetic average for F01*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! PS13 ! Arithmetic average for F01*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! P25 ! Arithmetic average for F01*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! T25 ! Arithmetic average for F01*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! P3 ! Arithmetic average for F01*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! T3 ! Arithmetic average for F01*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! T5 ! Arithmetic average for F01*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! VSV ! Arithmetic average for F01*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! VBV ! Arithmetic average for F01*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! HPT ! Arithmetic average for F01*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! LPT ! Arithmetic average for F01*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! GLE ! Arithmetic average for F01*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! PD ! Arithmetic average for F01*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! TN ! Arithmetic average for F01*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! PT2 ! Arithmetic average for F01*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! OIQH ! Value from the last calculation ! |
| !--------------!------------------------------------------------------! |
| ! VN * ! Arithmetic average for F01*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! VL * ! Arithmetic average for F01*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! PHA * ! Arithmetic average for F01*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! PHT * ! Arithmetic average for F01*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! VC ! Arithmetic average for F01*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! VH ! Arithmetic average for F01*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! EVM ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! OIP ! Arithmetic average for F01*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! OIT ! Arithmetic average for F01*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! ECW1 ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! SSEL ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! * Remark: Special logic for print values for the parameters in ! |
| ! report line V3, V4, V5 and V6 refer Report Logic ! |
| ! description item 9 and 10. ! |
| +---------------------------------------------------------------------+ |
(9) Engine Cruise Report Logic <01> (Engine Type CFMI with Advanced EVMU)
| +----------------------------------------------------------------------+ |
| !Code!Item ! !Progr.!Standard ! |
| ! No.!No. ! Description of Function Item !MCDU !Value or ! |
| ! ! ! !GSE !Table ! |
| !----!------!-----------------------------------------!------!---------! |
| ! !A ! Report Format ! ! ! |
| ! !B ! Parameter Table ! ! ! |
| ! !C ! First three lines of Report ! C ! Blank ! |
| ! !D ! Print-out Rules ! C ! 2 ! |
| ! !E ! Transfer to ACARS MU ! C ! No ! |
| ! !F ! Increment of the report counter if the ! C ! 1 ! |
| ! ! ! report was triggered by a code number ! ! ! |
| ! ! ! > 1000; 1=yes, 0=no ! ! ! |
| ! !G ! Average intervals in seconds ! C ! 20 ! |
| ! !H ! Overall average of 'F01' averages ! C ! 5 ! |
| ! !I.1 ! OIQ 'Y01.3' seconds before flight phase ! AI ! 5 ! |
| ! ! ! change from 2 to 3. ! ! ! |
| ! !I.2 ! OIQ 'Y01.4' seconds after beginning of ! AI ! 10 ! |
| ! ! ! flight phase 9. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !1000!1 ! Manual selection via MCDU ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !2000!2 ! Flight phase dependent manual ! ! ! |
| ! ! ! selection via remote print button ! ! ! |
| ! ! ! if programmed. ! ! ! |
| ! !2.1 ! Remote Print Button assignment. ! C ! not ! |
| !----!------!-----------------------------------------!------!---------! |
| !3000!3 ! Programmable Start Logic ! ! ! |
| ! !3.1 ! Trigger condition ! C ! not ! |
| !----!------!-----------------------------------------!------!---------! |
| !4000! ! The DMU generates the Engine Cruise ! ! ! |
| ! ! ! Report based on 'Flight Hours' or ! ! ! |
| ! ! ! Flight Legs' programmable via GSE. ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! Logic based on Flight Hours: ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! After starting each new time period of ! ! ! |
| ! ! ! 'Y01.1' flight hours and during the ! ! ! |
| ! ! ! first entry into flight phase 6 after ! ! ! |
| ! ! ! 'Y01.2' minutes the stable frame cri- ! ! ! |
| ! ! ! teria are not met, then an Eng. Cruise ! ! ! |
| ! ! ! Report is generated and stored in the ! ! ! |
| ! ! ! report buffer. The report contains in ! ! ! |
| ! ! ! the last line the message: ! ! ! |
| ! ! ! NO STABLE FRAME CONDITION ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! Logic based on Flight Legs: ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! Every 'Y01.3' flight legs and if 'Y01.2'! ! ! |
| ! ! ! minutes after entry in cruise phase the ! ! ! |
| ! ! ! stable frame criteria are not met an ! ! ! |
| ! ! ! Engine Cruise Report is generated and ! ! ! |
| ! ! ! stored in the report buffer. The report ! ! ! |
| ! ! ! contains in the last line the message: ! ! ! |
| ! ! ! NO STABLE FRAME CONDITION ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! In this case, the average interval is ! ! ! |
| ! ! ! fixed to 20 seconds. ! ! ! |
| ! ! ! ! ! ! |
| ! !4 ! The default programming is 'Flight Legs'! C ! Legs ! |
| ! ! ! ! ! ! |
| ! !4.1 ! 'Y01.1' flight hours ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.2 ! 'Y01.2' minutes after cruise ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.3 ! 'Y01.3' flight legs ! C ! limit- ! |
| ! ! ! ! ! table ! |
| !----!------!-----------------------------------------!------!---------! |
| !5000! ! The DMU shall generate the Engine ! ! ! |
| ! ! ! Cruise Report based on 'Flight Hours' ! ! ! |
| ! ! ! or 'Flight Legs' programmable via GSE. ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! Logic based on Flight Hours: ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! During a time frame of 'Y01.1' flight ! ! ! |
| ! ! ! hours, the DMU searches in flight ! ! ! |
| ! ! ! phase 6 for report generation with ! ! ! |
| ! ! ! stable frame criteria where the best ! ! ! |
| ! ! ! aircraft quality number QA is ! ! ! |
| ! ! ! calculated.The report with the best ! ! ! |
| ! ! ! quality number QA is stored in the ! ! ! |
| ! ! ! report buffer and the report stored ! ! ! |
| ! ! ! according to logic 4000 is deleted. ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! Logic based on Flight Legs: ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! Every 'Y01.3' flight legs, the DMU ! ! ! |
| ! ! ! searches in flight phase 6 for report ! ! ! |
| ! ! ! generation with stable frame criteria ! ! ! |
| ! ! ! where the best aircraft quality number ! ! ! |
| ! ! ! QA is calculated. ! ! ! |
| ! ! ! The report with the best quality number ! ! ! |
| ! ! ! QA is stored in the report buffer and ! ! ! |
| ! ! ! the report stored according to logic ! ! ! |
| ! ! ! 4000 is deleted. ! ! ! |
| ! ! ! ! ! ! |
| ! !5 ! The default programming is 'Flight Legs'! C ! Legs ! |
| ! ! ! ! ! ! |
| ! ! ! Parameter for stable frame criteria ! ! ! |
| ! !5.1 ! 'P01' stable period ! C ! limit- ! |
| ! ! ! (5 subperiods=100 sec.) ! ! table ! |
| ! ! ! Stable frame basic condition in order ! ! ! |
| ! ! ! to avoid report triggering in flight ! ! ! |
| ! ! ! phases where parameters are of no use. ! ! ! |
| ! !5.2 ! HPTL1 < HPT < HPTL2 ! ! ! |
| ! ! ! HPT = 7C.1.306.01 Eng 1 ! ! ! |
| ! ! ! 7C.2.306.10 Eng 2 ! ! ! |
| ! !5.2.1 ! HPTL1 lower limit in % ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.2.2 ! HPTL2 upper limit in % ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! ! ! Stable frame conditions: ! ! ! |
| ! ! ! During 'P01' seconds the following ! ! ! |
| ! ! ! parameters are stable as defined below: ! ! ! |
| ! ! ! ! ! ! |
| ! !5.3 ! IALT 04.1.361.-- ft ! C ! limit- ! |
| ! ! ! 04.2.361.-- ! ! table ! |
| ! !5.3.1 ! WA of IALT ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.4 ! GS 04.1.312.01 kts ! C ! limit- ! |
| ! ! ! 04.2.312.10 ! ! table ! |
| ! !5.4.1 ! WA of GS ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.5 ! ROLL 04.1.325.01 degr. ! C ! limit- ! |
| ! ! ! ANGLE 04.2.325.10 ! ! table ! |
| ! !5.5.1 ! WA of ROLL ANGLE ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.6 ! TAT 06.1.211.01 C ! C ! limit- ! |
| ! ! ! 06.2.211.10 ! ! table ! |
| ! !5.6.1 ! WA of TAT ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.7 ! N2 7C.1.344.01 Eng.1 % ! C ! limit- ! |
| ! ! ! 7C.2.344.10 Eng.2 ! ! table ! |
| ! !5.7.1 ! WA of N2 ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.8 ! EGT 7C.1.345.01 Eng.1 C ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.8.1 ! WA of EGT ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.9 ! VACC 04.1.364.01 g ! C ! limit- ! |
| ! ! ! 04.2.364.10 ! ! table ! |
| ! !5.9.1 ! WA of VACC ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.10 ! MN 06.1.205.01 Mach ! C ! limit- ! |
| ! ! ! 06.2.205.10 ! ! table ! |
| ! !5.10.1! WA of MN ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.11 ! N1 7C.1.346.01 Eng.1 % ! C ! limit- ! |
| ! ! ! 7C.2.346.10 Eng.2 ! ! table ! |
| ! !5.11.1! WA of N1 ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.12 ! PT2 7C.1.131.91 Eng.1 psia ! C ! limit- ! |
| ! ! ! 7C.2.131.10 Eng.2 ! ! table ! |
| ! !5.12.1! WA of PT2 ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.13 ! FF 7C.1.244.01 Eng.1 kg/h ! C ! limit- ! |
| ! ! ! 7C.2.244.10 Eng.2 ! ! table ! |
| ! !5.13.1! WA of FF ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.14 ! HPT 7C.1.306.01 Eng.1 % ! C ! limit- ! |
| ! ! ! 7C.2.306.10 Eng.2 ! ! table ! |
| ! !5.14.1! WA of HPT ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.15 ! LPT 7C.1.307.01 Eng.1 % ! C ! limit- ! |
| ! ! ! 7C.2.307.10 Eng.2 ! ! table ! |
| ! !5.15.1! WA of LPT ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! ! ! HPT and LPT variation are programmable ! ! ! |
| ! ! ! in the range from 0.0 to 99.9 %. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !6001!6 ! Independently of the other logic, a best! ! ! |
| !6002! ! stable frame search logic for an Eng. ! ! ! |
| !6003! ! Cruise Rep.<01> is started as long as ! ! ! |
| !6004! ! 'X01' is not zero (once per leg only). ! ! ! |
| !6005! ! Each time when an Eng. Cruise Rep. <01> ! ! ! |
| ! . ! ! was generated by this logic, the num- ! ! ! |
| ! . ! ! ber 'X01' is decremented until zero is ! ! ! |
| ! . ! ! reached. ! ! ! |
| ! . ! ! ! ! ! |
| !600X! ! The start value of 'X01' is programmable! ! ! |
| ! ! ! ! ! ! |
| ! ! ! In case of change engine serial number, ! ! ! |
| ! ! ! 'X01' is automatically set to 5. ! ! ! |
| ! ! ! ! ! ! |
| ! !6.1 ! Number 'X01' for consecutive reports up ! ! ! |
| ! ! ! to 9. ! C ! limit- ! |
| ! ! ! ! ! table ! |
| !----!------!-----------------------------------------!------!---------! |
| !7000!7 ! In case the ENGINE DIVERGENCE REPORT ! ! ! |
| ! ! ! <09> was generated, the stable frame ! ! ! |
| ! ! ! search logic for the ENGINE CRUISE REP. ! ! ! |
| ! ! ! <01> is started immediately independent-! ! ! |
| ! ! ! ly of the best stable frame logic and ! ! ! |
| ! ! ! the report is generated with code 7000. ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! In case that further Diver gence Reports! ! ! |
| ! ! ! are generated before a Cruise Report is ! ! ! |
| ! ! ! initiated, there is only one Eng. Cruise! ! ! |
| ! ! ! Report. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !8100!8.1 ! ACARS MU uplink request with IMI 'REQ01'! ! ! |
| ! ! ! The report <01> is immediately generated! ! ! |
| ! ! ! and transmitted to the ACARS MU. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !8200!8.2 ! ACARS MU uplink request with IMI 'G01' ! ! ! |
| ! ! ! The report <01> is generated as soon as ! ! ! |
| ! ! ! stable frame criteria are met, i.e. the ! ! ! |
| ! ! ! DMU immediately starts searching for ! ! ! |
| ! ! ! stable frame criteria independently of ! ! ! |
| ! ! ! any other logic. ! ! ! |
| !----------------------------------------------------------------------! |
| ! A = Programmable by Airbus ! |
| ! C = Programmable by Customer ! |
| +----------------------------------------------------------------------+ |
(10) Engine Cruise Report Logic (Engine Type CFMI)
| +----------------------------------------------------------------------+ |
| !Code!Item ! !Progr.!Standard ! |
| ! No.!No. ! Description of Function Item !MCDU !Value or ! |
| ! ! ! !/GSE !Table TXY! |
| !----!------!-----------------------------------------!------!---------! |
| ! !A ! Report Format ! ! ! |
| ! !B ! Parameter Table ! ! ! |
| ! !C ! First three lines of Report ! C ! Blank ! |
| ! !D ! Print-out Rules ! C ! see ! |
| ! ! ! ! ! separate! |
| ! ! ! ! ! list ! |
| ! !E ! Transfer to ACARS MU ! C ! see ! |
| ! ! ! ! ! separate! |
| ! ! ! ! ! list ! |
| ! !F ! Increment of the report counter if the ! C ! 1 ! |
| ! ! ! report was triggered by a code number ! ! ! |
| ! ! ! > 1000; 1=yes, 0=no ! ! ! |
| ! !G ! Average intervals in seconds ! C ! 20 ! |
| ! !H ! Overall average of 'F01' averages ! C ! 5 ! |
| ! !I.1 ! OIQ 'Y01.5' seconds before flight phase ! A ! 5 ! |
| ! ! ! change from 2 to 3. ! ! ! |
| ! !I.2 ! OIQ 'Y01.4' seconds after beginning of ! A ! 10 ! |
| ! ! ! flight phase 9. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !1000!1 ! Manual selection via MCDU ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !2000!2 ! Flight phase dependent manual ! ! ! |
| ! ! ! selection via remote print button ! ! ! |
| ! ! ! if programmed. ! ! ! |
| ! !2.1 ! Remote Print Button assignment. ! C ! not ass.! |
| !----!------!-----------------------------------------!------!---------! |
| !3000!3 ! Programmable Start Logic ! ! ! |
| ! !3.1 ! Trigger condition ! C ! not ! |
| ! ! ! ! ! progr. ! |
| !----!------!-----------------------------------------!------!---------! |
| !4000! ! The DMU generates the Engine Cruise ! ! ! |
| ! ! ! Report based on 'Flight Hours' or ! ! ! |
| ! ! ! 'Flight Legs' programmable via GSE. ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! Logic based on Flight Hours: ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! After starting each new time period of ! ! ! |
| ! ! ! 'Y01.1' flight hours and during the ! ! ! |
| ! ! ! first entry into flight phase 6 after ! ! ! |
| ! ! ! 'Y01.2' minutes the stable frame cri- ! ! ! |
| ! ! ! teria are not met, then an Eng. Cruise ! ! ! |
| ! ! ! Report is generated and stored in the ! ! ! |
| ! ! ! report buffer. The report contains in ! ! ! |
| ! ! ! the last line the message: ! ! ! |
| ! ! ! NO STABLE FRAME CONDITION ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! Logic based on Flight Legs: ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! Every 'Y01.3' flight legs and if 'Y01.2'! ! ! |
| ! ! ! minutes after entry in cruise phase the ! ! ! |
| ! ! ! stable frame criteria is not met, an ! ! ! |
| ! ! ! Engine Cruise Report is generated and ! ! ! |
| ! ! ! stored in the report buffer. The report ! ! ! |
| ! ! ! contains in the last line the message: ! ! ! |
| ! ! ! NO STABLE FRAME CONDITION ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! In this case the average interval is ! ! ! |
| ! ! ! fixed to 20 seconds. ! ! ! |
| ! ! ! ! ! ! |
| ! !4 ! The default programming is 'Flight Legs'! C ! Legs ! |
| !----!------!-----------------------------------------!------!---------! |
| ! !4.1 ! 'Y01.1' flight hours ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.2 ! 'Y01.2' minutes after cruise ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.3 ! 'Y01.3' flight legs ! C ! limit- ! |
| ! ! ! ! ! table ! |
| !----!------!-----------------------------------------!------!---------! |
| !5000! ! The DMU shall generate the Engine ! ! ! |
| ! ! ! Cruise Report based on 'Flight Hours' ! ! ! |
| ! ! ! or 'Flight Legs' programmable via GSE. ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! Logic based on Flight Hours: ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! During a time frame of 'Y01.1' flight ! ! ! |
| ! ! ! hours, the DMU searches in flight ! ! ! |
| ! ! ! phase 6 for report generation with ! ! ! |
| ! ! ! stable frame criteria where the best ! ! ! |
| ! ! ! aircraft quality number QE is ! ! ! |
| ! ! ! calculated.The report with the best ! ! ! |
| ! ! ! quality number QE is stored in the ! ! ! |
| ! ! ! report buffer and the report stored ! ! ! |
| ! ! ! according to logic 4000 is deleted. ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! Logic based on Flight Legs: ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! Every 'Y01.3' flight legs, the DMU ! ! ! |
| ! ! ! searches in flight phase 6 for report ! ! ! |
| ! ! ! generation with stable frame criteria ! ! ! |
| ! ! ! where the best aircraft quality number ! ! ! |
| ! ! ! QE is calculated. ! ! ! |
| ! ! ! The report with the best quality number ! ! ! |
| ! ! ! QE is stored in the report buffer and ! ! ! |
| ! ! ! the report stored according to logic ! ! ! |
| ! ! ! 4000 is deleted. ! ! ! |
| ! !5 ! The default programming is 'Flight Legs'! C ! Legs ! |
| !----!------!-----------------------------------------!------!---------! |
| ! ! ! ! ! ! |
| ! ! ! Parameter for stable frame criteria ! ! ! |
| ! !5.1 ! 'P01' stable period ! C ! limit- ! |
| ! ! ! (5 subperiods=100 sec.) ! ! table ! |
| ! ! ! Stable frame basic condition in order ! ! ! |
| ! ! ! to avoid report triggering in flight ! ! ! |
| ! ! ! phases where parameters are of no use. ! ! ! |
| ! !5.2 ! HPTL1 < HPT < HPTL2 ! ! ! |
| ! ! ! HPT = 7C.1.306.01 Eng 1 ! ! ! |
| ! ! ! 7C.2.306.10 Eng 2 ! ! ! |
| ! !5.2.1 ! HPTL1 lower limit in % ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.2.2 ! HPTL2 upper limit in % ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! ! ! Stable frame conditions: ! ! ! |
| ! ! ! During 'P01' seconds the following ! ! ! |
| ! ! ! parameters are stable as defined below: ! ! ! |
| ! ! ! ! ! ! |
| ! !5.3 ! IALT 04.1.361.-- ft ! C ! limit- ! |
| ! ! ! 04.2.361.-- ! ! table ! |
| ! !5.3.1 ! Wa of IALT ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.4 ! GS 04.1.312.01 kts ! C ! limit- ! |
| ! ! ! 04.2.312.10 ! ! table ! |
| ! !5.4.1 ! Wa of GS ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.5 ! ROLL 04.1.325.01 degr. ! C ! limit- ! |
| ! ! ! ANGLE 04.2.325.10 ! ! table ! |
| ! !5.5.1 ! Wa of ROLL ANGLE ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.6 ! TAT 06.1.211.01 C ! C ! limit- ! |
| ! ! ! 06.2.211.10 ! ! table ! |
| ! !5.6.1 ! Wa of TAT ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.7 ! N2 7C.1.344.01 Eng.1 % ! C ! limit- ! |
| ! ! ! 7C.2.344.10 Eng.2 ! ! table ! |
| ! !5.7.1 ! Wa of N2 ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.8 ! EGT 7C.1.345.01 Eng.1 C ! C ! limit- ! |
| ! ! ! 7C.1.345.10 Eng.2 ! ! table ! |
| ! !5.8.1 ! Wa of EGT ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.9 ! VACC 04.1.364.01 g ! C ! limit- ! |
| ! ! ! 04.2.364.10 ! ! table ! |
| ! !5.9.1 ! Wa of VACC ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.10 ! MN 06.1.205.01 Mach ! C ! limit- ! |
| ! ! ! 06.2.205.10 ! ! table ! |
| ! !5.10.1! Wa of MN ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.11 ! N1 7C.1.346.01 Eng.1 % ! C ! limit- ! |
| ! ! ! 7C.2.346.10 Eng.2 ! ! table ! |
| ! !5.11.1! Wa of N1 ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.12 ! PT2 7C.1.131.01 Eng.1 psia ! C ! limit- ! |
| ! ! ! 7C.2.131.10 Eng.2 ! ! table ! |
| ! !5.12.1! Wa of PT2 ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.13 ! FF 7C.1.244.01 Eng.1 kg/h ! C ! limit- ! |
| ! ! ! 7C.2.244.10 Eng.2 ! ! table ! |
| ! !5.13.1! Wa of FF ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.14 ! HPT 7C.1.306.01 Eng.1 % ! C ! limit- ! |
| ! ! ! 7C.2.306.10 Eng.2 ! ! table ! |
| ! !5.14.1! Wa of HPT ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.15 ! LPT 7C.1.307.01 Eng.1 % ! C ! limit- ! |
| ! ! ! 7C.2.307.10 Eng.2 ! ! table ! |
| ! !5.15.1! Wa of LPT ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! ! ! HPT and LPT variation are programmable ! ! ! |
| ! ! ! in the range from 0.0 to 99.9 %. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !6001!6 ! Independent from the other logic, a best! ! ! |
| !6002! ! stable frame search logic for an Eng. ! ! ! |
| !6003! ! Cruise Rep.<01> is started as long as ! ! ! |
| !6004! ! 'X01' is not zero (once per leg only). ! ! ! |
| !6005! ! Each time when an Eng. Cruise Rep. <01> ! ! ! |
| ! . ! ! was generated by this logic, the num- ! ! ! |
| ! . ! ! ber 'X01' is decremented until zero is ! ! ! |
| ! . ! ! reached. ! ! ! |
| ! . ! ! ! ! ! |
| !600X! ! The start value of 'X01' is programmable! ! ! |
| ! ! ! ! ! ! |
| ! ! ! In case of change engine serial number, ! ! ! |
| ! ! ! 'X01' is automatically set to 5. ! ! ! |
| ! ! ! ! ! ! |
| ! !6.1 ! Number 'X01' for consecutive reports up ! C ! limit- ! |
| ! ! ! to 9. ! ! table ! |
| !----!------!-----------------------------------------!------!---------! |
| !7000!7 ! In case the ENGINE DIVERGENCE REPORT ! ! ! |
| ! ! ! <09> was generated, the stable frame ! ! ! |
| ! ! ! search logic for the ENGINE CRUISE REP. ! ! ! |
| ! ! ! <01> is started immediately independent-! ! ! |
| ! ! ! ly of the best stable frame logic and ! ! ! |
| ! ! ! the report is generated with code 7000. ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! In case that further Divergence Reports ! ! ! |
| ! ! ! are generated before a Cruise Report is ! ! ! |
| ! ! ! initiated, there is only one Eng. Cruise! ! ! |
| ! ! ! Report. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !8100!8.1 ! ACARS MU uplink request with IMI 'REQ01'! ! ! |
| ! ! ! The report <01> is immediately generated! ! ! |
| ! ! ! and transmitted to the ACARS MU. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !8200!8.2 ! ACARS MU uplink request with IMI 'G01' ! ! ! |
| ! ! ! The report <01> is generated as soon as ! ! ! |
| ! ! ! stable frame criteria are met, i.e. the ! ! ! |
| ! ! ! DMU immediately starts searching for ! ! ! |
| ! ! ! stable frame criteria independently of ! ! ! |
| ! ! ! any other logic. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| ! ! 9 ! The parameters VN, VL, PHA, PHT and N1 ! ! ! |
| ! ! ! in report line V3 and V4 shall be from ! ! ! |
| ! ! ! the last descent (PH 7.1) when N1 is ! ! ! |
| ! ! ! within N1 target 'N1T.1'+/- a tolerance ! ! ! |
| ! ! ! band of 'X1.1' %rpm. This stable ! ! ! |
| ! ! ! conditions shall be kept for a time ! ! ! |
| ! ! ! period of 'T1.1' seconds. The vibration ! ! ! |
| ! ! ! parameters shall be average about the ! ! ! |
| ! ! ! 'T1.1' observing time period and stored ! ! ! |
| ! ! ! in the DMU until the next stable descent! ! ! |
| ! ! ! is detected. In case of report ! ! ! |
| ! ! ! generation the last stored value shall ! ! ! |
| ! ! ! be printed. ! ! ! |
| ! ! ! ! ! ! |
| ! !9.1 ! 'N1T.1' %rpm stable N1 value for descent! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !9.2 ! 'X1.1' %rpmn tolerance band for descent ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !9.3 ! 'T1.1' seconds stable observing time for! C ! limit- ! |
| ! ! ! descent (max. 20 sec) ! ! table ! |
| !----!------!-----------------------------------------!------!---------! |
| ! !10 ! The parameters VN, VL, PHA, PHT and N1 ! ! ! |
| ! ! ! in report line V5 and V6 shall be from ! ! ! |
| ! ! ! the last stable take-off. It means the ! ! ! |
| ! ! ! a.m. parameters shall be computed during! ! ! |
| ! ! ! climb (PH 5.1) when N1 is within N1 ! ! ! |
| ! ! ! target 'N1T.2' +/- a tolerance band of ! ! ! |
| ! ! ! 'X1.2' %rpm. This stable conditions ! ! ! |
| ! ! ! shall be kept for a time period of ! ! ! |
| ! ! ! 'T1.2' seconds. The vibration parameters! ! ! |
| ! ! ! shall be averaged about the 'T1.2' ! ! ! |
| ! ! ! observing time period and stored in the ! ! ! |
| ! ! ! DMU until the next stable take off is ! ! ! |
| ! ! ! detected. In case of report generation ! ! ! |
| ! ! ! the last stored value shall be printed. ! ! ! |
| ! ! 10.1 ! 'N1T.2' %rpm stable N1 value for climb ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! ! 10.2 ! 'X1.2' %rpm tolerance band for climb ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! ! 10.3 ! 'T1.2' seconds stable observing time for! C ! limit- ! |
| ! ! ! climb (max. 20 seconds) ! ! table ! |
| !----------------------------------------------------------------------! |
| ! A = Programmable by Airbus ! |
| ! C = Programmable by Customer ! |
| +----------------------------------------------------------------------+ |
(11) Engine Cruise Report Logic (Engine Type CFMI)
| +----------------------------------------------------------------------+ |
| !Code!Item ! !Progr.!Standard ! |
| ! No.!No. ! Description of Function Item !------!Value or ! |
| ! ! ! !MCDU/ !Table TXY! |
| ! ! ! !GSE ! ! |
| !----!------!-----------------------------------------!------!---------! |
| ! !A ! Report Format ! ! ! |
| ! !A.1 ! "R001RLID" Report Layout Identifier ! ! 01 ! |
| ! ! ! (for ACARS header) ! ! ! |
| ! !A.2 ! "R001RLIS" Report Layout Issue ! ! 01 ! |
| ! ! ! (for ACARS header) ! ! ! |
| ! !B ! Parameter Table ! ! ! |
| ! !C ! First three lines of Report ! C ! Blank ! |
| ! !D ! Print-out Rules ! C ! see ! |
| ! ! ! ! ! separate! |
| ! ! ! ! ! list ! |
| ! !E ! Transfer to ACARS MU ! C ! see ! |
| ! ! ! ! ! separate! |
| ! ! ! ! ! list ! |
| ! !F ! Increment of the report counter if the ! C ! 1 ! |
| ! ! ! report was triggered by a code number ! ! ! |
| ! ! ! > 1000; 1=yes, 0=no ! ! ! |
| ! !G ! Average intervals in seconds ! C ! 20 ! |
| ! !H ! Overall average of "F01" averages ! C ! 5 ! |
| ! !I.1 ! OIQ "Y01.5" seconds before flight phase ! A ! 5 ! |
| ! ! ! change from 2 to 3. ! ! ! |
| ! !I.2 ! OIQ "Y01.4" seconds after beginning of ! A ! 10 ! |
| ! ! ! flight phase 9. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !1000!1 ! Manual selection through MCDU ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !2000!2 ! Flight phase dependent manual ! ! ! |
| ! ! ! selection through remote print button ! ! ! |
| ! ! ! if programmed. ! ! ! |
| ! !2.1 ! Remote Print Button assignment. ! C ! not ass.! |
| !----!------!-----------------------------------------!------!---------! |
| !3000!3 ! Programmable Start Logic ! ! not ! |
| ! !3.1 ! Trigger condition ! C ! progr. ! |
| !----!------!-----------------------------------------!------!---------! |
| !4000! ! The DMU generates the Engine Cruise ! ! ! |
| ! ! ! Report based on "Flight Hours" or ! ! ! |
| ! ! ! "Flight Legs" programmable through GSE. ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! Logic based on Flight Hours: ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! After starting each new time period of ! ! ! |
| ! ! ! "Y01.1" flight hours and during the ! ! ! |
| ! ! ! first entry into flight phase 6 after ! ! ! |
| ! ! ! "Y01.2" minutes the stable frame cri- ! ! ! |
| ! ! ! teria are not met, then an Eng. Cruise ! ! ! |
| ! ! ! Report is generated and stored in the ! ! ! |
| ! ! ! report buffer. The report contains in ! ! ! |
| ! ! ! the last line the message: ! ! ! |
| ! ! ! NO STABLE FRAME CONDITION ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! Logic based on Flight Legs: ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! Every "Y01.3" flight legs and if "Y01.2"! ! ! |
| ! ! ! minutes after entry in cruise phase the ! ! ! |
| ! ! ! stable frame criteria is not met, an ! ! ! |
| ! ! ! Engine Cruise Report is generated and ! ! ! |
| ! ! ! stored in the report buffer. The report ! ! ! |
| ! ! ! contains in the last line the message: ! ! ! |
| ! ! ! NO STABLE FRAME CONDITION ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! In this case the average interval is ! ! ! |
| ! ! ! fixed to 20 seconds. ! ! ! |
| ! ! ! ! ! ! |
| ! !4 ! The default programming is "Flight Legs"! C ! Legs ! |
| !----!------!-----------------------------------------!------!---------! |
| ! !4.1 ! "Y01.1" flight hours ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.2 ! "Y01.2" minutes after cruise ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.3 ! "Y01.3" flight legs ! C ! limit- ! |
| ! ! ! ! ! table ! |
| !----!------!-----------------------------------------!------!---------! |
| !5000! ! The DMU generates the Engine Cruise ! ! ! |
| ! ! ! Report based on "Flight Hours" or ! ! ! |
| ! ! ! "Flight Legs" programmable through GSE. ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! Logic based on Flight Hours: ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! During a time frame of "Y01.1" flight ! ! ! |
| ! ! ! hours, the DMU searches in flight ! ! ! |
| ! ! ! phase 6 for report generation with ! ! ! |
| ! ! ! stable frame criteria. ! ! ! |
| ! ! ! The report with the best quality number ! ! ! |
| ! ! ! QE is stored in the report buffer and ! ! ! |
| ! ! ! the report stored according to logic ! ! ! |
| ! ! ! 4000 is deleted. ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! Logic based on Flight Legs: ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! Every "Y01.3" flight legs, the DMU ! ! ! |
| ! ! ! searches in flight phase 6 for report ! ! ! |
| ! ! ! generation with stable frame criteria ! ! ! |
| ! ! ! where the best aircraft quality number ! ! ! |
| ! ! ! QE is calculated. ! ! ! |
| ! ! ! The report with the best quality number ! ! ! |
| ! ! ! QE is stored in the report buffer and ! ! ! |
| ! ! ! the report stored according to logic ! ! ! |
| ! ! ! 4000 is deleted. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| ! !5 ! The default programming is 'Flight Legs'! C ! Legs ! |
| ! ! ! Parameter for stable frame criteria ! ! ! |
| ! ! ! ! ! ! |
| ! !5.1 ! "P01" stable period ! C ! limit- ! |
| ! ! ! (5 subperiods=100 sec.) ! ! table ! |
| ! ! ! Stable frame basic condition in order ! ! ! |
| ! ! ! to avoid report triggering in flight ! ! ! |
| ! ! ! phases where parameters are of no use. ! ! ! |
| ! !5.2 ! HPTL1 < HPT < HPTL2 ! ! ! |
| ! ! ! HPT = 7C.1.306.01 Engine 1 ! ! ! |
| ! ! ! 7C.1.306.10 Engine 2 ! ! ! |
| ! !5.2.1 ! HPTL1 lower limit in % ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.2.2 ! HPTL2 upper limit in % ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! ! ! Stable frame conditions: ! ! ! |
| ! ! ! During "P01" seconds the following ! ! ! |
| ! ! ! parameters are stable as defined below: ! ! ! |
| ! ! ! ! ! ! |
| ! !5.3 ! IALT 04.1.361.-- ft ! C ! limit- ! |
| ! ! ! 04.2.361.--# ! ! table ! |
| ! !5.3.1 ! Wa of IALT ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.4 ! GS 04.1.312.01 kts ! C ! limit- ! |
| ! ! ! 04.2.312.10# ! ! table ! |
| ! !5.4.1 ! Wa of GS ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! ! ! ! ! ! |
| ! ! ! ! ! ! |
| ! !5.5 ! ROLL 04.1.325.01 degr. ! C ! limit- ! |
| ! ! ! ANGLE 04.2.325.10# ! ! table ! |
| ! !5.5.1 ! Wa of ROLL ANGLE ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.6 ! TAT 06.1.211.01 ° ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! ! ! 06.2.211.10# ! ! ! |
| ! !5.6.1 ! Wa of TAT ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.7 ! N2 7C.1.344.01 Eng.1 % ! C ! limit- ! |
| ! ! ! 7C.2.344.10 Eng.2 ! ! table ! |
| ! !5.7.1 ! Wa of N2 ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.8 ! EGT 7C.1.345.01 Eng.1 °C ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! ! ! 7C.2.345.10 Eng.2 ! ! ! |
| ! !5.8.1 ! Wa of EGT ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.9 ! VACC 04.1.364.01 g ! C ! limit- ! |
| ! ! ! 04.2.364.10 ! ! table ! |
| ! !5.9.1 ! Wa of VACC ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.10 ! MN 06.1.205.01 Mach ! C ! limit- ! |
| ! ! ! 06.2.205.10# ! ! table ! |
| ! !5.10.1! Wa of MN ! ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.11 ! N1 7C.1.346.01 Eng.1 % ! C ! limit- ! |
| ! ! ! 7C.2.346.10# Eng.2 ! ! table ! |
| ! !5.11.1! Wa of N1 ! C ! ! |
| ! !5.12 ! PT2 7C.1.131.01 Eng.1 psia ! C ! limit- ! |
| ! ! ! 7C.2.131.10 Eng.2 ! ! table ! |
| ! !5.12.1! Wa of PT2 ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.13 ! FF 7C.1.244.01 Eng.1 kg/h ! C ! limit- ! |
| ! ! ! 7C.2.244.10 Eng.2 ! ! table ! |
| ! !5.13.1! Wa of FF ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.14 ! HPT 7C.1.306.01 Eng.1 % ! C ! limit- ! |
| ! ! ! 7C.2.306.10 Eng.2 ! ! table ! |
| ! !5.14.1! Wa of HPT ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.15 ! LPT 7C.1.307.01 Eng.1 % ! C ! limit- ! |
| ! ! ! 7C.2.307.10 Eng.2 ! ! table ! |
| ! !5.15.1! Wa of LPT ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! ! ! HPT and LPT variation are programmable ! ! ! |
| ! ! ! in the range from 0.0 to 99.9 %. ! ! ! |
| !6001!6 ! Independent from the other logic, a best! ! ! |
| !6002! ! stable frame search logic for an Engine ! ! ! |
| !6003! ! Cruise Rep.<01> is started as long as ! ! ! |
| !6004! ! 'X01' is not zero (once per leg only). ! ! ! |
| !6005! ! Each time when an Engine Cruise Report ! ! ! |
| ! ! ! <01> was generated by this logic, the ! ! ! |
| ! ! ! number "X01" is decremented until zero ! ! ! |
| ! ! ! is reached. ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! The start value of "X01" is programmable! ! ! |
| !600X! ! ! ! ! |
| ! ! ! In case of change engine serial number, ! ! ! |
| ! ! ! "X01" is automatically set to 5. ! ! ! |
| ! ! ! ! ! ! |
| ! !6.1 ! Number "X01" for consecutive reports up ! C ! limit- ! |
| ! ! ! to 9. ! ! table ! |
| !----!------!-----------------------------------------!------!---------! |
| !7000!7 ! In case the ENGINE DIVERGENCE REPORT ! ! ! |
| ! ! ! <09> was generated, the stable frame ! ! ! |
| ! ! ! search logic for the ENGINE CRUISE RE- ! ! ! |
| ! ! ! PORT <01> is started immediately inde- ! ! ! |
| ! ! ! pendently of the best stable frame logic! ! ! |
| ! ! ! and the report is generated with code ! ! ! |
| ! ! ! 7000. ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! In case that further Divergence Reports ! ! ! |
| ! ! ! are generated before a Cruise Report is ! ! ! |
| ! ! ! initiated, there is only one Eng. Cruise! ! ! |
| ! ! ! Report. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !8100!8.1 ! ACARS MU uplink request with IMI "REQ01"! ! ! |
| ! ! ! The report <01> is immediately generated! ! ! |
| ! ! ! and transmitted to the ACARS MU. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !8200!8.2 ! ACARS MU uplink request with IMI "G01" ! ! ! |
| ! ! ! The report <01> is generated as soon as ! ! ! |
| ! ! ! stable frame criteria are met, i.e. the ! ! ! |
| ! ! ! DMU immediately starts searching for ! ! ! |
| ! ! ! stable frame criteria independently of ! ! ! |
| ! ! ! any other logic. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| ! ! 9 ! The parameters VN, VL, PHA, PHT and N1 ! ! ! |
| ! ! ! in report line V3 and V4 are from the ! ! ! |
| ! ! ! last descent (PH 7.1) when N1 is within ! ! ! |
| ! ! ! N1 target "N1T.1"+/- a tolerance band of! ! ! |
| ! ! ! of "X1.1" %rpm. This stable conditions ! ! ! |
| ! ! ! are kept for a time period of "T1.1" ! ! ! |
| ! ! ! seconds. The vibration parameters are ! ! ! |
| ! ! ! average about the "T1.1" observing time ! ! ! |
| ! ! ! period and stored in the DMU until the ! ! ! |
| ! ! ! next stable descent is detected. In case! ! ! |
| ! ! ! of report generation the last stored ! ! ! |
| ! ! ! value is printed. ! ! ! |
| ! ! ! ! ! ! |
| ! !9.1 ! "N1T.1" %rpm stable N1 value for descent! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !9.2 ! "X1.1" %rpm tolerance band for descent ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !9.3 ! "T1.1" seconds stable observing time for! C ! limit- ! |
| ! ! ! descent (max. 20 seconds) ! ! table ! |
| !----!------!-----------------------------------------!------!---------! |
| ! !10 ! The parameters VN, VL, PHA, PHT and N1 ! ! ! |
| ! ! ! in report line V5 and V6 are from the ! ! ! |
| ! ! ! last stable take-off. It means the a.m. ! ! ! |
| ! ! ! parameters are computed during climb ! ! ! |
| ! ! ! (PH 5.1) when N1 is within N1 target ! ! ! |
| ! ! ! "N1T.2" +/- a tolerance band of "X1T.2" ! ! ! |
| ! ! ! %rpm. This stable conditions are kept ! ! ! |
| ! ! ! for a time period of "T1.2" seconds. The! ! ! |
| ! ! ! vibration parameters are averaged about ! ! ! |
| ! ! ! the "T1.2" observing time period and ! ! ! |
| ! ! ! stored in the DMU until the next stable ! ! ! |
| ! ! ! take off is detected. In case of report ! ! ! |
| ! ! ! generation the last stored value is ! ! ! |
| ! ! ! printed. ! ! ! |
| ! ! 10.1 ! "N1T.2" %rpm stable N1 value for climb ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! ! 10.2 ! "X1.2" %rpm tolerance band for climb ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! ! 10.3 ! "T1.2" seconds stable observing time for! C ! limit- ! |
| ! ! ! climb (max. 20 seconds) ! ! table ! |
| !----------------------------------------------------------------------! |
| ! A = Programmable by Airbus ! |
| ! C = Programmable by Customer ! |
| +----------------------------------------------------------------------+ |
B. AIDS Reports Print Rules - Default Values for Report <01>
| +------------------------------------------------+ |
| ! ! ! ! |
| ! Code ! Printer Output ! ACARS-output ! |
| ! ! ! ! |
| !-------!-----------------------!----------------! |
| ! ! ! ! |
| ! 1000 ! Print immediatly ! No ACARS ! |
| ! ! ! ! |
| !-------!-----------------------!----------------! |
| ! ! ! ! |
| ! 2000 ! Print immediatly ! No ACARS ! |
| ! ! ! ! |
| !-------!-----------------------!----------------! |
| ! ! ! ! |
| ! 4000 ! Print at landing ! ACARS VHF ! |
| ! ! ! ! |
| !-------!-----------------------!----------------! |
| ! ! ! ! |
| ! 5000 ! Print at landing ! ACARS VHF ! |
| ! ! ! ! |
| !-------!-----------------------!----------------! |
| ! ! ! ! |
| ! 600x ! Print at landing ! ACARS VHF ! |
| ! ! ! ! |
| !-------!-----------------------!----------------! |
| ! ! ! ! |
| ! 7000 ! Print at landing ! ACARS VHF ! |
| ! ! ! ! |
| !-------!-----------------------!----------------! |
| ! ! ! ! |
| ! 8100 ! No print ! ACARS VHF ! |
| ! ! ! ! |
| !-------!-----------------------!----------------! |
| ! ! ! ! |
| ! 8200 ! Print at landing ! ACARS VHF ! |
| ! ! ! ! |
| +------------------------------------------------+ |
| +-------------------------------------------------------------------------+ |
| !Trigger! to ACARS ! to printer ! store ! |
| ! Code !------------------------------ -!-----------------!--------------! |
| ! No !Ground ! VHF ! SAT- ! HF ! at ! imme- ! internal& ! |
| ! ! ! ! COM ! !landing ! diate ! external ! |
| ! ! ! ! ! ! ! !(build in RAM&! |
| ! ! ! ! ! ! ! ! PCMCIA) ! |
| !-------!-------!--------!-------!-------!--------!--------!--------------! |
| ! ! ! If ! ! ! ! If !PCMCIA only if! |
| ! 1000 ! NO ! 'SEND' ! NO ! NO ! !'PRINT' ! 'STORE' ! |
| ! ! !selected! ! ! !selected! selected on ! |
| ! ! !on MCDU ! ! ! !on MCDU ! MCDU ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 2000 ! NO ! NO ! NO ! NO ! ! YES ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 3000 ! NO ! NO ! NO ! NO ! ! NO ! YES ! |
| !-------!-------!--------!------ !-------! !--------!--------------! |
| ! 4000 ! NO ! NO ! NO ! NO ! ! NO ! YES ! |
| !-------!-------!--------!-------!-------! N !--------!--------------! |
| ! 5000 ! NO ! YES ! NO ! NO ! O ! NO ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 6001..! NO ! NO ! NO ! NO ! ! NO ! YES ! |
| ! 600X ! ! ! ! ! ! ! ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 7000 ! NO ! NO ! NO ! NO ! ! NO ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 8100 ! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 8200 ! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| +-------------------------------------------------------------------------+ |
| +-------------------------------------------------------------------------+ |
| !Trigger! to ACARS ! to printer ! store ! |
| ! Code !------------------------------ -!-----------------!--------------! |
| ! No !Ground ! VHF ! SAT- ! HF ! at ! imme- ! internal& ! |
| ! ! ! ! COM ! !landing ! diate ! external ! |
| ! ! ! ! ! ! ! !(build in RAM&! |
| ! ! ! ! ! ! ! ! PCMCIA) ! |
| !-------!-------!--------!-------!-------!--------!--------!--------------! |
| ! 1000 ! NO ! NO ! NO ! NO ! ! YES ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 2000 ! NO ! NO ! NO ! NO ! ! YES ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 3000 ! NO ! NO ! NO ! NO ! ! NO ! YES ! |
| !-------!-------!--------!------ !-------! !--------!--------------! |
| ! 4000 ! NO ! NO ! NO ! NO ! ! NO ! YES ! |
| !-------!-------!--------!-------!-------! N !--------!--------------! |
| ! 5000 ! NO ! YES ! NO ! NO ! O ! NO ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 6001..! NO ! NO ! NO ! NO ! ! NO ! YES ! |
| ! 600X ! ! ! ! ! ! ! ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 7000 ! NO ! NO ! NO ! NO ! ! NO ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 8100 ! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 8200 ! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| +-------------------------------------------------------------------------+ |
C. Cruise Performance Report <02>
Cruise Performance Report <02> (Engine Type CFMI with Advanced EVMU)
Cruise Performance Report <02> (Engine Type CFMI with Advanced EVMU)
Cruise Performance Report <02> (Engine Type CFMI with Advanced EVMU) ** ON A/C NOT FOR ALL
Cruise Performance Report <02> (Engine Type CFMI with Advanced EVMU) ** ON A/C NOT FOR ALL
The cruise performance report is a collection of aircraft and engine information averaged over a period of time in which both the engine and the aircraft met the appropriate stability criteria. The cruise performance report is generated when one of the logic conditions 1000 to 5000 (for details see cruise performance report logic) is present.
Cruise Performance Report <02> (Engine Type CFMI with Advanced EVMU) Cruise Performance Report <02> (Engine Type CFMI with Advanced EVMU) Cruise Performance Report <02> (Engine Type CFMI with Advanced EVMU) ** ON A/C NOT FOR ALL Cruise Performance Report <02> (Engine Type CFMI with Advanced EVMU) ** ON A/C NOT FOR ALL NOTE: For the standard header definition of the report refer to (Ref. AMM D/O 31-36-00-00).
(1) Cruise Performance Report Data Field Description <02> (Engine Type CFMI with Advanced EVMU)
NOTE: Reports that are transmitted from the ACARS system do not have report lines without a line identifier.
NOTE: Only the parts of the CRUISE PERFORMANCE REPORT <02> which are not included in the ENGINE CRUISE REPORT <01> are given in the subsequent table.
| +---------------------------------------------------------------------+ |
| ! Value ! Content Description ! |
| !--------------!------------------------------------------------------! |
| ! TAT ! Total Air Temperature ! |
| ! X999 ! ! |
| ! ! Format: Negative values are shown with '-' on the ! |
| ! ! first position. Otherwise the first ! |
| ! ! position contains '0'. ! |
| ! ! (-60.0 to 99.9 °) ! |
| ! ! ! |
| ! ! Source: ADIRU 06.1.211.01 ! |
| ! ! 06.2.211.10# ! |
| !--------------!------------------------------------------------------! |
| ! ALT ! Standard Altitude (1013 mbar) ! |
| ! X9999 ! ! |
| ! ! Format: Negative values are shown with '-' on the ! |
| ! ! first position. Otherwise the first ! |
| ! ! position is used for the value. ! |
| ! ! (-2000 to 50000 ft) ! |
| ! ! ! |
| ! ! Source: ADIRU 06.1.203.01 ! |
| ! ! 06.2.203.10# ! |
| !--------------!------------------------------------------------------! |
| ! CAS ! Computed Air Speed ! |
| ! 999 ! ! |
| ! ! Format: (30 to 450 kts) ! |
| ! ! ! |
| ! ! Source: ADIRU 06.1.206.01 ! |
| ! ! 06.2.206.10# ! |
| !--------------!------------------------------------------------------! |
| ! MN ! Mach Number ! |
| ! 999 ! ! |
| ! ! Format: (0.100 to 0.999) ! |
| ! ! ! |
| ! ! Source: ADIRU 06.1.205.01 ! |
| ! ! 06.2.205.10# ! |
| !--------------!------------------------------------------------------! |
| ! GW ! Gross Weight ! |
| ! 9999 ! ! |
| ! ! Format: (0 to 9000*10 kg) (0 to 1980*100 lbs) ! |
| ! ! ! |
| ! ! Source: FMGC 02.1.075.00 ! |
| ! ! 02.2.075.00# ! |
| !--------------!------------------------------------------------------! |
| ! CG ! Center of Gravity ! |
| ! 999 ! ! |
| ! ! Format: (0 to 35.0 %MAC) ! |
| ! ! ! |
| ! ! Source: FMGC 02.1.077.00 ! |
| ! ! 02.2.077.00# ! |
| !--------------!------------------------------------------------------! |
| ! QA ! Aircraft Quality Number, Report-Stability ! |
| ! 99 ! ! |
| ! ! Format: (00 to 99) ! |
| ! ! ! |
| ! ! Source: DMU ! |
| ! ! ! |
| ! ! Remark: 00 = best stable frame ! |
| ! ! 99 = worst stable frame ! |
| ! ! The quality number is represented in ! |
| ! ! mathematical form bellow: ! |
| ! ! ! |
| ! ! i=1 VARa(i) ! |
| ! ! QA= SIGMA(Wa(i)*--------------- ! |
| ! ! N TOLa(i)*TOLa(i) ! |
| ! ! ! |
| ! ! QA= Quality Number ! |
| ! ! Wa(i)= Individual weighting factors for the ! |
| ! ! individual quality parameters for the Cruise ! |
| ! ! Performance Report. ! |
| ! ! VARa(i)=Parameter variances ! |
| ! ! TOLa(i)= Variation values for the individual ! |
| ! ! quality parameters for the Cruise ! |
| ! ! Performance Report. ! |
| !--------------!------------------------------------------------------! |
| ! QE ! Engine Quality Number, Report-Stability ! |
| ! 99 ! ! |
| ! ! Format: (00 to 99) ! |
| ! ! ! |
| ! ! Source: DMU ! |
| ! ! ! |
| ! ! Remark: 00 = best stable frame ! |
| ! ! 99 = worst stable frame ! |
| ! ! The quality number is represented in ! |
| ! ! mathematical form bellow: ! |
| ! ! ! |
| ! ! i=1 VARe(i) ! |
| ! ! QE= SIGMA(We(i)*--------------- ! |
| ! ! N TOLe(i)*TOLe(i) ! |
| ! ! ! |
| ! ! QE= Engine quality number ! |
| ! ! We(i)= Individual weighting factors for the ! |
| ! ! individual quality parameters for the ! |
| ! ! Cruise Report. ! |
| ! ! VARe(i)= Parameter variances ! |
| ! ! TOLe(i)= Variation values for the individual ! |
| ! ! quality parameters for the Cruise Report. ! |
| !--------------!------------------------------------------------------! |
| ! WFQ ! Fuel Quantity Inner Cell ! |
| ! 99999 ! ! |
| ! ! Format: (0 to 99999 kg) ! |
| ! ! ! |
| ! ! Source: FQIC 5A.2.257.10 Left Inner Cell Fuel ! |
| ! ! Quantity ! |
| ! ! 5A.2.261.10 Right Inner Cell Fuel ! |
| ! ! Quantity ! |
| ! ! ! |
| ! ! Remark: Report line 'X1' shows Left Inner Cell ! |
| ! ! Fuel Quantity. ! |
| ! ! Report line 'X2' shows Right Inner Cell ! |
| ! ! Fuel Quantity. ! |
| !--------------!------------------------------------------------------! |
| ! ELEV ! Elevator Position ! |
| ! X999 ! ! |
| ! ! Format: Negative values are shown with '-' on the ! |
| ! ! first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-30 to 15 deg) ! |
| ! ! ! |
| ! ! Source: FCDC 6C.1.314.01 Left Elevator Position ! |
| ! ! 6C.2.314.10# ! |
| ! ! 6C.1.334.01 Right Elevator Position ! |
| ! ! 6C.2.334.10# ! |
| ! ! ! |
| ! ! Remark: Report line 'X1' shows the Left Elevator ! |
| ! ! Position. ! |
| ! ! Report line 'X2' shows the Right Elevator ! |
| ! ! Position. ! |
| !--------------!------------------------------------------------------! |
| ! AOA ! Corrected Angle of Attack ! |
| ! X999 ! ! |
| ! ! Format: Negative values are shown with '-' on the ! |
| ! ! first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-30.0 to 85.0 deg) ! |
| ! ! ! |
| ! ! Source: ADIRU 06.1.241.01 AOA System 1 ! |
| ! ! 06.2.241.10 AOA System 2 ! |
| ! ! ! |
| ! ! Remark: Report line 'X1' shows AOA System 1. ! |
| ! ! Report line 'X2' shows AOA System 2. ! |
| !--------------!------------------------------------------------------! |
| ! SLP ! Side Slip Angle ! |
| ! X999 ! ! |
| ! ! Format: Negative values are shown with '-' on the ! |
| ! ! first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-32.0 to 32.0 deg) ! |
| ! ! ! |
| ! ! Source: FAC 0A.1.226.00 SLP System 1 ! |
| ! ! 0A.2.226.00 SLP System 2 ! |
| ! ! ! |
| ! ! Remark: Report line 'X1' shows SLP System 1. ! |
| ! ! Report line 'X2' shows SLP System 2. ! |
| !--------------!------------------------------------------------------! |
| ! CFPG ! Calculated Flight Path Acceleration ! |
| ! X9999 ! ! |
| ! ! Format: Negative values are shown with '-' on the ! |
| ! ! first position. Otherwise the first ! |
| ! ! position is used for the value. ! |
| ! ! (-0.9999 to 4.0000 g) ! |
| ! ! ! |
| ! ! Source: DMU CFPG calculated value based on GS from! |
| ! ! System 1 ! |
| ! ! CFPG calculated value based on GS from! |
| ! ! System 2 ! |
| ! ! ! |
| ! ! GSAV last subperiod-GSAV 1st subperiod ! |
| ! ! CFPG=----------------------------------------------*! |
| ! ! Duration of subperiod*(Number of Subperiods-1) ! |
| ! ! ! |
| ! ! *0.05249 ! |
| ! ! ! |
| ! ! GSAV=Average of Ground Speed (GS) per subperiod ! |
| ! ! (label 04.1.312.01 and 04.2.312.10) ! |
| ! ! ! |
| ! ! Remark: Report line 'X1' shows CFPG calculated with! |
| ! ! GS from ADIRU System 1. ! |
| ! ! Report line' X2' shows CFPG calculated with! |
| ! ! GS from ADIRU System 2. ! |
| !--------------!------------------------------------------------------! |
| ! CIVV ! Calculated Inertial Vertical Speed ! |
| ! X999 ! ! |
| ! ! Format: Negative values are shown with '-' on the ! |
| ! ! first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-999 to 999 ft/min) ! |
| ! ! ! |
| ! ! Source: DMU CIVV calculated value based on IALT ! |
| ! ! from system 1. ! |
| ! ! CIVV calculated value based on IALT ! |
| ! ! from system 2. ! |
| ! ! ! |
| ! ! IALTAV last subperiod-IALTAV 1st subperiod ! |
| ! ! CIVV=----------------------------------------------*! |
| ! ! Duration of subperiod*(Number of Subperiods-1) ! |
| ! ! ! |
| ! ! *60 ! |
| ! ! ! |
| ! ! IALTAV=Average of Inertial Altitude (IALT) per ! |
| ! ! subperiod (label 04.1.361.XX and ! |
| ! ! 04.2.361.XX) ! |
| ! ! ! |
| ! ! Remark: Report line 'X1' shows CIVV calculated with! |
| ! ! IALT from ADIRU System 1. ! |
| ! ! Report line 'X2' shows CIVV calculated with! |
| ! ! IALT from ADIRU System 2. ! |
| !--------------!------------------------------------------------------! |
| ! RUDD ! Rudder Position ! |
| ! X999 ! ! |
| ! ! Format: Negative values are shown with '-' on the ! |
| ! ! first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-30.0 to 30.0 deg) ! |
| ! ! ! |
| ! ! Source: SDAC 29.1.312.00 ! |
| ! ! 29.2.312.00# ! |
| !--------------!------------------------------------------------------! |
| ! RUDT ! Rudder Trim Position ! |
| ! X999 ! ! |
| ! ! Format: Negative values are shown with '-' on the ! |
| ! ! first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-25.0 to 25.0 deg) ! |
| ! ! ! |
| ! ! Source: FAC 0A.1.313.00 ! |
| ! ! 0A.2.313.00# ! |
| !--------------!------------------------------------------------------! |
| ! AILL ! Left Aileron Position ! |
| ! X999 ! ! |
| ! ! Format: Negative values are shown with '-' on the ! |
| ! ! first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-25.0 to 25.0 deg) ! |
| ! ! ! |
| ! ! Source: FCDC 6C.1.310.01 ! |
| ! ! 6C.2.310.10# ! |
| !--------------!------------------------------------------------------! |
| ! AILR ! Right Aileron Position ! |
| ! X999 ! ! |
| ! ! Format: Negative values are shown with '-' on the ! |
| ! ! first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-25.0 to 25.0 deg) ! |
| ! ! ! |
| ! ! Source: FCDC 6C.1.330.01 ! |
| ! ! 6C.2.330.10# ! |
| !--------------!------------------------------------------------------! |
| ! STAB ! Stabilizer Position #1 ! |
| ! X999 ! ! |
| ! ! Format: Negative values are shown with '-' on the ! |
| ! ! first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-13.5 to 4.0 deg) ! |
| ! ! ! |
| ! ! Source: FCDC 6C.1.315.01 ! |
| ! ! 6C.2.315.10# ! |
| !--------------!------------------------------------------------------! |
| ! ROLL ! Roll Angle ! |
| ! X999 ! ! |
| ! ! Format: Negative values are shown with '-' on the ! |
| ! ! first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-90.0 to 90.0 deg) ! |
| ! ! ! |
| ! ! Source: ADIRU 04.1.325.01 ! |
| ! ! 04.2.325.10# ! |
| !--------------!------------------------------------------------------! |
| ! YAW ! Body Axis Yaw Rate ! |
| ! X999 ! ! |
| ! ! Format: Negative values are shown with '-' on the ! |
| ! ! first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-45.0 to 45.0 deg/sec) ! |
| ! ! ! |
| ! ! Source: ADIRU 04.1.330.01 ! |
| ! ! 04.2.330.10# ! |
| !--------------!------------------------------------------------------! |
| ! RSP2 ! Roll Spoiler 2 Position ! |
| ! X999 ! ! |
| ! ! Format: Negative values are shown with '-' on the ! |
| ! ! first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-45.0 to 0 deg) ! |
| ! ! ! |
| ! ! Source: FCDC 6C.1.362.01 Left Spoiler ! |
| ! ! 6C.2.362.10# ! |
| ! ! 6C.1.372.01 Right Spoiler ! |
| ! ! 6C.2.372.10# ! |
| ! ! ! |
| ! ! Remark: Report line 'X4' shows RSP2 left spoiler. ! |
| ! ! Report line 'X5' shows RSP2 right spoiler. ! |
| !--------------!------------------------------------------------------! |
| ! RSP3 ! Roll Spoiler 3 Position ! |
| ! X999 ! ! |
| ! ! Format: Negative values are shown with '-' on the ! |
| ! ! first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-45.0 to 0 deg) ! |
| ! ! ! |
| ! ! Source: FCDC 6C.1.363.01 Left Spoiler ! |
| ! ! 6C.2.363.10# ! |
| ! ! 6C.1.373.01 Right Spoiler ! |
| ! ! 6C.2.373.10# ! |
| ! ! ! |
| ! ! Remark: Report line 'X4' shows RSP3 left spoiler. ! |
| ! ! Report line 'X5' shows RSP3 right spoiler. ! |
| !--------------!------------------------------------------------------! |
| ! RSP4 ! Roll Spoiler 4 Position ! |
| ! X999 ! ! |
| ! ! Format: Negative values are shown with '-' on the ! |
| ! ! first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-45.0 to 0 deg) ! |
| ! ! ! |
| ! ! Source: FCDC 6C.1.364.01 Left Spoiler ! |
| ! ! 6C.2.364.10# ! |
| ! ! 6C.1.374.01 Right Spoiler ! |
| ! ! 6C.2.374.10# ! |
| ! ! ! |
| ! ! Remark: Report line 'X4' shows RSP4 left spoiler. ! |
| ! ! Report line 'X'5 shows RSP4 right spoiler ! |
| !--------------!------------------------------------------------------! |
| ! RSP5 ! Roll Spoiler 5 Position ! |
| ! X999 ! ! |
| ! ! Format: Negative values are shown with '-' on the ! |
| ! ! first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-45.0 to 0 deg) ! |
| ! ! ! |
| ! ! Source: FCDC 6C.1.365.01 Left Spoiler ! |
| ! ! 6C.2.365.10# ! |
| ! ! 6C.1.375.01 Right Spoiler ! |
| ! ! 6C.2.375.10# ! |
| ! ! ! |
| ! ! Remark: Report line 'X4' shows RSP5 left spoiler. ! |
| ! ! Report line 'X5' shows RSP5 right spoiler. ! |
| !--------------!------------------------------------------------------! |
| ! FLAP ! FLAP Actual Position ! |
| ! X999 ! ! |
| ! ! Format: Negative values are shown with '-' on the ! |
| ! ! first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (0.0 to 40.0 deg) ! |
| ! ! (see table DT40 for special conversion) ! |
| ! ! ! |
| ! ! Source: SFCC 1B.1.137.01 FLAP System 1 ! |
| ! ! 1B.2.137.10 FLAP System 2 ! |
| ! ! ! |
| ! ! Remark: Report line 'X4' shows FLAP System 1. ! |
| ! ! Report line 'X5' shows FLAP System 2. ! |
| !--------------!------------------------------------------------------! |
| ! SLAT ! SLAT Actual Position ! |
| ! X999 ! ! |
| ! ! Format: Negative values are shown with '-' on the ! |
| ! ! first position. Otherwise the first ! |
| ! ! position contains a'0'. ! |
| ! ! (0.0 to 27.0 deg) ! |
| ! ! ! |
| ! ! Source: SFCC 1B.1.127.01 SLAT System 1 ! |
| ! ! 1B.2.127.10 SLAT System 2 ! |
| ! ! ! |
| ! ! Remark: Report line 'X4' shows SLAT System 1. ! |
| ! ! Report line 'X5' shows SLAT System 2. ! |
| !--------------!------------------------------------------------------! |
| ! THDG ! True Heading (BCD) ! |
| ! 9999 ! ! |
| ! ! Format: (0 to 359.9 deg) ! |
| ! ! ! |
| ! ! Source: ADIRU 04.1.044.01 THDG System 1 ! |
| ! ! 04.2.044.10 THDG System 1 ! |
| ! ! ! |
| ! ! Remark: Report line 'X6' shows THDG System 1. ! |
| ! ! Report line 'X7' shows THDG System 2. ! |
| !--------------!------------------------------------------------------! |
| ! LONP ! Longitude Position ! |
| ! X9999 ! ! |
| ! ! Format: The first position shows if east or west. ! |
| ! ! 'E' for an East position and 'W' for a West! |
| ! ! position. ! |
| ! ! (East 179.9 deg to West 179.9 deg) ! |
| ! ! ! |
| ! ! Source: ADIRU 04.1.311.01 LONP System 1 ! |
| ! ! 04.2.311.10 LONP System 2 ! |
| ! ! ! |
| ! ! Remark: Report line 'X6' shows LONP System 1. ! |
| ! ! Report line 'X7' shows LONP System 2. ! |
| !--------------!------------------------------------------------------! |
| ! LATP ! Latitude Position ! |
| ! X999 ! ! |
| ! ! Format: The first position shows if north ! |
| ! ! or south 'N' for a North position and 'S' ! |
| ! ! for a South position. ! |
| ! ! (North 89.9 deg to South 89.9 deg) ! |
| ! ! ! |
| ! ! Source: ADIRU 04.1.310.XX LATP System 1 ! |
| ! ! 04.2.310.XX LATP System 2 ! |
| ! ! ! |
| ! ! Remark: Report line 'X6'shows LATP System 1. ! |
| ! ! Report line 'X7' shows LATP System 2. ! |
| !--------------!------------------------------------------------------! |
| ! WS ! Wind Speed ! |
| ! 999 ! ! |
| ! ! Format: (0 to 100 kts) ! |
| ! ! ! |
| ! ! Source: ADIRU 04.1.315.01 WS System 1 ! |
| ! ! 04.2.315.10 WS System 2 ! |
| ! ! ! |
| ! ! Remark: Report line 'X6' shows WS System 1. ! |
| ! ! Report line 'X7' shows WS System 2. ! |
| !--------------!------------------------------------------------------! |
| ! WD ! Wind Direction - True ! |
| ! 999 ! ! |
| ! ! Format: (0 to 359 deg) ! |
| ! ! ! |
| ! ! Source: ADIRU 04.1.316.01 WD System 1 ! |
| ! ! 04.2.316.10 WD System 2 ! |
| ! ! ! |
| ! ! Remark: Report line 'X6' shows WD System 1. ! |
| ! ! Report line 'X7' shows WD System 2. ! |
| !--------------!------------------------------------------------------! |
| ! FT ! Wing Fuel Temperature ! |
| ! X999 ! ! |
| ! ! Format: (-60.0 to 170.0°) ! |
| ! ! ! |
| ! ! Source: FQIC 5A.2.177.10 Fuel Temp. Left Wing Tank ! |
| ! ! 5A.2.210.10 Fuel Temp. Right Wing Tank! |
| ! ! ! |
| ! ! Remark: Report line 'X6' shows the fuel temperature! |
| ! ! from the Left Wing Tank. ! |
| ! ! Report line 'X7' shows the fuel temperature! |
| ! ! from the Right Wing Tank. ! |
| !--------------!------------------------------------------------------! |
| ! FD ! Fuel Density ! |
| ! 0999 ! ! |
| ! ! Format: (0 to 0.999 kg/l) ! |
| ! ! ! |
| ! ! Source: FQIC 5A.2.272.10 ! |
| ! ! ! |
| ! ! Remark: The Fuel Density value of the various tanks! |
| ! ! (Left Wing Tank, Center Tank and Right Wing! |
| ! ! Tank) is transmitted one after another on ! |
| ! ! label 272. The adequate tank identification! |
| ! ! is as follows: ! |
| ! ! ! |
| ! ! For A318, A319 and A320: ! |
| ! ! Bit 11-14 = 0.0001 ! |
| ! ! Bit 15-18 = 0.001 ! |
| ! ! Bit 19-22 = 0.01 ! |
| ! ! Bit 23-26 = 0.1 ! |
| ! ! Bit 27-29 = Fuel tank Ident (Left/Center/Right) ! |
| ! ! ! |
| ! ! For A321: ! |
| ! ! Bit 11-13 = Fuel tank Ident (Left/Center/Right) ! |
| ! ! Bit 14-17 = 0.0001 ! |
| ! ! Bit 18-21 = 0.001 ! |
| ! ! Bit 22-25 = 0.01 ! |
| ! ! Bit 26-29 = 0.1 ! |
| ! ! ! |
| ! ! The update rate of label 272 is 1 second. Due to ! |
| ! ! this fact the Fuel Density value of the dedicated ! |
| ! ! tank is available every 3 seconds. ! |
| +---------------------------------------------------------------------+ |
(2) Cruise Performance Report Data Field Description <02> (Engine Type CFMI with Advanced EVMU)
NOTE: Reports that are transmitted from the ACARS system do not have report lines without a line identifier.
| +---------------------------------------------------------------------+ |
| ! Value ! Content Description ! |
| !--------------!------------------------------------------------------! |
| ! TAT/ALT/CAS/! In the report line CE is the averange value for ! |
| ! MN/GW/CG ! F02 * 20 sec. of System 1 parameters printed. ! |
| ! ! ! |
| ! ! In the report line CN is the averange value for ! |
| ! ! F02 * 20 sec. of System 2 parameters printed. ! |
| !--------------!------------------------------------------------------! |
| ! ESN ! Engine Serial Number ! |
| ! 999999 ! ! |
| ! ! Format: (000000 to 999999) ! |
| ! ! ! |
| ! ! Source: ECU Engine 1 7C.1.046.01 digit 3, 2, 1 ! |
| ! ! 7C.1.047.01 digit 6, 5, 4 ! |
| ! ! ! |
| ! ! Engine 2 7C.2.046.01 digit 3, 2, 1 ! |
| ! ! 7C.2.047.01 digit 6, 5, 4 ! |
| !--------------!------------------------------------------------------! |
| ! EHRS ! Engine Flight Hours ! |
| ! 99999 ! ! |
| ! ! Format: (00000 to 99999 hours) ! |
| ! ! ! |
| ! ! Source: DMU Engine 1 ! |
| ! ! Engine 2 ! |
| ! ! ! |
| ! ! Remark: Time between "Main (LH and RH) Landing ! |
| ! ! Gear Decompressed" and "Main (LH and RH) ! |
| ! ! Landing Gear Compressed". The EHRS is set ! |
| ! ! to zero if a new ESN is recognized by the ! |
| ! ! DMU. It is possible to set the EHRS the ! |
| ! ! MCDU, e.g. if the DMU is changed on the . ! |
| ! ! a/c. ! |
| !--------------!------------------------------------------------------! |
| ! ERT ! Engine Running Time ! |
| ! 99999 ! ! |
| ! ! Format: 00000 to 65536 hours ! |
| ! ! ! |
| ! ! Source: ECU 7C.1.050.01 Engine 1 ! |
| ! ! 7C.2.050.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! ECYC ! Engine Cycle ! |
| ! 99999 ! ! |
| ! ! Format: 00000 to 99999 ! |
| ! ! ! |
| ! ! Source: DMU Engine 1 ! |
| ! ! Engine 2 ! |
| ! ! ! |
| ! ! Remark: Each time when flight phase 5 (climb) is ! |
| ! ! reached, the counter is incremented by one.! |
| ! ! incremented by one. The ECYC is set to zero! |
| ! ! if a new ESN is recognized by the DMU. ! |
| ! ! It is possible to set the ECYC via the ! |
| ! ! MCDU, if the DMU is changed on the a/c. ! |
| ! ! ! |
| !--------------!------------------------------------------------------! |
| ! AP ! Auto Pilot Status ! |
| ! 99 ! ! |
| ! ! Format: Number of respective status 00 to G8 ! |
| ! ! ! |
| ! ! Source: FMGC 1 and 2 (FGC part) for Auto Pilot ! |
| ! ! AP1 and AP2 ! |
| ! ! ! |
| ! ! XX Auto Pilot Modes: ! |
| ! ! !! ! |
| ! ! !!__Lateral Modes: 0 = NO MODE ! |
| ! ! ! 1 = HEADING ! |
| ! ! ! 2 = TRACK ! |
| ! ! ! 3 = NAV ! |
| ! ! ! 4 = LOC CAPTURE ! |
| ! ! ! 5 = LOC TRACK ! |
| ! ! ! 6 = LAND TRACK ! |
| ! ! ! 7 = RUNWAY ! |
| ! ! ! 8 = ROLL GO AROUND ! |
| ! ! ! ! |
| ! ! !__Longitudinal Modes: 0 = NO MODE ! |
| ! ! 1 = PITCH G/A ! |
| ! ! 2 = PITCH T/O ! |
| ! ! 3 = G/S TRACK ! |
| ! ! 4 = G/S CAPTURE ! |
| ! ! 5 = V/S ! |
| ! ! 6 = FPA ! |
| ! ! 7 = ALT ! |
| ! ! 8 = ALT ACQ ! |
| ! ! 9 = OPEN CLB ! |
| ! ! A = OPEN DES ! |
| ! ! B = IM CLB ! |
| ! ! C = IM DES ! |
| ! ! D = CLB ! |
| ! ! E = DES ! |
| ! ! F = FINAL DES ! |
| ! ! G = EXPEDITE ! |
| ! ! ! |
| ! ! AP1 ! AP2 ! |
| ! ! Report Line EC: ! Report Line EE: !Difinition: ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! / ! / !No Mode Act. ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.11 = 1 ! 01.2.275.00.11 = 1!RUNWAY Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.12 = 1 ! 01.2.275.00.12 = 1!NAV Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.13 = 1 ! 01.2.275.00.13 = 1!LOC CAPTURE ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.14 = 1 ! 01.2.275.00.14 = 1!LOC TRACK ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.15 = 1 ! 01.2.275.00.15 = 1!Roll GO ! |
| ! ! ! !AROUND Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.16 = 1 ! 01.2.275.00.16 = 1!HEADING Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.17 = 1 ! 01.2.275.00.17 = 1!TRACK Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.15 = 1 ! 01.2.274.00.15 = 1!PITCH TO Mode! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.16 = 1 ! 01.2.274.00.16 = 1!PITCH GA Mode! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.17 = 1 ! 01.2.274.00.17 = 1!V/S Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.18 = 1 ! 01.2.274.00.18 = 1!FPA Mode ! |
| ! ! -------------------!-------------------!-------------! |
| ! ! 01.1.274.00.19 = 1 ! 01.2.274.00.19 = 1!ALT Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.20 = 1 ! 01.2.274.00.20 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.19 = 1 ! 01.2.274.00.19 = 1!ALT ACQ ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.21 = 1 ! 01.2.274.00.21 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.20 = 1 ! 01.2.274.00.20 = 1!G/S TRACK ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.22 = 1 ! 01.2.274.00.22 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.21 = 1 ! 01.2.274.00.21 = 1!G/S CAPTURE ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.22 = 1 ! 01.2.274.00.22 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.23 = 1 ! 01.2.274.00.23 = 1!FINAL DES ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.2.274.00.24 = 1 ! 01.2.274.00.24 = 1!EXPED. Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.146.00.14 = 1 ! 01.2.146.00.14 = 1!LAND TRACK ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!CLB Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.13 = 0 ! 01.2.274.00.13 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.14 = 0 ! 01.2.274.00.14 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.24 = 0 ! 01.2.274.00.24 = 0! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!DES Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.13 = 0 ! 01.2.274.00.13 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.14 = 0 ! 01.2.274.00.14 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.24 = 0 ! 01.2.274.00.24 = 0! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!IM. CLIMB ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.13 = 1 ! 01.2.274.00.13 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!IM. DES Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.13 = 1 ! 01.2.274.00.13 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!OPEN CLB ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.14 = 1 ! 01.2.274.00.14 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!OPEN DES ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.14 = 1 ! 01.2.274.00.14 = 1! ! |
| ! ! ---------------------------------------------------- ! |
| ! ! Auto Pilot Status DMU: ! |
| ! ! AP1 printed in report line EC ! |
| ! ! AP2 printed in report line EE ! |
| !--------------!------------------------------------------------------! |
| ! QA ! Aircraft Quality Number, Report-Stability ! |
| ! 99 ! ! |
| ! ! Format: (00 to 99) ! |
| ! ! ! |
| ! ! Source: DMU ! |
| ! ! ! |
| ! ! Remark: 00 = best stable frame ! |
| ! ! 99 = worst stable frame ! |
| ! ! The quality number is represented in ! |
| ! ! mathematical form bellow: ! |
| ! ! ! |
| ! ! i=1 VARa(i) ! |
| ! ! QA= SIGMA(Wa(i)*--------------- ! |
| ! ! N TOLa(i)*TOLa(i) ! |
| ! ! ! |
| ! ! QA= Quality Number ! |
| ! ! Wa(i)= Individual weighting factors for the ! |
| ! ! individual quality parameters for the Cruise ! |
| ! ! Performance Report. ! |
| ! ! VARa(i)=Parameter variances ! |
| ! ! TOLa(i)= Variation values for the individual ! |
| ! ! quality parameters for the Cruise ! |
| ! ! Performance Report. ! |
| !--------------!------------------------------------------------------! |
| ! QE ! Engine Quality Number, Report-Stability ! |
| ! 99 ! ! |
| ! ! Format: (00 to 99) ! |
| ! ! ! |
| ! ! Source: DMU ! |
| ! ! ! |
| ! ! Remark: 00 = best stable frame ! |
| ! ! 99 = worst stable frame ! |
| ! ! The quality number is represented in ! |
| ! ! mathematical form bellow: ! |
| ! ! ! |
| ! ! i=1 VARe(i) ! |
| ! ! QE= SIGMA(We(i)*--------------- ! |
| ! ! N TOLe(i)*TOLe(i) ! |
| ! ! ! |
| ! ! QE= Engine quality number ! |
| ! ! We(i)= Individual weighting factors for the ! |
| ! ! individual quality parameters for the ! |
| ! ! Cruise Report. ! |
| ! ! VARe(i)= Parameter variances ! |
| ! ! TOLe(i)= Variation values for the individual ! |
| ! ! quality parameters for the Cruise Report. ! |
| !--------------!------------------------------------------------------! |
| ! N1 ! Selected N1 Actual ! |
| ! 9999 ! ! |
| ! ! Format: (0 to 120.0 %rpm) ! |
| ! ! ! |
| ! ! Source: ECU 7C.1.346.01 Engine 1 ! |
| ! ! 7C.2.346.10 Engine 1 ! |
| ! ! ! |
| ! ! Remark: In report lines 'V3' and 'V4' the values ! |
| ! ! from the last stable descent are printed. ! |
| ! ! In report lines 'V5' and 'V6' the values ! |
| ! ! from the last stable climb are printed. ! |
| ! ! ! |
| !--------------!------------------------------------------------------! |
| ! N1C ! N1 Command ! |
| ! 9999 ! ! |
| ! ! Format: (0 to 120.0 %rpm) ! |
| ! ! ! |
| ! ! Source: ECU 7C.1.341.01 Engine 1 ! |
| ! ! 7C.2.341.10 Engine 1 ! |
| !--------------!------------------------------------------------------! |
| ! N2 ! Selected N2 Actual ! |
| ! 9999 ! ! |
| ! ! Format: (0 to 120.0 %rpm) ! |
| ! ! ! |
| ! ! Source: ECU 7C.1.344.01 Engine 1 ! |
| ! ! 7C.2.344.10 Engine 1 ! |
| !--------------!------------------------------------------------------! |
| ! EGT ! Selected T494 (Exhaust Gas Temperature) ! |
| ! X999 ! ! |
| ! ! Format: Negative values are indicated by 'N' on the! |
| ! ! first position. Otherwise the first ! |
| ! ! position is used for value. ! |
| ! ! (-55 to 999.9 °) ! |
| ! ! ! |
| ! ! Source: ECU 7C.1.345.01 Engine 1 ! |
| ! ! 7C.2.345.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! FF ! Engine Fuel Flow ! |
| ! ! ! |
| ! 9999 ! Format: 0 to 7000 kg/h (0 to 15000 p/h) ! |
| ! ! ! |
| ! ! Source: ECU 7C.1.244.01 Engine 1 ! |
| ! ! 7C.2.244.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! PS13 ! PS13 Static Air Pressure at Position 1.3 ! |
| ! 99999 ! ! |
| ! ! Format: (0.0 to 30.000 psia) ! |
| ! ! ! |
| ! ! Source: ECU 7C.1.127.01 Engine 1 ! |
| ! ! 7C.2.127.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! P25 ! Total Air Pressure at Position 2.5 ! |
| ! 99999 ! ! |
| ! ! Format: (0.0 to 50.000 psia) ! |
| ! ! ! |
| ! ! Source: ECU 7C.1.262.01 Engine 1 ! |
| ! ! 7C.2.262.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! T25 ! Selected T25 ! |
| ! X999 ! ! |
| ! ! Format: Negative values are indicated by 'N' on ! |
| ! ! the first position. Otherwise the first ! |
| ! ! position is used for value. ! |
| ! ! (-55.0 to 120.0 °) ! |
| ! ! ! |
| ! ! Source: ECU 7C.1.263.01 Engine 1 ! |
| ! ! 7C.2.263.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! P3 ! Selected PS3 ! |
| ! 9999 ! ! |
| ! ! Format: ( 0.0 to 450.0 psia) ! |
| ! ! ! |
| ! ! Source: ECU 7C.1.264.01 Engine 1 ! |
| ! ! 7C.2.264.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! T3 ! Selected T3 ! |
| ! X999 ! ! |
| ! ! Format: Negative values are indicated by 'N' on ! |
| ! ! the first position. Otherwise the first ! |
| ! ! position is used for value. ! |
| ! ! (-55.0 to 850.0 °) ! |
| ! ! ! |
| ! ! Source: ECU 7C.1.265.01 Engine 1 ! |
| ! ! 7C.2.265.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! T5 ! Selected T5 ! |
| ! X999 ! ! |
| ! ! Format: Negative values are indicated by 'N' on ! |
| ! ! the first position. Otherwise the first ! |
| ! ! position is used for value. ! |
| ! ! (-55.0 to 850.0 °) ! |
| ! ! ! |
| ! ! Source: ECU 7C.1.260.01 Engine 1 ! |
| ! ! 7C.2.260.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! VSV ! Selected Variable Stator Vane Position ! |
| ! X99 ! ! |
| ! ! Format: Negative values are indicated by 'N' on ! |
| ! ! the first position. Otherwise the first ! |
| ! ! position is used for value. ! |
| ! ! (-5.0 to 45.0 deg) ! |
| ! ! ! |
| ! ! Source: ECU 7C.1.072.01 Engine 1 ! |
| ! ! 7C.2.072.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! VBV ! Variable Bleed Valve Position ! |
| ! X99 ! ! |
| ! ! Format: Negative values are indicated by 'N' on ! |
| ! ! the first position. Otherwise the first ! |
| ! ! position is used for value. ! |
| ! ! (-9.9 to 40.0 deg) ! |
| ! ! ! |
| ! ! Source: ECU 7C.1.071.01 Engine 1 ! |
| ! ! 7C.2.071.10 Engine 2 ! |
| ! ! ! |
| !--------------!------------------------------------------------------! |
| ! HPT ! Selected HPTC Postion ! |
| ! ! ! |
| ! X99 ! Format: (-10 to 100 %) ! |
| ! ! ! |
| ! ! Source: ECU 7C.1.306.01 Engine 1 ! |
| ! ! 7C.2.306.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! LPT ! Selected LPTC Position ! |
| ! X99 ! ! |
| ! ! Format: (-10 to 100 %) ! |
| ! ! ! |
| ! ! Source: ECU 7C.1.307.01 Engine 1 ! |
| ! ! 7C.2.307.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! GLE ! Engine Generator Load ! |
| ! 999 ! ! |
| ! ! Format: (0 to 100 %) ! |
| ! ! ! |
| ! ! Source: SDAC 29.1.077.01 Engine 1 ! |
| ! ! 29.2.077.01 # ! |
| ! ! 29.1.077.10 Engine 2 ! |
| ! ! 29.2.077.10 # ! |
| !--------------!------------------------------------------------------! |
| ! PD ! Precooler Inlet Pressure ! |
| ! 99 ! ! |
| ! ! Format: (0 to 50 psi) ! |
| ! ! ! |
| ! ! Source: BMC 6F.1.143.01 Engine 1 ! |
| ! ! 6F.2.143.10 ! |
| ! ! 6F.1.142.01 Engine 2 ! |
| ! ! 6F.2.142.10 ! |
| !--------------!------------------------------------------------------! |
| ! TN ! Nacelle Temperature ! |
| ! X99 ! ! |
| ! ! Format: Negative values are indicated by 'N' on ! |
| ! ! the first position. Otherwise the first ! |
| ! ! position is used for value. ! |
| ! ! (-55 to 300 °) ! |
| ! ! ! |
| ! ! Source: FWC 26.1.322.01 Engine 1 ! |
| ! ! 26.2.322.01 ! |
| ! ! 26.1.322.10 Engine 2 ! |
| ! ! 26.2.322.10 ! |
| !--------------!------------------------------------------------------! |
| ! PT2 ! Totale Air Pressure at Position 2 ! |
| ! 99999 ! ! |
| ! ! Format: (0.0 to 25.000 psia) ! |
| ! ! ! |
| ! ! Source: ECU 7C.1.131.01 Engine 1 ! |
| ! ! 7C.2.131.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! OIQH ! Oil Consumption from the previous flight ! |
| ! X999 ! ! |
| ! ! Format: (-9.99 to 20.00 qts/h) ! |
| ! ! ! |
| ! ! Source: DMU Engine 1 ! |
| ! ! Engine 2 ! |
| ! ! ! |
| ! ! Remark: Following formula is used. ! |
| ! ! ! |
| ! ! OIKa-OIKb ! |
| ! ! OIQH=---------(qts/h) ! |
| ! ! UTCb-UTCa ! |
| ! ! ! |
| ! ! OIK=oil quantity corrected ! |
| ! ! suffix a denotes taxi out condition ! |
| ! ! suffix b denotes taxi in condition ! |
| ! ! The calculation is done 'Y01.5' seconds before the ! |
| ! ! flight phase changes from 2 to 3 and ! |
| ! ! 'Y01.4' seconds after beginning of flight phase 9. ! |
| ! ! OIKa=OIQa*(A*OITa+B) ! |
| ! ! OIKb=OIQb*(A*OITb+B) ! |
| ! ! OIQ= measured oil quantity 26.1.073.01 Eng 1 ! |
| ! ! 26.2.073.01 # ! |
| ! ! 26.1.073.10 Engine 2 ! |
| ! ! 26.2.073.10 # ! |
| ! ! ! |
| ! ! OIT= oil temperature 26.1.316.01 Eng 1 ! |
| ! ! 26.2.316.01 # ! |
| ! ! 26.1.316.10 Eng 2 ! |
| ! ! 26.2.316.10 # ! |
| ! ! A=6.4*1/10000 ! |
| ! ! B=1.013 ! |
| ! ! UTC = universal time coordinated (BNR) ! |
| ! ! (attention to the date) ! |
| ! ! 17.1.150.00 ! |
| !--------------!------------------------------------------------------! |
| ! VN ! FAN Pick Up N1 Track Vibration ! |
| ! 99 ! ! |
| ! ! Format: (0.0 to 10.0) ! |
| ! ! If the value is 10.0 then 99 is printed. ! |
| ! ! ! |
| ! ! Source: EVM 3D.1.227.01 Engine 1 ! |
| ! ! 3D.1.227.10 Engine 2 ! |
| ! ! ! |
| ! ! Remark: In report lines 'V3' and 'V4' the values ! |
| ! ! from the last stable descent is printed. ! |
| ! ! In report lines 'V5' and 'V6' the values ! |
| ! ! from the last stable climb is printed. ! |
| !--------------!------------------------------------------------------! |
| ! VL ! TRF Pick Up N1 Track Vibration ! |
| ! 99 ! ! |
| ! ! Format: (0.0 to 10.0) ! |
| ! ! If the value is 10.0 then 99 is printed. ! |
| ! ! ! |
| ! ! Source: EVM 3D.1.227.11 Engine 1 ! |
| ! ! 3D.1.227.00 Engine 2 ! |
| ! ! ! |
| ! ! Remark: In report lines 'V3' and 'V4' the values ! |
| ! ! from the last stable descent is printed. ! |
| ! ! In report lines 'V5' and 'V6' the values ! |
| ! ! from the last stable climb is printed. ! |
| !--------------!------------------------------------------------------! |
| ! PHA ! FAN Pick Up Phase Angle ! |
| ! 999 ! ! |
| ! ! Format: (0 to 360 deg) ! |
| ! ! ! |
| ! ! Source: EVM 3D.1.226.01 Engine 1 ! |
| ! ! 3D.1.226.10 Engine 2 ! |
| ! ! ! |
| ! ! Remark: In report lines 'V3' and 'V4' the values ! |
| ! ! from the last stable descent are printed. ! |
| ! ! In report lines 'V5' and 'V6' the values ! |
| ! ! from the last stable climb are printed. ! |
| !--------------!------------------------------------------------------! |
| ! PHT ! TRF Pick Up Phase Angle ! |
| ! 999 ! ! |
| ! ! Format: (0 to 360 deg) ! |
| ! ! ! |
| ! ! Source: EVM 3D.1.226.11 Engine 1 ! |
| ! ! 3D.1.226.00 Engine 2 ! |
| ! ! ! |
| ! ! Remark: In report lines 'V3' and 'V4' the values ! |
| ! ! from the last stable descent are printed. ! |
| ! ! In report lines 'V5' and 'V6' the values ! |
| ! ! from the last stable climb are printed. ! |
| !--------------!------------------------------------------------------! |
| ! VC ! FAN Pick Up N2 Track Vibration ! |
| ! 99 ! ! |
| ! ! Format: (0.0 to 4.0) ! |
| ! ! ! |
| ! ! Source: EVM 3D.1.226.11 Engine 1 ! |
| ! ! 3D.1.226.00 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! VH ! TRF pick up N2 track vibration ! |
| ! 99 ! ! |
| ! ! Format: (0.0 to 4.0) ! |
| ! ! ! |
| ! ! Source: EVM 3D.1.230.11 Engine 1 ! |
| ! ! 3D.1.230.00 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! EVM ! Engine Vibration Status Word ! |
| ! XXXXX ! ! |
| ! ! Format: Each 'X' represents 4 bits in hexadecimal ! |
| ! ! presentation of a defined ARINC 429 word. ! |
| ! ! ! |
| ! ! XXXXX Bits HEX ! |
| ! ! !!!!!________14, 13, 12, 11 0..F ! |
| ! ! !!!!_________18, 17, 16, 15 0..F ! |
| ! ! !!!__________22, 21, 20, 19 0..F ! |
| ! ! !!___________26, 25, 24, 23 0..F ! |
| ! ! !____________ 29, 28, 27 0..F ! |
| ! ! ! |
| ! ! Sources: EVM 3D.1.035.01 Engine 1 ! |
| ! ! 3D.1.035.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! OIP ! Engine Oil Pressure ! |
| ! 999 ! ! |
| ! ! Format: (0 to 400 psia) ! |
| ! ! ! |
| ! ! Source: FWC 26.1.317.01 Engine 1 ! |
| ! ! 26.2.317.01# Engine 2 ! |
| ! ! 26.1.317.10 Engine 1 ! |
| ! ! 26.2.317.10# Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! OIT ! Engine Oil Temperature ! |
| ! X99 ! ! |
| ! ! Format: Negative values are indicated by 'N' on ! |
| ! ! the first position. Otherwise the firt ! |
| ! ! position is used for the value. ! |
| ! ! (-60 to 250 °) ! |
| ! ! ! |
| ! ! Source: FWC 26.1.316.01 Engine 1 ! |
| ! ! 26.2.316.01# Engine 2 ! |
| ! ! 26.1.316.10 Engine 1 ! |
| ! ! 26.2.316.10# Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! ECW1 ! Engine Control Word 1 ! |
| ! XXXXX ! ! |
| ! ! Each 'X' represents 4 Bits in hexadecimal code of ! |
| ! ! a defined ARINC 429 word: ! |
| ! ! XXXXX Bits HEX ! |
| ! ! !!!!!___________ 14, 13, 12, 11 0...F ! |
| ! ! !!!!____________ 18, 17, 16, 15 0...F ! |
| ! ! !!!_____________ 22, 21, 20, 19 0...F ! |
| ! ! !!______________ 26, 25, 24, 23 0...F ! |
| ! ! !_______________ 29, 28, 27 0...7 ! |
| ! ! -------------------------------------------- ! |
| ! ! Bit Label Parameter Description ! |
| ! ! 11 7C.X.272.XX.19 = 1 Auto Thrust Active ! |
| ! ! 12 7C.X.272.XX.20 = 1 VSV Position Fault ! |
| ! ! 13 SPARE ! |
| ! ! 14 SPARE ! |
| ! ! 15 7C.X.351.XX.29 = 1 Fuel Flow Measurement ! |
| ! ! Invalid ! |
| ! ! 16 7C.X.275.XX.15 = 1 N1/N2 Control ACtive ! |
| ! ! 17 7C.X.275.XX.26 = 1 Channel A Active ! |
| ! ! 18 7C.X.275.XX.27 = 1 Channel B Active ! |
| ! ! 19 SPARE ! |
| ! ! 20 SPARE ! |
| ! ! 21 SPARE ! |
| ! ! 22 SPARE ! |
| ! ! 23 SPARE ! |
| ! ! 24 SPARE ! |
| ! ! 25 SPARE ! |
| ! ! 26 SPARE ! |
| ! ! 27 SPARE ! |
| ! ! 28 SPARE ! |
| ! ! 29 SPARE ! |
| ! ! ! |
| ! ! The 'X' for the System and SDI definition of the ! |
| ! ! engine parameters are: ! |
| ! ! ! |
| ! ! System SDI ! |
| ! ! Engine 1 1 01 ! |
| ! ! Engine 2 2 10 ! |
| !--------------!------------------------------------------------------! |
| ! SSEL ! Engine Control Word 1 ! |
| ! XXXXXXX ! ! |
| ! XXXXXXX ! Status of different FADEC sensors ! |
| ! ! ! |
| ! ! Format: ! |
| ! ! XXXXXXXXXXXXXX Label: Selected: Bit 11 --> 15) ! |
| ! ! IIIIIIIIIIIIII__ 346 N1 actual ! |
| ! ! IIIIIIIIIIIII___ 345 EGT ! |
| ! ! IIIIIIIIIIII____ 344 N2 actual ! |
| ! ! IIIIIIIIIII_____ 263 T25 ! |
| ! ! IIIIIIIIII______ 264 PS3 ! |
| ! ! IIIIIIIII_______ 265 T3 ! |
| ! ! IIIIIIII________ 072 VSV Position ! |
| ! ! IIIIIII_________ 071 VBV Position ! |
| ! ! IIIIII__________ 306 HPTC Position ! |
| ! ! IIIII___________ 307 LPTC Position ! |
| ! ! IIII____________ 347 FMV Position ! |
| ! ! III_____________ 211 TAT ! |
| ! ! II______________ 114 P0 ! |
| ! ! I_______________ 133 TLA Position ! |
| ! ! (All labels Bit 11 --> 15) ! |
| ! ! ! |
| ! ! Source: ECU, different labels ! |
| ! ! The indicated values shall be coded as follows: ! |
| ! ! Bit: 15 14 13 12 11 ! indicated value ! |
| ! ! --------------------!---------------- ! |
| ! ! 0 0 0 0 0 ! 0 ! |
| ! ! 0 0 0 0 1 ! 1 ! |
| ! ! 0 0 0 1 0 ! 2 ! |
| ! ! 0 0 0 1 1 ! 3 ! |
| ! ! 0 0 1 0 0 ! 4 ! |
| ! ! 0 0 1 0 1 ! 5 ! |
| ! ! 0 0 1 1 0 ! 6 ! |
| ! ! 0 0 1 1 1 ! 7 ! |
| ! ! 0 1 0 0 0 ! 8 ! |
| ! ! 0 1 0 0 1 ! 9 ! |
| ! ! 0 1 0 1 0 ! A ! |
| ! ! 0 1 0 1 1 ! B ! |
| ! ! 0 1 1 0 0 ! C ! |
| ! ! 0 1 1 0 1 ! D ! |
| ! ! 0 1 1 1 0 ! E ! |
| ! ! 0 1 1 1 1 ! F ! |
| ! ! 1 0 0 0 0 ! G ! |
| ! ! 1 0 0 0 1 ! H ! |
| ! ! 1 0 0 1 0 ! I ! |
| ! ! 1 0 0 1 1 ! J ! |
| ! ! 1 0 1 0 0 ! K ! |
| ! ! 1 0 1 0 1 ! L ! |
| ! ! 1 0 1 1 0 ! M ! |
| ! ! 1 0 1 1 1 ! N ! |
| ! ! 1 1 0 0 0 ! O ! |
| ! ! 1 1 0 0 1 ! P ! |
| ! ! 1 1 0 1 0 ! Q ! |
| ! ! 1 1 0 1 1 ! R ! |
| ! ! 1 1 1 0 0 ! S ! |
| ! ! 1 1 1 0 1 ! T ! |
| ! ! 1 1 1 1 0 ! U ! |
| ! ! 1 1 1 1 1 ! V ! |
| !--------------!------------------------------------------------------! |
| ! WFQ ! Fuel Quantity Inner Cell ! |
| ! 99999 ! ! |
| ! ! Format: (0 to 99999 kg) ! |
| ! ! ! |
| ! ! Sources: FQIC 5A.2.257.10 Left Inner Cell Fuel ! |
| ! ! Quantity ! |
| ! ! 5A.2.261.10 Right Inner Cell Fuel ! |
| ! ! Quantity ! |
| ! ! ! |
| ! ! Remark: Report line 'X1' indicates Left Inner Cell ! |
| ! ! Fuel Quantity. ! |
| ! ! Report line 'X2' indicates Right Inner Cell! |
| ! ! Fuel Quantity. ! |
| !--------------!------------------------------------------------------! |
| ! ELEV ! Elevator Position ! |
| ! X999 ! ! |
| ! ! Format: Negative values are indicated by 'N' on ! |
| ! ! the first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-30 to 15 deg) ! |
| ! ! ! |
| ! ! Sources: FCDC 6C.1.314.01 Left Elevator Position ! |
| ! ! 6C.2.314.10# ! |
| ! ! 6C.1.334.01 Right Elevator Position! |
| ! ! 6C.2.334.10# ! |
| ! ! ! |
| ! ! Remark: Report line 'X1' shows the Left Elevator ! |
| ! ! Position. ! |
| ! ! Report line 'X2' shows the Right Elevator ! |
| ! ! Position. ! |
| !--------------!------------------------------------------------------! |
| ! AOA ! Corrected Angle of Attack ! |
| ! X999 ! ! |
| ! ! Format: Negative values are indicated by 'N' on ! |
| ! ! the first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-30.0 to 85.0 deg) ! |
| ! ! ! |
| ! ! Source: ADIRU 06.1.241.01 AOA System 1 ! |
| ! ! 06.2.241.10 AOA System 2 ! |
| ! ! ! |
| ! ! Remark: Report line 'X1' indicates AOA System 1. ! |
| ! ! Report line 'X2' indicates AOA System 2. ! |
| !--------------!------------------------------------------------------! |
| ! SLP ! Side Slip Angle ! |
| ! X999 ! ! |
| ! ! Format: Negative values are indicated by 'N' on ! |
| ! ! the first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-32.0 to 32.0 deg) ! |
| ! ! ! |
| ! ! Source: FAC 0A.1.226.00 SLP System 1 ! |
| ! ! 0A.2.226.00 SLP System 2 ! |
| ! ! ! |
| ! ! Remark: Report line 'X1' indicates SLP System 1. ! |
| ! ! Report line 'X2' indicates SLP System 2. ! |
| !--------------!------------------------------------------------------! |
| ! CFPG ! Calculated Flight Path Acceleration ! |
| ! X9999 ! ! |
| ! ! Format: Negative values are indicated by 'N' on ! |
| ! ! the first position. Otherwise the first ! |
| ! ! position is used for the value. ! |
| ! ! (-0.9999 to 4.0000 g) ! |
| ! ! ! |
| ! ! Sources: DMU CFPG calculated value based on GS ! |
| ! ! from System 1 ! |
| ! ! CFPG calculated value based on GS ! |
| ! ! from System 2 ! |
| ! ! ! |
| ! ! GSAV last subperiod-GSAV 1st subperiod ! |
| ! ! CFPG=----------------------------------------------*! |
| ! ! Duration of subperiod*(Number of Subperiods-1) ! |
| ! ! ! |
| ! ! *0.05249 ! |
| ! ! ! |
| ! ! GSAV=Average of Ground Speed (GS) per subperiod ! |
| ! ! (label 04.1.312.01 and 04.2.312.10) ! |
| ! ! ! |
| ! ! Remark: Report line 'X1' indicates CFPG calculated! |
| ! ! with GS from ADIRU System 1. ! |
| ! ! Report line 'X2' indicates CFPG calculated! |
| ! ! with GS from ADIRU System 2. ! |
| !--------------!------------------------------------------------------! |
| ! CIVV ! Calculated Inertial Vertical Speed ! |
| ! X999 ! ! |
| ! ! Format: Negative values are indicated by 'N' on ! |
| ! ! the first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-999 to 999 ft/min) ! |
| ! ! ! |
| ! ! Source: DMU CIVV calculated value based on IALT ! |
| ! ! from system 1. ! |
| ! ! CIVV calculated value based on IALT ! |
| ! ! from system 2. ! |
| ! ! ! |
| ! ! IALTAV last subperiod-IALTAV 1st subperiod ! |
| ! ! CIVV=----------------------------------------------*! |
| ! ! Duration of subperiod*(Number of Subperiods-1) ! |
| ! ! ! |
| ! ! *60 ! |
| ! ! ! |
| ! ! IALTAV=Average of Inertial Altitude (IALT) per ! |
| ! ! subperiod (label 04.1.361.XX and ! |
| ! ! 04.2.361.XX) ! |
| ! ! ! |
| ! ! Remark: Report line 'X1' indicates CIVV calculated! |
| ! ! with IALT from ADIRU System 1. ! |
| ! ! Report line 'X2' indicates CIVV calculated! |
| ! ! with IALT from ADIRU System 2. ! |
| !--------------!------------------------------------------------------! |
| ! RUDD ! Rudder Position ! |
| ! X999 ! ! |
| ! ! Format: Negative values are indicated by 'N' on ! |
| ! ! the first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-30.0 to 30.0 deg) ! |
| ! ! ! |
| ! ! Source: SDAC 29.1.312.00 ! |
| ! ! 29.2.312.00# ! |
| !--------------!------------------------------------------------------! |
| ! RUDT ! Rudder Trim Position ! |
| ! X999 ! ! |
| ! ! Format: Negative values area indicated by 'N' on ! |
| ! ! the first position. Otherwise the first ! |
| ! ! (-25.0 to 25.0 deg) ! |
| ! ! ! |
| ! ! Source: FAC 0A.1.313.00 ! |
| ! ! 0A.2.313.00# ! |
| !--------------!------------------------------------------------------! |
| ! AILL ! Left Aileron Position ! |
| ! X999 ! ! |
| ! ! Format: Negative values are indicated by 'N' on ! |
| ! ! the first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-25.0 to 25.0 deg) ! |
| ! ! ! |
| ! ! Soure: FCDC 6C.1.310.01 ! |
| ! ! 6C.2.310.10# ! |
| !--------------!------------------------------------------------------! |
| ! AILR ! Right Aileron Position ! |
| ! X999 ! ! |
| ! ! Format: Negative values are indicated by 'N' on ! |
| ! ! the first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-25.0 to 25.0 deg) ! |
| ! ! ! |
| ! ! Source: FCDC 6C.1.330.01 ! |
| ! ! 6C.2.330.10# ! |
| !--------------!------------------------------------------------------! |
| ! STAB ! Stabilizer Position #1 ! |
| ! X999 ! ! |
| ! ! Format: Negative values are indicated by 'N' on ! |
| ! ! the first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-13.5 to 4.0 deg) ! |
| ! ! ! |
| ! ! Soure: FCDC 6C.1.315.01 ! |
| ! ! 6C.2.315.10# ! |
| !--------------!------------------------------------------------------! |
| ! ROLL ! Roll Angle ! |
| ! X999 ! ! |
| ! ! Format: Negative values are indicated by '-' on ! |
| ! ! the first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-90.0 to 90.0 deg) ! |
| ! ! ! |
| ! ! Source: ADIRU 04.1.325.01 ! |
| ! ! 04.2.325.10# ! |
| !--------------!------------------------------------------------------! |
| ! YAW ! Body Axis Yaw Rate ! |
| ! X999 ! ! |
| ! ! Format: Negative values are indicated by 'N' on ! |
| ! ! the first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-45.0 to 45.0 deg/sec) ! |
| ! ! ! |
| ! ! Sources: ADIRU 04.1.330.01 ! |
| ! ! 04.2.330.10# ! |
| !--------------!------------------------------------------------------! |
| ! RSP2 ! Roll Spoiler 2 Position ! |
| ! X999 ! ! |
| ! ! Format: Negative values are indicated by 'N' on ! |
| ! ! the first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-45.0 to 0 deg) ! |
| ! ! ! |
| ! ! Sourc: FCDC 6C.1.362.01 Left Spoiler ! |
| ! ! 6C.2.362.10# ! |
| ! ! 6C.1.372.01 Right Spoiler ! |
| ! ! 6C.2.372.10# ! |
| ! ! ! |
| ! ! Remark: Report line 'X4' indicates RSP2 left ! |
| ! ! spoiler. ! |
| ! ! Report line 'X5' indicates RSP2 right ! |
| ! ! spoiler. ! |
| !--------------!------------------------------------------------------! |
| ! RSP3 ! Roll Spoiler 3 Position ! |
| ! X999 ! ! |
| ! ! Format: Negative values are indicated by 'N' on ! |
| ! ! the first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-45.0 to 0 deg) ! |
| ! ! ! |
| ! ! Source: FCDC 6C.1.363.01 Left Spoiler ! |
| ! ! 6C.2.363.10# ! |
| ! ! 6C.1.373.01 Right Spoiler ! |
| ! ! 6C.2.373.10# ! |
| ! ! ! |
| ! ! Remark: Report line 'X4' indicates RSP3 left ! |
| ! ! spoiler. ! |
| ! ! Report line 'X5' indicates RSP3 right ! |
| ! ! spoiler. ! |
| !--------------!------------------------------------------------------! |
| ! RSP4 ! Roll Spoiler 4 Position ! |
| ! X999 ! ! |
| ! ! Format: Negative values are indicated by 'N' on ! |
| ! ! the first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-45.0 to 0 deg) ! |
| ! ! ! |
| ! ! Source: FCDC 6C.1.364.01 Left Spoiler ! |
| ! ! 6C.2.364.10# ! |
| ! ! 6C.1.374.01 Right Spoiler ! |
| ! ! 6C.2.374.10# ! |
| ! ! ! |
| ! ! Remark: Report line 'X4' indicates RSP4 left ! |
| ! ! spoiler. ! |
| ! ! Report line 'X5' indicates RSP4 right ! |
| ! ! spoiler. ! |
| !--------------!------------------------------------------------------! |
| ! RSP5 ! Roll Spoiler 5 Position ! |
| ! X999 ! ! |
| ! ! Format: Negative values are indicated by 'N' on ! |
| ! ! the first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-45.0 to 0 deg) ! |
| ! ! ! |
| ! ! Source: FCDC 6C.1.365.01 Left Spoiler ! |
| ! ! 6C.2.365.10# ! |
| ! ! 6C.1.375.01 Right Spoiler ! |
| ! ! 6C.2.375.10# ! |
| ! ! ! |
| ! ! Remark: Report line 'X4' indicates RSP5 left ! |
| ! ! spoiler. ! |
| ! ! Report line 'X5' indicates RSP5 right ! |
| ! ! spoiler. ! |
| !--------------!------------------------------------------------------! |
| ! FLAP ! FLAP Actual Position ! |
| ! X999 ! ! |
| ! ! Format: Negative values are indicated by 'N' on ! |
| ! ! the first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-9.0 to 40.0 deg) ! |
| ! ! ! |
| ! ! Source: SFCC 1B.1.137.01 FLAP System 1 ! |
| ! ! 1B.2.137.10 FLAP System 2 ! |
| ! ! ! |
| ! ! Remark: Report line 'X4' indicates FLAP left ! |
| ! ! spoiler. ! |
| ! ! Report line 'X5' indicates FLAP right ! |
| ! ! spoiler. ! |
| !--------------!------------------------------------------------------! |
| ! SLAT ! SLAT Actual Position ! |
| ! X999 ! ! |
| ! ! Format: Negative values are indicated by 'N' on ! |
| ! ! the first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (0.0 to 27.0 deg) ! |
| ! ! ! |
| ! ! Source: SFCC 1B.1.127.01 SLAT System 1 ! |
| ! ! 1B.2.127.10 SLAT System 2 ! |
| ! ! ! |
| ! ! Remark: Report line 'X4' indicates SLAT left ! |
| ! ! spoiler. ! |
| ! ! Report line 'X5' indicates SLAT right ! |
| ! ! spoiler. ! |
| !--------------!------------------------------------------------------! |
| ! THDG ! True Heading (BCD) ! |
| ! 9999 ! ! |
| ! ! Format: (0 to 359.9 deg) ! |
| ! ! ! |
| ! ! Source: ADIRU 04.1.044.01 THDG System 1 ! |
| ! ! 04.2.044.10 THDG System 2 ! |
| ! ! ! |
| ! ! Remark: Report line 'X6' indicates THDG System 1. ! |
| ! ! Report line 'X7' indicates THDG System 2. ! |
| !--------------!------------------------------------------------------! |
| ! LONP ! Longitude Position ! |
| ! X9999 ! ! |
| ! ! Format: The first position indicates if east or ! |
| ! ! west. 'E' for an East position and 'W' for ! |
| ! ! a West position. ! |
| ! ! (East 179.9 deg to West 179.9 deg) ! |
| ! ! ! |
| ! ! Source: ADIRU 04.1.311.01 LONP System 1 ! |
| ! ! 04.2.311.10 LONP System 2 # ! |
| ! ! ! |
| ! ! Remark: Report line 'X6' indicates LONP System 1. ! |
| ! ! Report line 'X7' indicates LONP System 2. ! |
| !--------------!------------------------------------------------------! |
| ! LATP ! Latitude Position ! |
| ! X999 ! ! |
| ! ! Format: The first position indicates if north or ! |
| ! ! south 'N' for a North position and 'S' for ! |
| ! ! a South position. ! |
| ! ! (North 89.9 deg to South 89.9 deg) ! |
| ! ! ! |
| ! ! Source: ADIRU 04.1.310.XX LATP System 1 ! |
| ! ! 04.2.310.XX LATP System 2 # ! |
| ! ! ! |
| ! ! Remark: Report line 'X6' indicates LATP System 1. ! |
| ! ! Report line 'X7' indicates LATP System 2. ! |
| !--------------!------------------------------------------------------! |
| ! WS ! Wind Speed ! |
| ! 999 ! ! |
| ! ! Format: (0 to 100 kts) ! |
| ! ! ! |
| ! ! Source: ADIRU 04.1.315.01 WS System 1 ! |
| ! ! 04.2.315.10 WS System 2 ! |
| ! ! ! |
| ! ! Remark: Report line 'X6' indicates WS System 1. ! |
| ! ! Report line 'X7' indicates WS System 2. ! |
| !--------------!------------------------------------------------------! |
| ! WD ! Wind Direction - True ! |
| ! 999 ! ! |
| ! ! Format: (0 to 359 deg) ! |
| ! ! ! |
| ! ! Source: ADIRU 04.1.316.01 WD System 1 ! |
| ! ! 04.2.316.10 WD System 2 ! |
| ! ! ! |
| ! ! Remark: Report line 'X6' indicates WD System 1. ! |
| ! ! Report line 'X7' indicates WD System 2. ! |
| !--------------!------------------------------------------------------! |
| ! FT ! Fuel Temperature ! |
| ! X999 ! ! |
| ! ! Format: (-60.0 to 170.0 C) ! |
| ! ! ! |
| ! ! Source: FQIC 5A.2.177.10 Fuel Temp. Left Wing Tank ! |
| ! ! 5A.2.210.10 Fuel Temp. Right Wing Tank! |
| ! ! ! |
| ! ! Remark: Report line 'X6' contains the fuel ! |
| ! ! temperature from the Left Wing Tank. ! |
| ! ! Report line 'X7' contains the fuel ! |
| ! ! temperature from the Right Wing Tank. ! |
| !--------------!------------------------------------------------------! |
| ! FD ! Fuel Density ! |
| ! 0999 ! ! |
| ! ! Format: (0 to 0.999 kg/l) ! |
| ! ! ! |
| ! ! Source: FQIC 5A.2.272.10 ! |
| ! ! DMU Fuel Density Left Wing Tank ! |
| ! ! Fuel Density Right Wing Tank ! |
| ! ! ! |
| ! ! Remark: The Fuel Density value of the various tanks! |
| ! ! (Left Wing Tank, Center Tank and Right Wing! |
| ! ! Tank) is transmitted one after another on ! |
| ! ! label 272. The adequate tank identification! |
| ! ! as follows: ! |
| ! ! ! |
| ! ! For A318, A319 and A320: ! |
| ! ! Bit 11-14 = 0.0001 ! |
| ! ! Bit 15-18 = 0.001 ! |
| ! ! Bit 19-22 = 0.01 ! |
| ! ! Bit 23-26 = 0.1 ! |
| ! ! Bit 27-29 = Fuel tank Ident (Left/Center/Right) ! |
| ! ! ! |
| ! ! For A321: ! |
| ! ! Bit 11-13 = Fuel tank Ident (Left/Center/Right) ! |
| ! ! Bit 14-17 = 0.0001 ! |
| ! ! Bit 18-21 = 0.001 ! |
| ! ! Bit 22-25 = 0.01 ! |
| ! ! Bit 26-29 = 0.1 ! |
| ! ! ! |
| ! ! The update rate of label 272 is 1 second. Due to ! |
| ! ! this fact the Fuel Density value of the dedicated ! |
| ! ! tank is available every 3 seconds. ! |
| +---------------------------------------------------------------------+ |
(3) Cruise Performance Report Data Field Description <02> (Engine Type CFMI with Advanced EVMU)
NOTE: Reports that are transmitted from the ACARS system do not have report lines without a line identifier.
NOTE: Only the parts of the CRUISE PERFORMANCE REPORT <02> which are not included in the ENGINE CRUISE REPORT <01> are given in the subsequent table.
| +---------------------------------------------------------------------+ |
| ! Value ! Content Description ! |
| !--------------!------------------------------------------------------! |
| ! TAT/ALT/CAS/! The average value for the F02 * 20 sec. of System1 ! |
| ! MN/GW/CG ! is printed in the report line CE. ! |
| ! ! ! |
| ! ! The average value for the F02 * 20 sec. of System2 ! |
| ! ! is printed in the report line CN. ! |
| !--------------!------------------------------------------------------! |
| ! QA ! Aircraft Quality Number, Report-Stability ! |
| ! 99 ! ! |
| ! ! Format: (00 to 99) ! |
| ! ! ! |
| ! ! Source: DMU ! |
| ! ! ! |
| ! ! Remark: 00 = best stable frame ! |
| ! ! 99 = worst stable frame ! |
| ! ! ! |
| ! ! i=1 VARa(i) ! |
| ! ! QA= SIGMA(Wa(i)*---------------) ! |
| ! ! N TOLa(i)*TOLa(i) ! |
| ! ! ! |
| ! !QA= Quality Number ! |
| ! !Wa(i)= Individual weighting factors for the individual! |
| ! ! quality parameters for the Cruise Report. ! |
| ! !VARa(i)= Parameter variances ! |
| ! !TOLa(i)= Variation values for the individual quality ! |
| ! ! parameters for the Cruise Performance Report.! |
| !--------------!------------------------------------------------------! |
| ! QE ! Engine Quality Number, Report-Stability ! |
| ! 99 ! ! |
| ! ! Format: (00 to 99) ! |
| ! ! ! |
| ! ! Source: DMU ! |
| ! ! ! |
| ! ! Remark: QE has no effect to the trigger logic. ! |
| ! ! 99 = worst stable frame, 00 = best stable ! |
| ! ! frame. The quality number is represented ! |
| ! ! in the same mathematical form as QA. ! |
| !--------------!------------------------------------------------------! |
| ! WFQ ! Fuel Quantity Inner Cell ! |
| ! 99999 ! ! |
| ! ! Format: (0 to 99999 kg) ! |
| ! ! ! |
| ! ! Source: FQIC 5A.2.257.10 Left Inner Cell Fuel ! |
| ! ! Quantity ! |
| ! ! 5A.2.261.10 Right Inner Cell Fuel ! |
| ! ! Quantity ! |
| ! ! ! |
| ! ! Remark: Report line 'X1' shows Left Inner Cell ! |
| ! ! Fuel Quantity. ! |
| ! ! Report line 'X2' shows Right Inner Cell ! |
| ! ! Fuel Quantity. ! |
| !--------------!------------------------------------------------------! |
| ! ELEV ! Elevator Position ! |
| ! X999 ! ! |
| ! ! Format: Negative values are shown with 'N' on the ! |
| ! ! first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-30 to 15 deg) ! |
| ! ! ! |
| ! ! Source: FCDC 6C.1.314.01 Left Elevator Position ! |
| ! ! 6C.2.314.10# ! |
| ! ! 6C.1.334.01 Right Elevator Position ! |
| ! ! 6C.2.334.10# ! |
| ! ! ! |
| ! ! Remark: Report line 'X1' shows the Left Elevator ! |
| ! ! Position. ! |
| ! ! Report line 'X2' shows the Right Elevator ! |
| ! ! Position. ! |
| !--------------!------------------------------------------------------! |
| ! AOA ! Corrected Angle of Attack ! |
| ! X999 ! ! |
| ! ! Format: Negative values are shown with 'N' on the ! |
| ! ! first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-30.0 to 85.0 deg) ! |
| ! ! ! |
| ! ! Source: ADIRU 06.1.241.01 AOA System 1 ! |
| ! ! 06.2.241.10 AOA System 2 ! |
| ! ! ! |
| ! ! Remark: Report line 'X1' shows AOA System 1. ! |
| ! ! Report line 'X2' shows AOA System 2. ! |
| !--------------!------------------------------------------------------! |
| ! SLP ! Side Slip Angle ! |
| ! X999 ! ! |
| ! ! Format: Negative values are shown with 'N' on the ! |
| ! ! first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-32.0 to 32.0 deg) ! |
| ! ! ! |
| ! ! Source: FAC 0A.1.226.00 SLP System 1 ! |
| ! ! 0A.2.226.00 SLP System 2 ! |
| ! ! ! |
| ! ! Remark: Report line 'X1' shows SLP System 1. ! |
| ! ! Report line 'X2' shows SLP System 2. ! |
| !--------------!------------------------------------------------------! |
| ! CFPG ! Calculated Flight Path Acceleration ! |
| ! X9999 ! ! |
| ! ! Format: Negative values are shown with 'N' on the ! |
| ! ! first position. Otherwise the first ! |
| ! ! position is used for the value. ! |
| ! ! (-0.9999 to 4.0000 g) ! |
| ! ! ! |
| ! ! Source: DMU CFPG calculated value based on GS from! |
| ! ! System 1 ! |
| ! ! CFPG calculated value based on GS from! |
| ! ! System 2 ! |
| ! ! ! |
| ! ! GSAV last subperiod-GSAV 1st subperiod ! |
| ! ! CFPG=----------------------------------------------*! |
| ! ! Duration of subperiod*(Number of Subperiods-1) ! |
| ! ! ! |
| ! ! *0.05249 ! |
| ! ! ! |
| ! ! GSAV=Average of Ground Speed (GS) per subperiod ! |
| ! ! (label 04.1.312.01 and 04.2.312.10) ! |
| ! ! ! |
| ! ! Remark: Report line 'X1' indicates CFPG calculated ! |
| ! ! with GS from ADIRU System 1. ! |
| ! ! Report line 'X2' indicates CFPG calculated ! |
| ! ! with GS from ADIRU System 2. ! |
| !--------------!------------------------------------------------------! |
| ! CIVV ! Calculated Inertial Vertical Speed ! |
| ! X9999 ! ! |
| ! ! Format: Negative values are shown with 'N' on the ! |
| ! ! first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-999 to 999 ft/min) ! |
| ! ! ! |
| ! ! Source: DMU CIVV calculated value based on IALT ! |
| ! ! from system 1. ! |
| ! ! CIVV calculated value based on IALT ! |
| ! ! from system 2. ! |
| ! ! ! |
| ! ! IALTAV last subperiod-IALTAV 1st subperiod ! |
| ! ! CIVV=----------------------------------------------*! |
| ! ! Duration of subperiod*(Number of Subperiods-1) ! |
| ! ! ! |
| ! ! *60 ! |
| ! ! ! |
| ! ! IALTAV=Average of Inertial Altitude (IALT) per ! |
| ! ! subperiod (label 04.1.361.XX and ! |
| ! ! 04.2.361.XX) ! |
| ! ! ! |
| ! ! Remark: Report line 'X1' indicates CIVV calculated ! |
| ! ! with IALT from ADIRU System 1. ! |
| ! ! Report line 'X2' indicates CIVV calculated ! |
| ! ! with IALT from ADIRU System 2. ! |
| !--------------!------------------------------------------------------! |
| ! RUDD ! Rudder Position ! |
| ! X999 ! ! |
| ! ! Format: Negative values are shown with 'N' on the ! |
| ! ! first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-30.0 to 30.0 deg) ! |
| ! ! ! |
| ! ! Source: SDAC 29.1.312.00 ! |
| ! ! 29.2.312.00# ! |
| !--------------!------------------------------------------------------! |
| ! RUDT ! Rudder Trim Position ! |
| ! X999 ! ! |
| ! ! Format: Negative values are shown with 'N' on the ! |
| ! ! first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-25.0 to 25.0 deg) ! |
| ! ! ! |
| ! ! Source: FAC 0A.1.313.00 ! |
| ! ! 0A.2.313.00# ! |
| !--------------!------------------------------------------------------! |
| ! AILL ! Left Aileron Position ! |
| ! X999 ! ! |
| ! ! Format: Negative values are shown with 'N' on the ! |
| ! ! first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-25.0 to 25.0 deg) ! |
| ! ! ! |
| ! ! Source: FCDC 6C.1.310.01 ! |
| ! ! 6C.2.310.10# ! |
| !--------------!------------------------------------------------------! |
| ! AILR ! Right Aileron Position ! |
| ! X999 ! ! |
| ! ! Format: Negative values are shown with 'N' on the ! |
| ! ! first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-25.0 to 25.0 deg) ! |
| ! ! ! |
| ! ! Source: FCDC 6C.1.330.01 ! |
| ! ! 6C.2.330.10# ! |
| !--------------!------------------------------------------------------! |
| ! STAB ! Stabilizer Position #1 ! |
| ! X999 ! ! |
| ! ! Format: Negative values are shown with 'N' on the ! |
| ! ! first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-13.5 to 4.0 deg) ! |
| ! ! ! |
| ! ! Source: FCDC 6C.1.315.01 ! |
| ! ! 6C.2.315.10# ! |
| !--------------!------------------------------------------------------! |
| ! ROLL ! Roll Angle ! |
| ! X999 ! ! |
| ! ! Format: Negative values are shown with 'N' on the ! |
| ! ! first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-90.0 to 90.0 deg) ! |
| ! ! ! |
| ! ! Source: ADIRU 04.1.325.01 ! |
| ! ! 04.2.325.10# ! |
| !--------------!------------------------------------------------------! |
| ! YAW ! Body Axis Yaw Rate ! |
| ! X999 ! ! |
| ! ! Format: Negative values are shown with 'N' on the ! |
| ! ! first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-45.0 to 45.0 deg) ! |
| ! ! ! |
| ! ! Source: ADIRU 04.1.330.01 ! |
| ! ! 04.2.330.10# ! |
| !--------------!------------------------------------------------------! |
| ! RSP2 ! Roll Spoiler 2 Position ! |
| ! X999 ! ! |
| ! ! Format: Negative values are shown with 'N' on the ! |
| ! ! first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-45.0 to 0 deg) ! |
| ! ! ! |
| ! ! Source: FCDC 6C.1.362.01 Left Spoiler ! |
| ! ! 6C.2.362.10# ! |
| ! ! 6C.1.372.01 Right Spoiler ! |
| ! ! 6C.2.372.10# ! |
| ! ! ! |
| ! ! Remark: Report line 'X4' shows RSP2 left spoiler. ! |
| ! ! Report line 'X5' shows RSP2 right spoiler.! |
| !--------------!------------------------------------------------------! |
| ! RSP3 ! Roll Spoiler 3 Position ! |
| ! X999 ! ! |
| ! ! Format: Negative values are shown with 'N' on the ! |
| ! ! first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-45.0 to 0 deg) ! |
| ! ! ! |
| ! ! Source: FCDC 6C.1.363.01 Left Spoiler ! |
| ! ! 6C.2.363.10# ! |
| ! ! 6C.1.373.01 Right Spoiler ! |
| ! ! 6C.2.373.10# ! |
| ! ! ! |
| ! ! Remark: Report line 'X4' shows RSP3 left spoiler. ! |
| ! ! Report line 'X5' shows RSP3 right spoiler. ! |
| !--------------!------------------------------------------------------! |
| ! RSP4 ! Roll Spoiler 4 Position ! |
| ! X999 ! ! |
| ! ! Format: Negative values are shown with 'N' on the ! |
| ! ! first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-45.0 to 0 deg) ! |
| ! ! ! |
| ! ! Source: FCDC 6C.1.364.01 Left Spoiler ! |
| ! ! 6C.2.364.10# ! |
| ! ! 6C.1.374.01 Right Spoiler ! |
| ! ! 6C.2.374.10# ! |
| ! ! ! |
| ! ! Remark: Report line 'X4' shows RSP4 left spoiler. ! |
| ! ! Report line 'X5' shows RSP4 right spoiler. ! |
| !--------------!------------------------------------------------------! |
| ! RSP5 ! Roll Spoiler 5 Position ! |
| ! X999 ! ! |
| ! ! Format: Negative values are shown with 'N' on the ! |
| ! ! first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-45.0 to 0 deg) ! |
| ! ! ! |
| ! ! Source: FCDC 6C.1.365.01 Left Spoiler ! |
| ! ! 6C.2.365.10# ! |
| ! ! 6C.1.375.01 Right Spoiler ! |
| ! ! 6C.2.375.10# ! |
| ! ! ! |
| ! ! Remark: Report line 'X4' shows RSP5 left spoiler. ! |
| ! ! Report line 'X5' shows RSP5 right spoiler. ! |
| !--------------!------------------------------------------------------! |
| ! FLAP ! FLAP Actual Position ! |
| ! X999 ! ! |
| ! ! Format: Negative values are shown with 'N' on the ! |
| ! ! first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (0.0 to 40.0 deg) ! |
| ! ! ! |
| ! ! Source: SFCC 1B.1.137.01 FLAP System 1 ! |
| ! ! 1B.2.137.10 FLAP System 2 ! |
| ! ! ! |
| ! ! Remark: Report line 'X4' shows FLAP System 1. ! |
| ! ! Report line 'X5' shows FLAP System 2. ! |
| !--------------!------------------------------------------------------! |
| ! SLAT ! SLAT Actual Position ! |
| ! X999 ! ! |
| ! ! Format: Negative values are shown with 'N' on the ! |
| ! ! first position. Otherwise the first ! |
| ! ! position contains a'0'. ! |
| ! ! (0.0 to 27.0 deg) ! |
| ! ! ! |
| ! ! Source: SFCC 1B.1.127.01 SLAT System 1 ! |
| ! ! 1B.2.127.10 SLAT System 2 ! |
| ! ! ! |
| ! ! Remark: Report line 'X4' shows SLAT System 1. ! |
| ! ! Report line 'X5' shows SLAT System 2. ! |
| !--------------!------------------------------------------------------! |
| ! THDG ! True Heading (BCD) ! |
| ! 9999 ! ! |
| ! ! Format: (0 to 359.9 deg) ! |
| ! ! ! |
| ! ! Source: ADIRU 04.1.044.01 THDG System 1 ! |
| ! ! 04.2.044.10 THDG System 1 ! |
| ! ! ! |
| ! ! Remark: Report line 'X6' shows THDG System 1. ! |
| ! ! Report line 'X7' shows THDG System 2. ! |
| !--------------!------------------------------------------------------! |
| ! LONP ! Longitude Position ! |
| ! X9999 ! ! |
| ! ! Format: The first position shows if east or west. ! |
| ! ! 'E' for an East position and 'W' for a West! |
| ! ! position. ! |
| ! ! (East 179.9 deg to West 179.9 deg) ! |
| ! ! ! |
| ! ! Source: ADIRU 04.1.311.01 LONP System 1 ! |
| ! ! 04.2.311.10 LONP System 2 ! |
| ! ! ! |
| ! ! Remark: Report line 'X6' shows LONP System 1. ! |
| ! ! Report line 'X7' shows LONP System 2. ! |
| !--------------!------------------------------------------------------! |
| ! LATP ! Latitude Position ! |
| ! X999 ! ! |
| ! ! Format: The first position shows if north ! |
| ! ! or south 'N' for a North position and 'S' ! |
| ! ! for a South position. ! |
| ! ! (North 89.9 deg to South 89.9 deg) ! |
| ! ! ! |
| ! ! Source: ADIRU 04.1.310.XX LATP System 1 ! |
| ! ! 04.2.310.XX LATP System 2 ! |
| ! ! ! |
| ! ! Remark: Report line 'X6' shows LATP System 1. ! |
| ! ! Report line 'X7' shows LATP System 2. ! |
| !--------------!------------------------------------------------------! |
| ! WS ! Wind Speed ! |
| ! 999 ! ! |
| ! ! Format: (0 to 100 kts) ! |
| ! ! ! |
| ! ! Source: ADIRU 04.1.315.01 WS System 1 ! |
| ! ! 04.2.315.10 WS System 2 ! |
| ! ! ! |
| ! ! Remark: Report line 'X6' shows WS System 1. ! |
| ! ! Report line 'X7' shows WS System 2. ! |
| !--------------!------------------------------------------------------! |
| ! WD ! Wind Direction - True ! |
| ! 999 ! ! |
| ! ! Format: (0 to 359 deg) ! |
| ! ! ! |
| ! ! Source: ADIRU 04.1.316.01 WD System 1 ! |
| ! ! 04.2.316.10 WD System 2 ! |
| ! ! ! |
| ! ! Remark: Report line 'X6' shows WD System 1. ! |
| ! ! Report line 'X7' shows WD System 2. ! |
| !--------------!------------------------------------------------------! |
| ! FT ! Wing Fuel Temperature ! |
| ! X999 ! ! |
| ! ! Format: (-60.0 to 170.0 °) ! |
| ! ! ! |
| ! ! Source: FQIC 5A.2.177.10 Fuel Temp. Left Wing Tank ! |
| ! ! 5A.2.210.10 Fuel Temp. Right Wing Tank! |
| ! ! ! |
| ! ! Remark: Report line 'X6' shows the fuel temperature! |
| ! ! from the Left Wing Tank. ! |
| ! ! Report line 'X7' shows the fuel temperature! |
| ! ! from the Right Wing Tank. ! |
| !--------------!------------------------------------------------------! |
| ! FD ! Fuel Density ! |
| ! 0999 ! ! |
| ! ! Format: (0 to 0.999 kg/l) ! |
| ! ! ! |
| ! ! Source: FQIC 5A.2.272.10 ! |
| ! ! ! |
| ! ! Remark: The Fuel Density value of the various tanks! |
| ! ! (Left Wing Tank, Center Tank and Right Wing! |
| ! ! Tank) is transmitted one after another on ! |
| ! ! label 272. The adequate tank identification! |
| ! ! is as follows: ! |
| ! ! ! |
| ! ! For A318, A319 and A320: ! |
| ! ! Bit 11-14 = 0.0001 ! |
| ! ! Bit 15-18 = 0.001 ! |
| ! ! Bit 19-22 = 0.01 ! |
| ! ! Bit 23-26 = 0.1 ! |
| ! ! Bit 27-29 = Fuel tank Ident (Left/Center/Right) ! |
| ! ! ! |
| ! ! For A321: ! |
| ! ! Bit 11-13 = Fuel tank Ident (Left/Center/Right) ! |
| ! ! Bit 14-17 = 0.0001 ! |
| ! ! Bit 18-21 = 0.001 ! |
| ! ! Bit 22-25 = 0.01 ! |
| ! ! Bit 26-29 = 0.1 ! |
| ! ! ! |
| ! ! The update rate of label 272 is 1 second. Due to ! |
| ! ! this fact the Fuel Density value of the dedicated ! |
| ! ! tank is available every 3 seconds. ! |
| +---------------------------------------------------------------------+ |
(4) Cruise Performance Report Data Field Description <02> (Engine Type CFMI with Advanced EVMU)
NOTE: Reports that are transmitted from the ACARS system do not have report lines without a line identifier.
NOTE: Only the parts of the CRUISE PERFORMANCE REPORT <02> which are not included in the ENGINE CRUISE REPORT <01> are given in the subsequent table.
| +---------------------------------------------------------------------+ |
| ! Value ! Content Description ! |
| !--------------!------------------------------------------------------! |
| ! QA ! Aircraft Quality Number, Report-Stability ! |
| ! 99 ! ! |
| ! ! Format: (00 to 99) ! |
| ! ! ! |
| ! ! Source: DMU ! |
| ! ! ! |
| ! ! Remark: 00 = best stable frame ! |
| ! ! 99 = worst stable frame ! |
| ! ! The quality number is represented in ! |
| ! ! mathematical form bellow: ! |
| ! ! ! |
| ! ! i=1 VARa(i) ! |
| ! ! QA= SIGMA(Wa(i)*--------------- ! |
| ! ! N TOLa(i)*TOLa(i) ! |
| ! ! ! |
| ! ! QA= Quality Number ! |
| ! ! Wa(i)= Individual weighting factors for the ! |
| ! ! individual quality parameters for the Cruise ! |
| ! ! Performance Report. ! |
| ! ! VARa(i)=Parameter variances ! |
| ! ! TOLa(i)= Variation values for the individual ! |
| ! ! quality parameters for the Cruise ! |
| ! ! Performance Report. ! |
| !--------------!------------------------------------------------------! |
| ! WFQ ! Fuel Quantity Inner Cell ! |
| ! 99999 ! ! |
| ! ! Format: (0 to 99999 kg) ! |
| ! ! ! |
| ! ! Sources: FQIC 5A.2.257.10 Left Inner Cell Fuel ! |
| ! ! Quantity ! |
| ! ! 5A.2.261.10 Right Inner Cell Fuel ! |
| ! ! Quantity ! |
| ! ! ! |
| ! ! Remark: Report line 'X1' indicates Left Inner Cell ! |
| ! ! Fuel Quantity. ! |
| ! ! Report line 'X2' indicates Right Inner Cell! |
| ! ! Fuel Quantity. ! |
| !--------------!------------------------------------------------------! |
| ! ELEV ! Elevator Position ! |
| ! X999 ! ! |
| ! ! Format: Negative values are indicated by 'N' on ! |
| ! ! the first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-30 to 15 deg) ! |
| ! ! ! |
| ! ! Sources: FCDC 6C.1.314.01 Left Elevator Position ! |
| ! ! 6C.2.314.10# ! |
| ! ! 6C.1.334.01 Right Elevator Position! |
| ! ! 6C.2.334.10# ! |
| ! ! ! |
| ! ! Remark: Report line 'X1' shows the Left Elevator ! |
| ! ! Position. ! |
| ! ! Report line 'X2' shows the Right Elevator ! |
| ! ! Position. ! |
| !--------------!------------------------------------------------------! |
| ! AOA ! Corrected Angle of Attack ! |
| ! X999 ! ! |
| ! ! Format: Negative values are indicated by 'N' on ! |
| ! ! the first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-30.0 to 85.0 deg) ! |
| ! ! ! |
| ! ! Source: ADIRU 06.1.241.01 AOA System 1 ! |
| ! ! 06.2.241.10 AOA System 2 ! |
| ! ! ! |
| ! ! Remark: Report line 'X1' indicates AOA System 1. ! |
| ! ! Report line 'X2' indicates AOA System 2. ! |
| !--------------!------------------------------------------------------! |
| ! SLP ! Side Slip Angle ! |
| ! X999 ! ! |
| ! ! Format: Negative values are indicated by '-' on ! |
| ! ! the first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-32.0 to 32.0 deg) ! |
| ! ! ! |
| ! ! Source: FAC 0A.1.226.00 SLP System 1 ! |
| ! ! 0A.2.226.00 SLP System 2 ! |
| ! ! ! |
| ! ! Remark: Report line 'X1' indicates SLP System 1. ! |
| ! ! Report line 'X2' indicates SLP System 2. ! |
| !--------------!------------------------------------------------------! |
| ! CFPG ! Calculated Flight Path Acceleration ! |
| ! X9999 ! ! |
| ! ! Format: Negative values are shown with '-' on the ! |
| ! ! first position. Otherwise the first ! |
| ! ! position is used for the value. ! |
| ! ! (-0.9999 to 4.0000 g) ! |
| ! ! ! |
| ! ! Source: DMU CFPG calculated value based on GS from! |
| ! ! System 1 ! |
| ! ! CFPG calculated value based on GS from! |
| ! ! System 2 ! |
| ! ! ! |
| ! ! GSAV last subperiod-GSAV 1st subperiod ! |
| ! ! CFPG=----------------------------------------------*! |
| ! ! Duration of subperiod*(Number of Subperiods-1) ! |
| ! ! ! |
| ! ! *0.05249 ! |
| ! ! ! |
| ! ! GSAV=Average of Ground Speed (GS) per subperiod ! |
| ! ! (label 04.1.312.01 and 04.2.312.10) ! |
| ! ! ! |
| ! ! Remark: Report line 'X1' shows CFPG calculated with! |
| ! ! GS from ADIRU System 1. ! |
| ! ! Report line 'X2' shows CFPG calculated with! |
| ! ! GS from ADIRU System 2. ! |
| !--------------!------------------------------------------------------! |
| ! CIVV ! Calculated Inertial Vertical Speed ! |
| ! X999 ! ! |
| ! ! Format: Negative values are shown with '-' on the ! |
| ! ! first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-999 to 999 ft/min) ! |
| ! ! ! |
| ! ! Source: DMU CIVV calculated value based on IALT ! |
| ! ! from system 1. ! |
| ! ! CIVV calculated value based on IALT ! |
| ! ! from system 2. ! |
| ! ! ! |
| ! ! IALTAV last subperiod-IALTAV 1st subperiod ! |
| ! ! CIVV=----------------------------------------------*! |
| ! ! Duration of subperiod*(Number of Subperiods-1) ! |
| ! ! ! |
| ! ! *60 ! |
| ! ! ! |
| ! ! IALTAV=Average of Inertial Altitude (IALT) per ! |
| ! ! subperiod (label 04.1.361.XX and ! |
| ! ! 04.2.361.XX) ! |
| ! ! ! |
| ! ! Remark: Report line 'X1' shows CIVV calculated with! |
| ! ! IALT from ADIRU System 1. ! |
| ! ! Report line 'X2' shows CIVV calculated with! |
| ! ! IALT from ADIRU System 2. ! |
| !--------------!------------------------------------------------------! |
| ! RUDD ! Rudder Position ! |
| ! X999 ! ! |
| ! ! Format: Negative values are shown with '-' on the ! |
| ! ! first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-30.0 to 30.0 deg) ! |
| ! ! ! |
| ! ! Source: SDAC 29.1.312.00 ! |
| ! ! 29.2.312.00# ! |
| !--------------!------------------------------------------------------! |
| ! RUDT ! Rudder Trim Position ! |
| ! X999 ! ! |
| ! ! Format: Negative values are shown with '-' on the ! |
| ! ! first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-25.0 to 25.0 deg) ! |
| ! ! ! |
| ! ! Source: FAC 0A.1.313.00 ! |
| ! ! 0A.2.313.00# ! |
| !--------------!------------------------------------------------------! |
| ! AILL ! Left Aileron Position ! |
| ! X999 ! ! |
| ! ! Format: Negative values are shown with '-' on the ! |
| ! ! first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-25.0 to 25.0 deg) ! |
| ! ! ! |
| ! ! Source: FCDC 6C.1.310.01 ! |
| ! ! 6C.2.310.10# ! |
| !--------------!------------------------------------------------------! |
| ! AILR ! Right Aileron Position ! |
| ! X999 ! ! |
| ! ! Format: Negative values are shown with '-' on the ! |
| ! ! first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-25.0 to 25.0 deg) ! |
| ! ! ! |
| ! ! Source: FCDC 6C.1.330.01 ! |
| ! ! 6C.2.330.10# ! |
| !--------------!------------------------------------------------------! |
| ! STAB ! Stabilizer Position #1 ! |
| ! X999 ! ! |
| ! ! Format: Negative values are shown with '-' on the ! |
| ! ! first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-13.5 to 4.0 deg) ! |
| ! ! ! |
| ! ! Source: FCDC 6C.1.315.01 ! |
| ! ! 6C.2.315.10# ! |
| !--------------!------------------------------------------------------! |
| ! ROLL ! Roll Angle ! |
| ! X999 ! ! |
| ! ! Format: Negative values are shown with '-' on the ! |
| ! ! first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-90.0 to 90.0 deg) ! |
| ! ! ! |
| ! ! Source: ADIRU 04.1.325.01 ! |
| ! ! 04.2.325.10# ! |
| !--------------!------------------------------------------------------! |
| ! YAW ! Body Axis Yaw Rate ! |
| ! X999 ! ! |
| ! ! Format: Negative values are shown with '-' on the ! |
| ! ! first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-45.0 to 45.0 deg/sec) ! |
| ! ! ! |
| ! ! Source: ADIRU 04.1.330.01 ! |
| ! ! 04.2.330.10# ! |
| !--------------!------------------------------------------------------! |
| ! RSP2 ! Roll Spoiler 2 Position ! |
| ! X999 ! ! |
| ! ! Format: Negative values are shown with '-' on the ! |
| ! ! first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-45.0 to 0 deg) ! |
| ! ! ! |
| ! ! Source: FCDC 6C.1.362.01 Left Spoiler ! |
| ! ! 6C.2.362.10# ! |
| ! ! 6C.1.372.01 Right Spoiler ! |
| ! ! 6C.2.372.10# ! |
| ! ! ! |
| ! ! Remark: Report line 'X4' shows RSP2 left spoiler. ! |
| ! ! Report line 'X5' shows RSP2 right spoiler. ! |
| !--------------!------------------------------------------------------! |
| ! RSP3 ! Roll Spoiler 3 Position ! |
| ! X999 ! ! |
| ! ! Format: Negative values are shown with '-' on the ! |
| ! ! first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-45.0 to 0 deg) ! |
| ! ! ! |
| ! ! Source: FCDC 6C.1.363.01 Left Spoiler ! |
| ! ! 6C.2.363.10# ! |
| ! ! 6C.1.373.01 Right Spoiler ! |
| ! ! 6C.2.373.10# ! |
| ! ! ! |
| ! ! Remark: Report line 'X4' shows RSP3 left spoiler. ! |
| ! ! Report line 'X5' shows RSP3 right spoiler ! |
| !--------------!------------------------------------------------------! |
| ! RSP4 ! Roll Spoiler 4 Position ! |
| ! X999 ! ! |
| ! ! Format: Negative values are shown with '-' on the ! |
| ! ! first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-45.0 to 0 deg) ! |
| ! ! ! |
| ! ! Source: FCDC 6C.1.364.01 Left Spoiler ! |
| ! ! 6C.2.364.10# ! |
| ! ! 6C.1.374.01 Right Spoiler ! |
| ! ! 6C.2.374.10# ! |
| ! ! ! |
| ! ! Remark: Report line 'X4' shows RSP4 left spoiler. ! |
| ! ! Report line 'X5' shows RSP4 right spoiler. ! |
| !--------------!------------------------------------------------------! |
| ! RSP5 ! Roll Spoiler 5 Position ! |
| ! X999 ! ! |
| ! ! Format: Negative values are shown with '-' on the ! |
| ! ! first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-45.0 to 0 deg) ! |
| ! ! ! |
| ! ! Source: FCDC 6C.1.365.01 Left Spoiler ! |
| ! ! 6C.2.365.10# ! |
| ! ! 6C.1.375.01 Right Spoiler ! |
| ! ! 6C.2.375.10# ! |
| ! ! ! |
| ! ! Remark: Report line 'X4' shows RSP5 left spoiler. ! |
| ! ! Report line X5 shows RSP5 right spoiler. ! |
| !--------------!------------------------------------------------------! |
| ! FLAP ! FLAP Actual Position ! |
| ! X999 ! ! |
| ! ! Format: Negative values are shown with '-' on the ! |
| ! ! first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (0.0 to 40.0 deg) ! |
| ! ! (see table DT40 for special conversion) ! |
| ! ! ! |
| ! ! Source: SFCC 1B.1.137.01 FLAP System 1 ! |
| ! ! 1B.2.137.10 FLAP System 2 ! |
| ! ! ! |
| ! ! Remark: Report line 'X4' shows FLAP System 1. ! |
| ! ! Report line 'X5' shows FLAP System 2. ! |
| !--------------!------------------------------------------------------! |
| ! SLAT ! SLAT Actual Position ! |
| ! X999 ! ! |
| ! ! Format: Negative values are shown with '-' on the ! |
| ! ! first position. Otherwise the first ! |
| ! ! position contains a'0'. ! |
| ! ! (0.0 to 27.0 deg) ! |
| ! ! ! |
| ! ! Source: SFCC 1B.1.127.01 SLAT System 1 ! |
| ! ! 1B.2.127.10 SLAT System 2 ! |
| ! ! ! |
| ! ! Remark: Report line 'X4' shows SLAT System 1. ! |
| ! ! Report line 'X5' shows SLAT System 2. ! |
| !--------------!------------------------------------------------------! |
| ! THDG ! True Heading (BCD) ! |
| ! 9999 ! ! |
| ! ! Format: (0 to 359.9 deg) ! |
| ! ! ! |
| ! ! Source: ADIRU 04.1.044.01 THDG System 1 ! |
| ! ! 04.2.044.10 THDG System 1 ! |
| ! ! ! |
| ! ! Remark: Report line 'X6' shows THDG System 1. ! |
| ! ! Report line 'X7' shows THDG System 2. ! |
| !--------------!------------------------------------------------------! |
| ! LONP ! Longitude Position ! |
| ! X9999 ! ! |
| ! ! Format: The first position shows if east or west. ! |
| ! ! 'E' for an East position and 'W' for a West! |
| ! ! position. ! |
| ! ! (East 179.9 deg to West 179.9 deg) ! |
| ! ! ! |
| ! ! Source: ADIRU 04.1.311.01 LONP System 1 ! |
| ! ! 04.2.311.10 LONP System 2 ! |
| ! ! ! |
| ! ! Remark: Report line 'X6' shows LONP System 1. ! |
| ! ! Report line 'X7' shows LONP System 2. ! |
| !--------------!------------------------------------------------------! |
| ! LATP ! Latitude Position ! |
| ! X999 ! ! |
| ! ! Format: The first position shows if north ! |
| ! ! or south '-' for a North position and 'S' ! |
| ! ! for a South position. ! |
| ! ! (North 89.9 deg to South 89.9 deg) ! |
| ! ! ! |
| ! ! Source: ADIRU 04.1.310.XX LATP System 1 ! |
| ! ! 04.2.310.XX LATP System 2 ! |
| ! ! ! |
| ! ! Remark: Report line 'X6' shows LATP System 1. ! |
| ! ! Report line 'X7' shows LATP System 2. ! |
| !--------------!------------------------------------------------------! |
| ! WS ! Wind Speed ! |
| ! 999 ! ! |
| ! ! Format: (0 to 100 kts) ! |
| ! ! ! |
| ! ! Source: ADIRU 04.1.315.01 WS System 1 ! |
| ! ! 04.2.315.10 WS System 2 ! |
| ! ! ! |
| ! ! Remark: Report line 'X6' shows WS System 1. ! |
| ! ! Report line 'X7' shows WS System 2. ! |
| !--------------!------------------------------------------------------! |
| ! WD ! Wind Direction - True ! |
| ! 999 ! ! |
| ! ! Format: (0 to 359 deg) ! |
| ! ! ! |
| ! ! Source: ADIRU 04.1.316.01 WD System 1 ! |
| ! ! 04.2.316.10 WD System 2 ! |
| ! ! ! |
| ! ! Remark: Report line 'X6' shows WD System 1. ! |
| ! ! Report line 'X7' shows WD System 2. ! |
| !--------------!------------------------------------------------------! |
| ! FT ! Wing Fuel Temperature ! |
| ! X999 ! ! |
| ! ! Format: (-60.0 to 170.0°) ! |
| ! ! ! |
| ! ! Source: FQIC 5A.2.177.10 Fuel Temp. Left Wing Tank ! |
| ! ! 5A.2.210.10 Fuel Temp. Right Wing Tank! |
| ! ! ! |
| ! ! Remark: Report line 'X6' shows the fuel temperature! |
| ! ! from the Left Wing Tank. ! |
| ! ! Report line 'X7' shows the fuel temperature! |
| ! ! from the Right Wing Tank. ! |
| !--------------!------------------------------------------------------! |
| ! FD ! Fuel Density ! |
| ! 0999 ! ! |
| ! ! Format: (0 to 0.999 kg/l) ! |
| ! ! ! |
| ! ! Source: FQIC 5A.2.272.10 ! |
| ! ! ! |
| ! ! Remark: The Fuel Density value of the various tanks! |
| ! ! (Left Wing Tank, Center Tank and Right Wing! |
| ! ! Tank) is transmitted one after another on ! |
| ! ! label 272. The adequate tank identification! |
| ! ! is as follows: ! |
| ! ! ! |
| ! ! For A318, A319 and A320: ! |
| ! ! Bit 11-14 = 0.0001 ! |
| ! ! Bit 15-18 = 0.001 ! |
| ! ! Bit 19-22 = 0.01 ! |
| ! ! Bit 23-26 = 0.1 ! |
| ! ! Bit 27-29 = Fuel tank Ident (Left/Center/Right) ! |
| ! ! ! |
| ! ! For A321: ! |
| ! ! Bit 11-13 = Fuel tank Ident (Left/Center/Right) ! |
| ! ! Bit 14-17 = 0.0001 ! |
| ! ! Bit 18-21 = 0.001 ! |
| ! ! Bit 22-25 = 0.01 ! |
| ! ! Bit 26-29 = 0.1 ! |
| ! ! ! |
| ! ! The update rate of label 272 is 1 second. Due to ! |
| ! ! this fact the Fuel Density value of the dedicated ! |
| ! ! tank is available every 3 seconds. ! |
| +---------------------------------------------------------------------+ |
(5) Cruise Performance Report Data Field Description <02> (Engine Type CFMI with Advanced EVMU)
NOTE: Reports that are transmitted from the ACARS system do not have report lines without a line identifier.
| +---------------------------------------------------------------------+ |
| ! Value ! Content Description ! |
| !--------------!------------------------------------------------------! |
| ! TAT ! Total Air Temperature ! |
| ! X999 ! ! |
| ! ! Format: Negative values are shown with '-' on the ! |
| ! ! first position. Otherwise the first ! |
| ! ! position contains '0'. ! |
| ! ! (-60.0 to 99.9°) ! |
| ! ! ! |
| ! ! Source: ADIRU 06.1.211.01 ! |
| ! ! 06.2.211.10# ! |
| !--------------!------------------------------------------------------! |
| ! ALT ! Standard Altitude (1013mbar) ! |
| ! X9999 ! ! |
| ! ! Format: Negative values are shown with '-' on the ! |
| ! ! first position. Otherwise the first ! |
| ! ! position is used for the value. ! |
| ! ! (-2000 to 50000 ft) ! |
| ! ! ! |
| ! ! Source: ADIRU 06.1.203.01 ! |
| ! ! 06.2.203.10# ! |
| !--------------!------------------------------------------------------! |
| ! CAS ! Computed Air Speed ! |
| ! 999 ! ! |
| ! ! Format: (30 to 450 kts) ! |
| ! ! ! |
| ! ! Source: ADIRU 06.1.206.01 ! |
| ! ! 06.2.206.10# ! |
| !--------------!------------------------------------------------------! |
| ! MN ! Mach Number ! |
| ! 999 ! ! |
| ! ! Format: (0.100 to 0.999) ! |
| ! ! ! |
| ! ! Source: ADIRU 06.1.205.01 ! |
| ! ! 06.2.205.10# ! |
| !--------------!------------------------------------------------------! |
| ! GW ! Gross Weight ! |
| ! 9999 ! ! |
| ! ! Format: (0 to 8000*10 kg) ! |
| ! ! ! |
| ! ! Source: FMGC 02.1.075.00 ! |
| ! ! 02.2.075.00# ! |
| !--------------!------------------------------------------------------! |
| ! CG ! Center of Gravity ! |
| ! 999 ! ! |
| ! ! Format: (0 to 35.0 %MAC) ! |
| ! ! ! |
| ! ! Source: FMGC 02.1.077.00 ! |
| ! ! 02.2.077.00# ! |
| !--------------!------------------------------------------------------! |
| ! ESN ! Engine Serial Number ! |
| ! 999999 ! ! |
| ! ! Format: (000000 to 999999) ! |
| ! ! ! |
| ! ! Source: ECU Engine 1 ! |
| ! ! 7C.1.046.01 digit 3, 2, 1 ! |
| ! ! 7C.1.047.01 digit 6, 5, 4 ! |
| ! ! Engine 2 ! |
| ! ! 7C.2.046.10 digit 3, 2, 1 ! |
| ! ! 7C.2.047.10 digit 6, 5, 4 ! |
| !--------------!------------------------------------------------------! |
| ! EHRS ! Engine Flight Hours ! |
| ! ! ! |
| ! 99999 ! Format: (00000 to 99999 hours) ! |
| ! ! ! |
| ! ! Source: DMU Engine 1 ! |
| ! ! Engine 2 ! |
| ! ! ! |
| ! ! Remark: Time between "Main (LH and RH) Landing Gear! |
| ! ! Decompressed" and "Main (LH and RH) Landing! |
| ! ! Gear Compressed". The EHRS is be set to ! |
| ! ! zero if a new ESN is recognized by the DMU.! |
| ! ! It is be possible to set the EHRS via the ! |
| ! ! MCDU, e.g. if the DMU is changed on the ! |
| ! ! a/c. ! |
| !--------------!------------------------------------------------------! |
| ! ERT ! Engine Running Time ! |
| ! 99999 ! ! |
| ! ! Format: (00000 to 65536 hours) ! |
| ! ! ! |
| ! ! Source: ECU 7C.1.050.01 Engine 1 ! |
| ! ! 7C.2.050.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! ECYC ! Engine Cycle ! |
| ! 99999 ! ! |
| ! ! Format: (00000 to 99999) ! |
| ! ! ! |
| ! ! Source: DMU Engine 1 ! |
| ! ! Engine 2 ! |
| ! ! ! |
| ! ! Remark: Each time when flight phase 5 (climb) is ! |
| ! ! reached, the counter is incremented by one.! |
| ! ! The ECYC is set to zero if a new ESN is ! |
| ! ! recognized by the DMU. It is possible to ! |
| ! ! set ECYC via the MCDU, if the DMU is ! |
| ! ! changed on the a/c. ! |
| !--------------!------------------------------------------------------! |
| ! AP ! Auto Pilot Status ! |
| ! 99 ! ! |
| ! ! Format: Number of respective status (00 to G8) ! |
| ! ! ! |
| ! ! Source: FMGC 1 and 2 (FGC part) for Auto Pilot ! |
| ! ! AP1 and AP2 ! |
| ! ! ! |
| ! ! Parameter for AP1 ! Parameter for AP2 ! ! |
| ! ! Report Line EC: ! Report Line EE: !Definition: ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! / ! / !No Mode ! |
| ! ! ! !Active ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.11 = 1 ! 01.2.275.00.11 = 1!RUNWAY Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.12 = 1 ! 01.2.275.00.12 = 1!NAV Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.13 = 1 ! 01.2.275.00.13 = 1!LOC CAPTURE ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.14 = 1 ! 01.2.275.00.14 = 1!LOC TRACK ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.15 = 1 ! 01.2.275.00.15 = 1!Roll GO ! |
| ! ! ! !AROUND Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.16 = 1 ! 01.2.275.00.16 = 1!HEADING Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.17 = 1 ! 01.2.275.00.17 = 1!TRACK Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.15 = 1 ! 01.2.274.00.15 = 1!PITCH T/O ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.16 = 1 ! 01.2.274.00.16 = 1!PITCH GA Mode! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.17 = 1 ! 01.2.274.00.17 = 1!V/S Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.18 = 1 ! 01.2.274.00.18 = 1!FPA Mode ! |
| ! ! -------------------!-------------------!-------------! |
| ! ! 01.1.274.00.19 = 1 ! 01.2.274.00.19 = 1!ALT Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.20 = 1 ! 01.2.274.00.20 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.19 = 1 ! 01.2.274.00.19 = 1!ALT ACQ ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.21 = 1 ! 01.2.274.00.21 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.20 = 1 ! 01.2.274.00.20 = 1!G/S TRACK ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.22 = 1 ! 01.2.274.00.22 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.21 = 1 ! 01.2.274.00.21 = 1!G/S CAPTURE ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.22 = 1 ! 01.2.274.00.22 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.23 = 1 ! 01.2.274.00.23 = 1!FINAL DES ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.24 = 1 ! 01.2.274.00.24 = 1!EXPED. Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.146.00.14 = 1 ! 01.2.146.00.14 = 1!LAND TRACK ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!CLB Mode ! |
| ! ! AND ! AND ! ! |
| ! ! ! ! ! ! ! |
| ! ! -------------- ! -------------- ! ! |
| ! ! 01.1.274.00.13 = 0 ! 01.2.274.00.13 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.14 = 0 ! 01.2.274.00.14 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.24 = 0 ! 01.2.274.00.24 = 0! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!DES Mode ! |
| ! ! AND ! AND ! ! |
| ! ! ! ! ! ! ! |
| ! ! -------------- ! -------------- ! ! |
| ! ! 01.1.274.00.13 = 0 ! 01.2.274.00.13 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.14 = 0 ! 01.2.274.00.14 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.24 = 0 ! 01.2.274.00.24 = 0! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!IM. CLIMB ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.13 = 1 ! 01.2.274.00.13 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!IM. DES Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.13 = 1 ! 01.2.274.00.13 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!OPEN CLB ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.14 = 1 ! 01.2.274.00.14 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!OPEN. DES ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.14 = 1 ! 01.2.274.00.14 = 1! ! |
| ! ! ---------------------------------------------------- ! |
| ! ! Auto Pilot Status DMU: ! |
| ! ! Auto Pilot AP1 printed in report line EC ! |
| ! ! Auto Pilot AP2 printed in report line EE ! |
| ! ! Combined Auto Pilot Modes ! |
| ! ! The longitudinal auto pilot mode (1 to G) appears ! |
| ! ! on the left position for the AP1 and AP2 print ! |
| ! ! format. ! |
| ! ! The lateral auto pilot mode (1 to 8) appears on the ! |
| ! ! right position for the AP1 and AP2 print format. ! |
| ! ! In case of a combined auto pilot mode e.g. DES mode ! |
| ! ! and NAV mode are engaged simultaneously, the 'E3' ! |
| ! ! appears below AP1 and AP2. ! |
| ! ! XX Auto Pilot Modes: ! |
| ! ! !! ! |
| ! ! !!__Lateral Modes: 0 = NO MODE ! |
| ! ! ! 1 = HEADING ! |
| ! ! ! 2 = TRACK ! |
| ! ! ! 3 = NAV ! |
| ! ! ! 4 = LOC CAPTURE ! |
| ! ! ! 5 = LOCK TRACK ! |
| ! ! ! 6 = LAND TRACK ! |
| ! ! ! 7 = RUNWAY ! |
| ! ! ! 8 = ROLL GO AROUND ! |
| ! ! ! ! |
| ! ! !__Longitudinal Modes: 0 = NO MODE ! |
| ! ! 1 = PITCH G/A ! |
| ! ! 2 = PITCH TO ! |
| ! ! 3 = G/S TRACK ! |
| ! ! 4 = G/S CAPTURE ! |
| ! ! 5 = V/S ! |
| ! ! 6 = FPA ! |
| ! ! 7 = ALT ! |
| ! ! 8 = ALT ACQ ! |
| ! ! 9 = OPEN CLB ! |
| ! ! A = OPEN DES ! |
| ! ! B = IM CLB ! |
| ! ! C = IM DES ! |
| ! ! D = CLB ! |
| ! ! E = DES ! |
| ! ! F = FINAL DES ! |
| ! ! G = EXPEDITE ! |
| !--------------!------------------------------------------------------! |
| ! QA ! Aircraft Quality Number, Report Stability ! |
| ! 99 ! ! |
| ! ! Format: (00 to 99) ! |
| ! ! ! |
| ! ! Source: DMU ! |
| ! ! ! |
| ! ! Remark: 00 = best stable frame ! |
| ! ! 99 = worst stable frame ! |
| ! ! ! |
| ! ! i=1 VARa(i) ! |
| ! ! QA= SIGMA(Wa(i)*--------------- ! |
| ! ! N TOLa(i)*TOLa(i) ! |
| ! ! ! |
| ! !QA= Quality Number ! |
| ! !Wa(i)= Individual weighting factors for the individual! |
| ! ! quality parameters for the Cruise Report. ! |
| ! !VARa(i)= parameter variances ! |
| ! !TOLa(i)= Variation values for the individual quality ! |
| ! ! parameters for the Cruise Performance Report.! |
| !--------------!------------------------------------------------------! |
| ! QE ! Engine Quality Number, Report Stability ! |
| ! 99 ! ! |
| ! ! Format: (00 to 99) ! |
| ! ! ! |
| ! ! Source: DMU ! |
| ! ! ! |
| ! ! Remark: 00=best stable frame, ! |
| ! ! 99=worst stable frame. ! |
| ! ! ! |
| ! ! i=1 VARe(i) ! |
| ! ! QE= SIGMA(We(i)*--------------- ! |
| ! ! N TOLe(i)*TOLe(i) ! |
| ! ! ! |
| ! !QE= Engine quality number ! |
| ! !We(i)= Individual weighting factors for the individual! |
| ! ! quality parameters for the Cruise Report. ! |
| ! !VARe(i)= parameter variances ! |
| ! !TOLe(i)= Variation values for the individual quality ! |
| ! ! parameters for the cruise report. ! |
| !--------------!------------------------------------------------------! |
| ! N1 ! Selected N1 Actual ! |
| ! 9999 ! ! |
| ! ! Format: (0 to 120.0 %rpm) ! |
| ! ! ! |
| ! ! Source: ECU 7C.1.346.01 Engine 1 ! |
| ! ! 7C.2.346.10 Engine 2 ! |
| ! ! ! |
| ! ! Remark: In the report lines 'V3' and 'V4' the ! |
| ! ! values from the last stable descent are ! |
| ! ! printed. ! |
| ! ! In the report lines 'V5' and 'V6' the ! |
| ! ! values from the last stable climb are ! |
| ! ! printed. ! |
| !--------------!------------------------------------------------------! |
| ! N1C ! N1 Command ! |
| ! 9999 ! ! |
| ! ! Format: (0 to 120.0 %rpm) ! |
| ! ! ! |
| ! ! Source: ECU 7C.1.341.01 Engine 1 ! |
| ! ! 7C.2.341.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! N2 ! Selected N2 Actual ! |
| ! 9999 ! ! |
| ! ! Format: (0 to 120.0 %rpm) ! |
| ! ! ! |
| ! ! Source: ECU 7C.1.344.01 Engine 1 ! |
| ! ! 7C.2.344.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! EGT ! Selected T495 (Exhaust Gas Temperature) ! |
| ! X999 ! ! |
| ! ! Format: Negative values are indicated by '-' on the! |
| ! ! first position. Otherwise the first ! |
| ! ! position is used for the value. ! |
| ! ! (-55 to 999.9 °) ! |
| ! ! ! |
| ! ! Source: ECU 7C.1.345.01 Engine 1 ! |
| ! ! 7C.2.345.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! FF ! Engine Fuel Flow ! |
| ! 9999 ! ! |
| ! ! Format: 0 to 7000 kg/h (0 to 15000 p/h) ! |
| ! ! ! |
| ! ! Source: ECU 7C.1.244.01 Engine 1 ! |
| ! ! 7C.2.244.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! PS13 ! PS13 Static Air Pressure at Position 1.3 ! |
| ! 99999 ! ! |
| ! ! Format: (0.0 to 30.000 psia) ! |
| ! ! ! |
| ! ! Source: ECU 7C.1.127.01 Engine 1 ! |
| ! ! 7C.2.127.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! P25 ! P25 Total Air Pressure at Position 2.5 ! |
| ! 99999 ! ! |
| ! ! Format: (0.0 to 50.000 psia) ! |
| ! ! ! |
| ! ! Source: ECU 7C.1.262.01 Engine 1 ! |
| ! ! 7C.2.262.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! T25 ! Selected T25 ! |
| ! X999 ! ! |
| ! ! Format: Negative values are indicated by '-' on ! |
| ! ! the first position. Otherwise the first ! |
| ! ! position is used for the value. ! |
| ! ! (-55.0 to 120.0 [C) ! |
| ! ! ! |
| ! ! Source: ECU 7C.1.263.01 Engine 1 ! |
| ! ! 7C.2.263.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! P3 ! Selected PS3 ! |
| ! 9999 ! ! |
| ! ! Format: (0.0 to 450.0 psia) ! |
| ! ! ! |
| ! ! Source: ECU 7C.1.264.01 Engine 1 ! |
| ! ! 7C.2.264.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! T3 ! Selected T3 ! |
| ! X999 ! ! |
| ! ! Format: Negative values are indicated by '-' on ! |
| ! ! the first position. Otherwise the first ! |
| ! ! position is used for the value. ! |
| ! ! (-55.0 to 850.0 °) ! |
| ! ! ! |
| ! ! Source: ECU 7C.1.265.01 Engine 1 ! |
| ! ! 7C.2.265.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! T5 ! T5 Temperature at position T5 ! |
| ! X999 ! ! |
| ! ! Format: Negative values are indicated by '-' on ! |
| ! ! the first position. Otherwise the firt ! |
| ! ! position is used for the value. ! |
| ! ! (-55.0 to 850.0 °) ! |
| ! ! ! |
| ! ! Source: ECU 7C.1.260.01 Engine 1 ! |
| ! ! 7C.2.260.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! VSV ! Selected Variable Stator Vane Position ! |
| ! X99 ! ! |
| ! ! Format: Negative values are indicated by '-' on ! |
| ! ! the first position. Otherwise the first ! |
| ! ! position is used for the value. ! |
| ! ! (-5.0 to 45.0 deg) ! |
| ! ! ! |
| ! ! Source: ECU 7C.1.072.01 Engine 1 ! |
| ! ! 7C.2.072.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! VBV ! Variable Bleed Valve Position ! |
| ! X99 ! ! |
| ! ! Format: Negative values are indicated by '-' on ! |
| ! ! the first position. Otherwise the first ! |
| ! ! position is used for the value. ! |
| ! ! (-9.9 to 40.0 deg) ! |
| ! ! ! |
| ! ! Source: ECU 7C.1.071.01 Engine 1 ! |
| ! ! 7C.2.071.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! HPT ! Selected HPTC Position ! |
| ! X99 ! ! |
| ! ! Format: (-10 to 100 %) ! |
| ! ! ! |
| ! ! Source: ECU 7C.1.306.01 Engine 1 ! |
| ! ! 7C.2.306.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! LPT ! Selected LPTC Position ! |
| ! X99 ! ! |
| ! ! Format: (-10 to 100 %) ! |
| ! ! ! |
| ! ! Source: ECU 7C.1.307.01 Engine 1 ! |
| ! ! 7C.2.307.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! GLE ! Engine Generator Load ! |
| ! 999 ! ! |
| ! ! Format: (0 to 100%) ! |
| ! ! ! |
| ! ! Source: SDAC 29.1.077.01 Engine 1 ! |
| ! ! 29.2.077.01# ! |
| ! ! 29.1.077.10 Engine 2 ! |
| ! ! 29.2.077.10# ! |
| !--------------!------------------------------------------------------! |
| ! PD ! Precooler Inlet Pressure ! |
| ! 99 ! ! |
| ! ! Format: (0 to 50 psi) ! |
| ! ! ! |
| ! ! Source: BMC 06F.1.143.01 Engine 1 ! |
| ! ! 06F.2.143.10# ! |
| ! ! 06F.1.142.01 Engine 2 ! |
| ! ! 06F.2.142.10# ! |
| !--------------!------------------------------------------------------! |
| ! TN ! Nacelle Temperature ! |
| ! X99 ! ! |
| ! ! Format: Negative values are indicated by '-' on ! |
| ! ! the first position. Otherwise the first ! |
| ! ! position is used for the value. ! |
| ! ! (-55 to 300 °) ! |
| ! ! ! |
| ! ! Source: FWC 26.1.322.01 Engine 1 ! |
| ! ! 26.2.322.01# ! |
| ! ! 26.1.322.10 Engine 2 ! |
| ! ! 26.2.322.10# ! |
| !--------------!------------------------------------------------------! |
| ! PT2 ! PT2 Total Air Pressure at Position 2 ! |
| ! 99999 ! ! |
| ! ! Format: (0.0 to 25.000 psia) ! |
| ! ! ! |
| ! ! Source: ECU 7C.1.131.01 Engine 1 ! |
| ! ! 7C.2.131.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! OIQH ! Oil Consumption from the previous flight ! |
| ! X999 ! ! |
| ! ! Format: (-9.99 to 20.00 qts/h) ! |
| ! ! ! |
| ! ! Source: DMU Engine 1 ! |
| ! ! Engine 2 ! |
| ! ! ! |
| ! ! Remark: Following formula is used. ! |
| ! ! ! |
| ! ! OIKa-OIKb ! |
| ! ! OIQH=---------(qts/h) ! |
| ! ! UTCb-UTCa ! |
| ! ! ! |
| ! ! OIK=oil quantity corrected ! |
| ! ! suffix a denotes taxi out condition ! |
| ! ! suffix b denotes taxi in condition ! |
| ! ! The calculation is done 'Y01.5' seconds before the ! |
| ! ! flight phase changes from 2 to 3 and ! |
| ! ! 'Y01.4' seconds after beginning of flight phase 9. ! |
| ! ! OIKa=OIQa*(A*OITa+B) ! |
| ! ! OIKb=OIQb*(A*OITb+B) ! |
| ! ! OIQ= measured oil quantity 29.1.073.11 Engine 1 ! |
| ! ! 29.2.073.11# ! |
| ! ! 29.1.073.00 Engine 2 ! |
| ! ! 29.2.073.00# ! |
| ! ! OIQ= measured oil quantity 29.1.316.11 Engine 1 ! |
| ! ! 29.2.316.11# ! |
| ! ! 29.1.316.00 Engine 2 ! |
| ! ! 29.2.316.00# ! |
| ! ! A=6.4*1/10000 ! |
| ! ! B=1.013 ! |
| !--------------!------------------------------------------------------! |
| ! VN ! FAN Pick Up N1 Track Vibration ! |
| ! 99 ! ! |
| ! ! Format: (0.0 to 10.0) ! |
| ! ! If value is 10.0 then 99 is printed. ! |
| ! ! ! |
| ! ! Source: EVM 3D.1.227.01 Engine 1 ! |
| ! ! 3D.1.227.10 Engine 2 ! |
| ! ! ! |
| ! ! Remark: In report lines 'V3' and 'V4' the values ! |
| ! ! from the last stable descent are printed. ! |
| ! ! In report lines 'V5' and 'V6' the values ! |
| ! ! from the last stable climb are printed. ! |
| !--------------!------------------------------------------------------! |
| ! VL ! TRF Pick Up N1 Track Vibration ! |
| ! 99 ! ! |
| ! ! Format: (0.0 to 10.0) ! |
| ! ! If value is 10.0 then 99 is printed. ! |
| ! ! ! |
| ! ! Sources: EVM 3D.1.227.11 Engine 1 ! |
| ! ! 3D.1.227.00 Engine 2 ! |
| ! ! ! |
| ! ! Remark: In report lines 'V3' and 'V4' the values ! |
| ! ! from the last stable descent are printed. ! |
| ! ! In report lines 'V5' and 'V6' the values ! |
| ! ! from the last stable climb are printed. ! |
| !--------------!------------------------------------------------------! |
| ! PHT ! TRF Pick Up Phase Angle ! |
| ! 999 ! ! |
| ! ! Format: (0 to 360 deg) ! |
| ! ! ! |
| ! ! Sources: EVM 3D.1.226.11 Engine 1 ! |
| ! ! 3D.1.226.00 Engine 2 ! |
| ! ! ! |
| ! ! Remark: In report lines 'V3' and 'V4' the values ! |
| ! ! from the last stable descent are printed. ! |
| ! ! In report lines 'V5' and 'V6' the values ! |
| ! ! from the last stable climb are printed. ! |
| !--------------!------------------------------------------------------! |
| ! VC ! FAN Pick Up N2 Track Vibration ! |
| ! 99 ! ! |
| ! ! Format: (0.0 to 4.0) ! |
| ! ! ! |
| ! ! Sources: EVM 3D.1.230.01 Engine 1 ! |
| ! ! 3D.1.230.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! VH ! TRF Pick Up N2 Track Vibration ! |
| ! 99 ! ! |
| ! ! Format: (0.0 to 4.0) ! |
| ! ! ! |
| ! ! Sources: EVM 3D.1.230.01 Engine 1 ! |
| ! ! 3D.1.230.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! EVM ! Engine Vibration Status Word ! |
| ! XXXXX ! ! |
| ! ! Format: Each 'X' represents 4 bits in hexadecimal ! |
| ! ! presentation of a defined ARINC 429 word. ! |
| ! ! ! |
| ! ! XXXXX Bits HEX ! |
| ! ! !!!!!________14, 13, 12, 11 0..F ! |
| ! ! !!!!_________18, 17, 16, 15 0..F ! |
| ! ! !!!__________22, 21, 20, 19 0..F ! |
| ! ! !!___________26, 25, 24, 23 0..F ! |
| ! ! !____________ 29, 28, 27 0..F ! |
| ! ! ! |
| ! ! Sources: EVM 3D.1.035.01 Engine 1 ! |
| ! ! 3D.1.035.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! OIP ! Engine Oil Pressure ! |
| ! 999 ! ! |
| ! ! Format: (0 to 400 psia) ! |
| ! ! ! |
| ! ! Source: FWC 26.1.317.01 Engine 1 ! |
| ! ! 26.2.317.01# ! |
| ! ! 26.1.317.10 Engine 2 ! |
| ! ! 26.2.317.10# ! |
| !--------------!------------------------------------------------------! |
| ! OIT ! Engine Oil Temperature ! |
| ! X99 ! ! |
| ! ! Format: Negative values are indicated by '-' on ! |
| ! ! the first position. Otherwise the firt ! |
| ! ! position is used for the value. ! |
| ! ! (-60 to 250 °) ! |
| ! ! ! |
| ! ! Source: FWC 26.1.316.01 Engine 1 ! |
| ! ! 26.2.316.01# ! |
| ! ! 26.1.316.10 Engine 2 ! |
| ! ! 26.2.316.10# ! |
| !--------------!------------------------------------------------------! |
| ! ECW1 ! Engine Control Word 1 ! |
| ! XXXXX ! ! |
| ! ! Format: Each 'X' represents 4 bits in hexadecimal ! |
| ! ! presentation of a defined ARINC 429 word. ! |
| ! ! ! |
| ! ! Sources: DMU is composed of several ECU discrete ! |
| ! ! labels as defined below for engine 1 and ! |
| ! ! engine 2. ! |
| ! ! ! |
| ! ! XXXXX Bits HEX ! |
| ! ! !!!!!________14, 13, 12, 11 0..F ! |
| ! ! !!!!_________18, 17, 16, 15 0..F ! |
| ! ! !!!__________22, 21, 20, 19 0..F ! |
| ! ! !!___________26, 25, 24, 23 0..F ! |
| ! ! !____________ 29, 28, 27 0..F ! |
| ! ! Bit Label Parameter Description ! |
| ! ! 11 7C.X.272.XX.19 = 1 Auto Thrust Active ! |
| ! ! 12 7C.X.275.XX.20 = 1 VSV Position Fault ! |
| ! ! 13 SPARE ! |
| ! ! 14 SPARE ! |
| ! ! 15 7C.X.351.XX.29 = 1 Fuel Flow Measurement ! |
| ! ! Invalid ! |
| ! ! 16 7C.X.275.XX.15 = 1 N1/N2 Control Active ! |
| ! ! 17 7C.X.275.XX.26 = 1 Channel A Active ! |
| ! ! 18 7C.X.275.XX.27 = 1 Channel B Active ! |
| ! ! 19 SPARE ! |
| ! ! 20 SPARE ! |
| ! ! 21 SPARE ! |
| ! ! 22 SPARE ! |
| ! ! 23 SPARE ! |
| ! ! 24 SPARE ! |
| ! ! 25 SPARE ! |
| ! ! 26 SPARE ! |
| ! ! 27 SPARE ! |
| ! ! 28 SPARE ! |
| ! ! 29 SPARE ! |
| ! ! The 'X' for the System and SDI definition of the ! |
| ! ! engine parameters are as follows: ! |
| ! ! System SDI ! |
| ! ! Engine 1 1 01 ! |
| ! ! Engine 2 2 10 ! |
| !--------------!------------------------------------------------------! |
| ! SSEL ! Status of different FADEC sensors ! |
| ! XXXXXXX ! ! |
| ! XXXXXXX ! Format: ! |
| ! ! XXXXXXXXXXXXXX Label: Selected: ! |
| ! ! !!!!!!!!!!!!!!_ 346 N1 actual (Bit 11 -> 15)! |
| ! ! !!!!!!!!!!!!!__ 345 EGT (Bit 11 -> 15)! |
| ! ! !!!!!!!!!!!!___ 344 N2 actual (Bit 11 -> 15)! |
| ! ! !!!!!!!!!!!____ 263 T25 (Bit 11 -> 15)! |
| ! ! !!!!!!!!!!_____ 264 PS3 (Bit 11 -> 15)! |
| ! ! !!!!!!!!!______ 265 T3 (Bit 11 -> 15)! |
| ! ! !!!!!!!!_______ 072 VSV Position (Bit 11 -> 15)! |
| ! ! !!!!!!!________ 071 VBV Position (Bit 11 -> 15)! |
| ! ! !!!!!!_________ 306 HPTC Position (Bit 11 -> 15)! |
| ! ! !!!!!__________ 307 LPTH Position (Bit 11 -> 15)! |
| ! ! !!!!___________ 347 FMV Position (Bit 11 -> 15)! |
| ! ! !!!____________ 211 TAT (Bit 11 -> 15)! |
| ! ! !!_____________ 114 P0 (Bit 11 -> 15)! |
| ! ! !______________ 133 TLA Position (Bit 11 -> 15)! |
| ! ! ! |
| ! ! Source: ECU, different labels ! |
| ! ! ! |
| ! ! Remarks: The indicated values are coded as follows: ! |
| ! ! ! |
| ! ! Bit: 15 14 13 12 11 ! indicated value ! |
| ! ! --------------------!---------------- ! |
| ! ! 0 0 0 0 0 ! 0 ! |
| ! ! 0 0 0 0 1 ! 1 ! |
| ! ! 0 0 0 1 0 ! 2 ! |
| ! ! 0 0 0 1 1 ! 3 ! |
| ! ! 0 0 1 0 0 ! 4 ! |
| ! ! 0 0 1 0 1 ! 5 ! |
| ! ! 0 0 1 1 0 ! 6 ! |
| ! ! 0 0 1 1 1 ! 7 ! |
| ! ! 0 1 0 0 0 ! 8 ! |
| ! ! 0 1 0 0 1 ! 9 ! |
| ! ! 0 1 0 1 0 ! A ! |
| ! ! 0 1 0 1 1 ! B ! |
| ! ! 0 1 1 0 0 ! C ! |
| ! ! 0 1 1 0 1 ! D ! |
| ! ! 0 1 1 1 0 ! E ! |
| ! ! 0 1 1 1 1 ! F ! |
| ! ! 1 0 0 0 0 ! G ! |
| ! ! 1 0 0 0 1 ! H ! |
| ! ! 1 0 0 1 0 ! I ! |
| ! ! 1 0 0 1 1 ! J ! |
| ! ! 1 0 1 0 0 ! K ! |
| ! ! 1 0 1 0 1 ! L ! |
| ! ! 1 0 1 1 0 ! M ! |
| ! ! 1 0 1 1 1 ! N ! |
| ! ! 1 1 0 0 0 ! O ! |
| ! ! 1 1 0 0 1 ! P ! |
| ! ! 1 1 0 1 0 ! Q ! |
| ! ! 1 1 0 1 1 ! R ! |
| ! ! 1 1 1 0 0 ! S ! |
| ! ! 1 1 1 0 1 ! T ! |
| ! ! 1 1 1 1 0 ! U ! |
| ! ! 1 1 1 1 1 ! V ! |
| !--------------!------------------------------------------------------! |
| ! WFQ ! Fuel Quantity Inner Cell ! |
| ! 99999 ! ! |
| ! ! Format: (0 to 99999 kg) ! |
| ! ! ! |
| ! ! Sources: FQIC 5A.2.257.10 Left Inner Cell Fuel ! |
| ! ! Quantity ! |
| ! ! 5A.2.261.10 Right Inner Cell Fuel ! |
| ! ! Quantity ! |
| ! ! ! |
| ! ! Remark: Report line 'X1' indicates Left Inner Cell ! |
| ! ! Fuel Quantity. ! |
| ! ! Report line 'X2' indicates Right Inner Cell! |
| ! ! Fuel Quantity. ! |
| !--------------!------------------------------------------------------! |
| ! ELEV ! Elevator Position ! |
| ! X999 ! ! |
| ! ! Format: Negative values are indicated by '-' on ! |
| ! ! the first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-30 to 15 deg) ! |
| ! ! ! |
| ! ! Sources: FCDC 6C.1.314.01 Left Elevator Position ! |
| ! ! 6C.2.314.10# ! |
| ! ! 6C.1.334.01 Right Elevator Position! |
| ! ! 6C.2.334.10# ! |
| ! ! ! |
| ! ! Remark: Report line 'X1' shows the Left Elevator ! |
| ! ! Position. ! |
| ! ! Report line 'X2' shows the Right Elevator ! |
| ! ! Position. ! |
| !--------------!------------------------------------------------------! |
| ! AOA ! Corrected Angle of Attack ! |
| ! X999 ! ! |
| ! ! Format: Negative values are indicated by '-' on ! |
| ! ! the first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-30.0 to 85.0 deg) ! |
| ! ! ! |
| ! ! Source: ADIRU 06.1.241.01 AOA System 1 ! |
| ! ! 06.2.241.10 AOA System 2 ! |
| ! ! ! |
| ! ! Remark: Report line 'X1' indicates AOA System 1. ! |
| ! ! Report line 'X2' indicates AOA System 2. ! |
| !--------------!------------------------------------------------------! |
| ! SLP ! Side Slip Angle ! |
| ! X999 ! ! |
| ! ! Format: Negative values are indicated by '-' on ! |
| ! ! the first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-32.0 to 32.0 deg) ! |
| ! ! ! |
| ! ! Source: FAC 0A.1.226.00 SLP System 1 ! |
| ! ! 0A.2.226.00 SLP System 2 ! |
| ! ! ! |
| ! ! Remark: Report line 'X1' indicates SLP System 1. ! |
| ! ! Report line 'X2' indicates SLP System 2. ! |
| !--------------!------------------------------------------------------! |
| ! CFPG ! Calculated Flight Path Acceleration ! |
| ! X9999 ! ! |
| ! ! Format: Negative values are indicated by '-' on ! |
| ! ! the first position. Otherwise the first ! |
| ! ! position is used for the value. ! |
| ! ! (-0.9999 to 4.0000 g) ! |
| ! ! ! |
| ! ! Sources: DMU CFPG calculated value based on GS ! |
| ! ! from System 1 ! |
| ! ! CFPG calculated value based on GS ! |
| ! ! from System 2 ! |
| ! ! ! |
| ! ! GSAV last subperiod-GSAV 1st subperiod ! |
| ! ! CFPG=----------------------------------------------*! |
| ! ! Duration of subperiod*(Number of Subperiods-1) ! |
| ! ! ! |
| ! ! *0.05249 ! |
| ! ! ! |
| ! ! GSAV=Average of Ground Speed (GS) per subperiod ! |
| ! ! (label 04.1.312.01 and 04.2.312.10) ! |
| ! ! ! |
| ! ! Remark: Report line 'X1' indicates CFPG calculated ! |
| ! ! with GS from ADIRU System 1. ! |
| ! ! Report line 'X2' indicates CFPG calculated ! |
| ! ! with GS from ADIRU System 2. ! |
| !--------------!------------------------------------------------------! |
| ! CIVV ! Calculated Inertial Vertical Speed ! |
| ! X999 ! ! |
| ! ! Format: Negative values are indicated by '-' on ! |
| ! ! the first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-999 to 999 ft/min) ! |
| ! ! ! |
| ! ! Source: DMU CIVV calculated value based on IALT ! |
| ! ! from system 1. ! |
| ! ! CIVV calculated value based on IALT ! |
| ! ! from system 2. ! |
| ! ! ! |
| ! ! IALTAV last subperiod-IALTAV 1st subperiod ! |
| ! ! CIVV=----------------------------------------------*! |
| ! ! Duration of subperiod*(Number of Subperiods-1) ! |
| ! ! ! |
| ! ! *60 ! |
| ! ! ! |
| ! ! IALTAV=Average of Inertial Altitude (IALT) per ! |
| ! ! subperiod (label 04.1.361.XX and ! |
| ! ! 04.2.361.XX) ! |
| ! ! ! |
| ! ! Remark: Report line 'X1' indicates CIVV calculated ! |
| ! ! with IALT from ADIRU System 1. ! |
| ! ! Report line 'X2' indicates CIVV calculated ! |
| ! ! with IALT from ADIRU System 2. ! |
| !--------------!------------------------------------------------------! |
| ! RUDD ! Rudder Position ! |
| ! ! ! |
| ! X999 ! Format: Negative values are indicated by '-' on ! |
| ! ! the first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-30.0 to 30.0 deg) ! |
| ! ! ! |
| ! ! Source: SDAC 29.1.312.00 ! |
| ! ! 29.2.312.00# ! |
| !--------------!------------------------------------------------------! |
| ! RUDT ! Rudder Trim Position ! |
| ! X999 ! ! |
| ! ! Format: Negative values area indicated by '-' on ! |
| ! ! the first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-25.0 to 25.0 deg) ! |
| ! ! ! |
| ! ! Source: FAC 0A.1.313.00 ! |
| ! ! 0A.2.313.00# ! |
| !--------------!------------------------------------------------------! |
| ! AILL ! Left Aileron Position ! |
| ! X999 ! ! |
| ! ! Format: Negative values are indicated by '-' on ! |
| ! ! the first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-25.0 to 25.0 deg) ! |
| ! ! ! |
| ! ! Soure: FCDC 6C.1.310.01 ! |
| ! ! 6C.2.310.10# ! |
| !--------------!------------------------------------------------------! |
| ! AILR ! Right Aileron Position ! |
| ! X999 ! ! |
| ! ! Format: Negative values are indicated by '-' on ! |
| ! ! the first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-25.0 to 25.0 deg) ! |
| ! ! ! |
| ! ! Source: FCDC 6C.1.330.01 ! |
| ! ! 6C.2.330.10# ! |
| !--------------!------------------------------------------------------! |
| ! STAB ! Stabilizer Position #1 ! |
| ! X999 ! ! |
| ! ! Format: Negative values are indicated by '-' on ! |
| ! ! the first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-13.5 to 4.0 deg) ! |
| ! ! ! |
| ! ! Soure: FCDC 6C.1.315.01 ! |
| ! ! 6C.2.315.10# ! |
| !--------------!------------------------------------------------------! |
| ! ROLL ! Roll Angle ! |
| ! X999 ! ! |
| ! ! Format: Negative values are indicated by '-' on ! |
| ! ! the first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-90.0 to 90.0 deg) ! |
| ! ! ! |
| ! ! Source: ADIRU 04.1.325.01 ! |
| ! ! 04.2.325.10# ! |
| !--------------!------------------------------------------------------! |
| ! YAW ! Body Axis Yaw Rate ! |
| ! X999 ! ! |
| ! ! Format: Negative values are indicated by '-' on ! |
| ! ! the first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-45.0 to 45.0 deg/sec) ! |
| ! ! ! |
| ! ! Sources: ADIRU 04.1.330.01 ! |
| ! ! 04.2.330.10# ! |
| !--------------!------------------------------------------------------! |
| ! RSP2 ! Roll Spoiler 2 Position ! |
| ! X999 ! ! |
| ! ! Format: Negative values are indicated by '-' on ! |
| ! ! the first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-45.0 to 0 deg) ! |
| ! ! ! |
| ! ! Sourc: FCDC 6C.1.362.01 Left Spoiler ! |
| ! ! 6C.2.362.10# ! |
| ! ! 6C.1.372.01 Right Spoiler ! |
| ! ! 6C.2.372.10# ! |
| ! ! ! |
| ! ! Remark: Report line 'X4' indicates RSP2 left ! |
| ! ! spoiler. ! |
| ! ! Report line 'X5' indicates RSP2 right ! |
| ! ! spoiler. ! |
| !--------------!------------------------------------------------------! |
| ! RSP3 ! Roll Spoiler 3 Position ! |
| ! X999 ! ! |
| ! ! Format: Negative values are indicated by '-' on ! |
| ! ! the first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-45.0 to 0 deg) ! |
| ! ! ! |
| ! ! Source: FCDC 6C.1.363.01 Left Spoiler ! |
| ! ! 6C.2.363.10# ! |
| ! ! 6C.1.373.01 Right Spoiler ! |
| ! ! 6C.2.373.10# ! |
| ! ! ! |
| ! ! Remark: Report line 'X4' indicates RSP3 left ! |
| ! ! spoiler. ! |
| ! ! Report line 'X5' indicates RSP3 right ! |
| ! ! spoiler. ! |
| !--------------!------------------------------------------------------! |
| ! RSP4 ! Roll Spoiler 4 Position ! |
| ! X999 ! ! |
| ! ! Format: Negative values are indicated by '-' on ! |
| ! ! the first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-45.0 to 0 deg) ! |
| ! ! ! |
| ! ! Source: FCDC 6C.1.364.01 Left Spoiler ! |
| ! ! 6C.2.364.10# ! |
| ! ! 6C.1.374.01 Right Spoiler ! |
| ! ! 6C.2.374.10# ! |
| ! ! ! |
| ! ! Remark: Report line 'X4' indicates RSP4 left ! |
| ! ! spoiler. ! |
| ! ! Report line 'X5' indicates RSP4 right ! |
| ! ! spoiler. ! |
| !--------------!------------------------------------------------------! |
| ! RSP5 ! Roll Spoiler 5 Position ! |
| ! X999 ! ! |
| ! ! Format: Negative values are indicated by '-' on ! |
| ! ! the first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-45.0 to 0 deg) ! |
| ! ! ! |
| ! ! Source: FCDC 6C.1.365.01 Left Spoiler ! |
| ! ! 6C.2.365.10# ! |
| ! ! 6C.1.375.01 Right Spoiler ! |
| ! ! 6C.2.375.10# ! |
| ! ! ! |
| ! ! Remark: Report line 'X4' indicates RSP5 left ! |
| ! ! spoiler. ! |
| ! ! Report line 'X5' indicates RSP5 right ! |
| ! ! spoiler. ! |
| !--------------!------------------------------------------------------! |
| ! FLAP ! FLAP Actual Position ! |
| ! X999 ! ! |
| ! ! Format: Negative values are indicated by '-' on ! |
| ! ! the first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-9.0 to 40.0 deg) ! |
| ! ! ! |
| ! ! Source: SFCC 1B.1.137.01 FLAP System 1 ! |
| ! ! 1B.2.137.10 FLAP System 2 ! |
| ! ! ! |
| ! ! Remark: Report line 'X4' indicates FLAP left ! |
| ! ! spoiler. ! |
| ! ! Report line 'X5' indicates FLAP right ! |
| ! ! spoiler. ! |
| !--------------!------------------------------------------------------! |
| ! SLAT ! SLAT Actual Position ! |
| ! X999 ! ! |
| ! ! Format: Negative values are indicated by '-' on ! |
| ! ! the first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (0.0 to 27.0 deg) ! |
| ! ! ! |
| ! ! Source: SFCC 1B.1.127.01 SLAT System 1 ! |
| ! ! 1B.2.127.10 SLAT System 2 ! |
| ! ! ! |
| ! ! Remark: Report line 'X4' indicates SLAT System 1. ! |
| ! ! Report line 'X5' indicates SLAT System 2. ! |
| !--------------!------------------------------------------------------! |
| ! THDG ! True Heading (BCD) ! |
| ! 9999 ! ! |
| ! ! Format: (0 to 359.9 deg) ! |
| ! ! ! |
| ! ! Source: ADIRU 04.1.044.01 THDG System 1 ! |
| ! ! 04.2.044.10 THDG System 2 ! |
| ! ! ! |
| ! ! Remark: Report line 'X6' indicates THDG System 1. ! |
| ! ! Report line 'X7' indicates THDG System 2. ! |
| !--------------!------------------------------------------------------! |
| ! LONP ! Longitude Position ! |
| ! X9999 ! ! |
| ! ! Format: The first position indicates if east or ! |
| ! ! west. E for an East position and W for a ! |
| ! ! West position. ! |
| ! ! (East 179.9 deg to West 179.9 deg) ! |
| ! ! ! |
| ! ! Source: ADIRU 04.1.311.01 LONP System 1 ! |
| ! ! 04.2.311.10 LONP System 2 ! |
| ! ! ! |
| ! ! Remark: Report line 'X6' indicates LONP System 1. ! |
| ! ! Report line 'X7' indicates LONP System 2. ! |
| !--------------!------------------------------------------------------! |
| ! LATP ! Latitude Position ! |
| ! X999 ! ! |
| ! ! Format: The first position indicates if north or ! |
| ! ! south '-' for a North position and S for ! |
| ! ! a South position ! |
| ! ! (North 89.9 deg to South 89.9 deg) ! |
| ! ! ! |
| ! ! Source: ADIRU 04.1.310.XX LATP System 1 ! |
| ! ! 04.2.310.XX LATP System 2 ! |
| ! ! ! |
| ! ! Remark: Report line 'X6' indicates LATP System 1. ! |
| ! ! Report line 'X7' indicates LATP System 2. ! |
| !--------------!------------------------------------------------------! |
| ! WS ! Wind Speed ! |
| ! 999 ! ! |
| ! ! Format: (0 to 100 kts) ! |
| ! ! ! |
| ! ! Source: ADIRU 04.1.315.01 WS System 1 ! |
| ! ! 04.2.315.10 WS System 2 ! |
| ! ! ! |
| ! ! Remark: Report line 'X6' indicates WS System 1. ! |
| ! ! Report line 'X7' indicates WS System 2. ! |
| !--------------!------------------------------------------------------! |
| ! WD ! Wind Direction - True ! |
| ! 999 ! ! |
| ! ! Format: (0 to 359 deg) ! |
| ! ! ! |
| ! ! Source: ADIRU 04.1.316.01 WD System 1 ! |
| ! ! 04.2.316.10 WD System 2 ! |
| ! ! ! |
| ! ! Remark: Report line 'X6' indicates WD System 1. ! |
| ! ! Report line 'X7' indicates WD System 2. ! |
| !--------------!------------------------------------------------------! |
| ! FT ! Wing Fuel Temperature ! |
| ! X999 ! ! |
| ! ! Format: (-60.0 to 170.0 C) ! |
| ! ! ! |
| ! ! Source: FQIC 5A.2.177.10 Fuel Temp. Left Wing Tank ! |
| ! ! 5A.2.201.10 Fuel Temp. Right Wing Tank! |
| ! ! ! |
| ! ! Remark: Report line 'X6' indicates the fuel ! |
| ! ! temperature from the Left Wing Tank. ! |
| ! ! Report line 'X7' indicates the fuel ! |
| ! ! temperature from the Right Wing Tank. ! |
| !--------------!------------------------------------------------------! |
| ! FD ! Fuel Density ! |
| ! 0999 ! ! |
| ! ! Format: (0 to 0.999 kg/l) ! |
| ! ! ! |
| ! ! Source: FQIC 5A.2.272.10 ! |
| ! ! DMU Fuel Density Left Wing Tank ! |
| ! ! Fuel Density Right Wing Tank ! |
| ! ! ! |
| ! ! Remark: The Fuel Density value of the various tanks! |
| ! ! (Left Wing Tank, Center Tank and Right Wing! |
| ! ! Tank) is transmitted one after another on ! |
| ! ! label 272. The adequate tank identification! |
| ! ! as follows: ! |
| ! ! ! |
| ! ! For A318, A319 and A320: ! |
| ! ! Bit 11-14 = 0.0001 ! |
| ! ! Bit 15-18 = 0.001 ! |
| ! ! Bit 19-22 = 0.01 ! |
| ! ! Bit 23-26 = 0.1 ! |
| ! ! Bit 27-29 = Fuel tank Ident (Left/Center/Right) ! |
| ! ! ! |
| ! ! For A321: ! |
| ! ! Bit 11-13 = Fuel tank Ident (Left/Center/Right) ! |
| ! ! Bit 14-17 = 0.0001 ! |
| ! ! Bit 18-21 = 0.001 ! |
| ! ! Bit 22-25 = 0.01 ! |
| ! ! Bit 26-29 = 0.1 ! |
| ! ! ! |
| ! ! The update rate of label 272 is 1 second. Due to ! |
| ! ! this fact the Fuel Density value of the dedicated ! |
| ! ! tank is available every 3 seconds. ! |
| +---------------------------------------------------------------------+ |
(6) Cruise Performance Report Data Field Description <02> (Engine Type CFMI with Advanced EVMU)
NOTE: Reports that are transmitted from the ACARS system do not have report lines without a line identifier.
NOTE: Only the parts of the CRUISE PERFORMANCE REPORT <02> which are not included in the ENGINE CRUISE REPORT <01> are given in the subsequent table.
| +---------------------------------------------------------------------+ |
| ! Value ! Content Description ! |
| !--------------!------------------------------------------------------! |
| ! TAT/ALT/CAS/! In report line CE is printed the average value for ! |
| ! MN/GW/CG ! F02*20 sec. of System 1 parameters. ! |
| ! ! ! |
| ! ! In report line CE is printed the average value for ! |
| ! ! F02*20 sec. of System 1 parameters. ! |
| !--------------!------------------------------------------------------! |
| ! QA ! Aircraft Quality Number, Report-Stability ! |
| ! 99 ! ! |
| ! ! Format: (00 to 99) ! |
| ! ! ! |
| ! ! Source: DMU ! |
| ! ! ! |
| ! ! Remark: 00 = best stable frame ! |
| ! ! 99 = worst stable frame ! |
| ! ! ! |
| ! ! i=1 VARa(i) ! |
| ! ! QA= SIGMA(Wa(i)*---------------) ! |
| ! ! N TOLa(i)*TOLa(i) ! |
| ! ! ! |
| ! !QA= Quality Number ! |
| ! !Wa(i)= Individual weighting factors for the individual! |
| ! ! quality parameters for the Cruise Report. ! |
| ! !VARa(i)= Parameter variances ! |
| ! !TOLa(i)= Variation values for the individual quality ! |
| ! ! parameters for the Cruise Performance Report.! |
| !--------------!------------------------------------------------------! |
| ! QE ! Engine Quality Number, Report-Stability ! |
| ! 99 ! ! |
| ! ! Format: (00 to 99) ! |
| ! ! ! |
| ! ! Source: DMU ! |
| ! ! ! |
| ! ! Remark: QE has no effect to the trigger logic. ! |
| ! ! 99 = worst stable frame, 00 = best stable ! |
| ! ! frame. The quality number is represented ! |
| ! ! in the same mathematical form as QA. ! |
| !--------------!------------------------------------------------------! |
| ! WFQ ! Fuel Quantity Inner Cell ! |
| ! 9999 ! ! |
| ! ! Format: (0 to 99999 kg) ! |
| ! ! ! |
| ! ! Source: FQIC 5A.2.257.10 Left Inner Cell Fuel ! |
| ! ! Quantity ! |
| ! ! 5A.2.261.10 Right Inner Cell Fuel ! |
| ! ! Quantity ! |
| ! ! ! |
| ! ! Remark: Report line 'X1' shows Left Inner Cell ! |
| ! ! Fuel Quantity. ! |
| ! ! Report line 'X2' shows Right Inner Cell ! |
| ! ! Fuel Quantity. ! |
| !--------------!------------------------------------------------------! |
| ! ELEV ! Elevator Position ! |
| ! X999 ! ! |
| ! ! Format: Negative values are shown with 'N' on the ! |
| ! ! first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-30 to 15 deg) ! |
| ! ! ! |
| ! ! Source: FCDC 6C.1.314.01 Left Elevator Position ! |
| ! ! 6C.2.314.10# ! |
| ! ! 6C.1.334.01 Right Elevator Position ! |
| ! ! 6C.2.334.10# ! |
| ! ! ! |
| ! ! Remark: Report line 'X1' shows the Left Elevator ! |
| ! ! Position. ! |
| ! ! Report line 'X2' shows the Right Elevator ! |
| ! ! Position. ! |
| !--------------!------------------------------------------------------! |
| ! AOA ! Corrected Angle of Attack ! |
| ! X999 ! ! |
| ! ! Format: Negative values are shown with 'N' on the ! |
| ! ! first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-30.0 to 85.0 deg) ! |
| ! ! ! |
| ! ! Source: ADIRU 06.1.241.01 AOA System 1 ! |
| ! ! 06.2.241.10 AOA System 2 ! |
| ! ! ! |
| ! ! Remark: Report line 'X1' shows AOA System 1. ! |
| ! ! Report line 'X2' shows AOA System 2. ! |
| !--------------!------------------------------------------------------! |
| ! SLP ! Side Slip Angle ! |
| ! X999 ! ! |
| ! ! Format: Negative values are shown with 'N' on the ! |
| ! ! first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-32.0 to 32.0 deg) ! |
| ! ! ! |
| ! ! Source: FAC 0A.1.226.00 SLP System 1 ! |
| ! ! 0A.2.226.00 SLP System 2 ! |
| ! ! ! |
| ! ! Remark: Report line 'X1' shows SLP System 1. ! |
| ! ! Report line 'X2' shows SLP System 2. ! |
| !--------------!------------------------------------------------------! |
| ! CFPG ! Calculated Flight Path Acceleration ! |
| ! X9999 ! ! |
| ! ! Format: Negative values are shown with 'N' on the ! |
| ! ! first position. Otherwise the first ! |
| ! ! position is used for the value. ! |
| ! ! (-0.9999 to 4.0000 g) ! |
| ! ! ! |
| ! ! Source: DMU CFPG calculated value based on GS from! |
| ! ! System 1 ! |
| ! ! CFPG calculated value based on GS from! |
| ! ! System 2 ! |
| ! ! ! |
| ! ! GSAV last subperiod-GSAV 1st subperiod ! |
| ! ! CFPG=----------------------------------------------*! |
| ! ! Duration of subperiod*(Number of Subperiods-1) ! |
| ! ! ! |
| ! ! *0.05249 ! |
| ! ! ! |
| ! ! GSAV=Average of Ground Speed (GS) per subperiod ! |
| ! ! (label 04.1.312.01 and 04.2.312.10) ! |
| ! ! ! |
| ! ! Remark: Report line 'X1' indicates CFPG calculated ! |
| ! ! with GS from ADIRU System 1. ! |
| ! ! Report line 'X2' indicates CFPG calculated ! |
| ! ! with GS from ADIRU System 2. ! |
| !--------------!------------------------------------------------------! |
| ! CIVV ! Calculated Inertial Vertical Speed ! |
| ! X9999 ! ! |
| ! ! Format: Negative values are shown with 'N' on the ! |
| ! ! first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-999 to 999 ft/min) ! |
| ! ! ! |
| ! ! Source: DMU CIVV calculated value based on IALT ! |
| ! ! from system 1. ! |
| ! ! CIVV calculated value based on IALT ! |
| ! ! from system 2. ! |
| ! ! ! |
| ! ! IALTAV last subperiod-IALTAV 1st subperiod ! |
| ! ! CIVV=----------------------------------------------*! |
| ! ! Duration of subperiod*(Number of Subperiods-1) ! |
| ! ! ! |
| ! ! *60 ! |
| ! ! ! |
| ! ! IALTAV=Average of Inertial Altitude (IALT) per ! |
| ! ! subperiod (label 04.1.361.XX and ! |
| ! ! 04.2.361.XX) ! |
| ! ! ! |
| ! ! Remark: Report line 'X1' indicates CIVV calculated ! |
| ! ! with IALT from ADIRU System 1. ! |
| ! ! Report line 'X2' indicates CIVV calculated ! |
| ! ! with IALT from ADIRU System 2. ! |
| !--------------!------------------------------------------------------! |
| ! RUDD ! Rudder Position ! |
| ! X999 ! ! |
| ! ! Format: Negative values are shown with 'N' on the ! |
| ! ! first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-30.0 to 30.0 deg) ! |
| ! ! ! |
| ! ! Source: SDAC 29.1.312.00 ! |
| ! ! 29.2.312.00# ! |
| !--------------!------------------------------------------------------! |
| ! RUDT ! Rudder Trim Position ! |
| ! X999 ! ! |
| ! ! Format: Negative values are shown with 'N' on the ! |
| ! ! first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-25.0 to 25.0 deg) ! |
| ! ! ! |
| ! ! Source: FAC 0A.1.313.00 ! |
| ! ! 0A.2.313.00# ! |
| !--------------!------------------------------------------------------! |
| ! AILL ! Left Aileron Position ! |
| ! X999 ! ! |
| ! ! Format: Negative values are shown with 'N' on the ! |
| ! ! first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-25.0 to 25.0 deg) ! |
| ! ! ! |
| ! ! Source: FCDC 6C.1.310.01 ! |
| ! ! 6C.2.310.10# ! |
| !--------------!------------------------------------------------------! |
| ! AILR ! Right Aileron Position ! |
| ! X999 ! ! |
| ! ! Format: Negative values are shown with 'N' on the ! |
| ! ! first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-25.0 to 25.0 deg) ! |
| ! ! ! |
| ! ! Source: FCDC 6C.1.330.01 ! |
| ! ! 6C.2.330.10# ! |
| !--------------!------------------------------------------------------! |
| ! STAB ! Stabilizer Position #1 ! |
| ! X999 ! ! |
| ! ! Format: Negative values are shown with 'N' on the ! |
| ! ! first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-13.5 to 4.0 deg) ! |
| ! ! ! |
| ! ! Source: FCDC 6C.1.315.01 ! |
| ! ! 6C.2.315.10# ! |
| !--------------!------------------------------------------------------! |
| ! ROLL ! Roll Angle ! |
| ! X999 ! ! |
| ! ! Format: Negative values are shown with 'N' on the ! |
| ! ! first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-90.0 to 90.0 deg) ! |
| ! ! ! |
| ! ! Source: ADIRU 04.1.325.01 ! |
| ! ! 04.2.325.10# ! |
| !--------------!------------------------------------------------------! |
| ! YAW ! Body Axis Yaw Rate ! |
| ! X999 ! ! |
| ! ! Format: Negative values are shown with 'N' on the ! |
| ! ! first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-45.0 to 45.0 deg) ! |
| ! ! ! |
| ! ! Source: ADIRU 04.1.330.01 ! |
| ! ! 04.2.330.10# ! |
| !--------------!------------------------------------------------------! |
| ! RSP2 ! Roll Spoiler 2 Position ! |
| ! X999 ! ! |
| ! ! Format: Negative values are shown with 'N' on the ! |
| ! ! first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-45.0 to 0 deg) ! |
| ! ! ! |
| ! ! Source: FCDC 6C.1.362.01 Left Spoiler ! |
| ! ! 6C.2.362.10# ! |
| ! ! 6C.1.372.01 Right Spoiler ! |
| ! ! 6C.2.372.10# ! |
| ! ! ! |
| ! ! Remark: Report line 'X4' shows RSP2 left spoiler. ! |
| ! ! Report line 'X5' shows RSP2 right spoiler ! |
| !--------------!------------------------------------------------------! |
| ! RSP3 ! Roll Spoiler 3 Position ! |
| ! X999 ! ! |
| ! ! Format: Negative values are shown with 'N' on the ! |
| ! ! first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-45.0 to 0 deg) ! |
| ! ! ! |
| ! ! Source: FCDC 6C.1.363.01 Left Spoiler ! |
| ! ! 6C.2.363.10# ! |
| ! ! 6C.1.373.01 Right Spoiler ! |
| ! ! 6C.2.373.10# ! |
| ! ! ! |
| ! ! Remark: Report line 'X4' shows RSP3 left spoiler. ! |
| ! ! Report line 'X5' shows RSP3 right spoiler. ! |
| !--------------!------------------------------------------------------! |
| ! RSP4 ! Roll Spoiler 4 Position ! |
| ! X999 ! ! |
| ! ! Format: Negative values are shown with 'N' on the ! |
| ! ! first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-45.0 to 0 deg) ! |
| ! ! ! |
| ! ! Source: FCDC 6C.1.364.01 Left Spoiler ! |
| ! ! 6C.2.364.10# ! |
| ! ! 6C.1.374.01 Right Spoiler ! |
| ! ! 6C.2.374.10# ! |
| ! ! ! |
| ! ! Remark: Report line 'X4' shows RSP4 left spoiler. ! |
| ! ! Report line 'X5' shows RSP4 right spoiler ! |
| !--------------!------------------------------------------------------! |
| ! RSP5 ! Roll Spoiler 5 Position ! |
| ! X999 ! ! |
| ! ! Format: Negative values are shown with 'N' on the ! |
| ! ! first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (-45.0 to 0 deg) ! |
| ! ! ! |
| ! ! Source: FCDC 6C.1.365.01 Left Spoiler ! |
| ! ! 6C.2.365.10# ! |
| ! ! 6C.1.375.01 Right Spoiler ! |
| ! ! 6C.2.375.10# ! |
| ! ! ! |
| ! ! Remark: Report line 'X4' shows RSP5 left spoiler. ! |
| ! ! Report line 'X5' shows RSP5 right spoiler. ! |
| !--------------!------------------------------------------------------! |
| ! FLAP ! FLAP Actual Position ! |
| ! X999 ! ! |
| ! ! Format: Negative values are shown with 'N' on the ! |
| ! ! first position. Otherwise the first ! |
| ! ! position contains a '0'. ! |
| ! ! (0.0 to 40.0 deg) ! |
| ! ! ! |
| ! ! Source: SFCC 1B.1.137.01 FLAP System 1 ! |
| ! ! 1B.2.137.10 FLAP System 2 ! |
| ! ! ! |
| ! ! Remark: Report line 'X4' shows FLAP System 1. ! |
| ! ! Report line 'X5' shows FLAP System 2. ! |
| !--------------!------------------------------------------------------! |
| ! SLAT ! SLAT Actual Position ! |
| ! X999 ! ! |
| ! ! Format: Negative values are shown with 'N' on the ! |
| ! ! first position. Otherwise the first ! |
| ! ! position contains a'0'. ! |
| ! ! (0.0 to 27.0 deg) ! |
| ! ! ! |
| ! ! Source: SFCC 1B.1.127.01 SLAT System 1 ! |
| ! ! 1B.2.127.10 SLAT System 2 ! |
| ! ! ! |
| ! ! Remark: Report line 'X4' shows SLAT System 1. ! |
| ! ! Report line 'X5' shows SLAT System 2. ! |
| !--------------!------------------------------------------------------! |
| ! THDG ! True Heading (BCD) ! |
| ! 9999 ! ! |
| ! ! Format: (0 to 359.9 deg) ! |
| ! ! ! |
| ! ! Source: ADIRU 04.1.044.01 THDG System 1 ! |
| ! ! 04.2.044.10 THDG System 1 ! |
| ! ! ! |
| ! ! Remark: Report line 'X6' shows THDG System 1. ! |
| ! ! Report line 'X7' shows THDG System 2. ! |
| !--------------!------------------------------------------------------! |
| ! LONP ! Longitude Position ! |
| ! X9999 ! ! |
| ! ! Format: The first position shows if east or west. ! |
| ! ! 'E' for an East position and 'W' for a West! |
| ! ! position. ! |
| ! ! (East 179.9 deg to West 179.9 deg) ! |
| ! ! ! |
| ! ! Source: ADIRU 04.1.311.01 LONP System 1 ! |
| ! ! 04.2.311.10 LONP System 2 ! |
| ! ! ! |
| ! ! Remark: Report line 'X6' shows LONP System 1. ! |
| ! ! Report line 'X7' shows LONP System 2. ! |
| !--------------!------------------------------------------------------! |
| ! LATP ! Latitude Position ! |
| ! X999 ! ! |
| ! ! Format: The first position shows if north ! |
| ! ! or south '-' for a North position and 'S' ! |
| ! ! for a South position. ! |
| ! ! (North 89.9 deg to South 89.9 deg) ! |
| ! ! ! |
| ! ! Source: ADIRU 04.1.310.XX LATP System 1 ! |
| ! ! 04.2.310.XX LATP System 2 ! |
| ! ! ! |
| ! ! Remark: Report line 'X6' shows LATP System 1. ! |
| ! ! Report line 'X7' shows LATP System 2. ! |
| !--------------!------------------------------------------------------! |
| ! WS ! Wind Speed ! |
| ! 999 ! ! |
| ! ! Format: (0 to 100 kts) ! |
| ! ! ! |
| ! ! Source: ADIRU 04.1.315.01 WS System 1 ! |
| ! ! 04.2.315.10 WS System 2 ! |
| ! ! ! |
| ! ! Remark: Report line 'X6' shows WS System 1. ! |
| ! ! Report line 'X7' shows WS System 2. ! |
| !--------------!------------------------------------------------------! |
| ! WD ! Wind Direction - True ! |
| ! 999 ! ! |
| ! ! Format: (0 to 359 deg) ! |
| ! ! ! |
| ! ! Source: ADIRU 04.1.316.01 WD System 1 ! |
| ! ! 04.2.316.10 WD System 2 ! |
| ! ! ! |
| ! ! Remark: Report line 'X6' shows WD System 1. ! |
| ! ! Report line 'X7' shows WD System 2. ! |
| !--------------!------------------------------------------------------! |
| ! FT ! Wing Fuel Temperature ! |
| ! X999 ! ! |
| ! ! Format: (-60.0 to 170.0 °) ! |
| ! ! ! |
| ! ! Source: FQIC 5A.2.177.10 Fuel Temp. Left Wing Tank ! |
| ! ! 5A.2.210.10 Fuel Temp. Right Wing Tank! |
| ! ! ! |
| ! ! Remark: Report line 'X6' shows the fuel temperature! |
| ! ! from the Left Wing Tank. ! |
| ! ! Report line 'X7' shows the fuel temperature! |
| ! ! from the Right Wing Tank. ! |
| !--------------!------------------------------------------------------! |
| ! FD ! Fuel Density ! |
| ! 0999 ! ! |
| ! ! Format: (0 to 0.999 kg/l) ! |
| ! ! ! |
| ! ! Source: FQIC 5A.2.272.10 ! |
| ! ! ! |
| ! ! Remark: The Fuel Density value of the various tanks! |
| ! ! (Left Wing Tank, Center Tank and Right Wing! |
| ! ! Tank) is transmitted one after another on ! |
| ! ! label 272. The adequate tank identification! |
| ! ! is as follows: ! |
| ! ! ! |
| ! ! For A318, A319 and A320: ! |
| ! ! Bit 11-14 = 0.0001 ! |
| ! ! Bit 15-18 = 0.001 ! |
| ! ! Bit 19-22 = 0.01 ! |
| ! ! Bit 23-26 = 0.1 ! |
| ! ! Bit 27-29 = Fuel tank Ident (Left/Center/Right) ! |
| ! ! ! |
| ! ! For A321: ! |
| ! ! Bit 11-13 = Fuel tank Ident (Left/Center/Right) ! |
| ! ! Bit 14-17 = 0.0001 ! |
| ! ! Bit 18-21 = 0.001 ! |
| ! ! Bit 22-25 = 0.01 ! |
| ! ! Bit 26-29 = 0.1 ! |
| ! ! ! |
| ! ! The update rate of label 272 is 1 second. Due to ! |
| ! ! this fact the Fuel Density value of the dedicated ! |
| ! ! tank is available every 3 seconds. ! |
| +---------------------------------------------------------------------+ |
(7) Parameter Logic
| +---------------------------------------------------------------------+ |
| ! Param. ! Print Value (Standard Progr.) ! |
| !--------------!------------------------------------------------------! |
| ! TAT ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! ALT ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! CAS ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! MN ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! GW ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! CG ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! ESN ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! EHRS ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! ERT ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! ECYC ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! AP ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! QA ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! QE ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! N1 * ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! N1C ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! N2 ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! EGT ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! FF ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! PS13 ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! P25 ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! T25 ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! P3 ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! T3 ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! T5 ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! VSV ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! VBV ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! HPT ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! LPT ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! GLE ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! PD ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! TN ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! PT2 ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! OIQH ! Value from the Last calculation ! |
| !--------------!------------------------------------------------------! |
| ! VN * ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! VL * ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! PHA * ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! PHT * ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! VCT ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! VH ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! EVM ! Value at the moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! OIP ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! OIT ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! ECW1 ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! SSEL ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! WFQ ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! ELEV ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! AOA ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! SLP ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! CFPG ! Last DMU calculated value ! |
| !--------------!------------------------------------------------------! |
| ! CIVV ! Last DMU calculated value ! |
| !--------------!------------------------------------------------------! |
| ! RUDD ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! RUDT ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! AILL ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! AILR ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! STAB ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! ROLL ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! YAW ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! RSP2 ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! RSP3 ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! RSP4 ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! RSP5 ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! FLAP ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! SLAT ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! THDG ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! LONP ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! LATP ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! WS ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! WD ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! FT ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! FD ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! * Remark: Special logic for print values for the parameters in ! |
| ! report line V3, V4, V5 and V6 refer Report Logic ! |
| ! description item 6 and 7. ! |
| +---------------------------------------------------------------------+ |
(8) Parameter Logic
| +---------------------------------------------------------------------+ |
| ! Param. ! Print Value (Standard Progr.) ! |
| !--------------!------------------------------------------------------! |
| ! TAT ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! ALT ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! CAS ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! MN ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! GW ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! CG ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! ESN ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! EHRS ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! ERT ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! ECYC ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! AP ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! QA ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! QE ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! N1 * ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! N1C ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! N2 ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! EGT ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! FF ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! PS13 ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! P25 ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! T25 ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! P3 ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! T3 ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! T5 ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! VSV ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! VBV ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! HPT ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! LPT ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! GLE ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! PD ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! TN ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! PT2 ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! OIQH ! Value from the Last calculation ! |
| !--------------!------------------------------------------------------! |
| ! VN * ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! VL * ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! PHF * ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! PHT * ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! VC ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! VH ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! EVM ! Value at the moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! OIP ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! OIT ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! ECW1 ! Value at the moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! SSEL ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! WFQ ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! ELEV ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! AOA ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! SLP ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! CFPG ! Last DMU calculated value ! |
| !--------------!------------------------------------------------------! |
| ! CIVV ! Last DMU calculated value ! |
| !--------------!------------------------------------------------------! |
| ! RUDD ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! RUDT ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! AILL ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! AILR ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! STAB ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! ROLL ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! YAW ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! RSP2 ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! RSP3 ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! RSP4 ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! RSP5 ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! FLAP ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! SLAT ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! THDG ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! LONP ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! LATP ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! WS ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! WD ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! FT ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! FD ! Arithmetic average for F02*20 sec ! |
| !--------------!------------------------------------------------------! |
| ! * Remark: Special logic for print values for the parameters in ! |
| ! report line V3, V4, V5 and V6 refer Report Logic ! |
| ! description item 6 and 7. ! |
| +---------------------------------------------------------------------+ |
(9) Cruise Performance Report Logic <02> for CFMI Engine
| +----------------------------------------------------------------------+ |
| !Code!Item ! Description of Item !Progr.!Standard ! |
| ! No !No ! Cruise Performance Report <02> !MCDU !Value or ! |
| ! ! ! for CFMI Engine ! !Table ! |
| !----!------!-----------------------------------------!------!---------! |
| ! !A ! Report Format ! ! ! |
| ! !B ! Parameter Table ! ! ! |
| ! !C ! First three lines of Report ! C ! Blank ! |
| ! !D ! Print-out Rules ! C ! 2 ! |
| ! !E ! Transfer to ACARS MU ! C ! No ! |
| ! !F ! Increment of the report counter if the ! C ! 1 ! |
| ! ! ! report was triggered by a code number ! ! ! |
| ! ! ! > 1000; 1=yes, 0=no ! ! ! |
| ! !G ! Average intervals in seconds ! ! 20 ! |
| ! !H ! Overall average of "F02" averages ! A ! 5 ! |
| ! !I.1 ! OIQ "Y02.3" seconds before flight phase ! A ! 5 ! |
| ! ! ! from 2 to 3 ! ! ! |
| ! !I.2 ! OIQ "Y02.4" seconds after beginning of ! A ! 10 ! |
| ! ! ! flight phase 9 ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !1000!1 ! Manual selection through MCDU ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !2000!2 ! Flight phase dependent manual ! ! ! |
| ! ! ! selection through remote print button ! ! ! |
| ! ! ! if programmed. ! ! ! |
| ! !2.1 ! Logic algorithm ! ! ! |
| ! !2.2 ! Remote Print Button assignment ! C ! not ! |
| ! ! ! ! ! assign. ! |
| !----!------!-----------------------------------------!------!---------! |
| !3000!3 ! Programmable Start Logic ! ! ! |
| ! !3.1 ! Logic algorithm ! C ! ! |
| ! !3.2 ! Trigger condition ! C ! not ! |
| ! ! ! ! ! progr. ! |
| !----!------!-----------------------------------------!------!---------! |
| !4000!4 ! Every "Y02.1" flight legs and every ! ! ! |
| ! ! ! "Y02.5" minutes and extended stable ! ! ! |
| ! ! ! frame criteria is met. Cruise ! ! |
| ! ! ! Performance Report <02> is generated and! ! ! |
| ! ! ! stored in the print report buffer. ! ! ! |
| ! ! ! For "Y02.5" and "Y02.6" the same rules ! ! ! |
| ! ! ! as for Cruise Report <1> (Y01.5 and ! ! ! |
| ! ! ! Y01.6) are valid. The counter "Y02.5" ! ! ! |
| ! ! ! and delay time "Y02.6" is individually ! ! ! |
| ! ! ! programmable for report <01> and <02>. ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! If the number "Y01.5" is set to zero, ! ! ! |
| ! ! ! then only 1 report for each "Y01.1" ! ! ! |
| ! ! ! flight leg is generated. If, for ! ! ! |
| ! ! ! example, "Y02.6" is set to 10, then ! ! ! |
| ! ! ! for every "Y01.1"-flight leg the search ! ! ! |
| ! ! ! and generation logic will start at ! ! ! |
| ! ! ! every 10 minutes after cruise report ! ! ! |
| ! ! ! generation. ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! If, for example, number "Y02.1" is set ! ! ! |
| ! ! ! to 3, then the DMU will search at every ! ! ! |
| ! ! ! 3rd flight leg for stable frame ! ! ! |
| ! ! ! condition. In case that the 3rd flight ! ! ! |
| ! ! ! leg the stable frame criteria are not ! ! ! |
| ! ! ! met, then it is considered the next ! ! ! |
| ! ! ! flight leg with stable frame criteria: ! ! ! |
| ! ! ! for example, the 4th or 5th ("Y02.1"+n ! ! ! |
| ! ! ! for n+1, 2 ... "Y02.1"). ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| ! !4.2 ! Logic algorithm ! ! ! |
| ! !4.3 ! "Y02.1" flight legs ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.4 ! "Y02.5" minutes between cruise report ! C ! limit- ! |
| ! ! ! generation ! ! table ! |
| ! !4.5 ! "Y02.6" Delay time after entry in PH6 ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! ! ! ! ! ! |
| ! ! ! Stable frame basic condition to avoid ! ! ! |
| ! ! ! report triggering in flight phases where! ! ! |
| ! ! ! parameters are of no use. ! ! ! |
| ! ! ! ! ! ! |
| ! !4.6 ! HPTL1 < HPT < HPTL2 ! ! ! |
| ! ! ! HPT 7C.1.306.01 Engine 1 ! ! ! |
| ! ! ! 7C.2.306.10 Engine 2 ! ! ! |
| ! !4.6.1 ! HPTL1 lower limit in % ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.6.2 ! HPTL2 upper limit in % ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.7 ! "P02" stable period ! A ! limit- ! |
| ! ! ! ! ! table ! |
| ! ! ! Stable frame conditions: ! ! ! |
| ! ! ! During "P02" seconds the following ! ! ! |
| ! ! ! parameters are stable as defined below: ! ! ! |
| ! ! ! ! ! ! |
| ! !4.8 ! IALT 04.1.361.-- ft ! A ! limit- ! |
| ! ! ! 04.2.361.-- ! ! table ! |
| ! !W.1 ! WA of IALT ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.9 ! GS 04.1.312.01 kts ! A ! limit- ! |
| ! ! ! 04.2.312.10 ! ! table ! |
| ! !W.2 ! WA of IALT ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.10 ! ROLL ANGLE 04.1.325.01 deg. ! A ! limit- ! |
| ! ! ! 04.2.325.10 ! ! table ! |
| ! !W.3 ! WA of ROLL ANGLE ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.11 ! TAT 06.1.211.01 C ! A ! limit- ! |
| ! ! ! 06.2.211.10 ! ! table ! |
| ! !W.4 ! WA of TAT ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.12 ! N2 7C.1.344.01 Eng.1 % ! A ! limit- ! |
| ! ! ! 7C.2.344.10 Eng.2 ! ! table ! |
| ! !W.5 ! WA of N2 ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.13 ! EGT 7C.1.345.01 Eng.1 C ! A ! limit- ! |
| ! ! ! 7C.2.345.10 Eng 2 ! ! table ! |
| ! !W.6 ! WA of EGT ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.14 ! VACC 04.1.364.01 g ! A ! limit- ! |
| ! ! ! 04.2.364.10 ! ! table ! |
| ! !W.7 ! WA of VACC ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.15 ! MN 06.1.205.01 Mach ! A ! limit- ! |
| ! ! ! 06.2.205.10 ! ! table ! |
| ! !W.8 ! WA of MN ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.16 ! N1 7C.1.346.01 Eng.1 % ! A ! limit- ! |
| ! ! ! 7C.2.346.10 Eng.2 ! ! table ! |
| ! !W.9 ! WA of N1 ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.17 ! PT2 7C.1.131.01 Eng.1 psia ! A ! limit- ! |
| ! ! ! 7C.2.131.10 Eng.2 ! ! table ! |
| ! !W.10 ! WA of PT2 ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.18 ! FF 7C.1.244.01 Eng.1 kg/h ! A ! limit- ! |
| ! ! ! 7C.2.244.10 Eng.2 ! ! table ! |
| ! !W.11 ! WA of FF ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.19 ! HPT 7C.1.306.01 Eng.1 % ! A ! limit- ! |
| ! ! ! 7C.2.306.10 Eng.2 ! ! table ! |
| ! !W.12 ! WA of HPT ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.20 ! LPT 7C.1.307.01 Eng.1 % ! A ! limit- ! |
| ! ! ! 7C.2.307.10 Eng.2 ! ! table ! |
| ! !W.13 ! WA of LPT ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.21 ! RAC 7C.1.055.01 Eng.1 % ! A ! limit- ! |
| ! ! ! 7C.2.055.10 Eng.2 ! ! table ! |
| ! !W.14 ! WA of RAC ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! ! ! HPT, LPT and RAC variation are ! ! ! |
| ! ! ! programmable in the range from ! ! ! |
| ! ! ! 0.0 to 99.9 %. ! ! ! |
| !-----------------------------------------------------!------!---------! |
| ! A = Programmable by Airbus ! |
| ! C = Programmable by Customer ! |
| +----------------------------------------------------------------------+ |
(10) Cruise Performance Report Logic <02> (Engine Type CFMI)
| +----------------------------------------------------------------------+ |
| !Code!Item ! !Progr.!Standard ! |
| ! No.!No. ! Description of Function Item !MCDU !Value or ! |
| ! ! ! !/GSE !Table TXY! |
| !----!------!-----------------------------------------!------!---------! |
| ! !A ! Report Format ! ! ! |
| ! !B ! Parameter Table ! ! ! |
| ! !C ! First three lines of Report ! C ! Blank ! |
| ! !D ! Print-out Rules ! C ! see ! |
| ! ! ! ! ! separate! |
| ! ! ! ! ! list ! |
| ! !E ! Transfer to ACARS MU ! C ! see ! |
| ! ! ! ! ! separate! |
| ! ! ! ! ! list ! |
| ! !F ! Increment of the report counter if the ! C ! 1 ! |
| ! ! ! report was triggered by a code number ! ! ! |
| ! ! ! > 1000; 1=yes, 0=no ! ! ! |
| ! !G ! Average intervals in seconds ! A ! 20 ! |
| ! !H ! Overall average of 'F02' averages ! A ! 5 ! |
| ! !I ! OIQ values taken from 'taxi out' used ! A ! 5 ! |
| ! ! ! for QIQH calculation the same program- ! ! ! |
| ! ! ! ming as for Report <01> shall apply. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !1000!1 ! Manual selection via MCDU ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !2000!2 ! Flight phase dependent manual ! ! ! |
| ! ! ! selection via remote print button ! ! ! |
| ! ! ! if programmed. ! ! ! |
| ! !2.1 ! Remote Print Button assignment. ! C ! not ass.! |
| !----!------!-----------------------------------------!------!---------! |
| !3000!3 ! Programmable Start Logic ! ! ! |
| ! !3.1 ! Trigger condition ! C ! not ass.! |
| !----!------!-----------------------------------------!------!---------! |
| !5000! ! The DMU generates the Cruise Performance! ! ! |
| ! ! ! Report based on 'Flight Hours' or ! ! ! |
| ! ! ! 'Flight Legs' programmable via GSE. ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! Logic based on Flight Hours: ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! During a time frame of 'Y02.1' flight ! ! ! |
| ! ! ! hours the DMU searches in flight phase 6! ! ! |
| ! ! ! for report generation with stable frame ! ! ! |
| ! ! ! criteria where the best aircraft quality! ! ! |
| ! ! ! number QA is calculated. The report with! ! ! |
| ! ! ! the best quality number QA is stored in ! ! ! |
| ! ! ! the report buffer. Flight hours, to ! ! ! |
| ! ! ! trigger on with 'Y02.1', is counted ! ! ! |
| ! ! ! during PH 6. ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! Logic based on Flight Legs: ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! Every 'Y02.2' flight legs the DMU ! ! ! |
| ! ! ! searches in flight phase 6 for report ! ! ! |
| ! ! ! generation with stable frame criteria ! ! ! |
| ! ! ! where the best aircraft quality number ! ! ! |
| ! ! ! QA is calculated. The report with the ! ! ! |
| ! ! ! best quality number QA is stored in the ! ! ! |
| ! ! ! report buffer. ! ! ! |
| ! ! ! ! ! ! |
| ! !5 ! The default programming is 'Flight Legs'! C ! Legs ! |
| !----!------!-----------------------------------------!------!---------! |
| ! !5.1 ! 'Y02.1' flight hours ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.2 ! 'Y02.2' flight legs ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.3 ! 'PO2' stable periods ! A ! limit- ! |
| ! ! ! ! ! table ! |
| ! ! ! Stable frame basic condition in order to! ! ! |
| ! ! ! avoid report triggering in flight phases! ! ! |
| ! ! ! where parameters are of no use. ! ! ! |
| ! !5.4 ! HPTL1 < HPT < HPTL2 ! ! ! |
| ! ! ! param. 7C.1.306.01 Eng.1 ! ! ! |
| ! ! ! param. 7C.2.306.10 Eng.2 ! ! ! |
| ! !5.4.1 ! HPTL1 lower limit in % ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.4.2 ! HPTL2 upper limit in % ! C ! limit- ! |
| ! ! ! Stable frame conditions: ! ! table ! |
| ! ! ! During 'P02' seconds the following ! ! ! |
| ! ! ! parameters are stable as defined below: ! ! ! |
| ! ! ! ! ! ! |
| ! !5.5 ! IALT 04.1.361.-- ft ! A ! limit- ! |
| ! ! ! 04.2.361.-- ! ! table ! |
| ! ! ! ! ! ! |
| ! !5.5.1 ! Wa of IALT ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.6 ! GS 04.1.312.01 kts ! A ! limit- ! |
| ! ! ! 04.2.312.10 ! ! table ! |
| ! ! ! ! ! ! |
| ! !5.6.1 ! Wa of IALT ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.7 ! ROLL 04.1.325.01 degr. ! A ! limit- ! |
| ! ! ! 04.2.325.10 ! ! table ! |
| ! !5.7.1 ! Wa of ROLL ANGLE ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.8 ! TAT 06.1.211.01 deg C ! A ! limit- ! |
| ! ! ! 06.2.211.10 ! ! table ! |
| ! !5.8.1 ! Wa of TAT ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.9 ! N2 7C.1.344.01 Eng.1 % ! A ! limit- ! |
| ! ! ! 7C.2.344.10 Eng.2 ! ! table ! |
| ! !5.9.1 ! Wa of N2 ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.10 ! EGT 7C.1.345.01 Eng.1 deg C ! A ! limit- ! |
| ! ! ! 7C.2.345.10 Eng 2 ! ! table ! |
| ! !5.10.1! Wa of EGT ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.11 ! VACC 04.1.364.01 g ! A ! limit- ! |
| ! ! ! 04.2.364.10 ! ! table ! |
| ! !5.11.1! Wa of VACC ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.12 ! MN 06.1.205.01 Mach ! A ! limit- ! |
| ! ! ! 06.2.205.10 ! ! table ! |
| ! !5.12.1! Wa of MN ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.13 ! N1 7C.1.346.01 Eng.1 % ! A ! limit- ! |
| ! ! ! 7C.2.346.10 Eng.2 ! ! table ! |
| ! !5.13.1! Wa of N1 ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.14 ! PT2 7C.1.131.01 Eng.1 psia ! A ! limit- ! |
| ! ! ! 7C.2.131.10 Eng.2 ! ! table ! |
| ! !5.14.1! Wa of PT2 ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.15 ! FF 7C.1.244.01 Eng.1 kg/h ! A ! limit- ! |
| ! ! ! 7C.2.244.10 Eng.2 ! ! table ! |
| ! !5.15.1! Wa of FF ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.16 ! HPT 7C.1.306.01 Eng.1 % ! A ! limit- ! |
| ! ! ! 7C.2.306.10 Eng.2 ! ! table ! |
| ! !5.16.1! Wa of HPT ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.17 ! LPT 7C.1.307.01 Eng.1 % ! A ! limit- ! |
| ! ! ! 7C.2.307.10 Eng.2 ! ! table ! |
| ! !5.17.1! Wa of LPT ! C ! limit- ! |
| ! ! ! HPT and LPT variation are programmable ! ! table ! |
| ! ! ! in the range from 0.0 to 99.9 %. ! ! ! |
| ! ! ! ! ! ! |
| ! !6 ! The parameters VN, VL, PHA, PHT and N1 ! ! ! |
| ! ! ! in line V3 and V4 shall be from the ! ! ! |
| ! ! ! last stable descent. It means the a.m. ! ! ! |
| ! ! ! parameters shall be computed during ! ! ! |
| ! ! ! descent (PH 7.1) when N1 is with in N1 ! ! ! |
| ! ! ! target 'N1T.1' +/- a tolerance band of ! ! ! |
| ! ! ! 'X1.1' %rpm. These stable conditions ! ! ! |
| ! ! ! shall be kept for a time period of ! ! ! |
| ! ! ! 'T1.1' seconds. The vibration parameters! ! ! |
| ! ! ! shall be veraged about the 'T1.1' ! ! ! |
| ! ! ! observing time period and stored in the ! ! ! |
| ! ! ! DMU until the next stable descent is ! ! ! |
| ! ! ! detected. In case of report generation ! ! ! |
| ! ! ! the last stored value shall be printed. ! ! ! |
| ! ! 6.1 ! 'N1T.1' %rpm stable N1 value for descent! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! ! 6.2 ! 'X1.1' %rpm tolerance band for descent ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! ! 6.3 ! 'T1.1' seconds stable observing time for! C ! limit- ! |
| ! ! ! descent (max. 20 sec) ! ! table ! |
| !----!------!-----------------------------------------!------!---------! |
| ! ! 7 ! The parameter VN, VL, PHA, PHT and N1 in! ! ! |
| ! ! ! report line V and V6 shall be from the ! ! ! |
| ! ! ! last stable take off. It means the a.m. ! ! ! |
| ! ! ! parameters shall be computed during ! ! ! |
| ! ! ! climb (Ph 5.1) when N1 is with in N1 ! ! ! |
| ! ! ! target 'N1T.2' +/- a tolerance band of ! ! ! |
| ! ! ! shall be kept for a time period of ! ! ! |
| ! ! ! 'T1.2' observing time period and stored ! ! ! |
| ! ! ! in the DMU until the next stable take ! ! ! |
| ! ! ! off is detected. In case of report ! ! ! |
| ! ! ! generation the last stored value shall ! ! ! |
| ! ! ! be printed. ! ! ! |
| ! ! 7.1 ! 'N1T.2' %rpm stable N1 value for climb ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! ! 7.2 ! 'X1.2' %rpm tolerance band for climb ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! ! 7.3 ! 'T1.2' seconds stable observing time for! C ! limit- ! |
| ! ! ! climb (max. 20 sec). ! ! table ! |
| !----!------!-----------------------------------------!------!---------! |
| !8100!8.1 ! ACARS MU uplink request with IMI 'REQ02'! ! ! |
| ! ! ! The report <02> is immediately generated! ! ! |
| ! ! ! and transmitted to the ACARS MU. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !8200!8.2 ! ACARS MU uplink request with INI 'G02' ! ! ! |
| ! ! ! The report <02> is generated as soon as ! ! ! |
| ! ! ! stable frame criteria are met, i.e. the ! ! ! |
| ! ! ! DMU immediately starts searching for ! ! ! |
| ! ! ! stable frame ! ! ! |
| ! ! ! ! ! ! |
| !----------------------------------------------------------------------! |
| ! A = Programmable by Airbus ! |
| ! C = Programmable by Customer ! |
| +----------------------------------------------------------------------+ |
(11) Cruise Performance Report Logic <02> (Engine Type CFMI)
| +----------------------------------------------------------------------+ |
| !Code!Item ! !Progr.!Standard ! |
| ! No.!No. ! Description of Function Item !------!Value or ! |
| ! ! ! !MCDU/ !Table TXY! |
| ! ! ! !GSE ! ! |
| !----!------!-----------------------------------------!------!---------! |
| ! !A ! Report Format ! ! ! |
| ! !A.1 ! "R002RLID" Report Layout Identifier ! ! 01 ! |
| ! ! ! (for ACARS header) ! ! ! |
| ! !A.2 ! "R002RLIS" Report Layout Issue ! ! 01 ! |
| ! ! ! (for ACARS header) ! ! ! |
| ! !B ! Parameter Table ! ! ! |
| ! !C ! First three lines of Report ! C ! Blank ! |
| ! !D ! Print Out Rules ! C ! see ! |
| ! ! ! ! ! separate! |
| ! ! ! ! ! list ! |
| ! !E ! Transfer to ACARS MU ! C ! see ! |
| ! ! ! ! ! separate! |
| ! ! ! ! ! list ! |
| ! !F ! Increment of the report counter if the ! C ! 1 ! |
| ! ! ! report was triggered by a code number ! ! ! |
| ! ! ! > 1000; 1=yes, 0=no ! ! ! |
| ! !G ! Average intervals in seconds ! A ! 20 ! |
| ! !H ! Overall average of "F02" averages ! A ! 5 ! |
| ! !I ! OIQ values taken from "taxi out" used ! A ! 5 ! |
| ! ! ! for QIQH calculation the same program- ! ! ! |
| ! ! ! ming as for Report <01> is applied. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !1000!1 ! Manual selection through MCDU ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !2000!2 ! Flight phase dependent manual ! ! ! |
| ! ! ! selection through remote print button ! ! ! |
| ! ! ! if programmed. ! ! ! |
| ! !2.1 ! Remote Print Button assignment. ! C ! not ass.! |
| !----!------!-----------------------------------------!------!---------! |
| !3000!3 ! Programmable Start Logic ! ! ! |
| ! !3.1 ! Trigger condition ! C !not prog.! |
| !----!------!-----------------------------------------!------!---------! |
| !5000! ! The DMU generates the Cruise Performance! ! ! |
| ! ! ! Report based on "Flight Hours" or ! ! ! |
| ! ! ! "Flight Legs" programmable through GSE. ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! Logic based on Flight Hours: ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! During a time frame of "Y02.1" flight ! ! ! |
| ! ! ! hours the DMU searches in flight phase 6! ! ! |
| ! ! ! for report generation with stable frame ! ! ! |
| ! ! ! criteria. ! ! ! |
| ! ! ! The report with the best quality ! ! ! |
| ! ! ! number QA is stored in the report buffer! ! ! |
| ! ! ! ! ! ! |
| ! ! ! Logic based on Flight Legs: ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! Every "Y02.2" flight legs the DMU ! ! ! |
| ! ! ! searches in flight phase 6 for report ! ! ! |
| ! ! ! generation with stable frame criteria ! ! ! |
| ! ! ! where the best aircraft quality number ! ! ! |
| ! ! ! QA is calculated. The report with the ! ! ! |
| ! ! ! best quality number QA is stored in the ! ! ! |
| ! ! ! report buffer. ! ! ! |
| ! ! ! ! ! ! |
| ! !5 ! The default programming is "Flight Legs"! C ! Legs ! |
| !----!------!-----------------------------------------!------!---------! |
| ! !5.1 ! "Y02.1" flight hours ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.2 ! "Y02.2" flight legs ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.3 ! "P02" stable periods ! A ! limit- ! |
| ! ! ! (5 subperiods = 100 sec) ! ! table ! |
| ! ! ! Stable frame basic condition in order to! ! ! |
| ! ! ! avoid report triggering in flight phases! ! ! |
| ! ! ! where parameters are of no use. ! ! ! |
| ! !5.4 ! HPTL1 < HPT < HPTL2 ! ! ! |
| ! ! ! param. 7C.1.306.01 Engine 1 ! ! ! |
| ! ! ! param. 7C.2.306.10 Engine 2 ! ! ! |
| ! !5.4.1 ! HPTL1 lower limit in % ! A ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.4.2 ! HPTL2 upper limit in % ! A ! limit- ! |
| ! ! ! ! ! table ! |
| ! ! ! Stable frame conditions: ! ! ! |
| ! ! ! During "P02" seconds the following ! ! ! |
| ! ! ! parameters are stable as defined below: ! ! ! |
| ! ! ! ! ! ! |
| ! !5.5 ! IALT 04.1.361.-- ft ! A ! limit- ! |
| ! ! ! 04.2.361.--# ! ! table ! |
| ! ! ! ! ! ! |
| ! !5.5.1 ! Wa of IALT ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.6 ! GS 04.1.312.01 kts ! A ! limit- ! |
| ! ! ! 04.2.312.10# ! ! table ! |
| ! ! ! ! ! ! |
| ! !5.6.1 ! Wa of GS ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.7 ! ROLL 04.1.325.01 degr. ! A ! limit- ! |
| ! ! ! 04.2.325.10# ! ! table ! |
| ! !5.7.1 ! Wa of ROLL ANGLE ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.8 ! TAT 06.1.211.01 Degrees C ! A ! limit- ! |
| ! ! ! 06.2.211.10# ! ! table ! |
| ! !5.8.1 ! Wa of TAT ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.9 ! N2 7C.1.344.01 Eng.1 % ! A ! limit- ! |
| ! ! ! 7C.2.344.10 Eng.2 ! ! table ! |
| ! !5.9.1 ! Wa of N2 ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.10 ! EGT 7C.1.345.01 Eng.1 ! A ! limit- ! |
| ! ! ! Degrees C ! ! table ! |
| ! ! ! 7C.2.345.10 Eng 2 ! ! ! |
| ! !5.10.1! Wa of EGT ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.11 ! VACC 04.1.364.01 g ! A ! limit- ! |
| ! ! ! 04.2.364.10# ! ! table ! |
| ! !5.11.1! Wa of VACC ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.12 ! MN 06.1.205.01 Mach ! A ! limit- ! |
| ! ! ! 06.2.205.10# ! ! table ! |
| ! !5.12.1! Wa of MN ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.13 ! N1 7C.1.346.01 Eng.1 % ! A ! limit- ! |
| ! ! ! 7C.2.346.10 Eng.2 ! ! table ! |
| ! !5.13.1! Wa of N1 ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.14 ! PT2 7C.1.131.01 Eng.1 psia ! A ! limit- ! |
| ! ! ! 7C.2.131.10 Eng.2 ! ! table ! |
| ! !5.14.1! Wa of PT2 ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.15 ! FF 7C.1.244.01 Eng.1 kg/h ! A ! limit- ! |
| ! ! ! 7C.2.244.10 Eng.2 ! ! table ! |
| ! !5.15.1! Wa of FF ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.16 ! HPT 7C.1.306.01 Eng.1 % ! A ! limit- ! |
| ! ! ! 7C.2.306.10 Eng.2 ! ! table ! |
| ! !5.16.1! Wa of HPT ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.17 ! LPT 7C.1.307.01 Eng.1 % ! A ! limit- ! |
| ! ! ! 7C.2.307.10 Eng.2 ! ! table ! |
| ! !5.17.1! Wa of LPT ! C ! limit- ! |
| ! ! ! HPT and LPT variation are programmable ! ! table ! |
| ! ! ! in the range from 0.0 to 99.9 %. ! ! ! |
| ! ! ! ! ! ! |
| ! !6 ! The parameters VN, VL, PHA and N1 in ! ! ! |
| ! ! ! line V3 and V4 is from the last stable ! ! ! |
| ! ! ! descent. It means the a.m. parameters ! ! ! |
| ! ! ! are computed during descent (PH 7.1) ! ! ! |
| ! ! ! when N1 is with in N1 target "N1T.1" ! ! ! |
| ! ! ! +/- a tolerance band of "X1.1" %rpm. ! ! ! |
| ! ! ! These stable conditions are kept for a ! ! ! |
| ! ! ! time period of "T1.1" seconds. The vi- ! ! ! |
| ! ! ! bration parameters are averaged about ! ! ! |
| ! ! ! the "T1.1" observing time period and ! ! ! |
| ! ! ! stored in the DMU until the next stable ! ! ! |
| ! ! ! descent is detected. In case of report ! ! ! |
| ! ! ! generation the last stored value is ! ! ! |
| ! ! ! printed. ! ! ! |
| ! ! 6.1 ! "N1T.2" %rpm stable N1 value for descent! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! ! 6.2 ! "X1.1" %rpm tolerance band for descent ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! ! 6.3 ! "T1.1" seconds stable observing time for! C ! limit- ! |
| ! ! ! descent (max. 20 sec) ! ! table ! |
| !----!------!-----------------------------------------!------!---------! |
| ! ! 7 ! The parameter VN, VL, PHA, PHT and N1 in! ! ! |
| ! ! ! report line V and V6 are from the last ! ! ! |
| ! ! ! stable take off. It means the a.m. pa- ! ! ! |
| ! ! ! rameters are computed during climb ! ! ! |
| ! ! ! (Ph 5.1) when N1 is with in N1 target ! ! ! |
| ! ! ! "N1T.2" +/- a tolerance band of "X1.2" ! ! ! |
| ! ! ! %rpm. This stable conditions are kept ! ! ! |
| ! ! ! for a time period of "T1.2" seconds ! ! ! |
| ! ! ! observing time period and stored in the ! ! ! |
| ! ! ! DMU until the next stable take off is ! ! ! |
| ! ! ! detected. In case of report generation ! ! ! |
| ! ! ! the last stored value is printed. ! ! ! |
| ! ! 7.1 ! "N1T.2" %rpm stable N1 value for climb ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! ! 7.2 ! "X1.2" %rpm tolerance band for climb ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! ! 7.3 ! "T1.2" seconds stable observing time for! C ! limit- ! |
| ! ! ! climb (max. 20 sec). ! ! table ! |
| !----!------!-----------------------------------------!------!---------! |
| !8100!8.1 ! ACARS MU uplink request with IMI "REQ02"! ! ! |
| ! ! ! The report <02> is immediately generated! ! ! |
| ! ! ! and transmitted to the ACARS MU. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !8200!8.2 ! ACARS MU uplink request with INI "G02" ! ! ! |
| ! ! ! The report <02> is generated as soon as ! ! ! |
| ! ! ! stable frame criteria are met, i.e. the ! ! ! |
| ! ! ! DMU immediately starts searching for ! ! ! |
| ! ! ! stable frame ! ! ! |
| ! ! ! ! ! ! |
| !----------------------------------------------------------------------! |
| ! A = Programmable by Airbus ! |
| ! C = Programmable by Customer ! |
| +----------------------------------------------------------------------+ |
D. AIDS Reports Print Rules - Default Values for Report <02>
| +------------------------------------------------+ |
| ! ! ! ! |
| ! Code ! Printer Output ! ACARS-output ! |
| ! ! ! ! |
| !-------!-----------------------!----------------! |
| ! ! ! ! |
| ! 1000 ! Print immediatly ! No ACARS ! |
| ! ! ! ! |
| !-------!-----------------------!----------------! |
| ! ! ! ! |
| ! 2000 ! Print immediatly ! No ACARS ! |
| ! ! ! ! |
| !-------!-----------------------!----------------! |
| ! ! ! ! |
| ! 5000 ! Print at landing ! ACARS VHF ! |
| ! ! ! ! |
| !-------!-----------------------!----------------! |
| ! ! ! ! |
| ! 8100 ! No print ! ACARS VHF ! |
| ! ! ! ! |
| !-------!-----------------------!----------------! |
| ! ! ! ! |
| ! 8200 ! Print at landing ! ACARS VHF ! |
| ! ! ! ! |
| +------------------------------------------------+ |
| +-------------------------------------------------------------------------+ |
| !Trigger! to ACARS ! to printer ! store ! |
| ! Code !------------------------------ -!-----------------!--------------! |
| ! No !Ground ! VHF ! SAT- ! HF ! at ! imme- ! internal& ! |
| ! ! ! ! COM ! !landing ! diate ! external ! |
| ! ! ! ! ! ! ! !(build in RAM&! |
| ! ! ! ! ! ! ! ! PCMCIA) ! |
| !-------!-------!--------!-------!-------!--------!--------!--------------! |
| ! ! ! If ! ! ! ! If !PCMCIA only if! |
| ! 1000 ! NO ! 'SEND' ! NO ! NO ! !'PRINT' ! 'STORE' ! |
| ! ! !selected! ! ! !selected! selected on ! |
| ! ! !on MCDU ! ! ! !on MCDU ! MCDU ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 2000 ! NO ! NO ! NO ! NO ! ! YES ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 3000 ! NO ! NO ! NO ! NO ! ! NO ! YES ! |
| !-------!-------!--------!-------!-------! N !--------!--------------! |
| ! 5000 ! NO ! YES ! NO ! NO ! O ! NO ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 8100 ! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 8200 ! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| +-------------------------------------------------------------------------+ |
| +-------------------------------------------------------------------------+ |
| !Trigger! to ACARS ! to printer ! store ! |
| ! Code !------------------------------ -!-----------------!--------------! |
| ! No !Ground ! VHF ! SAT- ! HF ! at ! imme- ! internal& ! |
| ! ! ! ! COM ! !landing ! diate ! external ! |
| ! ! ! ! ! ! ! !(build in RAM&! |
| ! ! ! ! ! ! ! ! PCMCIA) ! |
| !-------!-------!--------!-------!-------!--------!--------!--------------! |
| ! 1000 ! NO ! NO ! NO ! NO ! NO ! YES ! YES ! |
| !-------!-------!--------!-------!-------!--------!--------!--------------! |
| ! 2000 ! NO ! NO ! NO ! NO ! NO ! YES ! YES ! |
| !-------!-------!--------!-------!-------!--------!--------!--------------! |
| ! 3000 ! NO ! NO ! NO ! NO ! NO ! NO ! YES ! |
| !-------!-------!--------!-------!-------!--------!--------!--------------! |
| ! 5000 ! NO ! YES ! NO ! NO ! NO ! NO ! YES ! |
| !-------!-------!--------!-------!-------!--------!--------!--------------! |
| ! 8100 ! NO ! YES ! NO ! NO ! NO ! NO ! YES ! |
| !-------!-------!--------!-------!-------!--------!--------!--------------! |
| ! 8200 ! NO ! YES ! NO ! NO ! NO ! NO ! YES ! |
| +-------------------------------------------------------------------------+ |
E. Engine Take-Off Report <04>
Engine Take-Off Report <04> (Engine Type CFMI with Advanced EVMU)
Engine Take-Off Report <04> (Engine Type CFMI with Advanced EVMU)
Engine Take-Off Report <04> (Engine Type CFMI with Advanced EVMU) ** ON A/C NOT FOR ALL
Engine Take-Off Report <04> (Engine Type CFMI with Advanced EVMU) ** ON A/C NOT FOR ALL
The Engine Take-Off Report is an average data collection of aircraft and engine around the point of peak N1 while in take-off flight phase.
The engine take-off report, is generated when one of the logic conditions 1000 to 5009 (for details see engine take-off report logic) is present.
Each Take-Off Report is contain a T/O delta N1 respective EPR summary.
Engine Take-Off Report <04> (Engine Type CFMI with Advanced EVMU) Engine Take-Off Report <04> (Engine Type CFMI with Advanced EVMU) Engine Take-Off Report <04> (Engine Type CFMI with Advanced EVMU) ** ON A/C NOT FOR ALL Engine Take-Off Report <04> (Engine Type CFMI with Advanced EVMU) ** ON A/C NOT FOR ALL The engine take-off report, is generated when one of the logic conditions 1000 to 5009 (for details see engine take-off report logic) is present.
Each Take-Off Report is contain a T/O delta N1 respective EPR summary.
NOTE: For the standard header definition of the report refer to (Ref. AMM D/O 31-36-00-00).
(1) Engine Take-Off Report Data Field Description <04> (Engine Type CFMI with Advanced EVMU)
NOTE: Reports that are transmitted from the ACARS system do not have report lines without a line identifier.
| +---------------------------------------------------------------------+ |
| ! Value ! Content Description ! |
| !--------------+------------------------------------------------------! |
| ! ESN ! Engine Serial Number ! |
| ! 999999 ! (000000 to 999999) ! |
| ! ! Eng 1 param. 7C.1.046.01 digit 3, 2, 1 ! |
| ! ! 7C.1.047.01 digit 6, 5, 4 ! |
| ! ! Eng 2 param. 7C.2.046.01 digit 3, 2, 1 ! |
| ! ! 7C.2.047.01 digit 6, 5, 4 ! |
| !--------------!------------------------------------------------------! |
| ! EHRS ! Engine Flight Hours ! |
| ! 99999 ! (00000 to 99999 hours) ! |
| ! ! DMU Engine 1 and Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! ERT ! Engine Running Time ! |
| ! 99999 ! (00000 to 65536 hours) ! |
| ! ! Eng 1 param. 7C.1.050.01 ! |
| ! ! Eng 2 param. 7C.2.050.10 ! |
| !--------------!------------------------------------------------------! |
| ! ECYC ! Engine Cycle ! |
| ! 99999 ! (00000 to 99999) ! |
| !--------------!------------------------------------------------------! |
| ! AP ! Auto Pilot Status ! |
| ! 99 ! (00 to G8) ! |
| ! ! FMGC 1 and 2 (FGC part) for Auto Pilot AP1 and AP2 ! |
| ! ! ! |
| ! ! XX Auto Pilot Modes: ! |
| ! ! !! ! |
| ! ! !!__Lateral Modes: 0 = NO MODE ! |
| ! ! ! 1 = HEADING ! |
| ! ! ! 2 = TRACK ! |
| ! ! ! 3 = NAV ! |
| ! ! ! 4 = LOC CAPTURE ! |
| ! ! ! 5 = LOC TRACK ! |
| ! ! ! 6 = LAND TRACK ! |
| ! ! ! 7 = RUNWAY ! |
| ! ! ! 8 = ROLL GO AROUND ! |
| ! ! ! ! |
| ! ! !__Longitudinal Modes: 0 = NO MODE ! |
| ! ! 1 = PITCH G/A ! |
| ! ! 2 = PITCH T/O ! |
| ! ! 3 = G/S TRACK ! |
| ! ! 4 = G/S CAPTURE ! |
| ! ! 5 = V/S ! |
| ! ! 6 = FPA ! |
| ! ! 7 = ALT ! |
| ! ! 8 = ALT ACQ ! |
| ! ! 9 = OPEN CLB ! |
| ! ! A = OPEN DES ! |
| ! ! B = IM CLB ! |
| ! ! C = IM DES ! |
| ! ! D = CLB ! |
| ! ! E = DES ! |
| ! ! F = FINAL DES ! |
| ! ! G = EXPEDITE ! |
| ! ! ! |
| ! ! AP1 ! AP2 ! |
| ! ! Report Line EC: ! Report Line EE: !Difinition: ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! / ! / !No Mode Act. ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.11 = 1 ! 01.2.275.00.11 = 1!RUNWAY Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.12 = 1 ! 01.2.275.00.12 = 1!NAV Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.13 = 1 ! 01.2.275.00.13 = 1!LOC CAPTURE ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.14 = 1 ! 01.2.275.00.14 = 1!LOC TRACK ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.15 = 1 ! 01.2.275.00.15 = 1!Roll GO ! |
| ! ! ! !AROUND Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.16 = 1 ! 01.2.275.00.16 = 1!HEADING Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.17 = 1 ! 01.2.275.00.17 = 1!TRACK Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.15 = 1 ! 01.2.274.00.15 = 1!PITCH TO Mode! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.16 = 1 ! 01.2.274.00.16 = 1!PITCH GA Mode! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.17 = 1 ! 01.2.274.00.17 = 1!V/S Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.18 = 1 ! 01.2.274.00.18 = 1!FPA Mode ! |
| ! ! -------------------!-------------------!-------------! |
| ! ! 01.1.274.00.19 = 1 ! 01.2.274.00.19 = 1!ALT Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.20 = 1 ! 01.2.274.00.20 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.19 = 1 ! 01.2.274.00.19 = 1!ALT ACQ ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.21 = 1 ! 01.2.274.00.21 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.20 = 1 ! 01.2.274.00.20 = 1!G/S TRACK ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.22 = 1 ! 01.2.274.00.22 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.21 = 1 ! 01.2.274.00.21 = 1!G/S CAPTURE ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.22 = 1 ! 01.2.274.00.22 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.23 = 1 ! 01.2.274.00.23 = 1!FINAL DES ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.2.274.00.24 = 1 ! 01.2.274.00.24 = 1!EXPED. Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.146.00.14 = 1 ! 01.2.146.00.14 = 1!LAND TRACK ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!CLB Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.13 = 0 ! 01.2.274.00.13 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.14 = 0 ! 01.2.274.00.14 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.24 = 0 ! 01.2.274.00.24 = 0! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!DES Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.13 = 0 ! 01.2.274.00.13 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.14 = 0 ! 01.2.274.00.14 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.24 = 0 ! 01.2.274.00.24 = 0! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!IM. CLIMB ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.13 = 1 ! 01.2.274.00.13 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!IM. DES Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.13 = 1 ! 01.2.274.00.13 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!OPEN CLB ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.14 = 1 ! 01.2.274.00.14 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!OPEN DES ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.14 = 1 ! 01.2.274.00.14 = 1! ! |
| ! ! ---------------------------------------------------- ! |
| ! ! Auto Pilot Status DMU: ! |
| ! ! AP1 printed in report line EC ! |
| ! ! AP2 printed in report line EE ! |
| !--------------!------------------------------------------------------! |
| ! T/O DELTA N1! Take Off delta N1 Summary of Eng.1 and Eng.2 ! |
| ! SUMMARY ! ! |
| ! ! 1 2 3 4 5 6 7 8 9 ! |
| ! ! ___!____!____!____!____!____!____!____!___ ! |
| ! ! N1 ! 99 ! 99 ! 99 ! 99 ! 99 ! 99 ! 99 ! 99 ! |
| ! ! N1 ! 99 ! 99 ! 99 ! 99 ! 99 ! 99 ! 99 ! 99 ! |
| ! ! ! |
| ! ! 1 N1/N2 = Report Line Identifier ! |
| ! ! 2 99/99 = Number of total Take-Offs since ! |
| ! ! - previous Take-Off report according ! |
| ! ! logic 4000 and 4100 ! |
| ! ! - ESN change ! |
| ! ! 3 99/99 = delta N1 =/< 0.2 % rpm ! |
| ! ! 4 99/99 = delta N1 > 0.2 % and =/< 2.0 % rpm ! |
| ! ! 5 99/99 = delta N1 > 2.0 % and =/< 4.0 % rpm ! |
| ! ! 6 99/99 = delta N1 > 4.0 % and =/< 6.0 % rpm ! |
| ! ! 7 99/99 = delta N1 > 6.0 % and =/< 8.0 % rpm ! |
| ! ! 8 99/99 = delta N1 > 8.0 % and =/< 10.0 % rpm ! |
| ! ! 9 99/99 = delta N1 > 10.0 % rpm ! |
| ! ! Eng.1 param. 7C.1.342.01 for N1MX ECU ! |
| ! ! Eng.2 param. 7C.2.342.10 ! |
| ! ! Eng.1 param. 7C.1.342.01 for N1 ECU ! |
| ! ! Eng.2 param. 7C.2.342.10 ! |
| ! ! delta N1 = N1MX - N1 ! |
| !--------------!------------------------------------------------------! |
| ! EGTM ! MAximum EGT during TAke Off observing time period ! |
| ! X999 ! (-55 to 999.9 C) ! |
| ! ! Eng 1 param. 7C.1.345.01 ! |
| ! ! Eng 2 param. 7C.2.345.10 ! |
| !--------------!------------------------------------------------------! |
| ! N1 ! Selected N1 Actual ! |
| ! 9999 ! (0 to 120.0 %rpm) ! |
| ! ! Eng 1 param. 7C.1.346.01 ! |
| ! ! Eng 2 param. 7C.2.346.10 ! |
| !--------------!------------------------------------------------------! |
| ! N1C ! N1 Command ! |
| ! 9999 ! (0 to 120.0 %rpm) ! |
| ! ! Eng 1 param. 7C.1.341.01 ! |
| ! ! Eng 2 param. 7C.2.341.10 ! |
| !--------------!------------------------------------------------------! |
| ! N2 ! Selected N2 Actual ! |
| ! 9999 ! (0 to 120.0 %rpm) ! |
| ! ! Eng 1 param. 7C.1.344.01 ! |
| ! ! Eng 2 param. 7C.2.344.10 ! |
| !--------------!------------------------------------------------------! |
| ! EGT ! Selected T494 (Exhaust Gas Temperature) ! |
| ! X999 ! (-55 to 999.9 C) ! |
| ! ! Eng 1 param. 7C.1.345.01 ! |
| ! ! Eng 2 param. 7C.2.345.10 ! |
| !--------------!------------------------------------------------------! |
| ! FF ! Engine Fuel Flow ! |
| ! 9999 ! ( 0 to 7000 kg/h) ! |
| ! ! Eng 1 param. 7C.1.244.01 ! |
| ! ! Eng 2 param. 7C.2.244.10 ! |
| !--------------!------------------------------------------------------! |
| ! P3 ! Selected PS3 ! |
| ! 9999 ! (0.0 to 450.0 psia) ! |
| ! ! Eng 1 param. 7C.1.264.01 ! |
| ! ! Eng 2 param. 7C.2.264.10 ! |
| !--------------!------------------------------------------------------! |
| ! N1MX ! N1 Maximum ! |
| ! 9999 ! (0.0 to 108.0 % rpm) ! |
| ! ! Eng 1 param. 7C.1.342.01 ! |
| ! ! Eng 2 param. 7C.2.342.10 ! |
| !--------------!------------------------------------------------------! |
| ! T3 ! Temperature at Position 3 ! |
| ! X999 ! (-55.0 to 850.0 C) ! |
| ! ! Eng 1 param. 7C.1.265.01 ! |
| ! ! Eng 2 param. 7C.2.265.10 ! |
| !--------------!------------------------------------------------------! |
| ! T25 ! Selected T25 ! |
| ! X999 ! (-55.0 to 120.0 C) ! |
| ! ! Eng 1 param. 7C.1.263.01 ! |
| ! ! Eng 2 param. 7C.2.263.10 ! |
| !--------------!------------------------------------------------------! |
| ! T12 ! T12 Fan Inlet Temperature ! |
| ! X99 ! (-55.0 to 85.0 C) ! |
| ! ! Eng 1 param. 7C.1.130.01 ! |
| ! ! Eng 2 param. 7C.2.130.10 ! |
| !--------------!------------------------------------------------------! |
| ! PO ! Selected PO Ambient Pressure ! |
| ! 999 ! (0 to 20.0 psia) ! |
| ! ! Eng 1 param. 7C.1.114.01 ! |
| ! ! Eng 2 param. 7C.2.114.10 ! |
| !--------------!------------------------------------------------------! |
| ! T5 ! Temperature at Position 5 ! |
| ! X999 ! (-55.0 to 850.0 C) ! |
| ! ! Eng 1 param. 7C.1.260.01 ! |
| ! ! Eng 2 param. 7C.2.260.10 ! |
| !--------------!------------------------------------------------------! |
| ! VSV ! Variable Statore Vane Position ! |
| ! X99 ! (-5.0 to 45.0 deg) ! |
| ! ! Eng 1 param. 7C.1.072.01 ! |
| ! ! Eng 2 param. 7C.2.072.10 ! |
| !--------------!------------------------------------------------------! |
| ! VBV ! Variable Bleed Valve Position ! |
| ! X99 ! (-9.9 to 40.0 deg) ! |
| ! ! Eng 1 param. 7C.1.071.01 ! |
| ! ! Eng 2 param. 7C.2.071.10 ! |
| !--------------!------------------------------------------------------! |
| ! VN ! FAN Pick Up N1 Track Vibration ! |
| ! 99 ! (0.0 to 10.0) ! |
| ! ! Eng 1 param. 3D.1.227.01 ! |
| ! ! Eng 2 param. 3D.1.227.10 ! |
| !--------------!------------------------------------------------------! |
| ! VL ! TRF Pick Up N1 Vibration ! |
| ! 99 ! (0.0 to 10.0) ! |
| ! ! Eng 1 param. 3D.1.227.11 ! |
| ! ! Eng 2 param. 3D.1.227.00 ! |
| !--------------!------------------------------------------------------! |
| ! PHA ! FAN Pick Up Phase Angle ! |
| ! 999 ! (0 to 360 deg) ! |
| ! ! Eng 1 param. 3D.1.226.11 ! |
| ! ! Eng 2 param. 3D.1.226.00 ! |
| !--------------!------------------------------------------------------! |
| ! PHT ! TRF Pick Up Phase Angle ! |
| ! 999 ! (0 to 360 deg) ! |
| ! ! Eng 1 param. 3D.1.226.11 ! |
| ! ! Eng 2 param. 3D.1.226.00 ! |
| !--------------!------------------------------------------------------! |
| ! VC ! FAN Pick Up N2 Track Vibration ! |
| ! 99 ! (0.0 to 4.0) ! |
| ! ! Eng 1 param. 3D.1.230.01 ! |
| ! ! Eng 2 param. 3D.1.230.10 ! |
| !--------------!------------------------------------------------------! |
| ! VH ! TRF Pick Up N2 Track Vibration ! |
| ! 99 ! (0.0 to 4.0) ! |
| ! ! Eng 1 param. 3D.1.230.11 ! |
| ! ! Eng 2 param. 3D.1.230.00 ! |
| !--------------!------------------------------------------------------! |
| ! EVM ! Engine Vibration Status Word ! |
| ! XXXXX ! Eng 1 param. 3D.1.035.01 ! |
| ! ! Eng 2 param. 3D.1.035.10 ! |
| ! ! Each 'X' represents 4 Bits in hexadecimal code of ! |
| ! ! a defined ARINC 429 word: ! |
| ! ! XXXXX Bits HEX ! |
| ! ! !!!!!___________ 14, 13, 12, 11 0...F ! |
| ! ! !!!!____________ 18, 17, 16, 15 0...F ! |
| ! ! !!!_____________ 22, 21, 20, 19 0...F ! |
| ! ! !!______________ 26, 25, 24, 23 0...F ! |
| ! ! !_______________ 29, 28, 27 0...7 ! |
| !--------------!------------------------------------------------------! |
| ! OIP ! Engine Oil Pressure ! |
| ! 999 ! (0 to 400 psia) ! |
| ! ! Eng 1 param. 26.1.317.01 ! |
| ! ! 26.2.317.01 ! |
| ! ! Eng 2 param. 26.1.317.10 ! |
| ! ! 26.2.317.10 ! |
| !--------------!------------------------------------------------------! |
| ! OIT ! Engine Oil Temperature ! |
| ! X99 ! (-60 to 250 C) ! |
| ! ! Eng 1 param. 26.1.316.01 ! |
| ! ! 26.2.316.01 ! |
| ! ! Eng 2 param. 26.1.316.10 ! |
| ! ! 26.2.316.10 ! |
| !--------------!------------------------------------------------------! |
| ! O/F ! Oil and Fuel Filter Clogged ! |
| ! 11 ! 1 1 ! |
| ! ! I I________Fuel filter clogged = 0 ! |
| ! ! I Fuel filter not clogged = 1 ! |
| ! ! I___________Oil filter clogged = 0 ! |
| ! ! Oil filter not clogged = 1 ! |
| ! ! Eng 1 param. 29.1.001.01.16 Oil filter ! |
| ! ! 29.2.001.01.16 ! |
| ! ! Eng 2 param. 29.1.001.10.16 Oil filter ! |
| ! ! 29.2.001.10.16 ! |
| ! ! Eng 1 param. 29.1.001.01.17 Fuel filter ! |
| ! ! 29.2.001.01.17 ! |
| ! ! Eng 2 param. 29.1.001.10.17 Fuel filter ! |
| ! ! 29.2.001.10.17 ! |
| !--------------!------------------------------------------------------! |
| ! ECW1 ! Engine Control Word 1 ! |
| ! XXXXX ! Each 'X' represents 4 Bits in hexadecimal code of ! |
| ! ! a defined ARINC 429 word: ! |
| ! ! XXXXX Bits HEX ! |
| ! ! !!!!!___________ 14, 13, 12, 11 0...F ! |
| ! ! !!!!____________ 18, 17, 16, 15 0...F ! |
| ! ! !!!_____________ 22, 21, 20, 19 0...F ! |
| ! ! !!______________ 26, 25, 24, 23 0...F ! |
| ! ! !_______________ 29, 28, 27 0...7 ! |
| ! ! -------------------------------------------- ! |
| ! ! Bit Label Parameter Description ! |
| ! ! 11 7C.X.272.XX.19 = 1 Auto Thrust Active ! |
| ! ! 12 7C.X.272.XX.20 = 1 VSV Position Fault ! |
| ! ! 13 SPARE ! |
| ! ! 14 SPARE ! |
| ! ! 15 7C.X.351.XX.29 = 1 Fuel Flow Measurement ! |
| ! ! Invalid ! |
| ! ! 16 7C.X.275.XX.15 = 1 N1/N2 Control ACtive ! |
| ! ! 17 7C.X.275.XX.26 = 1 Channel A Active ! |
| ! ! 18 7C.X.275.XX.27 = 1 Channel B Active ! |
| ! ! 19 SPARE ! |
| ! ! 20 SPARE ! |
| ! ! 21 SPARE ! |
| ! ! 22 SPARE ! |
| ! ! 23 SPARE ! |
| ! ! 24 SPARE ! |
| ! ! 25 SPARE ! |
| ! ! 26 SPARE ! |
| ! ! 27 SPARE ! |
| ! ! 28 SPARE ! |
| ! ! 29 SPARE ! |
| !--------------!------------------------------------------------------! |
| ! ECW2 ! Engine Control Word 2 ! |
| ! XXXXX ! Each 'X' represents 4 Bits in hexadecimal code of ! |
| ! ! a defined ARINC 429 word: ! |
| ! ! XXXXX Bits HEX ! |
| ! ! !!!!!___________ 14, 13, 12, 11 0...F ! |
| ! ! !!!!____________ 18, 17, 16, 15 0...F ! |
| ! ! !!!_____________ 22, 21, 20, 19 0...F ! |
| ! ! !!______________ 26, 25, 24, 23 0...F ! |
| ! ! !_______________ 29, 28, 27 0...7 ! |
| ! ! -------------------------------------------- ! |
| ! ! Bit Label Parameter Description ! |
| ! ! 11 7C.X.272.XX.12 = 1 Bump/Overboost #1 enable ! |
| ! ! 12 7C.X.272.XX.13 = 1 Bump/Overboost #2 enable ! |
| ! ! 13 7C.X.272.XX.14 = 1 Bump/Overboost #3 enable ! |
| ! ! 14 7C.X.272.XX.22 = 1 MTO. GA limit mode select.! |
| ! ! 15 7C.X.272.XX.23 = 1 Flex Take-Off limit mode ! |
| ! ! selected ! |
| ! ! 16 SPARE ! |
| ! ! 17 SPARE ! |
| ! ! 18 SPARE ! |
| ! ! 19 SPARE ! |
| ! ! 20 SPARE ! |
| ! ! 21 SPARE ! |
| ! ! 22 SPARE ! |
| ! ! 23 SPARE ! |
| ! ! 24 SPARE ! |
| ! ! 25 SPARE ! |
| ! ! 26 SPARE ! |
| ! ! 27 SPARE ! |
| ! ! 28 SPARE ! |
| ! ! 29 SPARE ! |
| !--------------!------------------------------------------------------! |
| ! PSEL ! Status of different FADEC sensors ! |
| ! XXXX ! X X X X Label: Selected: ! |
| ! ! ! ! ! !___ 211 TAT (Bit 11 --> 15) ! |
| ! ! ! ! ! ____ 344 N2 actual (Bit 11 --> 15) ! |
| ! ! ! !_______ 345 EGT (Bit 11 --> 15) ! |
| ! ! !_________ 346 N1 actual (Bit 11 --> 15) ! |
| ! ! ! |
| ! ! Source: ECU, different labels ! |
| ! ! NOTE: The shown values are coded as follows: ! |
| ! ! Bit: 15 14 13 12 11 ! Shown value ! |
| ! ! --------------------!---------------- ! |
| ! ! 0 0 0 0 0 ! 0 ! |
| ! ! 0 0 0 0 1 ! 1 ! |
| ! ! 0 0 0 1 0 ! 2 ! |
| ! ! 0 0 0 1 1 ! 3 ! |
| ! ! 0 0 1 0 0 ! 4 ! |
| ! ! 0 0 1 0 1 ! 5 ! |
| ! ! 0 0 1 1 0 ! 6 ! |
| ! ! 0 0 1 1 1 ! 7 ! |
| ! ! 0 1 0 0 0 ! 8 ! |
| ! ! 0 1 0 0 1 ! 9 ! |
| ! ! 0 1 0 1 0 ! A ! |
| ! ! 0 1 0 1 1 ! B ! |
| ! ! 0 1 1 0 0 ! C ! |
| ! ! 0 1 1 0 1 ! D ! |
| ! ! 0 1 1 1 0 ! E ! |
| ! ! 0 1 1 1 1 ! F ! |
| ! ! 1 0 0 0 0 ! G ! |
| ! ! 1 0 0 0 1 ! H ! |
| ! ! 1 0 0 1 0 ! I ! |
| ! ! 1 0 0 1 1 ! J ! |
| ! ! 1 0 1 0 0 ! K ! |
| ! ! 1 0 1 0 1 ! L ! |
| ! ! 1 0 1 1 0 ! M ! |
| ! ! 1 0 1 1 1 ! N ! |
| ! ! 1 1 0 0 0 ! O ! |
| ! ! 1 1 0 0 1 ! P ! |
| ! ! 1 1 0 1 0 ! Q ! |
| ! ! 1 1 0 1 1 ! R ! |
| ! ! 1 1 1 0 0 ! S ! |
| ! ! 1 1 1 0 1 ! T ! |
| ! ! 1 1 1 1 0 ! U ! |
| ! ! 1 1 1 1 1 ! V ! |
| ! ! ! |
| !--------------!------------------------------------------------------! |
| ! PT2 ! Total Air Pressure at Position 2 ! |
| ! 99999 ! (0.0 to 25.000 psia) ! |
| ! ! Eng 1 param. 7C.1.131.01 ! |
| ! ! Eng 2 param. 7C.2.131.10 ! |
| !--------------!------------------------------------------------------! |
| ! FT ! Fuel Temperature Inner Cell ! |
| ! X99 ! (-55.0 to 170.0 C) ! |
| ! ! param. 5A.2.177.10 Left Wing Tank ! |
| ! ! 5A.2.201.10 Right Wing Tank ! |
| !--------------!------------------------------------------------------! |
| ! HPT ! High-Pressure Turbine Clearance Position ! |
| ! X99 ! (-10 to 100 %) ! |
| ! ! Eng 1 param. 7C.1.306.01 ! |
| ! ! Eng 2 param. 7C.2.306.10 ! |
| !--------------!------------------------------------------------------! |
| ! LPT ! Low-Pressure Turbine Position ! |
| ! X99 ! (-10 to 100 %) ! |
| ! ! Eng 1 param. 7C.1.307.01 ! |
| ! ! Eng 2 param. 7C.2.307.10 ! |
| !--------------!------------------------------------------------------! |
| ! RALT ! Radio Height ! |
| ! X999 ! (-20 to 2500 ft) ! |
| ! ! param 25.1.164.01 Radio Altimeter #1 printed in ! |
| ! ! 25.2.164.01 report line X1 ! |
| ! ! param 25.1.164.10 Radio Altimeter #2 printed in ! |
| ! ! 25.2.164.10 report line X2 ! |
| +---------------------------------------------------------------------+ |
(2) Engine Take-Off Report Data Field Description <04> (Engine Type CFMI with Advanced EVMU)
NOTE: Reports that are transmitted from the ACARS system do not have report lines without a line identifier.
NOTE: Only the parts of the ENGINE TAKE OFF REPORT <04> which are not included in the ENGINE CRUISE REPORT <01> are given in the subsequent table.
| +---------------------------------------------------------------------+ |
| ! Value ! Content Description ! |
| !--------------!------------------------------------------------------! |
| ! T/O DELTA N1! Take Off Delta N1 Summary of Eng.1 and Eng.2 ! |
| ! SUMMARY ! ! |
| ! ! 1 2 3 4 5 6 7 8 9 ! |
| ! ! ___!____!____!____!____!____!____!____!___ ! |
| ! ! Engine 1 N1 ! 99 ! 99 ! 99 ! 99 ! 99 ! 99 ! 99 ! 99 ! |
| ! ! Engine 2 N2 ! 99 ! 99 ! 99 ! 99 ! 99 ! 99 ! 99 ! 99 ! |
| ! ! ! |
| ! ! 1 N1/N2 = Report Line Identifier ! |
| ! ! 2 99/99 = Number of total Take-Offs since ! |
| ! ! - previous Take-Off report according to ! |
| ! ! logic 4000 and 4100 ! |
| ! ! - ESN change ! |
| ! ! 3 99/99 = delta N1 is equal or less than 0.2 % rpm.! |
| ! ! 4 99/99 = delta N1 is more than 0.2 and equal or ! |
| ! ! less than 2.0 % rpm. ! |
| ! ! 5 99/99 = delta N1 is more than 2.0 and equal or ! |
| ! ! less than 4.0 % rpm. ! |
| ! ! 6 99/99 = delta N1 is more than 4.0 and equal or ! |
| ! ! less than 6.0% rpm. ! |
| ! ! 7 99/99 = delta N1 is more than 6.0 and equal or ! |
| ! ! less than 8.0% rpm. ! |
| ! ! 8 99/99 = delta N1 is more than 8.0 and is equal or! |
| ! ! less than 10.0% rpm. ! |
| ! ! 9 99/99 = delta N1 is more than 10.0 % rpm ! |
| ! ! Eng.1 param. 7C.1.342.01 for N1MX ECU ! |
| ! ! Eng.2 param. 7C.2.342.10 ! |
| ! ! Eng.1 param. 7C.1.346.01 for N1 ECU ! |
| ! ! Eng.2 param. 7C.2.346.10 ! |
| ! ! delta N1 = N1MX - N1 ! |
| !--------------!------------------------------------------------------! |
| ! EGTM ! Maximum EGT during Take Off observing time period ! |
| ! X999 ! ECU ! |
| ! ! Engine 1 7C.1.345.01 ! |
| ! ! Engine 2 7C.2.345.10 ! |
| ! ! NOTE: Negative values are shown with an 'N' in the ! |
| ! ! first position. If not, the first position ! |
| ! ! is used for the value. ! |
| !--------------!------------------------------------------------------! |
| ! N1MX ! N1 Maximum ! |
| ! 9999 ! ECU (0.0 to 108.0 % rpm) ! |
| ! ! Engine 1 7C.1.342.01 ! |
| ! ! Engine 2 7C.2.342.10 ! |
| !--------------!------------------------------------------------------! |
| ! T12 ! T12 Fan Inlet Temperature ! |
| ! X99 ! ECU (-55.0 to 85.0 C) ! |
| ! ! Engine 1 7C.1.130.01 ! |
| ! ! Engine 2 7C.2.130.10 ! |
| ! ! NOTE: Negative values are shown with an 'N' in the ! |
| ! ! first position. If not, the first position ! |
| ! ! contains a '0'. ! |
| !--------------!------------------------------------------------------! |
| ! PO ! Selected PO (Ambient Pressure) ! |
| ! 999 ! ECU (0 to 20.0 psia) ! |
| ! ! Engine 1 7C.1.114.01 ! |
| ! ! Engine 2 7C.2.114.10 ! |
| !--------------!------------------------------------------------------! |
| ! O/F (OF) ! Oil and Fuel Filter Clogged ! |
| ! 11 ! ! ! ! |
| ! ! ! !________Fuel filter clogged = 0 ! |
| ! ! ! Fuel filter not clogged = 1 ! |
| ! ! !___________Oil filter clogged = 0 ! |
| ! ! Oil filter not clogged = 1 ! |
| ! ! SDAC Engine 1 29.1.001.01.16 Oil filter ! |
| ! ! 29.2.001.01.16 ! |
| ! ! Engine 2 29.1.001.10.16 Oil filter ! |
| ! ! 29.2.001.10.16 ! |
| ! ! SDAC Engine 1 29.1.001.01.17 Fuel filter ! |
| ! ! 29.2.001.01.17 ! |
| ! ! Engine 2 29.1.001.10.17 Fuel filter ! |
| ! ! 29.2.001.10.17 ! |
| !--------------!------------------------------------------------------! |
| ! ECW2 ! Engine Control Word 2 ! |
| ! XXXXX ! Each 'X' represents 4 Bits in hexadecimal code of ! |
| ! ! a defined ARINC 429 word: ! |
| ! ! XXXXX Bits HEX ! |
| ! ! !!!!!___________ 14, 13, 12, 11 0...F ! |
| ! ! !!!!____________ 18, 17, 16, 15 0...F ! |
| ! ! !!!_____________ 22, 21, 20, 19 0...F ! |
| ! ! !!______________ 26, 25, 24, 23 0...F ! |
| ! ! !_______________ 29, 28, 27 0...7 ! |
| ! ! -------------------------------------------- ! |
| ! ! Bit Label Parameter Description ! |
| ! ! 11 7C.X.272.XX.12 = 1 Bump/Overboost #1 enable ! |
| ! ! 12 7C.X.272.XX.13 = 1 Bump/Overboost #2 enable ! |
| ! ! 13 7C.X.272.XX.14 = 1 Bump/Overboost #3 enable ! |
| ! ! 14 7C.X.272.XX.22 = 1 MTO. GA limit mode ! |
| ! ! selection ! |
| ! ! 15 7C.X.272.XX.23 = 1 Flex Take-Off limit mode ! |
| ! ! selection ! |
| ! ! 16 SPARE ! |
| ! ! 17 SPARE ! |
| ! ! 18 SPARE ! |
| ! ! 19 SPARE ! |
| ! ! 20 SPARE ! |
| ! ! 21 SPARE ! |
| ! ! 22 SPARE ! |
| ! ! 23 SPARE ! |
| ! ! 24 SPARE ! |
| ! ! 25 SPARE ! |
| ! ! 26 SPARE ! |
| ! ! 27 SPARE ! |
| ! ! 28 SPARE ! |
| ! ! 29 SPARE ! |
| !--------------!------------------------------------------------------! |
| ! PSEL ! Status of different FADEC sensors ! |
| ! XXXX ! X X X X Label: Selected: (Bit 11 -> 15) ! |
| ! ! ! ! ! !_____211 TAT ! |
| ! ! ! ! !_______344 N2 actual ! |
| ! ! ! !_________345 EGT ! |
| ! ! !___________346 N1 actual ! |
| ! ! (All labels Bit 11 -> 15) ! |
| ! ! Source: ECU, different labels ! |
| ! ! NOTE: The shown values are coded as follows: ! |
| ! ! Bit: 15 14 13 12 11 ! shown value ! |
| ! ! --------------------!---------------- ! |
| ! ! 0 0 0 0 0 ! 0 ! |
| ! ! 0 0 0 0 1 ! 1 ! |
| ! ! 0 0 0 1 0 ! 2 ! |
| ! ! 0 0 0 1 1 ! 3 ! |
| ! ! 0 0 1 0 0 ! 4 ! |
| ! ! 0 0 1 0 1 ! 5 ! |
| ! ! 0 0 1 1 0 ! 6 ! |
| ! ! 0 0 1 1 1 ! 7 ! |
| ! ! 0 1 0 0 0 ! 8 ! |
| ! ! 0 1 0 0 1 ! 9 ! |
| ! ! 0 1 0 1 0 ! A ! |
| ! ! 0 1 0 1 1 ! B ! |
| ! ! 0 1 1 0 0 ! C ! |
| ! ! 0 1 1 0 1 ! D ! |
| ! ! 0 1 1 1 0 ! E ! |
| ! ! 0 1 1 1 1 ! F ! |
| ! ! 1 0 0 0 0 ! G ! |
| ! ! 1 0 0 0 1 ! H ! |
| ! ! 1 0 0 1 0 ! I ! |
| ! ! 1 0 0 1 1 ! J ! |
| ! ! 1 0 1 0 0 ! K ! |
| ! ! 1 0 1 0 1 ! L ! |
| ! ! 1 0 1 1 0 ! M ! |
| ! ! 1 0 1 1 1 ! N ! |
| ! ! 1 1 0 0 0 ! O ! |
| ! ! 1 1 0 0 1 ! P ! |
| ! ! 1 1 0 1 0 ! Q ! |
| ! ! 1 1 0 1 1 ! R ! |
| ! ! 1 1 1 0 0 ! S ! |
| ! ! 1 1 1 0 1 ! T ! |
| ! ! 1 1 1 1 0 ! U ! |
| ! ! 1 1 1 1 1 ! V ! |
| ! ! ! |
| !--------------!------------------------------------------------------! |
| ! FT ! Fuel Temperature Inner Cell ! |
| ! X99 ! FQIC (-55.0 to 170.0 C) ! |
| ! ! 5A.2.177.10 Fuel Temperature Left Wing Tank ! |
| ! ! 5A.2.201.10 Fuel Temperature Right Wing Tank! |
| ! ! NOTE: Report line 'X1' shows Fuel Temperature Left ! |
| ! ! Wing Tank. ! |
| ! ! Report line 'X2' shows Fuel Temperature Right! |
| ! ! Wing Tank. ! |
| !--------------!------------------------------------------------------! |
| ! RALT ! Radio Height ! |
| ! X999 ! DMC (-20 to 2500 ft) ! |
| ! ! ! |
| ! ! 25.1.164.01 Radio Altimeter #1 printed in ! |
| ! ! 25.2.164.01 report line X1 ! |
| ! ! ! |
| ! ! 25.1.164.10 Radio Altimeter #2 printed in ! |
| ! ! 25.2.164.10 report line X2 ! |
| ! ! NOTE: Negative values are shown with an 'N' in the ! |
| ! ! first position. If not, the first position ! |
| ! ! is used for the value. ! |
| +--------------+------------------------------------------------------+ |
(3) Engine Take-Off Report Data Field Description <04> (Engine Type CFMI with Advanced EVMU)
NOTE: Reports that are transmitted from the ACARS system do not have report lines without a line identifier.
NOTE: Only the parts of the ENGINE TAKE OFF REPORT <04> which are not included in the ENGINE CRUISE REPORT <01> are given in the subsequent table.
| +---------------------------------------------------------------------+ |
| ! Value ! Content Description ! |
| !--------------!------------------------------------------------------! |
| ! T/O Sum ! Take Off Delta N1 Summary of Eng.1 and Eng.2 ! |
| ! ! ! |
| ! ! 1 2 3 4 5 6 7 8 9 ! |
| ! ! ___!____!____!____!____!____!____!____!___ ! |
| ! ! Engine 1 N1 ! 99 ! 99 ! 99 ! 99 ! 99 ! 99 ! 99 ! 99 ! |
| ! ! Engine 2 N2 ! 99 ! 99 ! 99 ! 99 ! 99 ! 99 ! 99 ! 99 ! |
| ! ! ! |
| ! ! 1 - Report Line Identifier ! |
| ! ! 2 - Number of total Take-Offs since ! |
| ! ! - previous Take-Off report according to ! |
| ! ! logic 4000 and 4100 ! |
| ! ! - ESN change ! |
| ! ! 3 - delta N1 <= 0.2 % rpm. ! |
| ! ! 4 - 0.2 < delta N1 <= 2.0 %rpm ! |
| ! ! 5 - 2.0 < delta N1 <= 4.0 %rpm ! |
| ! ! 6 - 4.0 < delta N1 <= 6.0 %rpm ! |
| ! ! 7 - 6.0 < delta N1 <= 8.0 %rpm ! |
| ! ! 8 - 8.0 < delta N1 <=10.0 %rpm ! |
| ! ! 9 - delta N1 > 10.0 %rpm ! |
| ! ! Eng.1 param. 7C.1.342.01 for N1MX ECU ! |
| ! ! Eng.2 param. 7C.2.342.10 ! |
| ! ! Eng.1 param. 7C.1.346.01 for N1 ECU ! |
| ! ! Eng.2 param. 7C.2.346.10 ! |
| ! ! delta N1 = N1MX - N1 ! |
| ! ! All other trigger conditions (1000, 2000, 3000, ! |
| ! ! 500X, 8X00) shall not reset the deltaN1 Derate ! |
| ! ! Counter ! |
| !--------------!------------------------------------------------------! |
| ! EGTM ! Maximum EGT during Take Off observing time period ! |
| ! X999 ! ECU ! |
| ! ! Engine 1 7C.1.345.01 ! |
| ! ! Engine 2 7C.2.345.10 ! |
| ! ! Negative values shall be indicated by '-' on the ! |
| ! ! first position. Otherwise the first position shall ! |
| ! ! be used for the value. ! |
| !--------------!------------------------------------------------------! |
| ! N1MX ! N1 Maximum ! |
| ! 9999 ! ECU (0.0 to 108.0 % rpm) ! |
| ! ! Engine 1 7C.1.342.01 ! |
| ! ! Engine 2 7C.2.342.10 ! |
| !--------------!------------------------------------------------------! |
| ! T12 ! T12 Fan Inlet Temperature ! |
| ! X999 ! ECU (-55.0 to 85.0 C) ! |
| ! ! Engine 1 7C.1.130.01 ! |
| ! ! Engine 2 7C.2.130.10 ! |
| ! ! Negative values shall be indicated by '-' on the ! |
| ! ! first position. Otherwise the first position ! |
| ! ! contains a '0'. ! |
| !--------------!------------------------------------------------------! |
| ! P0 ! Selected P0 (Ambient Pressure) ! |
| ! 999 ! ECU (0 to 20.0 psia) ! |
| ! ! Engine 1 7C.1.114.01 ! |
| ! ! Engine 2 7C.2.114.10 ! |
| !--------------!------------------------------------------------------! |
| ! O/F (OF) ! Oil and Fuel Filter Clogged ! |
| ! ! 1 1 ! |
| ! ! ! ! ! |
| ! ! ! !________Fuel filter clogged = 0 ! |
| ! ! ! Fuel filter not clogged = 1 ! |
| ! ! !___________Oil filter clogged = 0 ! |
| ! ! Oil filter not clogged = 1 ! |
| ! ! SDAC Engine 1 29.1.001.01.16 Oil filter ! |
| ! ! 29.2.001.01.16 ! |
| ! ! Engine 2 29.1.001.10.16 Oil filter ! |
| ! ! 29.2.001.10.16 ! |
| ! ! SDAC Engine 1 29.1.001.01.17 Fuel filter ! |
| ! ! 29.2.001.01.17 ! |
| ! ! Engine 2 29.1.001.10.17 Fuel filter ! |
| ! ! 29.2.001.10.17 ! |
| !--------------!------------------------------------------------------! |
| ! ECW2 ! Engine Control Word 2 ! |
| ! XXXXX ! Each 'X' represents 4 Bits in hexadecimal code of ! |
| ! ! a defined ARINC 429 word: ! |
| ! ! XXXXX Bits HEX ! |
| ! ! !!!!!___________ 14, 13, 12, 11 0...F ! |
| ! ! !!!!____________ 18, 17, 16, 15 0...F ! |
| ! ! !!!_____________ 22, 21, 20, 19 0...F ! |
| ! ! !!______________ 26, 25, 24, 23 0...F ! |
| ! ! !_______________ 29, 28, 27 0...7 ! |
| ! ! System SDI ! |
| ! ! Engine 1 1 01 ! |
| ! ! Engine 2 2 10 ! |
| ! ! Bit Label Parameter Description ! |
| ! ! 11 7C.X.272.XX.12 = 1 Bump/Overboost #1 enable ! |
| ! ! 12 7C.X.272.XX.13 = 1 Bump/Overboost #2 enable ! |
| ! ! 13 7C.X.272.XX.14 = 1 Bump/Overboost #3 enable ! |
| ! ! 14 7C.X.272.XX.22 = 1 MTO. GA limit mode ! |
| ! ! selected ! |
| ! ! 15 7C.X.272.XX.23 = 1 Flex Take-Off limit mode ! |
| ! ! selected ! |
| ! ! 16 SPARE ! |
| ! ! 17 SPARE ! |
| ! ! 18 SPARE ! |
| ! ! 19 SPARE ! |
| ! ! 20 SPARE ! |
| ! ! 21 SPARE ! |
| ! ! 22 SPARE ! |
| ! ! 23 SPARE ! |
| ! ! 24 SPARE ! |
| ! ! 25 SPARE ! |
| ! ! 26 SPARE ! |
| ! ! 27 SPARE ! |
| ! ! 28 SPARE ! |
| ! ! 29 SPARE ! |
| !--------------!------------------------------------------------------! |
| ! PSEL ! Status of different FADEC sensors ! |
| ! XXXX ! X X X X Label: Selected: ! |
| ! ! ! ! ! !_____211 TAT (Bit 11 -> 15) ! |
| ! ! ! ! !_______344 N2 actual (Bit 11 -> 15) ! |
| ! ! ! !_________345 EGT (Bit 11 -> 15) ! |
| ! ! !___________346 N1 actual (Bit 11 -> 15) ! |
| ! ! Source: ECU, different labels ! |
| ! ! NOTE: The shown values are coded as follows: ! |
| ! ! Bit: 15 14 13 12 11 ! Shown value ! |
| ! ! --------------------!---------------- ! |
| ! ! 0 0 0 0 0 ! 0 ! |
| ! ! 0 0 0 0 1 ! 1 ! |
| ! ! 0 0 0 1 0 ! 2 ! |
| ! ! 0 0 0 1 1 ! 3 ! |
| ! ! 0 0 1 0 0 ! 4 ! |
| ! ! 0 0 1 0 1 ! 5 ! |
| ! ! 0 0 1 1 0 ! 6 ! |
| ! ! 0 0 1 1 1 ! 7 ! |
| ! ! 0 1 0 0 0 ! 8 ! |
| ! ! 0 1 0 0 1 ! 9 ! |
| ! ! 0 1 0 1 0 ! A ! |
| ! ! 0 1 0 1 1 ! B ! |
| ! ! 0 1 1 0 0 ! C ! |
| ! ! 0 1 1 0 1 ! D ! |
| ! ! 0 1 1 1 0 ! E ! |
| ! ! 0 1 1 1 1 ! F ! |
| ! ! 1 0 0 0 0 ! G ! |
| ! ! 1 0 0 0 1 ! H ! |
| ! ! 1 0 0 1 0 ! I ! |
| ! ! 1 0 0 1 1 ! J ! |
| ! ! 1 0 1 0 0 ! K ! |
| ! ! 1 0 1 0 1 ! L ! |
| ! ! 1 0 1 1 0 ! M ! |
| ! ! 1 0 1 1 1 ! N ! |
| ! ! 1 1 0 0 0 ! O ! |
| ! ! 1 1 0 0 1 ! P ! |
| ! ! 1 1 0 1 0 ! Q ! |
| ! ! 1 1 0 1 1 ! R ! |
| ! ! 1 1 1 0 0 ! S ! |
| ! ! 1 1 1 0 1 ! T ! |
| ! ! 1 1 1 1 0 ! U ! |
| ! ! 1 1 1 1 1 ! V ! |
| ! ! ! |
| !--------------!------------------------------------------------------! |
| ! FT ! Fuel Temperature Inner Cell ! |
| ! X99 ! FQIC (-55.0 to 170.0 C) ! |
| ! ! 5A.2.177.10 Fuel Temp. Left Wing Tank ! |
| ! ! 5A.2.201.10 Fuel Temp. Right Wing Tank ! |
| ! ! Remark: Report line X1 indicates Fuel Temperature ! |
| ! ! Left Wing ! |
| ! ! Report line X2 indicates Fuel Temperature ! |
| ! ! Right Wing ! |
| !--------------!------------------------------------------------------! |
| ! RALT ! Radio Altitude ! |
| ! X999 ! DMC (-20 to 2500 ft) ! |
| ! ! ! |
| ! ! 25.1.164.01 Radio Altimeter #1 printed in ! |
| ! ! 25.2.164.01 report line X1 ! |
| ! ! ! |
| ! ! 25.1.164.10 Radio Altimeter #2 printed in ! |
| ! ! 25.2.164.10 report line X2 ! |
| ! ! Negative values shall be indicated by '-' on the ! |
| ! ! first position. Otherwise the first position shall ! |
| ! ! be used for the value. ! |
| +---------------------------------------------------------------------+ |
(4) Engine Take-Off Report Data Field Description <04> (Engine Type CFMI with Advanced EVMU)
NOTE: Reports that are transmitted from the ACARS system do not have report lines without a line identifier.
NOTE: Only the parts of the ENGINE TAKE OFF REPORT <04> which are not included in the ENGINE CRUISE REPORT <01> are given in the subsequent table.
| +---------------------------------------------------------------------+ |
| ! Value ! Content Description ! |
| !--------------!------------------------------------------------------! |
| ! T/O Delta N1! Take Off Delta N1 Summary of Eng.1 and Eng.2 ! |
| ! Summary ! ! |
| ! ! 1 2 3 4 5 6 7 8 9 ! |
| ! ! ___!____!____!____!____!____!____!____!___ ! |
| ! ! Engine 1 N1 ! 99 ! 99 ! 99 ! 99 ! 99 ! 99 ! 99 ! 99 ! |
| ! ! Engine 2 N2 ! 99 ! 99 ! 99 ! 99 ! 99 ! 99 ! 99 ! 99 ! |
| ! ! ! |
| ! ! 1 - Report Line Identifier ! |
| ! ! 2 - Number of total Take-Off since ! |
| ! ! - previous Take-Off report according to ! |
| ! ! logic 4000 and 4100 ! |
| ! ! - ESN change ! |
| ! ! 3 - delta N1 <= 0.2 % rpm. ! |
| ! ! 4 - 0.2 < delta N1 <= 2.0 %rpm ! |
| ! ! 5 - 2.0 < delta N1 <= 4.0 %rpm ! |
| ! ! 6 - 4.0 < delta N1 <= 6.0 %rpm ! |
| ! ! 7 - 6.0 < delta N1 <= 8.0 %rpm ! |
| ! ! 8 - 8.0 < delta N1 <=10.0 %rpm ! |
| ! ! 9 - delta N1 > 10.0 %rpm ! |
| ! ! Eng.1 param. 7C.1.342.01 for N1MX ECU ! |
| ! ! Eng.2 param. 7C.2.342.10 ! |
| ! ! Eng.1 param. 7C.1.346.01 for N1 ECU ! |
| ! ! Eng.2 param. 7C.2.346.10 ! |
| ! ! delta N1 = N1MX - N1 ! |
| ! ! All other trigger conditions (1000, 2000, 3000, ! |
| ! ! 5000) shall not reset the deltaN1 Derate Counter ! |
| !--------------!------------------------------------------------------! |
| ! EGTM ! Maximum EGT during Take Off observing time period ! |
| ! X999 ! ECU ! |
| ! ! Engine 1 7C.1.345.01 ! |
| ! ! Engine 2 7C.2.345.10 ! |
| ! ! Negative values shall be indicated by 'N' on the ! |
| ! ! first position. Otherwise the first position shall ! |
| ! ! be used for the value. ! |
| !--------------!------------------------------------------------------! |
| ! N1MX ! N1 Maximum ! |
| ! 9999 ! ECU (0.0 to 108.0 % rpm) ! |
| ! ! Engine 1 7C.1.342.01 ! |
| ! ! Engine 2 7C.2.342.10 ! |
| !--------------!------------------------------------------------------! |
| ! T12 ! T12 Fan Inlet Temperature ! |
| ! X999 ! ECU (-55.0 to 85.0 C) ! |
| ! ! Engine 1 7C.1.130.01 ! |
| ! ! Engine 2 7C.2.130.10 ! |
| ! ! Negative values shall be indicated by 'N' on the ! |
| ! ! first position. Otherwise the first position ! |
| ! ! contains a '0'. ! |
| !--------------!------------------------------------------------------! |
| ! P0 ! Selected P0 (Ambient Pressure) ! |
| ! 999 ! ECU (0 to 20.0 psia) ! |
| ! ! Engine 1 7C.1.114.01 ! |
| ! ! Engine 2 7C.2.114.10 ! |
| !--------------!------------------------------------------------------! |
| ! O/F (OF) ! Oil and Fuel Filter Clogged ! |
| ! ! 1 1 ! |
| ! ! ! ! ! |
| ! ! ! !________Fuel filter clogged = 0 ! |
| ! ! ! Fuel filter not clogged = 1 ! |
| ! ! !___________Oil filter clogged = 0 ! |
| ! ! Oil filter not clogged = 1 ! |
| ! ! SDAC Engine 1 29.1.001.01.16 Oil filter ! |
| ! ! 29.2.001.01.16 ! |
| ! ! Engine 2 29.1.001.10.16 Oil filter ! |
| ! ! 29.2.001.10.16 ! |
| ! ! SDAC Engine 1 29.1.001.01.17 Fuel filter ! |
| ! ! 29.2.001.01.17 ! |
| ! ! Engine 2 29.1.001.10.17 Fuel filter ! |
| ! ! 29.2.001.10.17 ! |
| !--------------!------------------------------------------------------! |
| ! ECW2 ! Engine Control Word 2 ! |
| ! XXXXX ! Each 'X' represents 4 Bits in hexadecimal code of ! |
| ! ! a defined ARINC 429 word: ! |
| ! ! XXXXX Bits HEX ! |
| ! ! !!!!!___________ 14, 13, 12, 11 0...F ! |
| ! ! !!!!____________ 18, 17, 16, 15 0...F ! |
| ! ! !!!_____________ 22, 21, 20, 19 0...F ! |
| ! ! !!______________ 26, 25, 24, 23 0...F ! |
| ! ! !_______________ 29, 28, 27 0...7 ! |
| ! ! System SDI ! |
| ! ! Engine 1 1 01 ! |
| ! ! Engine 2 2 10 ! |
| ! ! Bit Label Parameter Description ! |
| ! ! 11 7C.X.272.XX.12 = 1 Bump/Overboost #1 enable ! |
| ! ! 12 7C.X.272.XX.13 = 1 Bump/Overboost #2 enable ! |
| ! ! 13 7C.X.272.XX.14 = 1 Bump/Overboost #3 enable ! |
| ! ! 14 7C.X.272.XX.22 = 1 MTO. GA limit mode ! |
| ! ! selection ! |
| ! ! 15 7C.X.272.XX.23 = 1 Flex Take-Off limit mode ! |
| ! ! selection ! |
| ! ! 16 SPARE ! |
| ! ! 17 SPARE ! |
| ! ! 18 SPARE ! |
| ! ! 19 SPARE ! |
| ! ! 20 SPARE ! |
| ! ! 21 SPARE ! |
| ! ! 22 SPARE ! |
| ! ! 23 SPARE ! |
| ! ! 24 SPARE ! |
| ! ! 25 SPARE ! |
| ! ! 26 SPARE ! |
| ! ! 27 SPARE ! |
| ! ! 28 SPARE ! |
| ! ! 29 SPARE ! |
| !--------------!------------------------------------------------------! |
| ! PSEL ! Status of different FADEC sensors ! |
| ! XXXX ! X X X X Label: Selected: ! |
| ! ! ! ! ! !_____211 TAT (Bit 11 -> 15) ! |
| ! ! ! ! !_______344 N2 actual (Bit 11 -> 15) ! |
| ! ! ! !_________345 EGT (Bit 11 -> 15) ! |
| ! ! !___________346 N1 actual (Bit 11 -> 15) ! |
| ! ! Source: ECU, different labels ! |
| ! ! NOTE: The shown values are coded as follows: ! |
| ! ! Bit: 15 14 13 12 11 ! Shown value ! |
| ! ! --------------------!---------------- ! |
| ! ! 0 0 0 0 0 ! 0 ! |
| ! ! 0 0 0 0 1 ! 1 ! |
| ! ! 0 0 0 1 0 ! 2 ! |
| ! ! 0 0 0 1 1 ! 3 ! |
| ! ! 0 0 1 0 0 ! 4 ! |
| ! ! 0 0 1 0 1 ! 5 ! |
| ! ! 0 0 1 1 0 ! 6 ! |
| ! ! 0 0 1 1 1 ! 7 ! |
| ! ! 0 1 0 0 0 ! 8 ! |
| ! ! 0 1 0 0 1 ! 9 ! |
| ! ! 0 1 0 1 0 ! A ! |
| ! ! 0 1 0 1 1 ! B ! |
| ! ! 0 1 1 0 0 ! C ! |
| ! ! 0 1 1 0 1 ! D ! |
| ! ! 0 1 1 1 0 ! E ! |
| ! ! 0 1 1 1 1 ! F ! |
| ! ! 1 0 0 0 0 ! G ! |
| ! ! 1 0 0 0 1 ! H ! |
| ! ! 1 0 0 1 0 ! I ! |
| ! ! 1 0 0 1 1 ! J ! |
| ! ! 1 0 1 0 0 ! K ! |
| ! ! 1 0 1 0 1 ! L ! |
| ! ! 1 0 1 1 0 ! M ! |
| ! ! 1 0 1 1 1 ! N ! |
| ! ! 1 1 0 0 0 ! O ! |
| ! ! 1 1 0 0 1 ! P ! |
| ! ! 1 1 0 1 0 ! Q ! |
| ! ! 1 1 0 1 1 ! R ! |
| ! ! 1 1 1 0 0 ! S ! |
| ! ! 1 1 1 0 1 ! T ! |
| ! ! 1 1 1 1 0 ! U ! |
| ! ! 1 1 1 1 1 ! V ! |
| ! ! ! |
| !--------------!------------------------------------------------------! |
| ! FT ! Fuel Temperature Inner Cell ! |
| ! X999 ! FQIC (-55.0 to 170.0 C) ! |
| ! ! 5A.2.177.10 Fuel Temp. Left Wing Tank ! |
| ! ! 5A.2.201.10 Fuel Temp. Right Wing Tank ! |
| ! ! Remark: Report line X1 indicates Fuel Temperature ! |
| ! ! Left Wing ! |
| ! ! Report line X2 indicates Fuel Temperature ! |
| ! ! Right Wing ! |
| !--------------!------------------------------------------------------! |
| ! RALT ! Radio Altitude ! |
| ! X999 ! DMC (-20 to 2500 ft) ! |
| ! ! ! |
| ! ! 25.1.164.01 Radio Altimeter #1 printed in ! |
| ! ! 25.2.164.01 report line X1 ! |
| ! ! ! |
| ! ! 25.1.164.10 Radio Altimeter #2 printed in ! |
| ! ! 25.2.164.10 report line X2 ! |
| ! ! Negative values shall be indicated by 'N' on the ! |
| ! ! first position. Otherwise the first position shall ! |
| ! ! be used for the value. ! |
| +---------------------------------------------------------------------+ |
(5) Engine Take-Off Report Data Field Description <04> (Engine Type CFMI with Advanced EVMU)
NOTE: Reports that are transmitted from the ACARS system do not have report lines without a line identifier.
NOTE: Only the parts of the ENGINE TAKE OFF REPORT <04> which are not included in the ENGINE CRUISE REPORT <01> are given in the subsequent table.
| +---------------------------------------------------------------------+ |
| ! Value ! Content Description ! |
| !--------------+------------------------------------------------------! |
| ! T/O Sum ! Take Off Delta N1 Summary of Eng.1 and Eng.2 ! |
| ! ! ! |
| ! ! 1 2 3 4 5 6 7 8 9 10 ! |
| ! ! ___!___!___!___!___!___!___!___!__ !__! ! |
| ! ! Engine 1 N1 !99 !99 !99 !99 !99 !99 !99 !99 !99! ! |
| ! ! Engine 2 N2 !99 !99 !99 !99 !99 !99 !99 !99 !99! ! |
| ! ! ! |
| ! ! 1 - Report Line Identifier ! |
| ! ! 2 - Number of total Take-Offs since ! |
| ! ! - previous Take-Off report according to ! |
| ! ! logic 4000 and 4100 ! |
| ! ! - ESN change ! |
| ! ! 3 - Number of Take Off with Take Off Thrust ! |
| ! ! bumb active ! |
| ! ! 4 - delta N1 <= 0.2 % rpm. ! |
| ! ! 5 - 0.2 < delta N1 <= 2.0 %rpm ! |
| ! ! 6 - 2.0 < delta N1 <= 4.0 %rpm ! |
| ! ! 7 - 4.0 < delta N1 <= 6.0 %rpm ! |
| ! ! 8 - 6.0 < delta N1 <= 8.0 %rpm ! |
| ! ! 9 - 8.0 < delta N1 <=10.0 %rpm ! |
| ! ! 10 - delta N1 > 10.0 %rpm ! |
| ! ! Eng.1 param. 7C.1.342.01 for N1MX ECU ! |
| ! ! Eng.2 param. 7C.2.342.10 ! |
| ! ! Eng.1 param. 7C.1.346.01 for N1 ECU ! |
| ! ! Eng.2 param. 7C.2.346.10 ! |
| ! ! delta N1 = N1MX - N1 ! |
| ! ! All other trigger conditions (1000, 2000, 3000, ! |
| ! ! 500X, 8X00) do not reset the deltaN1 Derate Counter! |
| ! ! and the Take Off Thrust Bump counter. ! |
| ! ! If the Take Off Thrust Bump counter reaches the ! |
| ! ! value "99" the next value is "01". ! |
| ! ! ! |
| ! ! Indication of Take Off Thrust bump: ! |
| ! ! Thrust Bump is active EEC 7C.1.272.01.18=1 Engine 1! |
| ! ! EEC 7C.2.272.10.18=1 Engine 2! |
| !--------------!------------------------------------------------------! |
| ! EGTM ! Maximum EGT during Take Off observing time period ! |
| ! X999 ! ECU ! |
| ! ! Engine 1 7C.1.345.01 ! |
| ! ! Engine 2 7C.2.345.10 ! |
| ! ! Negative values are shown with '-' on the first ! |
| ! ! position. If not, the first position is used for ! |
| ! ! the value. ! |
| !--------------!------------------------------------------------------! |
| ! N1MX ! N1 Maximum ! |
| ! 9999 ! ECU (0.0 to 108.0 % rpm) ! |
| ! ! Engine 1 7C.1.342.01 ! |
| ! ! Engine 2 7C.2.342.10 ! |
| !--------------!------------------------------------------------------! |
| ! T12 ! T12 Fan Inlet Temperature ! |
| ! X99 ! ECU (-55.0 deg.C to 85.0 deg.C) ! |
| ! ! Engine 1 7C.1.130.01 ! |
| ! ! Engine 2 7C.2.130.10 ! |
| ! ! Negative values are shown with '-' on the first ! |
| ! ! position. If not, the first position contains a ! |
| ! ! '0'. ! |
| !--------------!------------------------------------------------------! |
| ! P0 ! Selected P0 (Ambient Pressure) ! |
| ! 999 ! ECU (0 to 20.0 psia) ! |
| ! ! Engine 1 7C.1.114.01 ! |
| ! ! Engine 2 7C.2.114.10 ! |
| !--------------!------------------------------------------------------! |
| ! O/F (OF) ! Oil and Fuel Filter Clogged ! |
| ! ! 1 1 ! |
| ! ! ! ! ! |
| ! ! ! !________Fuel filter clogged = 0 ! |
| ! ! ! Fuel filter not clogged = 1 ! |
| ! ! !___________Oil filter clogged = 0 ! |
| ! ! Oil filter not clogged = 1 ! |
| ! ! SDAC Engine 1 29.1.001.01.16 Oil filter ! |
| ! ! 29.2.001.01.16# ! |
| ! ! Engine 2 29.1.001.10.16 Oil filter ! |
| ! ! 29.2.001.10.16# ! |
| ! ! SDAC Engine 1 29.1.001.01.17 Fuel filter ! |
| ! ! 29.2.001.01.17# ! |
| ! ! Engine 2 29.1.001.10.17 Fuel filter ! |
| ! ! 29.2.001.10.17# ! |
| !--------------!------------------------------------------------------! |
| ! ECW2 ! Engine Control Word 2 ! |
| ! XXXXX ! Each 'X' represents 4 Bits in hexadecimal code of ! |
| ! ! a defined ARINC 429 word: ! |
| ! ! XXXXX Bits HEX ! |
| ! ! !!!!!___________ 14, 13, 12, 11 0...F ! |
| ! ! !!!!____________ 18, 17, 16, 15 0...F ! |
| ! ! !!!_____________ 22, 21, 20, 19 0...F ! |
| ! ! !!______________ 26, 25, 24, 23 0...F ! |
| ! ! !_______________ 29, 28, 27 0...7 ! |
| ! ! System SDI ! |
| ! ! Engine 1 1 01 ! |
| ! ! Engine 2 2 10 ! |
| ! ! Bit Label Parameter Description ! |
| ! ! 11 7C.X.272.XX.12 = 1 Bump/Overboost #1 enable ! |
| ! ! 12 7C.X.272.XX.13 = 1 Bump/Overboost #2 enable ! |
| ! ! 13 7C.X.272.XX.14 = 1 Bump/Overboost #3 enable ! |
| ! ! 14 7C.X.272.XX.22 = 1 MTO. GA limit mode ! |
| ! ! selected ! |
| ! ! 15 7C.X.272.XX.23 = 1 Flex Take-Off limit mode ! |
| ! ! selected ! |
| ! ! 16 SPARE ! |
| ! ! 17 SPARE ! |
| ! ! 18 SPARE ! |
| ! ! 19 SPARE ! |
| ! ! 20 SPARE ! |
| ! ! 21 SPARE ! |
| ! ! 22 SPARE ! |
| ! ! 23 SPARE ! |
| ! ! 24 SPARE ! |
| ! ! 25 SPARE ! |
| ! ! 26 SPARE ! |
| ! ! 27 SPARE ! |
| ! ! 28 SPARE ! |
| ! ! 29 SPARE ! |
| !--------------!------------------------------------------------------! |
| ! PSEL ! Status of different FADEC sensors ! |
| ! XXXX ! X X X X Label: Selected: ! |
| ! ! ! ! ! !_____211 TAT (Bit 11 -> 15) ! |
| ! ! ! ! !_______344 N2 actual (Bit 11 -> 15) ! |
| ! ! ! !_________345 EGT (Bit 11 -> 15) ! |
| ! ! !___________346 N1 actual (Bit 11 -> 15) ! |
| ! ! Source: ECU, different labels ! |
| ! ! NOTE: The shown values are coded as follows: ! |
| ! ! Bit: 15 14 13 12 11 ! Shown value ! |
| ! ! --------------------!---------------- ! |
| ! ! 0 0 0 0 0 ! 0 ! |
| ! ! 0 0 0 0 1 ! 1 ! |
| ! ! 0 0 0 1 0 ! 2 ! |
| ! ! 0 0 0 1 1 ! 3 ! |
| ! ! 0 0 1 0 0 ! 4 ! |
| ! ! 0 0 1 0 1 ! 5 ! |
| ! ! 0 0 1 1 0 ! 6 ! |
| ! ! 0 0 1 1 1 ! 7 ! |
| ! ! 0 1 0 0 0 ! 8 ! |
| ! ! 0 1 0 0 1 ! 9 ! |
| ! ! 0 1 0 1 0 ! A ! |
| ! ! 0 1 0 1 1 ! B ! |
| ! ! 0 1 1 0 0 ! C ! |
| ! ! 0 1 1 0 1 ! D ! |
| ! ! 0 1 1 1 0 ! E ! |
| ! ! 0 1 1 1 1 ! F ! |
| ! ! 1 0 0 0 0 ! G ! |
| ! ! 1 0 0 0 1 ! H ! |
| ! ! 1 0 0 1 0 ! I ! |
| ! ! 1 0 0 1 1 ! J ! |
| ! ! 1 0 1 0 0 ! K ! |
| ! ! 1 0 1 0 1 ! L ! |
| ! ! 1 0 1 1 0 ! M ! |
| ! ! 1 0 1 1 1 ! N ! |
| ! ! 1 1 0 0 0 ! O ! |
| ! ! 1 1 0 0 1 ! P ! |
| ! ! 1 1 0 1 0 ! Q ! |
| ! ! 1 1 0 1 1 ! R ! |
| ! ! 1 1 1 0 0 ! S ! |
| ! ! 1 1 1 0 1 ! T ! |
| ! ! 1 1 1 1 0 ! U ! |
| ! ! 1 1 1 1 1 ! V ! |
| ! ! ! |
| !--------------!------------------------------------------------------! |
| ! FT ! Fuel Temperature Inner Cell ! |
| ! X99 ! FQIC (-55.0 to 170.0 deg.C) ! |
| ! ! 5A.2.177.10 Fuel Temp. Left Wing Tank ! |
| ! ! 5A.2.201.10 Fuel Temp. Right Wing Tank ! |
| ! ! Remark: Report line X1 shows Fuel Temperature ! |
| ! ! Left Wing. ! |
| ! ! Report line X2 shows Fuel Temperature Right Wing. ! |
| !--------------!------------------------------------------------------! |
| ! RALT ! Radio Altitude ! |
| ! X999 ! DMC (-20 to 2500 ft) ! |
| ! ! ! |
| ! ! 25.1.164.01 Radio Altimeter #1 printed in ! |
| ! ! 25.2.164.01# report line X1 ! |
| ! ! ! |
| ! ! 25.1.164.10 Radio Altimeter #2 printed in ! |
| ! ! 25.2.164.10# report line X2 ! |
| ! ! Negative values are shown '-' on the first position! |
| ! ! If not, the first position is used for the value. ! |
| +--------------+------------------------------------------------------+ |
(6) Engine Take-Off Report Data Field Description <04> (Engine Type CFMI with Advanced EVMU)
NOTE: Reports that are transmitted from the ACARS system do not have report lines without a line identifier.
NOTE: Only the parts of the ENGINE TAKE OFF REPORT <04> which are not included in the ENGINE CRUISE REPORT <01> are given in the subsequent table.
| +---------------------------------------------------------------------+ |
| ! Value ! Content Description ! |
| !--------------+------------------------------------------------------! |
| ! T/O Delta N1! Take Off Delta N1 Summary of Eng.1 and Eng.2 ! |
| ! Summary ! ! |
| ! ! 1 2 3 4 5 6 7 8 9 ! |
| ! ! ___!____!____!____!____!____!____!____!___ ! |
| ! ! Engine 1 N1 ! 99 ! 99 ! 99 ! 99 ! 99 ! 99 ! 99 ! 99 ! |
| ! ! Engine 2 N2 ! 99 ! 99 ! 99 ! 99 ! 99 ! 99 ! 99 ! 99 ! |
| ! ! ! |
| ! ! 1 - Report Line Identifier ! |
| ! ! 2 - Number of total Take-Off since ! |
| ! ! - previous Take-Off report according to ! |
| ! ! logic 4000 and 4100 ! |
| ! ! - ESN change ! |
| ! ! 3 - delta N1 <= 0.2 % rpm. ! |
| ! ! 4 - 0.2 < delta N1 <= 2.0 %rpm ! |
| ! ! 5 - 2.0 < delta N1 <= 4.0 %rpm ! |
| ! ! 6 - 4.0 < delta N1 <= 6.0 %rpm ! |
| ! ! 7 - 6.0 < delta N1 <= 8.0 %rpm ! |
| ! ! 8 - 8.0 < delta N1 <=10.0 %rpm ! |
| ! ! 9 - delta N1 > 10.0 %rpm ! |
| ! ! Eng.1 param. 7C.1.342.01 for N1MX ECU ! |
| ! ! Eng.2 param. 7C.2.342.10 ! |
| ! ! Eng.1 param. 7C.1.346.01 for N1 ECU ! |
| ! ! Eng.2 param. 7C.2.346.10 ! |
| ! ! delta N1 = N1MX - N1 ! |
| ! ! All other trigger conditions (1000, 2000, 3000, ! |
| ! ! 5000) must not reset the deltaN1 Derate Counter ! |
| !--------------!------------------------------------------------------! |
| ! EGTM ! Maximum EGT during Take Off observing time period ! |
| ! X999 ! ECU ! |
| ! ! Engine 1 7C.1.345.01 ! |
| ! ! Engine 2 7C.2.345.10 ! |
| ! ! Negative values are shown with an 'N' on the ! |
| ! ! first position. If not, the first position is used ! |
| ! ! for the value. ! |
| !--------------!------------------------------------------------------! |
| ! N1MX ! N1 Maximum ! |
| ! 9999 ! ECU (0.0 to 108.0 % rpm) ! |
| ! ! Engine 1 7C.1.342.01 ! |
| ! ! Engine 2 7C.2.342.10 ! |
| !--------------!------------------------------------------------------! |
| ! T12 ! T12 Fan Inlet Temperature ! |
| ! X99 ! ECU (-55.0 to 85.0 C) ! |
| ! ! Engine 1 7C.1.130.01 ! |
| ! ! Engine 2 7C.2.130.10 ! |
| ! ! Negative values are shown with an 'N' on the ! |
| ! ! first position. If not, the first position ! |
| ! ! contains a '0'. ! |
| !--------------!------------------------------------------------------! |
| ! P0 ! Selected P0 (Ambient Pressure) ! |
| ! 999 ! ECU (0 to 20.0 psia) ! |
| ! ! Engine 1 7C.1.114.01 ! |
| ! ! Engine 2 7C.2.114.10 ! |
| !--------------!------------------------------------------------------! |
| ! O/F (OF) ! Oil and Fuel Filter Clogged ! |
| ! ! 1 1 ! |
| ! ! ! ! ! |
| ! ! ! !________Fuel filter clogged = 0 ! |
| ! ! ! Fuel filter not clogged = 1 ! |
| ! ! !___________Oil filter clogged = 0 ! |
| ! ! Oil filter not clogged = 1 ! |
| ! ! SDAC Engine 1 29.1.001.01.16 Oil filter ! |
| ! ! 29.2.001.01.16 ! |
| ! ! Engine 2 29.1.001.10.16 Oil filter ! |
| ! ! 29.2.001.10.16 ! |
| ! ! SDAC Engine 1 29.1.001.01.17 Fuel filter ! |
| ! ! 29.2.001.01.17 ! |
| ! ! Engine 2 29.1.001.10.17 Fuel filter ! |
| ! ! 29.2.001.10.17 ! |
| !--------------!------------------------------------------------------! |
| ! ECW2 ! Engine Control Word 2 ! |
| ! XXXXX ! Each 'X' represents 4 Bits in hexadecimal code of ! |
| ! ! a defined ARINC 429 word: ! |
| ! ! XXXXX Bits HEX ! |
| ! ! !!!!!___________ 14, 13, 12, 11 0...F ! |
| ! ! !!!!____________ 18, 17, 16, 15 0...F ! |
| ! ! !!!_____________ 22, 21, 20, 19 0...F ! |
| ! ! !!______________ 26, 25, 24, 23 0...F ! |
| ! ! !_______________ 29, 28, 27 0...7 ! |
| ! ! System SDI ! |
| ! ! Engine 1 1 01 ! |
| ! ! Engine 2 2 10 ! |
| ! ! Bit Label Parameter Description ! |
| ! ! 11 7C.X.272.XX.12 = 1 Bump/Overboost #1 enable ! |
| ! ! 12 7C.X.272.XX.13 = 1 Bump/Overboost #2 enable ! |
| ! ! 13 7C.X.272.XX.14 = 1 Bump/Overboost #3 enable ! |
| ! ! 14 7C.X.272.XX.22 = 1 MTO. GA limit mode ! |
| ! ! selection ! |
| ! ! 15 7C.X.272.XX.23 = 1 Flex Take-Off limit mode ! |
| ! ! selection ! |
| ! ! 16 SPARE ! |
| ! ! 17 SPARE ! |
| ! ! 18 SPARE ! |
| ! ! 19 SPARE ! |
| ! ! 20 SPARE ! |
| ! ! 21 SPARE ! |
| ! ! 22 SPARE ! |
| ! ! 23 SPARE ! |
| ! ! 24 SPARE ! |
| ! ! 25 SPARE ! |
| ! ! 26 SPARE ! |
| ! ! 27 SPARE ! |
| ! ! 28 SPARE ! |
| ! ! 29 SPARE ! |
| !--------------!------------------------------------------------------! |
| ! PSEL ! Status of different FADEC sensors ! |
| ! XXXX ! X X X X Label: Selected: ! |
| ! ! ! ! ! !_____211 TAT (Bit 11 -> 15) ! |
| ! ! ! ! !_______344 N2 actual (Bit 11 -> 15) ! |
| ! ! ! !_________345 EGT (Bit 11 -> 15) ! |
| ! ! !___________346 N1 actual (Bit 11 -> 15) ! |
| ! ! Source: ECU, different labels ! |
| ! ! NOTE: The shown values are coded as follows: ! |
| ! ! Bit: 15 14 13 12 11 ! Shown value ! |
| ! ! --------------------!---------------- ! |
| ! ! 0 0 0 0 0 ! 0 ! |
| ! ! 0 0 0 0 1 ! 1 ! |
| ! ! 0 0 0 1 0 ! 2 ! |
| ! ! 0 0 0 1 1 ! 3 ! |
| ! ! 0 0 1 0 0 ! 4 ! |
| ! ! 0 0 1 0 1 ! 5 ! |
| ! ! 0 0 1 1 0 ! 6 ! |
| ! ! 0 0 1 1 1 ! 7 ! |
| ! ! 0 1 0 0 0 ! 8 ! |
| ! ! 0 1 0 0 1 ! 9 ! |
| ! ! 0 1 0 1 0 ! A ! |
| ! ! 0 1 0 1 1 ! B ! |
| ! ! 0 1 1 0 0 ! C ! |
| ! ! 0 1 1 0 1 ! D ! |
| ! ! 0 1 1 1 0 ! E ! |
| ! ! 0 1 1 1 1 ! F ! |
| ! ! 1 0 0 0 0 ! G ! |
| ! ! 1 0 0 0 1 ! H ! |
| ! ! 1 0 0 1 0 ! I ! |
| ! ! 1 0 0 1 1 ! J ! |
| ! ! 1 0 1 0 0 ! K ! |
| ! ! 1 0 1 0 1 ! L ! |
| ! ! 1 0 1 1 0 ! M ! |
| ! ! 1 0 1 1 1 ! N ! |
| ! ! 1 1 0 0 0 ! O ! |
| ! ! 1 1 0 0 1 ! P ! |
| ! ! 1 1 0 1 0 ! Q ! |
| ! ! 1 1 0 1 1 ! R ! |
| ! ! 1 1 1 0 0 ! S ! |
| ! ! 1 1 1 0 1 ! T ! |
| ! ! 1 1 1 1 0 ! U ! |
| ! ! 1 1 1 1 1 ! V ! |
| ! ! ! |
| !--------------!------------------------------------------------------! |
| ! FT ! Fuel Temperature Inner Cell ! |
| ! X999 ! FQIC (-55.0 to 170.0 C) ! |
| ! ! 5A.2.177.10 Fuel Temp. Left Wing Tank ! |
| ! ! 5A.2.201.10 Fuel Temp. Right Wing Tank ! |
| ! ! Remark: Report line X1 shows Fuel Temperature Left ! |
| ! ! Wing ! |
| ! ! Report line X2 shows Fuel Temperature ! |
| ! ! Right Wing ! |
| !--------------!------------------------------------------------------! |
| ! RALT ! Radio Height ! |
| ! X999 ! DMC (-20 to 2500 ft) ! |
| ! ! ! |
| ! ! 25.1.164.01 Radio Altimeter #1 printed in ! |
| ! ! 25.2.164.01 report line X1 ! |
| ! ! ! |
| ! ! 25.1.164.10 Radio Altimeter #2 printed in ! |
| ! ! 25.2.164.10 report line X2 ! |
| ! ! Negative values are shown with an 'N' on the first ! |
| ! ! position. If not, the first position is used for ! |
| ! ! the value. ! |
| +---------------------------------------------------------------------+ |
(7) Engine Take-Off Report Data Field Description <04> (Engine Type CFMI with Advanced EVMU)
NOTE: Reports that are transmitted from the ACARS system do not have report lines without a line identifier.
NOTE: Only the parts of the ENGINE TAKE OFF REPORT <04> which are not included in the ENGINE CRUISE REPORT <01> are given in the subsequent table.
| +---------------------------------------------------------------------+ |
| ! Value ! Content Description ! |
| !--------------!------------------------------------------------------! |
| ! T/O Delta N1! Take Off Delta N1 Summary of Eng.1 and Eng.2 ! |
| ! Summary ! ! |
| ! ! 1 2 3 4 5 6 7 8 9 10! |
| ! ! ___!____!____!____!____!____!____!____!___!___! |
| ! ! Eng. 1 N1 ! 99 ! 99 ! 99 ! 99 ! 99 ! 99 ! 99 ! 99! 99! |
| ! ! Eng. 2 N2 ! 99 ! 99 ! 99 ! 99 ! 99 ! 99 ! 99 ! 99! 99! |
| ! ! ! |
| ! ! 1 - Report Line Identifier ! |
| ! ! 2 - Number of total Take-Off since ! |
| ! ! - previous Take-Off report according to ! |
| ! ! logic 4000 and 4100 ! |
| ! ! - ESN change ! |
| ! ! 3 - Number of Take Off with Take Off Thrust ! |
| ! ! Bump active ! |
| ! ! 4 - delta N1 <= 0.2 % rpm. ! |
| ! ! 5 - 0.2 < delta N1 <= 2.0 %rpm ! |
| ! ! 6 - 2.0 < delta N1 <= 4.0 %rpm ! |
| ! ! 7 - 4.0 < delta N1 <= 6.0 %rpm ! |
| ! ! 8 - 6.0 < delta N1 <= 8.0 %rpm ! |
| ! ! 9 - 8.0 < delta N1 <=10.0 %rpm ! |
| ! ! 10- delta N1 > 10.0 %rpm ! |
| ! ! N1MX ECU Eng.1 param. 7C.1.342.01 ! |
| ! ! Eng.2 param. 7C.2.342.10 ! |
| ! ! N1 ECU Eng.1 param. 7C.1.346.01 ! |
| ! ! Eng.2 param. 7C.2.346.10 ! |
| ! ! delta N1 = N1MX - N1 ! |
| ! ! All other trigger conditions (1000, 2000, 3000, ! |
| ! ! 500X, 8X00) does not reset the deltaN1 Derate ! |
| ! ! Counter and the Take Off Thrust Bump counter. ! |
| ! ! If the Take Off Thrust Bump reaches the value '99' ! |
| ! ! the next value is '01'. ! |
| ! ! Indication of Take Off Thrust Bump: ! |
| ! ! Thrust Bump is active EEC 7C.1.272.01.18 = 1 Eng 1 ! |
| ! ! EEC 7C.2.272.10.18 = 2 Eng 2 ! |
| !--------------!------------------------------------------------------! |
| ! EGTM ! Maximum EGT during Take Off observing time period ! |
| ! X999 ! ! |
| ! ! ECU Engine 1 7C.1.345.01 ! |
| ! ! Engine 2 7C.2.345.10 ! |
| ! ! Negative values are indicated by 'N' on the first ! |
| ! ! position. Otherwise the first position is used for ! |
| ! ! value. ! |
| !--------------!------------------------------------------------------! |
| ! N1MX ! N1 Maximum ! |
| ! 9999 ! (0.0 to 108.0 % rpm) ! |
| ! ! ECU Engine 1 7C.1.342.01 ! |
| ! ! Engine 2 7C.2.342.10 ! |
| !--------------!------------------------------------------------------! |
| ! T12 ! T12 Fan Inlet Temperature ! |
| ! X999 ! (-55.0 to 85.0 °C) ! |
| ! ! ECU Engine 1 7C.1.130.01 ! |
| ! ! Engine 2 7C.2.130.10 ! |
| ! ! Negative values are indicated by 'N' on the first ! |
| ! ! position. Otherwise the first position contains a ! |
| ! ! '0'. ! |
| !--------------!------------------------------------------------------! |
| ! P0 ! Selected P0 (Ambient Pressure) ! |
| ! 999 ! ECU (0 to 20.0 psia) ! |
| ! ! Engine 1 7C.1.114.01 ! |
| ! ! Engine 2 7C.2.114.10 ! |
| !--------------!------------------------------------------------------! |
| ! O/F (OF) ! Oil and Fuel Filter Clogged ! |
| ! ! 1 1 ! |
| ! ! ! ! ! |
| ! ! ! !________Fuel filter clogged = 0 ! |
| ! ! ! Fuel filter not clogged = 1 ! |
| ! ! !___________Oil filter clogged = 0 ! |
| ! ! Oil filter not clogged = 1 ! |
| ! ! SDAC Engine 1 29.1.001.01.16 Oil filter ! |
| ! ! 29.2.001.01.16 ! |
| ! ! Engine 2 29.1.001.10.16 Oil filter ! |
| ! ! 29.2.001.10.16 ! |
| ! ! SDAC Engine 1 29.1.001.01.17 Fuel filter ! |
| ! ! 29.2.001.01.17 ! |
| ! ! Engine 2 29.1.001.10.17 Fuel filter ! |
| ! ! 29.2.001.10.17 ! |
| !--------------!------------------------------------------------------! |
| ! ECW2 ! Engine Control Word 2 ! |
| ! XXXXX ! Each 'X' represents 4 Bits in hexadecimal code of ! |
| ! ! a defined ARINC 429 word: ! |
| ! ! XXXXX Bits HEX ! |
| ! ! !!!!!___________ 14, 13, 12, 11 0...F ! |
| ! ! !!!!____________ 18, 17, 16, 15 0...F ! |
| ! ! !!!_____________ 22, 21, 20, 19 0...F ! |
| ! ! !!______________ 26, 25, 24, 23 0...F ! |
| ! ! !_______________ 29, 28, 27 0...7 ! |
| ! ! System SDI ! |
| ! ! Engine 1 1 01 ! |
| ! ! Engine 2 2 10 ! |
| ! ! Bit Label Parameter Description ! |
| ! ! 11 7C.X.272.XX.12 = 1 Bump/Overboost #1 enable ! |
| ! ! 12 7C.X.272.XX.13 = 1 Bump/Overboost #2 enable ! |
| ! ! 13 7C.X.272.XX.14 = 1 Bump/Overboost #3 enable ! |
| ! ! 14 7C.X.272.XX.22 = 1 MTO. GA limit mode ! |
| ! ! selection ! |
| ! ! 15 7C.X.272.XX.23 = 1 Flex Take-Off limit mode ! |
| ! ! selection ! |
| ! ! 16 SPARE ! |
| ! ! 17 SPARE ! |
| ! ! 18 SPARE ! |
| ! ! 19 SPARE ! |
| ! ! 20 SPARE ! |
| ! ! 21 SPARE ! |
| ! ! 22 SPARE ! |
| ! ! 23 SPARE ! |
| ! ! 24 SPARE ! |
| ! ! 25 SPARE ! |
| ! ! 26 SPARE ! |
| ! ! 27 SPARE ! |
| ! ! 28 SPARE ! |
| ! ! 29 SPARE ! |
| !--------------!------------------------------------------------------! |
| ! PSEL ! Status of different FADEC sensors ! |
| ! XXXX ! X X X X Label: Selected: ! |
| ! ! ! ! ! !_____211 TAT (Bit 11 -> 15) ! |
| ! ! ! ! !_______344 N2 actual (Bit 11 -> 15) ! |
| ! ! ! !_________345 EGT (Bit 11 -> 15) ! |
| ! ! !___________346 N1 actual (Bit 11 -> 15) ! |
| ! ! Source: ECU, different labels ! |
| ! ! NOTE: The shown values are coded as follows: ! |
| ! ! Bit: 15 14 13 12 11 ! Shown value ! |
| ! ! --------------------!---------------- ! |
| ! ! 0 0 0 0 0 ! 0 ! |
| ! ! 0 0 0 0 1 ! 1 ! |
| ! ! 0 0 0 1 0 ! 2 ! |
| ! ! 0 0 0 1 1 ! 3 ! |
| ! ! 0 0 1 0 0 ! 4 ! |
| ! ! 0 0 1 0 1 ! 5 ! |
| ! ! 0 0 1 1 0 ! 6 ! |
| ! ! 0 0 1 1 1 ! 7 ! |
| ! ! 0 1 0 0 0 ! 8 ! |
| ! ! 0 1 0 0 1 ! 9 ! |
| ! ! 0 1 0 1 0 ! A ! |
| ! ! 0 1 0 1 1 ! B ! |
| ! ! 0 1 1 0 0 ! C ! |
| ! ! 0 1 1 0 1 ! D ! |
| ! ! 0 1 1 1 0 ! E ! |
| ! ! 0 1 1 1 1 ! F ! |
| ! ! 1 0 0 0 0 ! G ! |
| ! ! 1 0 0 0 1 ! H ! |
| ! ! 1 0 0 1 0 ! I ! |
| ! ! 1 0 0 1 1 ! J ! |
| ! ! 1 0 1 0 0 ! K ! |
| ! ! 1 0 1 0 1 ! L ! |
| ! ! 1 0 1 1 0 ! M ! |
| ! ! 1 0 1 1 1 ! N ! |
| ! ! 1 1 0 0 0 ! O ! |
| ! ! 1 1 0 0 1 ! P ! |
| ! ! 1 1 0 1 0 ! Q ! |
| ! ! 1 1 0 1 1 ! R ! |
| ! ! 1 1 1 0 0 ! S ! |
| ! ! 1 1 1 0 1 ! T ! |
| ! ! 1 1 1 1 0 ! U ! |
| ! ! 1 1 1 1 1 ! V ! |
| ! ! ! |
| !--------------!------------------------------------------------------! |
| ! FT ! Fuel Temperature Inner Cell ! |
| ! X999 ! (-55.0 to 170.0 °C) ! |
| ! ! FQIC 5A.2.177.10 Left Inner Cell Fuel Temp. ! |
| ! ! 5A.2.201.10 Right Inner Cell Fuel Temp. ! |
| ! ! Remark: Report line X1 indicates Left Inner Cell ! |
| ! ! Fuel Temp ! |
| ! ! Report line X2 indicates Right Inner Cell ! |
| ! ! Fuel Temp. ! |
| !--------------!------------------------------------------------------! |
| ! RALT ! Radio Height ! |
| ! X999 ! (-20 to 2500 ft) ! |
| ! ! ! |
| ! ! DMC 25.1.164.01 Radio Altimeter #1 printed in ! |
| ! ! 25.2.164.01 report line X1 ! |
| ! ! ! |
| ! ! 25.1.164.10 Radio Altimeter #2 printed in ! |
| ! ! 25.2.164.10 report line X2 ! |
| ! ! Negative values are indicated by 'N' on the first ! |
| ! ! position. Otherwise the first position is used for ! |
| ! ! the value. ! |
| +---------------------------------------------------------------------+ |
(8) Parameter Logic
| +---------------------------------------------------------------------+ |
| ! Param. ! Print Value (Standard Progr.) ! |
| !--------------!------------------------------------------------------! |
| ! ESN ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! EHRS ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! ERT ! Value at moment of trigger ! |
| !--------------! -----------------------------------------------------! |
| ! ECYC ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! AP ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! T/O Sum ! Value 'Y04.3' seconds after entry PH4. ! |
| !--------------!------------------------------------------------------! |
| ! EGTM ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! N1 ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! N1C ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! N2 ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! EGT ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! FF ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! P3 ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! N1MX ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! T3 ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! T25 ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! T12 ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! PO ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! T5 ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! VSV ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! VBV ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! VN ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! VL ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! PHA ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! PHT ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! VC ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! VH ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! EVM ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! OIP ! Arithmetic average for 'Y04.2' seconds ! |
| !--------------!------------------------------------------------------! |
| ! OIT ! Arithmetic average for 'Y04.2' seconds ! |
| !--------------!------------------------------------------------------! |
| ! O/F ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! ECW1 ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! ECW2 ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! PSEL ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! PT2 ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! FT ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! HPT ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! LPT ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! RALT ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
(9) Parameter Logic
| +---------------------------------------------------------------------+ |
| ! Param. ! Print Value (Standard Progr.) ! |
| !--------------!------------------------------------------------------! |
| ! ESN ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! EHRS ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! ERT ! Value at moment of trigger ! |
| !--------------! -----------------------------------------------------! |
| ! ECYC ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! AP ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! T/O Sum ! Value 'Y04.3' seconds after entry PH4. ! |
| !--------------!------------------------------------------------------! |
| ! EGTM ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! N1 ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! N1C ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! N2 ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! EGT ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! FF ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! P3 ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! N1MX ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! T3 ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! T25 ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! T12 ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! PO ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! T5 ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! VSV ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! VBV ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! VN ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! VL ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! PHA ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! PHT ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! VC ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! VH ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! EVM ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! OIP ! Arithmetic average for 'Y04.2' seconds ! |
| !--------------!------------------------------------------------------! |
| ! OIT ! Arithmetic average for 'Y04.2' seconds ! |
| !--------------!------------------------------------------------------! |
| ! O/F ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! ECW1 ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! ECW2 ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! PSEL ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! PT2 ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! FT ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! HPT ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! LPT ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! RALT ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
(10) Engine Take Off Report Logic <04> (Engine Type CFMI with Advanced EVMU)
| +----------------------------------------------------------------------+ |
| !Code!Item ! !Progr.!Standard ! |
| ! No.!No. ! Description of Function Item !MCDU !Value or ! |
| ! ! ! !GSE !Table ! |
| !----!------!-----------------------------------------!------!---------! |
| ! !A ! Report Format ! ! ! |
| ! !B ! Parameter Table ! ! ! |
| ! !C ! First three lines of Report ! C ! Blank ! |
| ! !D ! Print-out Rules ! C ! 2 ! |
| ! !E ! Transfer to ACARS MU ! C ! No ! |
| ! !F ! Increment of the report counter if the ! C ! 1 ! |
| ! ! ! report was triggered by a code number ! ! ! |
| ! ! ! > 1000; 1=yes, 0=no ! ! ! |
| ! !G ! 'Y04.2' Average intervals in seconds ! C ! 2 ! |
| ! ! ! for OIT, OIP, VB1, VB2 and PHA. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !1000!1 ! Manual selection via MCDU ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !2000!2 ! Flight phase dependent manual ! ! ! |
| ! ! ! selection via remote print button ! ! ! |
| ! ! ! if programmed. ! ! ! |
| ! !2.1 ! Remote Print Button assignment. ! C ! not ! |
| !----!------!-----------------------------------------!------!---------! |
| !3000!3 ! Programmable Start Logic ! ! ! |
| ! !3.1 ! Trigger condition ! C ! not ! |
| !----!------!-----------------------------------------!------!---------! |
| !4000!4 ! The report is generated and stored every! ! ! |
| ! ! ! 'F04' Take-Off and is triggered when, ! ! ! |
| ! ! ! during a searching time period of 20 ! ! ! |
| ! ! ! seconds, the sum of the EGT of both ! ! ! |
| ! ! ! engines is maximal. The searching time ! ! ! |
| ! ! ! period is started 'Y04.1' seconds after ! ! ! |
| ! ! ! entering flight phase 4. ! ! ! |
| ! ! ! ! ! ! |
| ! !4.1 ! The report is postponed to the next ! ! ! |
| ! ! ! flight leg if at least one of the EGT ! ! ! |
| ! ! ! values on Eng.1 or Eng.2 is below EGTL ! ! ! |
| ! ! ! at the moment when the starter air valve! ! ! |
| ! ! ! switched from closed position to open ! ! ! |
| ! ! ! position at engine start. ! ! ! |
| ! ! ! Starter Air Valve open: ! ! ! |
| ! ! ! Eng.1 param. 7C.1.270.01.13 = 1 ! ! ! |
| ! ! ! Eng.2 param. 7C.2.270.10.13 = 1 ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! or ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! if the Wing Anti-Ice Status or the Na- ! ! ! |
| ! ! ! celle Anti-Ice Status is switched during! ! ! |
| ! ! ! the search time period. ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! Wing Anti-Ice Valve closed: ! ! ! |
| ! ! ! param. 29.1.001.00.18 = 0 right hand ! ! ! |
| ! ! ! 29.2.001.00.18 = 0 right hand ! ! ! |
| ! ! ! param. 29.1.001.11.18 = 0 left hand ! ! ! |
| ! ! ! 29.2.001.11.18 = 0 left hand ! ! ! |
| ! ! ! Nacelle Anti-Ice Valve closed: ! ! ! |
| ! ! ! Eng.1 param. 5D.2.061.10.28 = 0 ! ! ! |
| ! ! ! Eng.2 param. 5D.2.061.10.27 = 0 ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !4100!4.1.1 ! The same rules as described for Log. No.! C ! disarmed! |
| ! ! ! 4000 is valid and in addition the report! ! ! |
| ! ! ! is postponed when the Wing Anti-Ice ! ! ! |
| ! ! ! Status or Nacelle Anti-Ice Status is ! ! ! |
| ! ! ! open during the search time period. This! ! ! |
| ! ! ! trigger condition is basically disarmed ! ! ! |
| ! ! ! and can be armed via a GSE programmable.! ! ! |
| ! ! ! ! ! ! |
| ! !4.2 ! The report trigger logic is restarted in! ! ! |
| ! ! ! flight leg 'F04+n' (n=1, 2, ..F04) after! ! ! |
| ! ! ! no report generation in the previous leg! ! ! |
| ! ! ! 'F04+ (n-1)'. ! ! ! |
| ! ! ! ! ! ! |
| ! !4.3 ! EGTL = EGT + TAT ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.4 ! 'F04' Take Off ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.5 ! 'Y04.1' seconds after PH 4 entry ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.6 ! T/O delta N1 summary limits ! ! ! |
| ! ! ! delta N1 = N1MX - N1 ! ! ! |
| ! ! ! N1MX = 7C.1.342.01 Eng.1 ! ! ! |
| ! ! ! 7C.2.342.10 Eng.2 ! ! ! |
| ! ! ! N1 = 7C.1.346.01 Eng.1 ! ! ! |
| ! ! ! 7C.2.346.10 Eng.2 ! ! ! |
| ! ! ! ! ! ! |
| ! !4.7.1 ! delta N1 > 10 % rpm ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.7.2 ! delta N1 > 8 % rpm and =/< 10 % rpm ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.7.3 ! delta N1 > 6 % rpm and =/< 8 % rpm ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.7.4 ! delta N1 > 4 % rpm and =/< 6 % rpm ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.7.5 ! delta N1 > 2 % rpm and =/< 4 % rpm ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.7.6 ! delta N1 > 0.2 % rpm and =/< 2 % rpm ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.7.7 ! delta N1 =/< 0.2 % ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! ! ! ! ! ! |
| ! !4.8 ! The calculation is made 'Y04.3' seconds ! ! ! |
| ! ! ! after entry into flight phase 4. ! ! ! |
| ! ! ! ! ! ! |
| ! !4.8.1 ! 'Y04.3' seconds after PH 4 entry. ! C ! limit- ! |
| ! ! ! ! ! table ! |
| !----!------!-----------------------------------------!------!---------! |
| !5001!5 ! Each time when a report is generated by ! ! ! |
| !5002! ! this logic the number (X04) is decremen-! ! ! |
| !5003! ! ted until zero is reached. The condi- ! ! ! |
| !5004! ! tions are described under code No. 4000/! ! ! |
| !5005! ! 4001 (without item 4.2). ! ! ! |
| !. ! ! ! ! ! |
| !. ! ! The number (X04) is programmable. ! ! ! |
| !. ! ! ! ! ! |
| !. ! ! In case of change of the engine serial ! ! ! |
| !500X! ! number, (X04) are automatically set to ! ! ! |
| ! ! ! five. ! ! ! |
| ! ! ! The code is shown in an increasing ! ! ! |
| ! ! ! order, i.e. the first report have the ! ! ! |
| ! ! ! code 5001, the next code is 5002 and so ! ! ! |
| ! ! ! on until 5005 is reached. ! ! ! |
| ! ! ! ! ! ! |
| ! !5.1 ! Number 'X04' for consecutive legs up to ! C ! limit- ! |
| ! ! ! 9. ! ! table ! |
| ! !5.2 ! Number 'X04' in case of ESN change. ! ! 5 ! |
| ! ! ! ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !8100!8.1 ! ACARS MU uplink request with IMI 'REQ04'! ! ! |
| ! ! ! The report <04> is immediately generated! ! ! |
| ! ! ! and transmitted to the ACARS MU. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !8200!8.2 ! ACARS MU uplink request with IMI 'G04' ! ! ! |
| ! ! ! The report <04> is generated as the next! ! ! |
| ! ! ! take-off according to code 4000 or 4100 ! ! ! |
| ! ! ! depending on which logic is armed. ! ! ! |
| !----------------------------------------------------------------------! |
| ! A = Programmable by Airbus ! |
| ! C = Programmable by Customer ! |
| +----------------------------------------------------------------------+ |
(11) Engine Take Off Report Logic <04> (Engine Type CFMI with Advanced EVMU)
| +----------------------------------------------------------------------+ |
| !Code!Item ! !Progr.!Standard ! |
| ! No.!No. ! Description of Function Item !------!Value or ! |
| ! ! ! !MCDU/ !Table TXY! |
| ! ! ! !GSE ! ! |
| !----!------!-----------------------------------------!------!---------! |
| ! !A ! Report Format ! ! ! |
| ! !A.1 ! "R004RLID" Report Layout Identifier ! ! 01 ! |
| ! ! ! (for ACARS header) ! ! ! |
| ! !A.2 ! "R004RLIS" Report Layout Issue ! ! 01 ! |
| ! ! ! (for ACARS header) ! ! ! |
| ! !B ! Parameter Table ! ! ! |
| ! !C ! First Three lines of Report ! C ! Blank ! |
| ! !D ! Print-out Rules ! C ! See ! |
| ! ! ! ! ! separate! |
| ! ! ! ! ! list ! |
| ! !E ! Transfer to ACARS MU ! C ! see ! |
| ! ! ! ! ! separate! |
| ! ! ! ! ! list ! |
| ! !F ! Increment of the report counter if the ! C ! 1 ! |
| ! ! ! report was triggered by a code number ! ! ! |
| ! ! ! > 1000; 1=yes, 0=no ! ! ! |
| ! !G ! "Y04.2" Average intervals in seconds ! C ! 2 ! |
| ! ! ! for OIT, OIP ! ! ! |
| ! ! ! The data is averaged over the last Y04.2! ! ! |
| ! ! ! second interval before trigger time. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !1000!1 ! Manual selection through MCDU ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !2000!2 ! Flight phase dependent manual ! ! ! |
| ! ! ! selection through remote print button ! ! ! |
| ! ! ! if programmed. ! ! ! |
| ! !2.1 ! Remote Print Button assignment. ! C ! not ! |
| ! ! ! ! ! assigned! |
| !----!------!-----------------------------------------!------!---------! |
| !3000!3 ! Programmable Start Logic ! ! ! |
| ! !3.1 ! Trigger condition ! C ! not ! |
| ! ! ! ! ! progr. ! |
| !----!------!-----------------------------------------!------!---------! |
| !4000!4 ! The report is generated and stored every! ! ! |
| ! ! ! "F04"th Take-Off and is triggered when, ! ! ! |
| ! ! ! during a searching time period of 20 ! ! ! |
| ! ! ! seconds, the sum of the EGT of both ! ! ! |
| ! ! ! engines is maximal. The searching time ! ! ! |
| ! ! ! period is started "Y04.1" seconds after ! ! ! |
| ! ! ! entering flight phase 4. ! ! ! |
| ! ! ! The trigger stays armed during flight ! ! ! |
| ! ! ! phase 5. ! ! ! |
| ! ! ! ! ! ! |
| ! !4.1 ! The report is postponed to the next ! ! ! |
| ! ! ! flight leg if at least one of the EGT ! ! ! |
| ! ! ! values on Eng.1 or Eng.2 is below EGTL ! ! ! |
| ! ! ! at the moment when the starter air valve! ! ! |
| ! ! ! switches from the closed position to the! ! ! |
| ! ! ! open position at engine start. ! ! ! |
| ! ! ! Starter Air Valve open: ! ! ! |
| ! ! ! Eng.1 param. 7C.1.270.01.13 = 1 ! ! ! |
| ! ! ! Eng.2 param. 7C.2.270.10.13 = 1 ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! or ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! if the Wing Anti-Ice Status or the Na- ! ! ! |
| ! ! ! celle Anti-Ice Status is switched during! ! ! |
| ! ! ! the search time period. ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! Wing Anti-Ice Valve closed: ! ! ! |
| ! ! ! 29.1.001.00.18 = 0 right hand ! ! ! |
| ! ! ! 29.2.001.00.18 = 0# ! ! ! |
| ! ! ! 29.1.001.11.18 = 0 left hand ! ! ! |
| ! ! ! 29.2.001.11.18 = 0# ! ! ! |
| ! ! ! Nacelle Anti-Ice Valve closed: ! ! ! |
| ! ! ! Eng.1 param. 5D.2.061.10.28 = 0 ! ! ! |
| ! ! ! Eng.2 param. 5D.2.061.10.27 = 0 ! ! ! |
| !4100!4.1.1 ! The same rules as described for Log. No.! C ! disarmed! |
| ! ! ! 4000 are valid and in addition the ! ! ! |
| ! ! ! report is postponed when the Wing ! ! ! |
| ! ! ! Anti-Ice Status or the Nacelle Anti-Ice ! ! ! |
| ! ! ! Status is open during the search time ! ! ! |
| ! ! ! period. This trigger condition is ! ! ! |
| ! ! ! basically disarmed and can be armed ! ! ! |
| ! ! ! through a GSE programming. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| ! !4.2 ! The report trigger logic is restarted in! ! ! |
| ! ! ! flight leg "F04+n" (n=1, 2, ..F04) after! ! ! |
| ! ! ! no report generation in the previous leg! ! ! |
| ! ! ! 'F04+ (n-1)'. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| ! !4.3 ! EGTL ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.4 ! "F04"th Take Off ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.5 ! "Y04.1" seconds after PH 4 entry ! C ! limit- ! |
| ! ! table ! |
| ! !4.6 ! T/O delta N1 summary limits ! ! ! |
| ! ! ! delta N1 = N1MX - N1 ! ! ! |
| ! ! ! N1MX = 7C.1.342.01 Eng.1 ! ! ! |
| ! ! ! 7C.2.342.10 Eng.2 ! ! ! |
| ! ! ! N1 = 7C.1.346.01 Eng.1 ! ! ! |
| ! ! ! 7C.2.346.10 Eng.2 ! ! ! |
| ! ! ! ! ! ! |
| ! !4.7.1 ! delta N1 >10 %rpm ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.7.2 ! delta N1> 8 %rpm and <= 10 %rpm ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.7.3 ! delta N1 >6 %rpm and <= 8 %rpm ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.7.4 ! delta N1 >4 %rpm and <= 6 %rpm ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.7.5 ! delta N1 >2 %rpm and <= 4 %rpm ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.7.6 ! delta N1 >0.2 %rpm and <=2 %rpm ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.7.7 ! delta N1 <0.2 %rpm ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.8 ! The calculation is made "Y04.3" seconds ! ! ! |
| ! ! ! after entry into flight phase 4. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| ! !4.8.1 ! "Y04.3" seconds after PH 4 entry. ! C ! limit- ! |
| ! ! ! ! ! table ! |
| !----!------!-----------------------------------------!------!---------! |
| !5001!5 ! Each time when a report is generated by ! ! ! |
| !5002! ! this logic the number "X04" is decreased! ! ! |
| !5003! ! until zero is reached. The conditions ! ! ! |
| !5004! ! are described under code No. 4000/4100 ! ! ! |
| !5005! ! (without item 4.2). ! ! ! |
| !. ! ! ! ! ! |
| !. ! ! The number (X04) is programmable. ! ! ! |
| !. ! ! ! ! ! |
| !. ! ! In case of change of the engine serial ! ! ! |
| !. ! ! number, (X04) are automatically set to ! ! ! |
| !. ! ! five. ! ! ! |
| !500X! ! The code is shown in an increasing ! ! ! |
| ! ! ! order, i.e. the first report has the ! ! ! |
| ! ! ! code 5001, the next code is 5002 and so ! ! ! |
| ! ! ! on until 5005 is reached. ! ! ! |
| ! ! ! ! ! ! |
| ! !5.1 ! Number "X04" for consecutive legs up to ! C ! limit- ! |
| ! ! ! 9. ! ! table ! |
| ! !5.2 ! Number "X04" in case of ESN change. ! ! 5 ! |
| ! ! ! ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !8100!8.1 ! ACARS MU uplink request with IMI ! ! ! |
| ! ! ! "REQ04": ! ! ! |
| ! ! ! The report <04> is immediately generated! ! ! |
| ! ! ! and transmitted to the ACARS MU. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !8200!8.2 ! ACARS MU uplink request with IMI "G04": ! ! ! |
| ! ! ! The report <04> is generated as the next! ! ! |
| ! ! ! take-off according to code 4000 or 4100 ! ! ! |
| ! ! ! depending on which logic is armed. ! ! ! |
| !----------------------------------------------------------------------! |
| ! A = Programmable by Airbus ! |
| ! C = Programmable by Customer ! |
| +----------------------------------------------------------------------+ |
(12) Engine Take Off Report Logic <04> (Engine Type CFMI with Advanced EVMU)
| +----------------------------------------------------------------------+ |
| !Code!Item ! !Progr.!Standard ! |
| ! No.!No. ! Description of Function Item !MCDU !Value or ! |
| ! ! ! !/GSE !Table TXY! |
| !----!------!-----------------------------------------!------!---------! |
| ! !A ! Report Format ! ! ! |
| ! !B ! Parameter Table ! ! ! |
| ! !C ! First three lines of Report ! C ! Blank ! |
| ! !D ! Print-out Rules ! C ! See ! |
| ! ! ! ! ! separate! |
| ! ! ! ! ! list ! |
| ! !E ! Transfer to ACARS MU ! C ! see ! |
| ! ! ! ! ! separate! |
| ! ! ! ! ! list ! |
| ! !F ! Increment of the report counter if the ! C ! 1 ! |
| ! ! ! report was triggered by a code number ! ! ! |
| ! ! ! > 1000; 1=yes, 0=no ! ! ! |
| ! !G ! 'Y04.2' Average intervals in seconds ! C ! 2 ! |
| ! ! ! for OIT, OIP, VB1, VB2 and PHA. ! ! ! |
| ! ! ! Data shall be averaged over the last ! ! ! |
| ! ! ! Y04.2 second interval before trigger ! ! ! |
| ! ! ! time. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !1000!1 ! Manual selection via MCDU ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !2000!2 ! Flight phase dependent manual ! ! ! |
| ! ! ! selection via remote print button ! ! ! |
| ! ! ! if programmed. ! ! ! |
| ! !2.1 ! Remote Print Button assignment. ! C ! not ! |
| ! ! ! ! ! assigned! |
| !----!------!-----------------------------------------!------!---------! |
| !3000!3 ! Programmable Start Logic ! ! ! |
| ! !3.1 ! Trigger condition ! C ! not ! |
| ! ! ! ! ! progr. ! |
| !----!------!-----------------------------------------!------!---------! |
| !4000!4 ! The report is generated and stored every! ! ! |
| ! ! ! 'F04'th Take-Off and is triggered when, ! ! ! |
| ! ! ! during a searching time period of 20 ! ! ! |
| ! ! ! seconds, the sum of the EGT of both ! ! ! |
| ! ! ! engines is maximal. The searching time ! ! ! |
| ! ! ! period is started 'Y04.1' seconds after ! ! ! |
| ! ! ! entering flight phase 4. ! ! ! |
| ! ! ! The trigger stays armed during flight ! ! ! |
| ! ! ! phase 5. ! ! ! |
| ! ! ! ! ! ! |
| ! !4.1 ! The report is postponed to the next ! ! ! |
| ! ! ! flight leg if at least one of the EGT ! ! ! |
| ! ! ! values on Eng.1 or Eng.2 is below EGTL ! ! ! |
| ! ! ! at the moment when the starter air valve! ! ! |
| ! ! ! switches from the closed position to the! ! ! |
| ! ! ! open position at engine start. ! ! ! |
| ! ! ! Starter Air Valve open: ! ! ! |
| ! ! ! Eng.1 param. 7C.1.270.01.13 = 1 ! ! ! |
| ! ! ! Eng.2 param. 7C.2.270.10.13 = 1 ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! or ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! if the Wing Anti-Ice Status or the Na- ! ! ! |
| ! ! ! celle Anti-Ice Status is switched during! ! ! |
| ! ! ! the search time period. ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! Wing Anti-Ice Valve closed: ! ! ! |
| ! ! ! 29.1.001.00.18 = 0 right hand ! ! ! |
| ! ! ! 29.2.001.00.18 = 0 ! ! ! |
| ! ! ! 29.1.001.11.18 = 0 left hand ! ! ! |
| ! ! ! 29.2.001.11.18 = 0 ! ! ! |
| ! ! ! Nacelle Anti-Ice Valve closed: ! ! ! |
| ! ! ! Eng.1 param. 5D.2.061.10.28 = 0 ! ! ! |
| ! ! ! Eng.2 param. 5D.2.061.10.27 = 0 ! ! ! |
| !4100!4.1.1 ! The same rules as described for Log. No.! C ! disarmed! |
| ! ! ! 4000 are valid and in addition the ! ! ! |
| ! ! ! report is postponed when the Wing ! ! ! |
| ! ! ! Anti-Ice Status or the Nacelle Anti-Ice ! ! ! |
| ! ! ! Status is open during the search time ! ! ! |
| ! ! ! period. This trigger condition is ! ! ! |
| ! ! ! basically disarmed and can be armed via ! ! ! |
| ! ! ! a GSE programming. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| ! !4.2 ! The report trigger logic is restarted in! ! ! |
| ! ! ! flight leg 'F04+n' (n=1, 2, ..F04) after! ! ! |
| ! ! ! no report generation in the previous leg! ! ! |
| ! ! ! 'F04+ (n-1)'. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| ! !4.3 ! EGTL ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.4 ! 'F04'th Take Off ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.5 ! 'Y04.1' seconds after PH 4 entry ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.6 ! T/O delta N1 summary limits ! ! ! |
| ! ! ! delta N1 = N1MX - N1 ! ! ! |
| ! ! ! N1MX = 7C.1.342.01 Eng.1 ! ! ! |
| ! ! ! 7C.2.342.10 Eng.2 ! ! ! |
| ! ! ! N1 = 7C.1.346.01 Eng.1 ! ! ! |
| ! ! ! 7C.2.346.10 Eng.2 ! ! ! |
| ! ! ! ! ! ! |
| ! !4.7.1 ! delta N1 >10 %rpm ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.7.2 ! 8 < delta N1 <= 10 %rpm ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.7.3 ! 6 < delta N1 <= 8 %rpm ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.7.4 ! 4 < delta N1 <= 6 %rpm ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.7.5 ! 2 < delta N1 <= 4 %rpm ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.7.6 ! 0.2 < delta N1 <= 2 %rpm ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.7.7 ! delta N1 <= 0.2 %rpm ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.8 ! The calculation is made 'Y04.3' seconds ! ! ! |
| ! ! ! after entry into flight phase 4. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| ! !4.8.1 ! 'Y04.3' seconds after PH 4 entry. ! C ! limit- ! |
| ! ! ! ! ! table ! |
| !----!------!-----------------------------------------!------!---------! |
| !5001!5 ! Each time when a report is generated by ! ! ! |
| !5002! ! this logic the number 'X04' is decreased! ! ! |
| !5003! ! until zero is reached. The conditions ! ! ! |
| !5004! ! are described under code No. 4000/4100 ! ! ! |
| ! ! ! (without item 4.2). ! ! ! |
| ! ! ! ! ! ! |
| !5005! ! The number (X04) is programmable. ! ! ! |
| !. ! ! ! ! ! |
| !. ! ! In case of change of the engine serial ! ! ! |
| !. ! ! number, (X04) are automatically set to ! ! ! |
| !. ! ! five. ! ! ! |
| !500X! ! The code is shown in an increasing ! ! ! |
| ! ! ! order, i.e. the first report has the ! ! ! |
| ! ! ! code 5001, the next code is 5002 and so ! ! ! |
| ! ! ! on until 5005 is reached. ! ! ! |
| ! ! ! ! ! ! |
| ! !5.1 ! Number 'X04' for consecutive legs up to ! C ! limit- ! |
| ! ! ! 9. ! ! table ! |
| ! !5.2 ! Number 'X04' in case of ESN change. ! ! 5 ! |
| ! ! ! ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !8100!8.1 ! ACARS MU uplink request with IMI ! ! ! |
| ! ! ! 'REQ04': ! ! ! |
| ! ! ! The report <04> is immediately generated! ! ! |
| ! ! ! and transmitted to the ACARS MU. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !8200!8.2 ! ACARS MU uplink request with IMI 'G04': ! ! ! |
| ! ! ! The report <04> is generated as the next! ! ! |
| ! ! ! take-off according to code 4000 or 4100 ! ! ! |
| ! ! ! depending on which logic is armed. ! ! ! |
| !----------------------------------------------------------------------! |
| ! A = Programmable by Airbus ! |
| ! C = Programmable by Customer ! |
| +----------------------------------------------------------------------+ |
(13) Engine Take Off Report Logic <04> (Engine Type CFMI with Advanced EVMU)
| +----------------------------------------------------------------------+ |
| !Code!Item ! !Progr.!Standard ! |
| ! No.!No. ! Description of Function Item !MCDU !Value or ! |
| ! ! ! !/GSE !Table TXY! |
| !----!------!-----------------------------------------!------!---------! |
| ! !A ! Report Format ! ! ! |
| ! !B ! Parameter Table ! ! ! |
| ! !C ! First three lines of Report ! C ! Blank ! |
| ! !D ! Print-out Rules ! C ! See ! |
| ! ! ! ! ! separate! |
| ! ! ! ! ! list ! |
| ! !E ! Transfer to ACARS MU ! C ! see ! |
| ! ! ! ! ! separate! |
| ! ! ! ! ! list ! |
| ! !F ! Increment of the report counter if the ! C ! 1 ! |
| ! ! ! report was triggered by a code number ! ! ! |
| ! ! ! > 1000; 1=yes, 0=no ! ! ! |
| ! !G ! 'Y04.2' Average intervals in seconds ! C ! 2 ! |
| ! ! ! for OIT, OIP, VB1, VB2 and PHA. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !1000!1 ! Manual selection via MCDU ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !2000!2 ! Flight phase dependent manual ! ! ! |
| ! ! ! selection via remote print button ! ! ! |
| ! ! ! if programmed. ! ! ! |
| ! !2.1 ! Remote Print Button assignment. ! C ! not ! |
| ! ! ! ! ! assigned! |
| !----!------!-----------------------------------------!------!---------! |
| !3000!3 ! Programmable Start Logic ! ! ! |
| ! !3.1 ! Trigger condition ! C ! not ! |
| ! ! ! ! ! progr. ! |
| !----!------!-----------------------------------------!------!---------! |
| !4000!4 ! The report is generated and stored every! ! ! |
| ! ! ! 'F04'th Take-Off and is triggered when, ! ! ! |
| ! ! ! during a searching time period of 20 ! ! ! |
| ! ! ! seconds, the sum of the EGT of both ! ! ! |
| ! ! ! engines is maximal. The searching time ! ! ! |
| ! ! ! period is started 'Y04.1' seconds after ! ! ! |
| ! ! ! entering flight phase 4. ! ! ! |
| ! ! ! The trigger stays armed during flight ! ! ! |
| ! ! ! phase 5. ! ! ! |
| ! ! ! ! ! ! |
| ! !4.1 ! The report is postponed to the next ! ! ! |
| ! ! ! flight leg if at least one of the EGT ! ! ! |
| ! ! ! values on Eng.1 or Eng.2 is below EGTL ! ! ! |
| ! ! ! at the moment when the starter air valve! ! ! |
| ! ! ! switches from the closed position to the! ! ! |
| ! ! ! open position at engine start. ! ! ! |
| ! ! ! Starter Air Valve open: ! ! ! |
| ! ! ! Eng.1 param. 7C.1.270.01.13 = 1 ! ! ! |
| ! ! ! Eng.2 param. 7C.2.270.10.13 = 1 ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! or ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! if the Wing Anti-Ice Status or the Na- ! ! ! |
| ! ! ! celle Anti-Ice Status is switched during! ! ! |
| ! ! ! the search time period. ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! Wing Anti-Ice Valve closed: ! ! ! |
| ! ! ! 29.1.001.00.18 = 0 right hand ! ! ! |
| ! ! ! 29.2.001.00.18 = 0 ! ! ! |
| ! ! ! 29.1.001.11.18 = 0 left hand ! ! ! |
| ! ! ! 29.2.001.11.18 = 0 ! ! ! |
| ! ! ! Nacelle Anti-Ice Valve closed: ! ! ! |
| ! ! ! Eng.1 param. 5D.2.061.10.28 = 0 ! ! ! |
| ! ! ! Eng.2 param. 5D.2.061.10.27 = 0 ! ! ! |
| !4100!4.1.1 ! The same rules as described for Log. No.! C ! disarmed! |
| ! ! ! 4000 are valid and in addition the ! ! ! |
| ! ! ! report is postponed when the Wing ! ! ! |
| ! ! ! Anti-Ice Status or the Nacelle Anti-Ice ! ! ! |
| ! ! ! Status is open during the search time ! ! ! |
| ! ! ! period. This trigger condition is ! ! ! |
| ! ! ! basically disarmed and can be armed via ! ! ! |
| ! ! ! a GSE programmable. ! ! ! |
| ! ! ! ! ! ! |
| ! !4.2 ! The report trigger logic is restarted in! ! ! |
| ! ! ! flight leg 'F04+n' (n=1, 2, ..F04) after! ! ! |
| ! ! ! no report generation in the previous leg! ! ! |
| ! ! ! 'F04+ (n-1)'. ! ! ! |
| ! ! ! ! ! ! |
| ! !4.3 ! EGTL ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.4 ! 'F04'th Take Off ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.5 ! 'Y04.1' seconds after PH 4 entry ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.6 ! T/O delta N1 summary limits ! ! ! |
| ! ! ! delta N1 = N1MX - N1 ! ! ! |
| ! ! ! N1MX = 7C.1.342.01 Eng.1 ! ! ! |
| ! ! ! 7C.2.342.10 Eng.2 ! ! ! |
| ! ! ! N1 = 7C.1.346.01 Eng.1 ! ! ! |
| ! ! ! 7C.2.346.10 Eng.2 ! ! ! |
| ! ! ! ! ! ! |
| ! !4.7.1 ! delta N1 >10 %rpm ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.7.2 ! delta N1 >8 %rpm and <= 10 %rpm ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.7.3 ! delta N1 >6 %rpm and <= 8 %rpm ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.7.4 ! delta N1 >4 %rpm and <= 6 %rpm ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.7.5 ! delta N1 >2 %rpm and <= 4 %rpm ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.7.6 ! delta N1 >0.2 %rpm and <= 10 %rpm ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.7.7 ! delta N1 <=0.2 %rpm ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.8 ! The calculation is made 'Y04.3' seconds ! ! ! |
| ! ! ! after entry into flight phase 4. ! ! ! |
| ! ! ! ! ! ! |
| ! !4.8.1 ! 'Y04.3' seconds after PH 4 entry. ! C ! limit- ! |
| ! ! ! ! ! table ! |
| !----!------!-----------------------------------------!------!---------! |
| !5001!5 ! Each time when a report is generated by ! ! ! |
| !5002! ! this logic the number 'X04' is decreased! ! ! |
| !5003! ! until zero is reached. The conditions ! ! ! |
| !5004! ! are described under code No. 4000/4001 ! ! ! |
| !5005! ! (without item 4.2). ! ! ! |
| !. ! ! ! ! ! |
| !. ! ! The number (X04) is programmable. ! ! ! |
| !. ! ! ! ! ! |
| !. ! ! In case of change of the engine serial ! ! ! |
| !. ! ! number, (X04) are automatically set to ! ! ! |
| !. ! ! five. ! ! ! |
| !500X! ! The code is shown in an increasing ! ! ! |
| ! ! ! order, i.e. the first report has the ! ! ! |
| ! ! ! code 5001, the next code is 5002 and so ! ! ! |
| ! ! ! on until 5005 is reached. ! ! ! |
| ! ! ! ! ! ! |
| ! !5.1 ! Number 'X04' for consecutive legs up to ! C ! limit- ! |
| ! ! ! 9. ! ! table ! |
| ! !5.2 ! Number 'X04' in case of ESN change. ! ! 5 ! |
| ! ! ! ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !8100!8.1 ! ACARS MU uplink request with IMI ! ! ! |
| ! ! ! 'REQ04': ! ! ! |
| ! ! ! The report <04> is immediately generated! ! ! |
| ! ! ! and transmitted to the ACARS MU. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !8200!8.2 ! ACARS MU uplink request with IMI 'G04': ! ! ! |
| ! ! ! The report <04> is generated as the next! ! ! |
| ! ! ! take-off according to code 4000 or 4100 ! ! ! |
| ! ! ! depending on which logic is armed. ! ! ! |
| !----------------------------------------------------------------------! |
| ! A = Programmable by Airbus ! |
| ! C = Programmable by Customer ! |
| +----------------------------------------------------------------------+ |
(14) Engine Take Off Report Logic <04> (Engine Type CFMI with Advanced EVMU)
| +----------------------------------------------------------------------+ |
| !Code!Item ! !Progr.!Standard ! |
| ! No.!No. ! Description of Function Item !MCDU !Value or ! |
| ! ! ! !/GSE !Table TXY! |
| !----!------!-----------------------------------------!------!---------! |
| ! !A ! Report Format ! ! ! |
| ! !B ! Parameter Table ! ! ! |
| ! !C ! First three lines of Report ! C ! Blank ! |
| ! !D ! Print-out Rules ! C ! See ! |
| ! ! ! ! ! separate! |
| ! ! ! ! ! list ! |
| ! !E ! Transfer to ACARS MU ! C ! see ! |
| ! ! ! ! ! separate! |
| ! ! ! ! ! list ! |
| ! !F ! Increment of the report counter if the ! C ! 1 ! |
| ! ! ! report was triggered by a code number ! ! ! |
| ! ! ! > 1000; 1=yes, 0=no ! ! ! |
| ! !G ! 'Y04.2' Average intervals in seconds ! C ! 2 ! |
| ! ! ! for OIT, OIP, VB1, VB2 and PHA. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !1000!1 ! Manual selection via MCDU ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !2000!2 ! Flight phase dependent manual ! ! ! |
| ! ! ! selection via remote print button ! ! ! |
| ! ! ! if programmed. ! ! ! |
| ! !2.1 ! Remote Print Button assignment. ! C ! not ! |
| ! ! ! ! ! assigned! |
| !----!------!-----------------------------------------!------!---------! |
| !3000!3 ! Programmable Start Logic ! ! ! |
| ! !3.1 ! Trigger condition ! C ! not ! |
| ! ! ! ! ! progr. ! |
| !----!------!-----------------------------------------!------!---------! |
| !4000!4 ! The report is generated and stored every! ! ! |
| ! ! ! 'F04'th Take-Off and is triggered when, ! ! ! |
| ! ! ! during a searching time period of 20 ! ! ! |
| ! ! ! seconds, the sum of the EGT of both ! ! ! |
| ! ! ! engines is maximal. The searching time ! ! ! |
| ! ! ! period is started 'Y04.1' seconds after ! ! ! |
| ! ! ! entering flight phase 4. ! ! ! |
| ! ! ! The trigger stays armed during flight ! ! ! |
| ! ! ! phase 5. ! ! ! |
| ! ! ! ! ! ! |
| ! !4.1 ! The report is postponed to the next ! ! ! |
| ! ! ! flight leg if at least one of the EGT ! ! ! |
| ! ! ! values on Eng.1 or Eng.2 is below EGTL ! ! ! |
| ! ! ! at the moment when the starter air valve! ! ! |
| ! ! ! switches from the closed position to the! ! ! |
| ! ! ! open position at engine start. ! ! ! |
| ! ! ! Starter Air Valve open: ! ! ! |
| ! ! ! Eng.1 param. 7C.1.270.01.13 = 1 ! ! ! |
| ! ! ! Eng.2 param. 7C.2.270.10.13 = 1 ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! or ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! if the Wing Anti-Ice Status or the Na- ! ! ! |
| ! ! ! celle Anti-Ice Status is switched during! ! ! |
| ! ! ! the search time period. ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! Wing Anti-Ice Valve closed: ! ! ! |
| ! ! ! 29.1.001.00.18 = 0 right hand ! ! ! |
| ! ! ! 29.2.001.00.18 = 0 ! ! ! |
| ! ! ! 29.1.001.11.18 = 0 left hand ! ! ! |
| ! ! ! 29.2.001.11.18 = 0 ! ! ! |
| ! ! ! Nacelle Anti-Ice Valve closed: ! ! ! |
| ! ! ! Eng.1 param. 5D.2.061.10.28 = 0 ! ! ! |
| ! ! ! Eng.2 param. 5D.2.061.10.27 = 0 ! ! ! |
| !4100!4.1.1 ! The same rules as described for Log. No.! C ! disarmed! |
| ! ! ! 4000 are valid and in addition the ! ! ! |
| ! ! ! report is postponed when the Wing ! ! ! |
| ! ! ! Anti-Ice Status or the Nacelle Anti-Ice ! ! ! |
| ! ! ! Status is open during the search time ! ! ! |
| ! ! ! period. This trigger condition is ! ! ! |
| ! ! ! basically disarmed and can be armed via ! ! ! |
| ! ! ! a GSE programming. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| ! !4.2 ! The report trigger logic is restarted in! ! ! |
| ! ! ! flight leg 'F04+n' (n=1, 2, ..F04) after! ! ! |
| ! ! ! no report generation in the previous leg! ! ! |
| ! ! ! 'F04+ (n-1)'. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| ! !4.3 ! EGTL ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.4 ! 'F04'th Take Off ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.5 ! 'Y04.1' seconds after PH 4 entry ! C ! limit- ! |
| ! ! ! ! table ! |
| ! !4.6 ! T/O delta N1 summary limits ! ! ! |
| ! ! ! delta N1 = N1MX - N1 ! ! ! |
| ! ! ! N1MX = 7C.1.342.01 Eng.1 ! ! ! |
| ! ! ! 7C.2.342.10 Eng.2 ! ! ! |
| ! ! ! N1 = 7C.1.346.01 Eng.1 ! ! ! |
| ! ! ! 7C.2.346.10 Eng.2 ! ! ! |
| ! ! ! ! ! ! |
| ! !4.7.1 ! delta N1 >10 %rpm ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.7.2 ! 8 < delta N1 <=10 %rpm ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.7.2 ! delta N1 >8 %rpm and <= 10 %rpm ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.7.3 ! delta N1 >6 %rpm and <= 8 %rpm ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.7.4 ! delta N1 >4 %rpm and <= 6 %rpm ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.7.5 ! delta N1 >2 %rpm and <= 4 %rpm ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.7.6 ! delta N1 >0.2 %rpm and <= 10 %rpm ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.7.7 ! delta N1 <0.2 %rpm ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.8 ! The calculation is made 'Y04.3' seconds ! ! ! |
| ! ! ! after entry into flight phase 4. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| ! !4.8.1 ! 'Y04.3' seconds after PH 4 entry. ! C ! limit- ! |
| ! ! ! ! ! table ! |
| !----!------!-----------------------------------------!------!---------! |
| !5001!5 ! Each time when a report is generated by ! ! ! |
| !5002! ! this logic the number 'X04' is decreased! ! ! |
| !5003! ! until zero is reached. The conditions ! ! ! |
| !5004! ! are described under code No. 4000/4100 ! ! ! |
| !5005! ! (without item 4.2). ! ! ! |
| !. ! ! ! ! ! |
| !. ! ! The number (X04) is programmable. ! ! ! |
| !. ! ! ! ! ! |
| !. ! ! In case of change of the engine serial ! ! ! |
| !. ! ! number, (X04) are automatically set to ! ! ! |
| !. ! ! five. ! ! ! |
| !500X! ! The code is shown in an increasing ! ! ! |
| ! ! ! order, i.e. the first report has the ! ! ! |
| ! ! ! code 5001, the next code is 5002 and so ! ! ! |
| ! ! ! on until 5005 is reached. ! ! ! |
| ! ! ! ! ! ! |
| ! !5.1 ! Number 'X04' for consecutive legs up to ! C ! limit- ! |
| ! ! ! 9. ! ! table ! |
| ! !5.2 ! Number 'X04' in case of ESN change. ! ! 5 ! |
| ! ! ! ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !8100!8.1 ! ACARS MU uplink request with IMI ! ! ! |
| ! ! ! 'REQ04': ! ! ! |
| ! ! ! The report <04> is immediately generated! ! ! |
| ! ! ! and transmitted to the ACARS MU. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !8200!8.2 ! ACARS MU uplink request with IMI 'G04': ! ! ! |
| ! ! ! The report <04> is generated as the next! ! ! |
| ! ! ! take-off according to code 4000 or 4100 ! ! ! |
| ! ! ! depending on which logic is armed. ! ! ! |
| !----------------------------------------------------------------------! |
| ! A = Programmable by Airbus ! |
| ! C = Programmable by Customer ! |
| +----------------------------------------------------------------------+ |
F. AIDS Reports Print Rules - Default Values for Report <04>
| +------------------------------------------------+ |
| ! ! ! ! |
| ! Code ! Printer Output ! ACARS-output ! |
| ! ! ! ! |
| !-------!-----------------------!----------------! |
| ! ! ! ! |
| ! 1000 ! Print immediatly ! No ACARS ! |
| ! ! ! ! |
| !-------!-----------------------!----------------! |
| ! ! ! ! |
| ! 2000 ! Print immediatly ! No ACARS ! |
| ! ! ! ! |
| !-------!-----------------------!----------------! |
| ! ! ! ! |
| ! 4000 ! Print at landing ! ACARS VHF ! |
| ! ! ! ! |
| !-------!-----------------------!----------------! |
| ! ! ! ! |
| ! 4100 ! Print at landing ! ACARS VHF ! |
| ! ! ! ! |
| !-------!-----------------------!----------------! |
| ! ! ! ! |
| ! 500x ! Print at landing ! ACARS VHF ! |
| ! ! ! ! |
| !-------!-----------------------!----------------! |
| ! ! ! ! |
| ! 8100 ! No print ! ACARS VHF ! |
| ! ! ! ! |
| !-------!-----------------------!----------------! |
| ! ! ! ! |
| ! 8200 ! Print at landing ! ACARS VHF ! |
| ! ! ! ! |
| +------------------------------------------------+ |
| +-------------------------------------------------------------------------+ |
| !Trigger! to ACARS ! to printer ! store ! |
| ! Code !------------------------------ -!-----------------!--------------! |
| ! No !Ground ! VHF ! SAT- ! HF ! at ! imme- ! internal& ! |
| ! ! ! ! COM ! !landing ! diate ! external ! |
| ! ! ! ! ! ! ! !(build in RAM&! |
| ! ! ! ! ! ! ! ! PCMCIA) ! |
| !-------!-------!--------!-------!-------!--------!--------!--------------! |
| ! ! ! If ! ! ! ! If !PCMCIA only if! |
| ! 1000 ! NO ! 'SEND' ! NO ! NO ! !'PRINT' ! 'STORE' ! |
| ! ! !selected! ! ! !selected! selected on ! |
| ! ! !on MCDU ! ! ! !on MCDU ! MCDU ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 2000 ! NO ! NO ! NO ! NO ! ! YES ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 3000 ! NO ! NO ! NO ! NO ! N ! NO ! YES ! |
| !-------!-------!--------!------ !-------! O !--------!--------------! |
| ! 4000 ! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 4100 ! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 5001..! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| ! 500x ! ! ! ! ! ! ! ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 8100 ! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 8200 ! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| +-------------------------------------------------------------------------+ |
| +-------------------------------------------------------------------------+ |
| !Trigger! to ACARS ! to printer ! store ! |
| ! Code !------------------------------ -!-----------------!--------------! |
| ! No !Ground ! VHF ! SAT- ! HF ! at ! imme- ! internal& ! |
| ! ! ! ! COM ! !landing ! diate ! external ! |
| ! ! ! ! ! ! ! !(build in RAM&! |
| ! ! ! ! ! ! ! ! PCMCIA) ! |
| !-------!-------!--------!-------!-------!--------!--------!--------------! |
| ! 1000 ! NO ! NO ! NO ! NO ! NO ! YES ! YES ! |
| !-------!-------!--------!-------!-------!--------!--------!--------------! |
| ! 2000 ! NO ! NO ! NO ! NO ! NO ! YES ! YES ! |
| !-------!-------!--------!-------!-------!--------!--------!--------------! |
| ! 3000 ! NO ! NO ! NO ! NO ! NO ! NO ! YES ! |
| !-------!-------!--------!------ !-------!--------!--------!--------------! |
| ! 4000 ! NO ! YES ! NO ! NO ! NO ! NO ! YES ! |
| !-------!-------!--------!-------!-------!--------!--------!--------------! |
| ! 4100 ! NO ! YES ! NO ! NO ! NO ! NO ! YES ! |
| !-------!-------!--------!-------!-------!--------!--------!--------------! |
| ! 5001..! NO ! YES ! NO ! NO ! NO ! NO ! YES ! |
| ! 500x ! ! ! ! ! ! ! ! |
| !-------!-------!--------!-------!-------!--------!--------!--------------! |
| ! 8100 ! NO ! YES ! NO ! NO ! NO ! NO ! YES ! |
| !-------!-------!--------!-------!-------!--------!--------!--------------! |
| ! 8200 ! NO ! YES ! NO ! NO ! NO ! NO ! YES ! |
| +-------------------------------------------------------------------------+ |
G. Engine Report On Request <05>
Engine Report On Request <05> (Engine Type CFMI with Advanced EVMU)
Engine Report On Request <05> (Engine Type CFMI with Advanced EVMU)
Engine Report On Request <05> (Engine Type CFMI with Advanced EVMU) ** ON A/C NOT FOR ALL
Engine Report On Request <05> (Engine Type CFMI with Advanced EVMU) ** ON A/C NOT FOR ALL
Engine Report On Request <05> (Engine Type CFMI with Advanced EVMU) ** ON A/C NOT FOR ALL
The engine on request report is a time series collection of aircraft and engine parameters as a function of a manually initiated trigger. The report is generated when one of the logic conditions 1000 to 3000 (for details see engine report O/R logic) is present.
Engine Report On Request <05> (Engine Type CFMI with Advanced EVMU) Engine Report On Request <05> (Engine Type CFMI with Advanced EVMU) Engine Report On Request <05> (Engine Type CFMI with Advanced EVMU) ** ON A/C NOT FOR ALL Engine Report On Request <05> (Engine Type CFMI with Advanced EVMU) ** ON A/C NOT FOR ALL Engine Report On Request <05> (Engine Type CFMI with Advanced EVMU) ** ON A/C NOT FOR ALL NOTE: For the standard header definition of the report refer to (Ref. AMM D/O 31-36-00-00).
(1) Engine Report O/R Data Field Description <05> (Engine Type CFMI with Advanced EVMU)
NOTE: Reports that are transmitted from the ACARS system do not have report lines without a line identifier.
| +---------------------------------------------------------------------+ |
| ! Value ! Content Description ! |
| !--------------!------------------------------------------------------! |
| ! ESN ! Engine Serial Number ! |
| ! 999999 ! (000000 to 999999) ! |
| ! ! Eng 1 param. 7C.1.046.01 digit 3, 2, 1 ! |
| ! ! 7C.1.047.01 digit 6, 5, 4 ! |
| ! ! Eng 2 param. 7C.2.046.01 digit 3, 2, 1 ! |
| ! ! 7C.2.047.01 digit 6, 5, 4 ! |
| !--------------!------------------------------------------------------! |
| ! EHRS ! Engine Flight Hours ! |
| ! 99999 ! (00000 to 99999 hours) ! |
| ! ! DMU Engine 1 and Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! ERT ! Engine Running Time ! |
| ! 99999 ! (00000 to 65536 hours) ! |
| ! ! Eng 1 param. 7C.1.050.01 ! |
| ! ! Eng 2 param. 7C.2.050.10 ! |
| !--------------!------------------------------------------------------! |
| ! ECYC ! Engine Cycle ! |
| ! 99999 ! (00000 to 99999) ! |
| !--------------!------------------------------------------------------! |
| ! AP ! Auto Pilot Status ! |
| ! 99 ! (00 to G8) ! |
| ! ! FMGC 1 and 2 (FGC part) for Auto Pilot AP1 and AP2 ! |
| ! ! ! |
| ! ! XX Auto Pilot Modes: ! |
| ! ! !! ! |
| ! ! !!__Lateral Modes: 0 = NO MODE ! |
| ! ! ! 1 = HEADING ! |
| ! ! ! 2 = TRACK ! |
| ! ! ! 3 = NAV ! |
| ! ! ! 4 = LOC CAPTURE ! |
| ! ! ! 5 = LOC TRACK ! |
| ! ! ! 6 = LAND TRACK ! |
| ! ! ! 7 = RUNWAY ! |
| ! ! ! 8 = ROLL GO AROUND ! |
| ! ! ! ! |
| ! ! !__Longitudinal Modes: 0 = NO MODE ! |
| ! ! 1 = PITCH G/A ! |
| ! ! 2 = PITCH T/O ! |
| ! ! 3 = G/S TRACK ! |
| ! ! 4 = G/S CAPTURE ! |
| ! ! 5 = V/S ! |
| ! ! 6 = FPA ! |
| ! ! 7 = ALT ! |
| ! ! 8 = ALT ACQ ! |
| ! ! 9 = OPEN CLB ! |
| ! ! A = OPEN DES ! |
| ! ! B = IM CLB ! |
| ! ! C = IM DES ! |
| ! ! D = CLB ! |
| ! ! E = DES ! |
| ! ! F = FINAL DES ! |
| ! ! G = EXPEDITE ! |
| ! ! ! |
| ! ! AP1 ! AP2 ! |
| ! ! Report Line EC: ! Report Line EE: !Difinition: ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! / ! / !No Mode Act. ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.11 = 1 ! 01.2.275.00.11 = 1!RUNWAY Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.12 = 1 ! 01.2.275.00.12 = 1!NAV Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.13 = 1 ! 01.2.275.00.13 = 1!LOC CAPTURE ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.14 = 1 ! 01.2.275.00.14 = 1!LOC TRACK ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.15 = 1 ! 01.2.275.00.15 = 1!Roll GO ! |
| ! ! ! !AROUND Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.16 = 1 ! 01.2.275.00.16 = 1!HEADING Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.17 = 1 ! 01.2.275.00.17 = 1!TRACK Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.15 = 1 ! 01.2.274.00.15 = 1!PITCH TO Mode! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.16 = 1 ! 01.2.274.00.16 = 1!PITCH GA Mode! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.17 = 1 ! 01.2.274.00.17 = 1!V/S Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.18 = 1 ! 01.2.274.00.18 = 1!FPA Mode ! |
| ! ! -------------------!-------------------!-------------! |
| ! ! 01.1.274.00.19 = 1 ! 01.2.274.00.19 = 1!ALT Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.20 = 1 ! 01.2.274.00.20 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.19 = 1 ! 01.2.274.00.19 = 1!ALT ACQ ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.21 = 1 ! 01.2.274.00.21 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.20 = 1 ! 01.2.274.00.20 = 1!G/S TRACK ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.22 = 1 ! 01.2.274.00.22 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.21 = 1 ! 01.2.274.00.21 = 1!G/S CAPTURE ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.22 = 1 ! 01.2.274.00.22 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.23 = 1 ! 01.2.274.00.23 = 1!FINAL DES ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.2.274.00.24 = 1 ! 01.2.274.00.24 = 1!EXPED. Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.146.00.14 = 1 ! 01.2.146.00.14 = 1!LAND TRACK ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!CLB Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.13 = 0 ! 01.2.274.00.13 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.14 = 0 ! 01.2.274.00.14 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.24 = 0 ! 01.2.274.00.24 = 0! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!DES Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.13 = 0 ! 01.2.274.00.13 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.14 = 0 ! 01.2.274.00.14 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.24 = 0 ! 01.2.274.00.24 = 0! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!IM. CLIMB ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.13 = 1 ! 01.2.274.00.13 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!IM. DES Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.13 = 1 ! 01.2.274.00.13 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!OPEN CLB ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.14 = 1 ! 01.2.274.00.14 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!OPEN DES ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.14 = 1 ! 01.2.274.00.14 = 1! ! |
| ! ! ---------------------------------------------------- ! |
| ! ! Auto Pilot Status DMU: ! |
| ! ! AP1 printed in report line EC ! |
| ! ! AP2 printed in report line EE ! |
| !--------------!------------------------------------------------------! |
| ! ECW2 ! Engine Control Word 2 ! |
| ! XXXXX ! Each 'X' represents 4 Bits in hexadecimal code of ! |
| ! ! a defined ARINC 429 word: ! |
| ! ! XXXXX Bits HEX ! |
| ! ! !!!!!___________ 14, 13, 12, 11 0...F ! |
| ! ! !!!!____________ 18, 17, 16, 15 0...F ! |
| ! ! !!!_____________ 22, 21, 20, 19 0...F ! |
| ! ! !!______________ 26, 25, 24, 23 0...F ! |
| ! ! !_______________ 29, 28, 27 0...7 ! |
| ! ! -------------------------------------------- ! |
| ! ! Bit Label Parameter Description ! |
| ! ! 11 7C.X.272.XX.12 = 1 Bump/Overboost #1 enable ! |
| ! ! 12 7C.X.272.XX.13 = 1 Bump/Overboost #2 enable ! |
| ! ! 13 7C.X.272.XX.14 = 1 Bump/Overboost #3 enable ! |
| ! ! 14 7C.X.272.XX.22 = 1 MTO. GA limit mode select.! |
| ! ! 15 7C.X.272.XX.23 = 1 Flex Take-Off limit mode ! |
| ! ! selected ! |
| ! ! 16 SPARE ! |
| ! ! 17 SPARE ! |
| ! ! 18 SPARE ! |
| ! ! 19 SPARE ! |
| ! ! 20 SPARE ! |
| ! ! 21 SPARE ! |
| ! ! 22 SPARE ! |
| ! ! 23 SPARE ! |
| ! ! 24 SPARE ! |
| ! ! 25 SPARE ! |
| ! ! 26 SPARE ! |
| ! ! 27 SPARE ! |
| ! ! 28 SPARE ! |
| ! ! 29 SPARE ! |
| !--------------!------------------------------------------------------! |
| ! ECW5 ! Engine Control Word 5 ! |
| ! XXXXX ! Each 'X' represents 4 Bits in hexadecimal code of ! |
| ! ! a defined ARINC 429 word: ! |
| ! ! XXXXX Bits HEX ! |
| ! ! !!!!!___________ 14, 13, 12, 11 0...F ! |
| ! ! !!!!____________ 18, 17, 16, 15 0...F ! |
| ! ! !!!_____________ 22, 21, 20, 19 0...F ! |
| ! ! !!______________ 26, 25, 24, 23 0...F ! |
| ! ! !_______________ 29, 28, 27 0...7 ! |
| ! ! -------------------------------------------- ! |
| ! ! Bit Label Parameter Description ! |
| ! ! 11 7C.X.270.XX.11 = 1 Ignition 1 primary select.! |
| ! ! 12 SPARE ! |
| ! ! 13 7C.X.270.XX.13 = 1 Starter Air Valve open ! |
| ! ! local switch ! |
| ! ! 14 7C.X.270.XX.14 = 1 HP Fuel Valve closed local! |
| ! ! 15 7C.X.270.XX.15 = 1 SAV demand/position disag.! |
| ! ! 16 7C.X.270.XX.16 = 1 HPSOV demand/podition ! |
| ! ! disagree ! |
| ! ! 17 7C.X.270.XX.17 = 1 Start EGT overtemp detec. ! |
| ! ! 18 7C.X.270.XX.18 = 1 Start Stall detected ! |
| ! ! 19 7C.X.270.XX.19 = 1 No/Low fan speed for core ! |
| ! ! speed ! |
| ! ! 20 7C.X.270.XX.20 = 1 No Eng. light off detected! |
| ! ! 21 7C.X.270.XX.21 = 1 Starter time limit exceed.! |
| ! ! 22 7C.X.270.XX.22 = 1 Fuel schedule derich activ! |
| ! ! 23 7C.X.270.XX.23 = 1 TLA not idle start initia.! |
| ! ! 24 SPARE ! |
| ! ! 25 7C.X.270.XX.25 = 1 Low Sap detected ! |
| ! ! 26 7C.X.270.XX.28 = 1 50% thrust limit active ! |
| ! ! 27 SPARE ! |
| ! ! 28 SPARE ! |
| ! ! 29 SPARE ! |
| !--------------!------------------------------------------------------! |
| ! EVM ! Engine Vibration Status Word ! |
| ! XXXXX ! Eng 1 param. 3D.1.035.01 ! |
| ! ! Eng 2 param. 3D.1.035.10 ! |
| ! ! Each 'X' represents 4 Bits in hexadecimal code of ! |
| ! ! a defined ARINC 429 word: ! |
| ! ! XXXXX Bits HEX ! |
| ! ! !!!!!___________ 14, 13, 12, 11 0...F ! |
| ! ! !!!!____________ 18, 17, 16, 15 0...F ! |
| ! ! !!!_____________ 22, 21, 20, 19 0...F ! |
| ! ! !!______________ 26, 25, 24, 23 0...F ! |
| ! ! !_______________ 29, 28, 27 0...7 ! |
| !--------------!------------------------------------------------------! |
| ! N1 ! Selected N1 Actual ! |
| ! 9999 ! (0 to 120.0 %rpm) ! |
| ! ! Eng 1 param. 7C.1.346.01 ! |
| ! ! Eng 2 param. 7C.2.346.10 ! |
| !--------------!------------------------------------------------------! |
| ! N1C ! N1 Command ! |
| ! 9999 ! (0 to 120.0 %rpm) ! |
| ! ! Eng 1 param. 7C.1.341.01 ! |
| ! ! Eng 2 param. 7C.2.341.10 ! |
| !--------------!------------------------------------------------------! |
| ! N2 ! Selected N2 Actual ! |
| ! 9999 ! (0 to 120.0 %rpm) ! |
| ! ! Eng 1 param. 7C.1.344.01 ! |
| ! ! Eng 2 param. 7C.2.344.10 ! |
| !--------------!------------------------------------------------------! |
| ! EGT ! Selected T494 (Exhaust Gas Temperature) ! |
| ! X999 ! (-55 to 999.9 C) ! |
| ! ! Eng 1 param. 7C.1.345.01 ! |
| ! ! Eng 2 param. 7C.2.345.10 ! |
| !--------------!------------------------------------------------------! |
| ! FF ! Engine Fuel Flow ! |
| ! 9999 ! ( 0 to 7000 kg/h) ! |
| ! ! Eng 1 param. 7C.1.244.01 ! |
| ! ! Eng 2 param. 7C.2.244.10 ! |
| !--------------!------------------------------------------------------! |
| ! VN ! FAN Pick Up N1 Track Vibration ! |
| ! 99 ! (0.0 to 10.0) ! |
| ! ! Eng 1 param. 3D.1.227.01 ! |
| ! ! Eng 2 param. 3D.1.227.10 ! |
| !--------------!------------------------------------------------------! |
| ! VC ! FAN Pick Up N2 Track Vibration ! |
| ! 99 ! (0.0 to 4.0) ! |
| ! ! Eng 1 param. 3D.1.230.01 ! |
| ! ! Eng 2 param. 3D.1.230.10 ! |
| !--------------!------------------------------------------------------! |
| ! VH ! TRF Pick Up N2 Track Vibration ! |
| ! 99 ! (0.0 to 4.0) ! |
| ! ! Eng 1 param. 3D.1.230.11 ! |
| ! ! Eng 2 param. 3D.1.230.00 ! |
| !--------------!------------------------------------------------------! |
| ! VL ! TRF Pick Up N1 Vibration ! |
| ! 99 ! (0.0 to 10.0) ! |
| ! ! Eng 1 param. 3D.1.227.11 ! |
| ! ! Eng 2 param. 3D.1.227.00 ! |
| +---------------------------------------------------------------------+ |
(2) Engine Report O/R Data Field Description <05> (Engine Type CFMI with Advanced EVMU)
NOTE: Reports that are transmitted from the ACARS system do not have report lines without a line identifier.
NOTE: Only the parts of the ENGINE REPORT O/R <05> which are not included in the ENGINE CRUISE REPORT <01> are given in the subsequent table.
| +---------------------------------------------------------------------+ |
| ! Value ! Content Description ! |
| !--------------!------------------------------------------------------! |
| ! ECW2 ! Engine Control Word 2 ! |
| ! XXXXX ! Each 'X' represents 4 Bits in hexadecimal code of ! |
| ! ! a defined ARINC 429 word: ! |
| ! ! XXXXX Bits HEX ! |
| ! ! !!!!!___________ 14, 13, 12, 11 0...F ! |
| ! ! !!!!____________ 18, 17, 16, 15 0...F ! |
| ! ! !!!_____________ 22, 21, 20, 19 0...F ! |
| ! ! !!______________ 26, 25, 24, 23 0...F ! |
| ! ! !_______________ 29, 28, 27 0...7 ! |
| ! ! -------------------------------------------- ! |
| ! ! Bit Label Parameter Description ! |
| ! ! 11 7C.X.272.XX.12 = 1 Bump/Overboost #1 enable ! |
| ! ! 12 7C.X.272.XX.13 = 1 Bump/Overboost #2 enable ! |
| ! ! 13 7C.X.272.XX.14 = 1 Bump/Overboost #3 enable ! |
| ! ! 14 7C.X.272.XX.22 = 1 MTO. GA limit mode select.! |
| ! ! 15 7C.X.272.XX.23 = 1 Flex Take-Off limit mode ! |
| ! ! selection ! |
| ! ! 16 SPARE ! |
| ! ! 17 SPARE ! |
| ! ! 18 SPARE ! |
| ! ! 19 SPARE ! |
| ! ! 20 SPARE ! |
| ! ! 21 SPARE ! |
| ! ! 22 SPARE ! |
| ! ! 23 SPARE ! |
| ! ! 24 SPARE ! |
| ! ! 25 SPARE ! |
| ! ! 26 SPARE ! |
| ! ! 27 SPARE ! |
| ! ! 28 SPARE ! |
| ! ! 29 SPARE ! |
| !--------------!------------------------------------------------------! |
| ! ECW5 ! Engine Control Word 5 ! |
| ! XXXXX ! Each 'X' represents 4 Bits in hexadecimal code of ! |
| ! ! a defined ARINC 429 word: ! |
| ! ! XXXXX Bits HEX ! |
| ! ! !!!!!___________ 14, 13, 12, 11 0...F ! |
| ! ! !!!!____________ 18, 17, 16, 15 0...F ! |
| ! ! !!!_____________ 22, 21, 20, 19 0...F ! |
| ! ! !!______________ 26, 25, 24, 23 0...F ! |
| ! ! !_______________ 29, 28, 27 0...7 ! |
| ! ! -------------------------------------------- ! |
| ! ! Bit Label Parameter Description ! |
| ! ! 11 7C.X.270.XX.11 = 1 Ignition 1 primary select.! |
| ! ! 12 SPARE ! |
| ! ! 13 7C.X.270.XX.13 = 1 Starter Air Valve open ! |
| ! ! local switch ! |
| ! ! 14 7C.X.270.XX.14 = 1 HP Fuel Valve closed local! |
| ! ! 15 7C.X.270.XX.15 = 1 SAV demand/position ! |
| ! ! disagree ! |
| ! ! 16 7C.X.270.XX.16 = 1 HPSOV demand/position ! |
| ! ! disagree ! |
| ! ! 17 7C.X.270.XX.17 = 1 Start EGT overtemp detec. ! |
| ! ! 18 7C.X.270.XX.18 = 1 Start Stall detected ! |
| ! ! 19 7C.X.270.XX.19 = 1 No/Low fan speed for core ! |
| ! ! speed ! |
| ! ! 20 7C.X.270.XX.20 = 1 No Eng. light off detected! |
| ! ! 21 7C.X.270.XX.21 = 1 Starter time limit exceed.! |
| ! ! 22 7C.X.270.XX.22 = 1 Fuel schedule derich activ! |
| ! ! 23 7C.X.270.XX.23 = 1 TLA not idle start initia.! |
| ! ! 24 SPARE ! |
| ! ! 25 7C.X.270.XX.25 = 1 Low Sap detected ! |
| ! ! 26 7C.X.270.XX.28 = 1 50% thrust limit active ! |
| ! ! 27 SPARE ! |
| ! ! 28 SPARE ! |
| ! ! 29 SPARE ! |
| !--------------!------------------------------------------------------! |
| ! TAT/ALT/CAS/! For parameter description see "Standard Header for ! |
| ! MN/GW/CG ! Print Report" (Refer to 31-36-00). ! |
| ! ! ! |
| ! ! Parameter in Report Line C1/CE: Ambient Condition ! |
| ! ! at the time "S1"/"T1". ! |
| ! ! ! |
| ! ! Parameter in Report Line C3: Ambient Condition at ! |
| ! ! the time "V1"/"X1". ! |
| !--------------!------------------------------------------------------! |
(3) Engine Report O/R Data Field Description <05> (Engine Type CFMI with Advanced EVMU)
| +---------------------------------------------------------------------+ |
| ! Value ! Content Description ! |
| !--------------!------------------------------------------------------! |
| ! ESN ! Engine Serial Number ! |
| ! 999999 ! (000000 to 999999) ! |
| ! ! ECU Engine 1 7C.1.046.01 digit 3, 2, 1 ! |
| ! ! 7C.1.047.01 digit 6, 5, 4 ! |
| ! ! Engine 2 7C.2.046.10 digit 3, 2, 1 ! |
| ! ! 7C.2.047.10 digit 6, 5, 4 ! |
| !--------------!------------------------------------------------------! |
| ! EHRS ! Engine Flight Hours ! |
| ! 99999 ! (00000 to 99999 hours) ! |
| ! ! DMU Engine 1 ! |
| ! ! Engine 2 ! |
| ! ! Remark: Time between "Main (LH and RH) Landing Gear! |
| ! ! Decompressed" and "Main (LH and RH) Landing! |
| ! ! Gear Compressed". The EHRS shall be ste to ! |
| ! ! zero if a new ESN is recognized by the DMU.! |
| ! ! It shall be possible to set the EHRS via ! |
| ! ! the MCDU, e.g. if the DMU is changed on the! |
| ! ! a/c. ! |
| !--------------!------------------------------------------------------! |
| ! ERT ! Engine Running Time ! |
| ! 99999 ! (00000 to 65536 hours) ! |
| ! ! ECU 7C.1.050.01 Engine 1 ! |
| ! ! 7C.2.050.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! ECYC ! Engine Cycle ! |
| ! 99999 ! (00000 to 99999) ! |
| ! ! DMU Engine 1 ! |
| ! ! Engine 2 ! |
| ! ! Remark: Each time when flight phase 5 (climb) is ! |
| ! ! reached, the counter shall be incremented ! |
| ! ! by one. The ECYC is set to zero if a new ! |
| ! ! ESN is recognized by the DMU. It shall be ! |
| ! ! possible to set ECYC via the MCDU, if the ! |
| ! ! DMU is changed on the a/c. ! |
| !--------------!------------------------------------------------------! |
| ! AP ! Auto Pilot Status ! |
| ! 99 ! Number of respective status (00 to G8) ! |
| ! ! FMGC 1 and 2 (FGC part) for Auto Pilot AP1 and AP2 ! |
| ! ! ! |
| ! ! Parameter for AP1 ! Parameter for AP2 ! ! |
| ! ! Report Line EC: ! Report Line EE: !Definition: ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! / ! / !No Mode ! |
| ! ! ! !Active ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.11 = 1 ! 01.2.275.00.11 = 1!RUNWAY Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.12 = 1 ! 01.2.275.00.12 = 1!NAV Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.13 = 1 ! 01.2.275.00.13 = 1!LOC CAPTURE ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.14 = 1 ! 01.2.275.00.14 = 1!LOC TRACK ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.15 = 1 ! 01.2.275.00.15 = 1!Roll GO ! |
| ! ! ! !AROUND Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.16 = 1 ! 01.2.275.00.16 = 1!HEADING Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.17 = 1 ! 01.2.275.00.17 = 1!TRACK Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.15 = 1 ! 01.2.274.00.15 = 1!PITCH T/O ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.16 = 1 ! 01.2.274.00.16 = 1!PITCH GA Mode! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.17 = 1 ! 01.2.274.00.17 = 1!V/S Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.18 = 1 ! 01.2.274.00.18 = 1!FPA Mode ! |
| ! ! -------------------!-------------------!-------------! |
| ! ! 01.1.274.00.19 = 1 ! 01.2.274.00.19 = 1!ALT Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.20 = 1 ! 01.2.274.00.20 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.19 = 1 ! 01.2.274.00.19 = 1!ALT ACQ ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.21 = 1 ! 01.2.274.00.21 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.20 = 1 ! 01.2.274.00.20 = 1!G/S TRACK ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.22 = 1 ! 01.2.274.00.22 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.21 = 1 ! 01.2.274.00.21 = 1!G/S CAPTURE ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.22 = 1 ! 01.2.274.00.22 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.23 = 1 ! 01.2.274.00.23 = 1!FINAL DES ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.24 = 1 ! 01.2.274.00.24 = 1!EXPED. Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.146.00.14 = 1 ! 01.2.146.00.14 = 1!LAND TRACK ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!CLB Mode ! |
| ! ! AND ! AND ! ! |
| ! ! ! ! ! ! ! |
| ! ! -------------- ! -------------- ! ! |
| ! ! 01.1.274.00.13 = 0 ! 01.2.274.00.13 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.14 = 0 ! 01.2.274.00.14 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.24 = 0 ! 01.2.274.00.24 = 0! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!DES Mode ! |
| ! ! AND ! AND ! ! |
| ! ! ! ! ! ! ! |
| ! ! -------------- ! -------------- ! ! |
| ! ! 01.1.274.00.13 = 0 ! 01.2.274.00.13 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.14 = 0 ! 01.2.274.00.14 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.24 = 0 ! 01.2.274.00.24 = 0! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!IM. CLIMB ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.13 = 1 ! 01.2.274.00.13 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!IM. DES Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.13 = 1 ! 01.2.274.00.13 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!OPEN CLB ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.14 = 1 ! 01.2.274.00.14 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!OPEN. DES ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.14 = 1 ! 01.2.274.00.14 = 1! ! |
| ! ! ---------------------------------------------------- ! |
| ! ! Auto Pilot Status DMU: ! |
| ! ! Auto Pilot AP1 printed in report line EC ! |
| ! ! Auto Pilot AP2 printed in report line EE ! |
| ! ! Combined Auto Pilot Modes ! |
| ! ! The longitudinal auto pilot mode (1 to G) shall ! |
| ! ! appear on the left position for the AP1 and AP2 print! |
| ! ! format. ! |
| ! ! The lateral auto pilot mode (1 to 8) shall appear on ! |
| ! ! the right position for the AP1 and AP2 print format. ! |
| ! ! In case of a combined auto pilot mode e.g. DES mode ! |
| ! ! and NAV mode are engaged simultaneously, the 'E3' ! |
| ! ! shall appear below AP1 and AP2. ! |
| ! ! XX Auto Pilot Modes: ! |
| ! ! !! ! |
| ! ! !!__Lateral Modes: 0 = NO MODE ! |
| ! ! ! 1 = HEADING ! |
| ! ! ! 2 = TRACK ! |
| ! ! ! 3 = NAV ! |
| ! ! ! 4 = LOC CAPTURE ! |
| ! ! ! 5 = LOCK TRACK ! |
| ! ! ! 6 = LAND TRACK ! |
| ! ! ! 7 = RUNWAY ! |
| ! ! ! 8 = ROLL GO AROUND ! |
| ! ! ! ! |
| ! ! !__Longitudinal Modes: 0 = NO MODE ! |
| ! ! 1 = PITCH G/A ! |
| ! ! 2 = PITCH TO ! |
| ! ! 3 = G/S TRACK ! |
| ! ! 4 = G/S CAPTURE ! |
| ! ! 5 = V/S ! |
| ! ! 6 = FPA ! |
| ! ! 7 = ALT ! |
| ! ! 8 = ALT ACQ ! |
| ! ! 9 = OPEN CLB ! |
| ! ! A = OPEN DES ! |
| ! ! B = IM CLB ! |
| ! ! C = IM DES ! |
| ! ! D = CLB ! |
| ! ! E = DES ! |
| ! ! F = FINAL DES ! |
| ! ! G = EXPEDITE ! |
| !--------------!------------------------------------------------------! |
| ! ECW2 ! Engine Control Word 2 ! |
| ! XXXXX ! XXXXX Bits HEX ! |
| ! ! !!!!!________14, 13, 12, 11 0..F ! |
| ! ! !!!!_________18, 17, 16, 15 0..F ! |
| ! ! !!!__________22, 21, 20, 19 0..F ! |
| ! ! !!___________26, 25, 24, 23 0..F ! |
| ! ! !____________ 29, 28, 27 0..F ! |
| ! ! Bit Label Parameter Description ! |
| ! ! 11 7C.X.272.XX.12 = 1 Bump/Overboost #1 Enable ! |
| ! ! 12 7C.X.272.XX.13 = 1 Bump/Overboost #2 Enable ! |
| ! ! 13 7C.X.272.XX.14 = 1 Bump/Overboost #3 Enable ! |
| ! ! 14 7C.X.272.XX.22 = 1 MTO. GA Limit Mode Selected! |
| ! ! 15 7C.X.272.XX.23 = 1 Flex Take Off Limit Mode ! |
| ! ! Selected ! |
| ! ! 16 SPARE ! |
| ! ! 17 SPARE ! |
| ! ! 18 SPARE ! |
| ! ! 19 SPARE ! |
| ! ! 20 SPARE ! |
| ! ! 21 SPARE ! |
| ! ! 22 SPARE ! |
| ! ! 23 SPARE ! |
| ! ! 24 SPARE ! |
| ! ! 25 SPARE ! |
| ! ! 26 SPARE ! |
| ! ! 27 SPARE ! |
| ! ! 28 SPARE ! |
| ! ! 29 SPARE ! |
| ! ! The 'X' for the System and SDI definition of the ! |
| ! ! engine parameters shall be as follows: ! |
| ! ! System SDI ! |
| ! ! Engine 1 1 01 ! |
| ! ! Engine 2 2 10 ! |
| !--------------!------------------------------------------------------! |
| ! ECW5 ! Engine Control Word 5 ! |
| ! XXXXX ! XXXXX Bits HEX ! |
| ! ! !!!!!________14, 13, 12, 11 0..F ! |
| ! ! !!!!_________18, 17, 16, 15 0..F ! |
| ! ! !!!__________22, 21, 20, 19 0..F ! |
| ! ! !!___________26, 25, 24, 23 0..F ! |
| ! ! !____________ 29, 28, 27 0..F ! |
| ! ! Bit Label Parameter Description ! |
| ! ! 11 7C.X.270.XX.11 = 1 Ignition 1 Primary Selected ! |
| ! ! 12 SPARE ! |
| ! ! 13 7C.X.270.XX.13 = 1 Starter Air Valve Open ! |
| ! ! Local Switch ! |
| ! ! 14 7C.X.270.XX.14 = 1 HP Fuel Valve Closed Local ! |
| ! ! 15 7C.X.270.XX.15 = 1 SAV Demand/Position Disagree! |
| ! ! 16 7C.X.270.XX.16 = 1 HPSOV Demand/Position ! |
| ! ! Disagree ! |
| ! ! 17 7C.X.270.XX.17 = 1 Start EGT Overtemp-Detected ! |
| ! ! 18 7C.X.270.XX.18 = 1 Start Stall Detected ! |
| ! ! 19 7C.X.270.XX.19 = 1 No/Low Fan Speed for Core ! |
| ! ! Speed ! |
| ! ! 20 7C.X.270.XX.20 = 1 No Engine Light Off Detected! |
| ! ! 21 7C.X.270.XX.21 = 1 Starter Time Limit Exceeded ! |
| ! ! 22 7C.X.270.XX.22 = 1 Fuel Schedule Derich Active ! |
| ! ! 23 7C.X.270.XX.23 = 1 TLA Not at Idle for Start ! |
| ! ! Initiation ! |
| ! ! 24 SPARE ! |
| ! ! 25 7C.X.270.XX.25 = 1 Low Sap-(Slow Start) ! |
| ! ! Detected ! |
| ! ! 26 7C.X.270.XX.28 = 1 50% Thrust Limit Active ! |
| ! ! 27 SPARE ! |
| ! ! 28 SPARE ! |
| ! ! 29 SPARE ! |
| ! ! The 'X' for the System and SDI definition of the ! |
| ! ! engine parameters shall be as follows: ! |
| ! ! System SDI ! |
| ! ! Engine 1 1 01 ! |
| ! ! Engine 2 2 10 ! |
| !--------------!------------------------------------------------------! |
| ! EVM ! Engine Vibration Status Word ! |
| ! XXXXX ! EVM 3D.1.035.01 Engine 1 ! |
| ! ! 3D.1.035.10 Engine 2 ! |
| ! ! XXXXX Bits HEX ! |
| ! ! !!!!!________14, 13, 12, 11 0..F ! |
| ! ! !!!!_________18, 17, 16, 15 0..F ! |
| ! ! !!!__________22, 21, 20, 19 0..F ! |
| ! ! !!___________26, 25, 24, 23 0..F ! |
| ! ! !____________ 29, 28, 27 0..F ! |
| !--------------!------------------------------------------------------! |
| ! TAT ! Total Air Temperature ! |
| ! X999 ! (-60.0 to 99.9 deg C) ! |
| ! ! Negative values shall be indicated by '-' on the ! |
| ! ! first position. Otherwise the first position shall ! |
| ! ! be filled by '0'. ! |
| ! ! ADIRU 06.1.211.01 ! |
| ! ! 06.2.211.10 ! |
| !--------------!------------------------------------------------------! |
| ! ALT ! Standard Altitude (1013mbar) ! |
| ! X9999 ! (-2000 to 50000 ft) ! |
| ! ! Negative values shall be indicated by '-' on the ! |
| ! ! first position. Otherwise the first position shall ! |
| ! ! be used for the value. ! |
| ! ! ADIRU 06.1.203.01 ! |
| ! ! 06.2.203.10 ! |
| !--------------!------------------------------------------------------! |
| ! MN ! Mach Number ! |
| ! 999 ! (0.1 to 0.999) ! |
| ! ! ADIRU 06.1.205.01 ! |
| ! ! 06.2.205.10 ! |
| !--------------!------------------------------------------------------! |
| ! BLEED STATUS! ! |
| ! ! 99 1111 1 1111 99! |
| ! ! LH Pack Flow E.1.126.11_____!! !!!! ! !!!! !!! |
| ! ! 0 to 1.0 kg/sec (*) !!!! ! !!!! !!! |
| ! ! LH Wing AI/V Pos 29.1.001.11.18____!!!! ! !!!! !!! |
| ! ! Closed = 0 29.2.001.11.18 !!! ! !!!! !!! |
| ! ! Eng.1 Nacelle AI Pos 5D.2.061.10.28_____!!! ! !!!! !!! |
| ! ! Open = 1 !! ! !!!! !!! |
| ! ! Eng.1 PRV Pos. 6F.1.067.01.18______!! ! !!!! !!! |
| ! ! Fully Closed = 0 6F.2.067.10.17 ! ! !!!! !!! |
| ! ! Eng.1 HPV Pos. 6F.1.067.01.15_______! ! !!!! !!! |
| ! ! Fully Close = 0 6F.1.067.10.15 ! !!!! !!! |
| ! ! Cross Feed Valve Pos 29.1.055.01.16_________! !!!! !!! |
| ! ! Fully Closed = 0 29.2.055.01.16 !!!! !!! |
| ! ! Eng.2 HPV Pos. 6F.2.066.01.15___________!!!! !!! |
| ! ! Fully Closed = 0 6F.2.066.10.15 !!! !!! |
| ! ! Eng.2 PRV Pos. 6F.1.066.01.17____________!!! !!! |
| ! ! Fully Closed = 0 6F.2.066.10.17 !! !!! |
| ! ! Eng.2 Nacelle AI Pos 5D.2.061.10.27_____________!! !!! |
| ! ! Open = 1 ! !!! |
| ! ! RH Wing AI/V Pos. 29.1.001.00.18______________! !!! |
| ! ! Closed = 0 28.2.001.00.18 !!! |
| ! ! RH Pack Flow 8E.2.126.00___________________!!! |
| ! ! 0 to 1.0 Kg/sec (*) ! |
| ! ! (*) Remark: If the RH or LH Pack Flow shall be ! |
| ! ! displayed in lbs/sec, the range is 0.0 to! |
| ! ! 9.9 lbs/sec. ! |
| ! ! If the RH or LH Pack Flow value is ! |
| ! ! greater than the range display 'EE'. ! |
| !--------------!------------------------------------------------------! |
| ! APU ! APU Bleed Valve State ! |
| ! 1 ! Bit Status 1 = APU Bleed Valve Open ! |
| ! ! ECB 7A.1.037.01.11 ! |
| !--------------!------------------------------------------------------! |
| ! N1 ! Selected N1 Actual ! |
| ! 9999 ! (0 to 120.0 %rpm) ! |
| ! ! ECU 7C.1.346.01 Engine 1 ! |
| ! ! 7C.2.346.10 Engine 2 ! |
| ! ! Remark: In the report line V3 and V4 the values ! |
| ! ! from the last stable descent shall be ! |
| ! ! printed. ! |
| ! ! In the report line V5 and V6 the values ! |
| ! ! from the last stable climb shall be ! |
| ! ! printed. ! |
| !--------------!------------------------------------------------------! |
| ! N1C ! N1 Command ! |
| ! 9999 ! (0 to 120.0 %rpm) ! |
| ! ! ECU 7C.1.341.01 Engine 1 ! |
| ! ! 7C.2.341.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! N2 ! Selected N2 Actual ! |
| ! 9999 ! (0 to 120.0 %rpm) ! |
| ! ! ECU 7C.1.344.01 Engine 1 ! |
| ! ! 7C.2.344.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! EGT ! Selected T495 (Exhaust Gas Temperature) ! |
| ! X999 ! (-55 to 999.9 [C) ! |
| ! ! Negative values shall be indicated by '-' on the ! |
| ! ! first position. Otherwise the first position shall ! |
| ! ! be used for the value. ! |
| ! ! ECU 7C.1.345.01 Engine 1 ! |
| ! ! 7C.2.345.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! FF ! Engine Fuel Flow ! |
| ! 9999 ! 0 to 7000 kg/h (0 to 15000 p/h) ! |
| ! ! ECU 7C.1.244.01 Engine 1 ! |
| ! ! 7C.2.244.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! VN ! FAN Pick Up N1 Track Vibration ! |
| ! 99 ! (0.0 to 10.0) ! |
| ! ! If value is 10.0 then 99 shall be printed. ! |
| ! ! EVM 3D.1.227.01 Engine 1 ! |
| ! ! 3D.1.227.10 Engine 2 ! |
| ! ! Remark: In report line V3 and V4 the values from ! |
| ! ! the last stable descent shall be ! |
| ! ! printed. ! |
| ! ! In report line V5 and V6 the values from ! |
| ! ! the last stable climb shall be printed. ! |
| !--------------!------------------------------------------------------! |
| ! VC ! FAN Pick Up N2 Track Vibration ! |
| ! 99 ! (0.0 to 4.0) ! |
| ! ! EVM 3D.1.230.01 Engine 1 ! |
| ! ! 3D.1.230.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! VH ! TRF Pick Up N2 Track Vibration ! |
| ! 99 ! (0.0 to 4.0) ! |
| ! ! EVM 3D.1.230.11 Engine 1 ! |
| ! ! 3D.1.230.00 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! VL ! TRF Pick Up N1 Vibration ! |
| ! 99 ! (0.0 to 10.0) ! |
| ! ! If value is 10.0 then 99 shall be printed. ! |
| ! ! EVM 3D.1.227.11 Engine 1 ! |
| ! ! 3D.1.227.00 Engine 2 ! |
| ! ! Remark: In report line V3 and V4 the values frome ! |
| ! ! the last stable descent shall be ! |
| ! ! printed. ! |
| ! ! In report line V5 and V6 the values frome ! |
| ! ! the last stable climb shall be printed. ! |
| !--------------!------------------------------------------------------! |
| +---------------------------------------------------------------------+ |
(4) Engine Report O/R Data Field Description <05> (Engine Type CFMI with Advanced EVMU)
NOTE: Reports that are transmitted from the ACARS system do not have report lines without a line identifier.
| +---------------------------------------------------------------------+ |
| ! Value ! Content Description ! |
| !--------------!------------------------------------------------------! |
| ! ESN ! Engine Serial Number ! |
| ! 999999 ! (000000 to 999999) ! |
| ! ! ECU Engine 1 7C.1.046.01 digit 3, 2, 1 ! |
| ! ! 7C.1.047.01 digit 6, 5, 4 ! |
| ! ! Engine 2 7C.2.046.10 digit 3, 2, 1 ! |
| ! ! 7C.2.047.10 digit 6, 5, 4 ! |
| !--------------!------------------------------------------------------! |
| ! EHRS ! Engine Flight Hours ! |
| ! 99999 ! (00000 to 99999 hours) ! |
| ! ! DMU Engine 1 ! |
| ! ! Engine 2 ! |
| ! ! Remark: Time between "Main (LH and RH) Landing Gear! |
| ! ! Decompressed" and "Main (LH and RH) Landing! |
| ! ! Gear Compressed". The EHRS shall be set to ! |
| ! ! zero if a new ESN is recognized by the DMU.! |
| ! ! It shall be possible to set the EHRS via ! |
| ! ! the MCDU, e.g. if the DMU is changed on the! |
| ! ! a/c. ! |
| !--------------!------------------------------------------------------! |
| ! ERT ! Engine Running Time ! |
| ! 99999 ! (00000 to 65536 hours) ! |
| ! ! ECU 7C.1.050.01 Engine 1 ! |
| ! ! 7C.2.050.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! ECYC ! Engine Cycle ! |
| ! 99999 ! (00000 to 99999) ! |
| ! ! DMU Engine 1 ! |
| ! ! Engine 2 ! |
| ! ! Remark: Each time when flight phase 5 (climb) is ! |
| ! ! reached, the counter shall be incremented ! |
| ! ! by one. The ECYC is set to zero if a new ! |
| ! ! ESN is recognized by the DMU. It shall be ! |
| ! ! possible to set ECYC via the MCDU, if the ! |
| ! ! DMU is changed on the a/c. ! |
| !--------------!------------------------------------------------------! |
| ! AP ! Auto Pilot Status ! |
| ! 99 ! Number of respective status (00 to G8) ! |
| ! ! FMGC 1 and 2 (FGC part) for Auto Pilot AP1 and AP2 ! |
| ! ! ! |
| ! ! Parameter for AP1 ! Parameter for AP2 ! ! |
| ! ! Report Line EC: ! Report Line EE: !Definition: ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! / ! / !No Mode ! |
| ! ! ! !Active ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.11 = 1 ! 01.2.275.00.11 = 1!RUNWAY Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.12 = 1 ! 01.2.275.00.12 = 1!NAV Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.13 = 1 ! 01.2.275.00.13 = 1!LOC CAPTURE ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.14 = 1 ! 01.2.275.00.14 = 1!LOC TRACK ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.15 = 1 ! 01.2.275.00.15 = 1!Roll GO ! |
| ! ! ! !AROUND Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.16 = 1 ! 01.2.275.00.16 = 1!HEADING Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.17 = 1 ! 01.2.275.00.17 = 1!TRACK Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.15 = 1 ! 01.2.274.00.15 = 1!PITCH T/O ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.16 = 1 ! 01.2.274.00.16 = 1!PITCH GA Mode! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.17 = 1 ! 01.2.274.00.17 = 1!V/S Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.18 = 1 ! 01.2.274.00.18 = 1!FPA Mode ! |
| ! ! -------------------!-------------------!-------------! |
| ! ! 01.1.274.00.19 = 1 ! 01.2.274.00.19 = 1!ALT Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.20 = 1 ! 01.2.274.00.20 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.19 = 1 ! 01.2.274.00.19 = 1!ALT ACQ ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.21 = 1 ! 01.2.274.00.21 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.20 = 1 ! 01.2.274.00.20 = 1!G/S TRACK ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.22 = 1 ! 01.2.274.00.22 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.21 = 1 ! 01.2.274.00.21 = 1!G/S CAPTURE ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.22 = 1 ! 01.2.274.00.22 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.23 = 1 ! 01.2.274.00.23 = 1!FINAL DES ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.24 = 1 ! 01.2.274.00.24 = 1!EXPED. Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.146.00.14 = 1 ! 01.2.146.00.14 = 1!LAND TRACK ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!CLB Mode ! |
| ! ! AND ! AND ! ! |
| ! ! ! ! ! ! ! |
| ! ! -------------- ! -------------- ! ! |
| ! ! 01.1.274.00.13 = 0 ! 01.2.274.00.13 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.14 = 0 ! 01.2.274.00.14 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.24 = 0 ! 01.2.274.00.24 = 0! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!DES Mode ! |
| ! ! AND ! AND ! ! |
| ! ! ! ! ! ! ! |
| ! ! -------------- ! -------------- ! ! |
| ! ! 01.1.274.00.13 = 0 ! 01.2.274.00.13 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.14 = 0 ! 01.2.274.00.14 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.24 = 0 ! 01.2.274.00.24 = 0! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!IM. CLIMB ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.13 = 1 ! 01.2.274.00.13 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!IM. DES Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.13 = 1 ! 01.2.274.00.13 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!OPEN CLB ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.14 = 1 ! 01.2.274.00.14 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!OPEN. DES ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.14 = 1 ! 01.2.274.00.14 = 1! ! |
| ! ! ---------------------------------------------------- ! |
| ! ! Auto Pilot Status DMU: ! |
| ! ! Auto Pilot AP1 printed in report line EC ! |
| ! ! Auto Pilot AP2 printed in report line EE ! |
| ! ! Combined Auto Pilot Modes ! |
| ! ! The longitudinal auto pilot mode (1 to G) shall ! |
| ! ! appear on the left position for the AP1 and AP2 print! |
| ! ! format. ! |
| ! ! The lateral auto pilot mode (1 to 8) shall appear on ! |
| ! ! the right position for the AP1 and AP2 print format. ! |
| ! ! In case of a combined auto pilot mode e.g. DES mode ! |
| ! ! and NAV mode are engaged simultaneously, the 'E3' ! |
| ! ! shall appear below AP1 and AP2. ! |
| ! ! XX Auto Pilot Modes: ! |
| ! ! !! ! |
| ! ! !!__Lateral Modes: 0 = NO MODE ! |
| ! ! ! 1 = HEADING ! |
| ! ! ! 2 = TRACK ! |
| ! ! ! 3 = NAV ! |
| ! ! ! 4 = LOC CAPTURE ! |
| ! ! ! 5 = LOCK TRACK ! |
| ! ! ! 6 = LAND TRACK ! |
| ! ! ! 7 = RUNWAY ! |
| ! ! ! 8 = ROLL GO AROUND ! |
| ! ! ! ! |
| ! ! !__Longitudinal Modes: 0 = NO MODE ! |
| ! ! 1 = PITCH G/A ! |
| ! ! 2 = PITCH TO ! |
| ! ! 3 = G/S TRACK ! |
| ! ! 4 = G/S CAPTURE ! |
| ! ! 5 = V/S ! |
| ! ! 6 = FPA ! |
| ! ! 7 = ALT ! |
| ! ! 8 = ALT ACQ ! |
| ! ! 9 = OPEN CLB ! |
| ! ! A = OPEN DES ! |
| ! ! B = IM CLB ! |
| ! ! C = IM DES ! |
| ! ! D = CLB ! |
| ! ! E = DES ! |
| ! ! F = FINAL DES ! |
| ! ! G = EXPEDITE ! |
| !--------------!------------------------------------------------------! |
| ! ECW2 ! Engine Control Word 2 ! |
| ! XXXXX ! XXXXX Bits HEX ! |
| ! ! !!!!!________14, 13, 12, 11 0..F ! |
| ! ! !!!!_________18, 17, 16, 15 0..F ! |
| ! ! !!!__________22, 21, 20, 19 0..F ! |
| ! ! !!___________26, 25, 24, 23 0..F ! |
| ! ! !____________ 29, 28, 27 0..F ! |
| ! ! Bit Label Parameter Description ! |
| ! ! 11 7C.X.272.XX.12 = 1 Bump/Overboost #1 Enable ! |
| ! ! 12 7C.X.272.XX.13 = 1 Bump/Overboost #2 Enable ! |
| ! ! 13 7C.X.272.XX.14 = 1 Bump/Overboost #3 Enable ! |
| ! ! 14 7C.X.272.XX.22 = 1 MTO. GA Limit Mode Selected! |
| ! ! 15 7C.X.272.XX.23 = 1 Flex Take Off Limit Mode ! |
| ! ! Selected ! |
| ! ! 16 SPARE ! |
| ! ! 17 SPARE ! |
| ! ! 18 SPARE ! |
| ! ! 19 SPARE ! |
| ! ! 20 SPARE ! |
| ! ! 21 SPARE ! |
| ! ! 22 SPARE ! |
| ! ! 23 SPARE ! |
| ! ! 24 SPARE ! |
| ! ! 25 SPARE ! |
| ! ! 26 SPARE ! |
| ! ! 27 SPARE ! |
| ! ! 28 SPARE ! |
| ! ! 29 SPARE ! |
| ! ! The 'X' for the System and SDI definition of the ! |
| ! ! engine parameters shall be as follows: ! |
| ! ! System SDI ! |
| ! ! Engine 1 1 01 ! |
| ! ! Engine 2 2 10 ! |
| !--------------!------------------------------------------------------! |
| ! ECW5 ! Engine Control Word 5 ! |
| ! XXXXX ! XXXXX Bits HEX ! |
| ! ! !!!!!________14, 13, 12, 11 0..F ! |
| ! ! !!!!_________18, 17, 16, 15 0..F ! |
| ! ! !!!__________22, 21, 20, 19 0..F ! |
| ! ! !!___________26, 25, 24, 23 0..F ! |
| ! ! !____________ 29, 28, 27 0..F ! |
| ! ! Bit Label Parameter Description ! |
| ! ! 11 7C.X.270.XX.11 = 1 Ignition 1 Primary Selected ! |
| ! ! 12 SPARE ! |
| ! ! 13 7C.X.270.XX.13 = 1 Starter Air Valve Open ! |
| ! ! Local Switch ! |
| ! ! 14 7C.X.270.XX.14 = 1 HP Fuel Valve Closed Local ! |
| ! ! 15 7C.X.270.XX.15 = 1 SAV Demand/Position Disagree! |
| ! ! 16 7C.X.270.XX.16 = 1 HPSOV Demand/Position ! |
| ! ! Disagree ! |
| ! ! 17 7C.X.270.XX.17 = 1 Start EGT Overtemp-Detected ! |
| ! ! 18 7C.X.270.XX.18 = 1 Start Stall Detected ! |
| ! ! 19 7C.X.270.XX.19 = 1 No/Low Fan Speed for Core ! |
| ! ! Speed ! |
| ! ! 20 7C.X.270.XX.20 = 1 No Engine Light Off Detected! |
| ! ! 21 7C.X.270.XX.21 = 1 Starter Time Limit Exceeded ! |
| ! ! 22 7C.X.270.XX.22 = 1 Fuel Schedule Derich Active ! |
| ! ! 23 7C.X.270.XX.23 = 1 TLA Not at Idle for Start ! |
| ! ! Initiation ! |
| ! ! 24 SPARE ! |
| ! ! 25 7C.X.270.XX.25 = 1 Low Sap-(Slow Start) ! |
| ! ! Detected ! |
| ! ! 26 7C.X.270.XX.28 = 1 50% Thrust Limit Active ! |
| ! ! 27 SPARE ! |
| ! ! 28 SPARE ! |
| ! ! 29 SPARE ! |
| ! ! The 'X' for the System and SDI definition of the ! |
| ! ! engine parameters shall be as follows: ! |
| ! ! System SDI ! |
| ! ! Engine 1 1 01 ! |
| ! ! Engine 2 2 10 ! |
| !--------------!------------------------------------------------------! |
| ! EVM ! Engine Vibration Status Word ! |
| ! XXXXX ! EVM 3D.1.035.01 Engine 1 ! |
| ! ! 3D.1.035.10 Engine 2 ! |
| ! ! XXXXX Bits HEX ! |
| ! ! !!!!!________14, 13, 12, 11 0..F ! |
| ! ! !!!!_________18, 17, 16, 15 0..F ! |
| ! ! !!!__________22, 21, 20, 19 0..F ! |
| ! ! !!___________26, 25, 24, 23 0..F ! |
| ! ! !____________ 29, 28, 27 0..F ! |
| !--------------!------------------------------------------------------! |
| ! TAT/ALT/MN/ ! Parameter in Report Line C1/CE: Ambient Condition ! |
| ! BLEED STATUS! at the time S1/T1 ! |
| ! /APU ! Parameter in Report Line C2: Ambient Condition ! |
| ! ! at the time V1/X1l ! |
| !--------------!------------------------------------------------------! |
| ! N1 ! Selected N1 Actual ! |
| ! 9999 ! (0 to 120.0 %rpm) ! |
| ! ! ECU 7C.1.346.01 Engine 1 ! |
| ! ! 7C.2.346.10 Engine 2 ! |
| ! ! Remark: In the report line V3 and V4 the values ! |
| ! ! from the last stable descent shall be ! |
| ! ! printed. ! |
| ! ! In the report line V5 and V6 the values ! |
| ! ! from the last stable climb shall be ! |
| ! ! printed. ! |
| !--------------!------------------------------------------------------! |
| ! N1C ! N1 Command ! |
| ! 9999 ! (0 to 120.0 %rpm) ! |
| ! ! ECU 7C.1.341.01 Engine 1 ! |
| ! ! 7C.2.341.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! N2 ! Selected N2 Actual ! |
| ! 9999 ! (0 to 120.0 %rpm) ! |
| ! ! ECU 7C.1.344.01 Engine 1 ! |
| ! ! 7C.2.344.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! EGT ! Selected T495 (Exhaust Gas Temperature) ! |
| ! X999 ! (-55 to 999.9 [C) ! |
| ! ! Negative values are indicated by 'N' on the ! |
| ! ! first position. Otherwise the first position is ! |
| ! ! used for the value. ! |
| ! ! ECU 7C.1.345.01 Engine 1 ! |
| ! ! 7C.2.345.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! FF ! Engine Fuel Flow ! |
| ! 9999 ! 0 to 7000 kg/h (0 to 15000 p/h) ! |
| ! ! ECU 7C.1.244.01 Engine 1 ! |
| ! ! 7C.2.244.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! VN ! FAN Pick Up N1 Track Vibration ! |
| ! 99 ! (0.0 to 10.0) ! |
| ! ! If value is 10.0 then 99 shall be printed. ! |
| ! ! EVM 3D.1.227.01 Engine 1 ! |
| ! ! 3D.1.227.10 Engine 2 ! |
| ! ! Remark: In report line V3 and V4 the values from ! |
| ! ! the last stable descent shall be ! |
| ! ! printed. ! |
| ! ! In report line V5 and V6 the values from ! |
| ! ! the last stable climb shall be printed. ! |
| !--------------!------------------------------------------------------! |
| ! VC ! FAN Pick Up N2 Track Vibration ! |
| ! 99 ! (0.0 to 4.0) ! |
| ! ! EVM 3D.1.230.01 Engine 1 ! |
| ! ! 3D.1.230.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! VH ! TRF Pick Up N2 Track Vibration ! |
| ! 99 ! (0.0 to 4.0) ! |
| ! ! EVM 3D.1.230.11 Engine 1 ! |
| ! ! 3D.1.230.00 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! VL ! TRF Pick Up N1 Vibration ! |
| ! 99 ! (0.0 to 10.0) ! |
| ! ! If value is 10.0 then 99 shall be printed. ! |
| ! ! EVM 3D.1.227.11 Engine 1 ! |
| ! ! 3D.1.227.00 Engine 2 ! |
| ! ! Remark: In report line V3 and V4 the values frome ! |
| ! ! the last stable descent shall be ! |
| ! ! printed. ! |
| ! ! In report line V5 and V6 the values frome ! |
| ! ! the last stable climb shall be printed. ! |
| +---------------------------------------------------------------------+ |
(5) Engine Report O/R Data Field Description <05> (Engine Type CFMI with Advanced EVMU)
NOTE: Reports that are transmitted from the ACARS system do not have report lines without a line identifier.
NOTE: Only the parts of the ENGINE O/R <05> which are not included in the ENGINE CRUISE REPORT <01> are given in the subsequent table.
| +---------------------------------------------------------------------+ |
| ! Value ! Content Description ! |
| !--------------!------------------------------------------------------! |
| ! ECW2 ! Engine Control Word 2 ! |
| ! XXXXX ! XXXXX Bits HEX ! |
| ! ! !!!!!________14, 13, 12, 11 0..F ! |
| ! ! !!!!_________18, 17, 16, 15 0..F ! |
| ! ! !!!__________22, 21, 20, 19 0..F ! |
| ! ! !!___________26, 25, 24, 23 0..F ! |
| ! ! !____________ 29, 28, 27 0..F ! |
| ! ! Bit Label Parameter Description ! |
| ! ! 11 7C.X.272.XX.12 = 1 Bump/Overboost #1 Enable ! |
| ! ! 12 7C.X.272.XX.13 = 1 Bump/Overboost #2 Enable ! |
| ! ! 13 7C.X.272.XX.14 = 1 Bump/Overboost #3 Enable ! |
| ! ! 14 7C.X.272.XX.22 = 1 MTO. GA Limit Mode Selected! |
| ! ! 15 7C.X.272.XX.23 = 1 Flex Take Off Limit Mode ! |
| ! ! Selected ! |
| ! ! 16 SPARE ! |
| ! ! 17 SPARE ! |
| ! ! 18 SPARE ! |
| ! ! 19 SPARE ! |
| ! ! 20 SPARE ! |
| ! ! 21 SPARE ! |
| ! ! 22 SPARE ! |
| ! ! 23 SPARE ! |
| ! ! 24 SPARE ! |
| ! ! 25 SPARE ! |
| ! ! 26 SPARE ! |
| ! ! 27 SPARE ! |
| ! ! 28 SPARE ! |
| ! ! 29 SPARE ! |
| ! ! The 'X' for the System and SDI definition of the ! |
| ! ! engine parameters is as follows: ! |
| ! ! System SDI ! |
| ! ! Engine 1 1 01 ! |
| ! ! Engine 2 2 10 ! |
| !--------------!------------------------------------------------------! |
| ! ECW5 ! Engine Control Word 5 ! |
| ! XXXXX ! XXXXX Bits HEX ! |
| ! ! !!!!!________14, 13, 12, 11 0..F ! |
| ! ! !!!!_________18, 17, 16, 15 0..F ! |
| ! ! !!!__________22, 21, 20, 19 0..F ! |
| ! ! !!___________26, 25, 24, 23 0..F ! |
| ! ! !____________ 29, 28, 27 0..F ! |
| ! ! Bit Label Parameter Description ! |
| ! ! 11 7C.X.270.XX.11 = 1 Ignition 1 Primary Selected ! |
| ! ! 12 SPARE ! |
| ! ! 13 7C.X.270.XX.13 = 1 Starter Air Valve Open ! |
| ! ! Local Switch ! |
| ! ! 14 7C.X.270.XX.14 = 1 HP Fuel Valve Closed Local ! |
| ! ! 15 7C.X.270.XX.15 = 1 SAV Demand/Position Disagree! |
| ! ! 16 7C.X.270.XX.16 = 1 HPSOV Demand/Position ! |
| ! ! Disagree ! |
| ! ! 17 7C.X.270.XX.17 = 1 Start EGT Overtemp-Detected ! |
| ! ! 18 7C.X.270.XX.18 = 1 Start Stall Detected ! |
| ! ! 19 7C.X.270.XX.19 = 1 No/Low Fan Speed for Core ! |
| ! ! Speed ! |
| ! ! 20 7C.X.270.XX.20 = 1 No Engine Light Off Detected! |
| ! ! 21 7C.X.270.XX.21 = 1 Starter Time Limit Exceeded ! |
| ! ! 22 7C.X.270.XX.22 = 1 Fuel Schedule Derich Active ! |
| ! ! 23 7C.X.270.XX.23 = 1 TLA Not at Idle for Start ! |
| ! ! Initiation ! |
| ! ! 24 SPARE ! |
| ! ! 25 7C.X.270.XX.25 = 1 Low Sap-(Slow Start) ! |
| ! ! Detected ! |
| ! ! 26 7C.X.275.XX.28 = 1 All Channel Controls Active ! |
| ! ! 27 SPARE ! |
| ! ! 28 SPARE ! |
| ! ! 29 SPARE ! |
| ! ! The 'X' for the System and SDI definition of the ! |
| ! ! engine parameters is as follows: ! |
| ! ! System SDI ! |
| ! ! Engine 1 1 01 ! |
| ! ! Engine 2 2 10 ! |
| !--------------!------------------------------------------------------! |
| ! TAT ! Total Air Temperature ! |
| ! X999 ! (-60.0 to 99.9 deg C) ! |
| ! ! Negative values are shown with '-' on the first ! |
| ! ! position. Otherwise the first position contains a ! |
| ! ! a '0'. ! |
| ! ! ADIRU 06.1.211.01 ! |
| ! ! 06.2.211.10# ! |
| !--------------!------------------------------------------------------! |
| ! ALT ! Standard Altitude (1013 mbar) ! |
| ! X9999 ! (-2000 to 50000 ft) ! |
| ! ! Negative values are shown with '-' on the first ! |
| ! ! position. Otherwise the first position is used for ! |
| ! ! the value. ! |
| ! ! ADIRU 06.1.203.01 ! |
| ! ! 06.2.203.10# ! |
| !--------------!------------------------------------------------------! |
| ! MN ! Mach Number ! |
| ! 999 ! (0.100 to 0.999) ! |
| ! ! ADIRU 06.1.205.01 ! |
| ! ! 06.2.205.10# ! |
| !--------------!------------------------------------------------------! |
| ! BLEED STATUS ! Discrete and numeric coded information ! |
| ! ! 99 1111 1 1111 99 ! |
| ! ! ^^ !!!! ! !!!! ^^ ! |
| ! ! ! !!!! ! !!!! !__ 8E.2.126.00 RH Pack Flow ! |
| ! ! ! !!!! ! !!!! 0 to 1.0 kg/sec. ! |
| ! ! ! !!!! ! !!!!____ 29.1.001.00.18 RH Wing AI/V Pos ! |
| ! ! ! !!!! ! !!! 29.2.001.00.18# Closed = 0 ! |
| ! ! ! !!!! ! !!!_____ 5D.2.061.10.27 Eng.2 Nascelle ! |
| ! ! ! !!!! ! !! AI Pos. Open = 1 ! |
| ! ! ! !!!! ! !!______ 6F.2.066.01.17 Eng.2 PRV Pos. ! |
| ! ! ! !!!! ! ! 6F.2.066.10.17# Fully Closed = 0! |
| ! ! ! !!!! ! !_______ 6F.2.066.01.15 Eng.2 HPV Pos. ! |
| ! ! ! !!!! ! 6F.2.066.10.15# Fully Closed = 0! |
| ! ! ! !!!! !_________ 29.1.055.01.16 Cross Feed Valve ! |
| ! ! ! !!!! 29.2.055.01.16# Pos Fully Clo.=0! |
| ! ! ! !!!!___________ 6F.1.067.01.15 Eng.1 HPV Pos. ! |
| ! ! ! !!! 6F.1.067.10.15# Fully Close = 0 ! |
| ! ! ! !!!____________ 6F.1.067.01.17 Eng.1 PRV Pos. ! |
| ! ! ! !! 6F.2.067.10.17# Fully Closed = 0! |
| ! ! ! !!_____________ 5D.2.061.10.28 Eng.1 Nacelle AI ! |
| ! ! ! ! Pos. Open = 1 ! |
| ! ! ! !______________ 29.1.001.11.18 LH Wing AI/V Pos ! |
| ! ! ! 29.2.001.11.18# Closed = 0 ! |
| ! ! !________________ 8E.1.126.11 LH Pack Flow ! |
| ! ! 0 to 1.0 kg/sec.! |
| ! ! ! |
| !--------------!------------------------------------------------------! |
| ! APU ! APU Bleed Valve State ! |
| ! 1 ! APU Bleed V. State param. 7A.1.037.01.11 ! |
| ! ! APU Bleed Valve Open =1 ! |
| +---------------------------------------------------------------------+ |
(6) Engine Report O/R Data Field Description <05> (Engine Type CFMI with Advanced EVMU)
NOTE: Reports that are transmitted from the ACARS system do not have report lines without a line identifier.
NOTE: Only the parts of the ENGINE O/R <05> which are not included in the ENGINE CRUISE REPORT <01> are given in the subsequent table.
| +---------------------------------------------------------------------+ |
| ! Value ! Content Description ! |
| !--------------!------------------------------------------------------! |
| ! ECW2 ! Engine Control Word 2 ! |
| ! XXXXX ! XXXXX Bits HEX ! |
| ! ! !!!!!________14, 13, 12, 11 0..F ! |
| ! ! !!!!_________18, 17, 16, 15 0..F ! |
| ! ! !!!__________22, 21, 20, 19 0..F ! |
| ! ! !!___________26, 25, 24, 23 0..F ! |
| ! ! !____________ 29, 28, 27 0..7 ! |
| ! ! Bit Label Parameter Description ! |
| ! ! 11 7C.X.272.XX.12 = 1 Bump/Overboost #1 Enable ! |
| ! ! 12 7C.X.272.XX.13 = 1 Bump/Overboost #2 Enable ! |
| ! ! 13 7C.X.272.XX.14 = 1 Bump/Overboost #3 Enable ! |
| ! ! 14 7C.X.272.XX.22 = 1 MTO. GA Limit Mode Selected! |
| ! ! 15 7C.X.272.XX.23 = 1 Flex Take Off Limit Mode ! |
| ! ! Selected ! |
| ! ! 16 SPARE ! |
| ! ! 17 SPARE ! |
| ! ! 18 SPARE ! |
| ! ! 19 SPARE ! |
| ! ! 20 SPARE ! |
| ! ! 21 SPARE ! |
| ! ! 22 SPARE ! |
| ! ! 23 SPARE ! |
| ! ! 24 SPARE ! |
| ! ! 25 SPARE ! |
| ! ! 26 SPARE ! |
| ! ! 27 SPARE ! |
| ! ! 28 SPARE ! |
| ! ! 29 SPARE ! |
| ! ! The 'X' for the System and SDI definition of the ! |
| ! ! engine parameters is as follows: ! |
| ! ! System SDI ! |
| ! ! Engine 1 1 01 ! |
| ! ! Engine 2 2 10 ! |
| !--------------!------------------------------------------------------! |
| ! ECW5 ! Engine Control Word 5 ! |
| ! XXXXX ! XXXXX Bits HEX ! |
| ! ! !!!!!________14, 13, 12, 11 0..F ! |
| ! ! !!!!_________18, 17, 16, 15 0..F ! |
| ! ! !!!__________22, 21, 20, 19 0..F ! |
| ! ! !!___________26, 25, 24, 23 0..F ! |
| ! ! !____________ 29, 28, 27 0..7 ! |
| ! ! Bit Label Parameter Description ! |
| ! ! 11 7C.X.270.XX.11 = 1 Ignition 1 Primary Selected ! |
| ! ! 12 SPARE ! |
| ! ! 13 7C.X.270.XX.13 = 1 Starter Air Valve Open ! |
| ! ! Local Switch ! |
| ! ! 14 7C.X.270.XX.14 = 1 HP Fuel Valve Closed Local ! |
| ! ! 15 7C.X.270.XX.15 = 1 SAV Demand/Position Disagree! |
| ! ! 16 7C.X.270.XX.16 = 1 HPSOV Demand/Position ! |
| ! ! Disagree ! |
| ! ! 17 7C.X.270.XX.17 = 1 Start EGT Overtemp-Detected ! |
| ! ! 18 7C.X.270.XX.18 = 1 Start Stall Detected ! |
| ! ! 19 7C.X.270.XX.19 = 1 No/Low Fan Speed for Core ! |
| ! ! Speed ! |
| ! ! 20 7C.X.270.XX.20 = 1 No Engine Light Off Detected! |
| ! ! 21 7C.X.270.XX.21 = 1 Starter Time Limit Exceeded ! |
| ! ! 22 7C.X.270.XX.22 = 1 Fuel Schedule Derich Active ! |
| ! ! 23 7C.X.270.XX.23 = 1 TLA Not at Idle for Start ! |
| ! ! Initiation ! |
| ! ! 24 SPARE ! |
| ! ! 25 7C.X.270.XX.25 = 1 Low Sap-(Slow Start) ! |
| ! ! Detected ! |
| ! ! 26 7C.X.270.XX.28 = 1 50% Thrust Limit Active ! |
| ! ! 27 SPARE ! |
| ! ! 28 SPARE ! |
| ! ! 29 SPARE ! |
| ! ! The 'X' for the System and SDI definition of the ! |
| ! ! engine parameters is as follows: ! |
| ! ! System SDI ! |
| ! ! Engine 1 1 01 ! |
| ! ! Engine 2 2 10 ! |
| !--------------!------------------------------------------------------! |
| ! TAT/ALT/MN/ ! For parameter description see "Standard Header for ! |
| ! BLEED STATUS! Print Reports" ! |
| ! /APU ! Parameter in Report Line C1/CE: Ambient Condition ! |
| ! ! at the time "S1"/"T1" ! |
| ! ! Parameter in Report Line C2: Ambient Condition ! |
| ! ! at the time "V1"/"X1" ! |
| +---------------------------------------------------------------------+ |
(7) Engine Report O/R Data Field Description <05> (Engine Type CFMI with Advanced EVMU)
NOTE: Reports that are transmitted from the ACARS system do not have report lines without a line identifier.
NOTE: Only the parts of the ENGINE O/R <05> which are not included in the ENGINE CRUISE REPORT <01> are given in the subsequent table.
| +---------------------------------------------------------------------+ |
| ! Value ! Content Description ! |
| !--------------!------------------------------------------------------! |
| ! ECW2 ! Engine Control Word 2 ! |
| ! XXXXX ! XXXXX Bits HEX ! |
| ! ! !!!!!________14, 13, 12, 11 0..F ! |
| ! ! !!!!_________18, 17, 16, 15 0..F ! |
| ! ! !!!__________22, 21, 20, 19 0..F ! |
| ! ! !!___________26, 25, 24, 23 0..F ! |
| ! ! !____________ 29, 28, 27 0..7 ! |
| ! ! Bit Label Parameter Description ! |
| ! ! 11 7C.X.272.XX.12 = 1 Bump/Overboost #1 Enable ! |
| ! ! 12 7C.X.272.XX.13 = 1 Bump/Overboost #2 Enable ! |
| ! ! 13 7C.X.272.XX.14 = 1 Bump/Overboost #3 Enable ! |
| ! ! 14 7C.X.272.XX.22 = 1 MTO. GA Limit Mode ! |
| ! ! Selection ! |
| ! ! 15 7C.X.272.XX.23 = 1 Flex Take Off Limit Mode ! |
| ! ! Selection ! |
| ! ! 16 SPARE ! |
| ! ! 17 SPARE ! |
| ! ! 18 SPARE ! |
| ! ! 19 SPARE ! |
| ! ! 20 SPARE ! |
| ! ! 21 SPARE ! |
| ! ! 22 SPARE ! |
| ! ! 23 SPARE ! |
| ! ! 24 SPARE ! |
| ! ! 25 SPARE ! |
| ! ! 26 SPARE ! |
| ! ! 27 SPARE ! |
| ! ! 28 SPARE ! |
| ! ! 29 SPARE ! |
| ! ! The 'X' for the System and SDI definition of the ! |
| ! ! engine parameters is as follows: ! |
| ! ! System SDI ! |
| ! ! Engine 1 1 01 ! |
| ! ! Engine 2 2 10 ! |
| !--------------!------------------------------------------------------! |
| ! ECW5 ! Engine Control Word 5 ! |
| ! XXXXX ! XXXXX Bits HEX ! |
| ! ! !!!!!________14, 13, 12, 11 0..F ! |
| ! ! !!!!_________18, 17, 16, 15 0..F ! |
| ! ! !!!__________22, 21, 20, 19 0..F ! |
| ! ! !!___________26, 25, 24, 23 0..F ! |
| ! ! !____________ 29, 28, 27 0..7 ! |
| ! ! Bit Label Parameter Description ! |
| ! ! 11 7C.X.270.XX.11 = 1 Ignition 1 Primary Selected ! |
| ! ! 12 SPARE ! |
| ! ! 13 7C.X.270.XX.13 = 1 Starter Air Valve Open ! |
| ! ! Local Switch ! |
| ! ! 14 7C.X.270.XX.14 = 1 HP Fuel Valve Closed Local ! |
| ! ! 15 7C.X.270.XX.15 = 1 SAV Demand/Position Disagree! |
| ! ! 16 7C.X.270.XX.16 = 1 HPSOV Demand/Position ! |
| ! ! Disagree ! |
| ! ! 17 7C.X.270.XX.17 = 1 Start EGT Overtemp-Detected ! |
| ! ! 18 7C.X.270.XX.18 = 1 Start Stall Detected ! |
| ! ! 19 7C.X.270.XX.19 = 1 No/Low Fan Speed for Core ! |
| ! ! Speed ! |
| ! ! 20 7C.X.270.XX.20 = 1 No Engine Light Off Detected! |
| ! ! 21 7C.X.270.XX.21 = 1 Starter Time Limit Exceeded ! |
| ! ! 22 7C.X.270.XX.22 = 1 Fuel Schedule Derich Active ! |
| ! ! 23 7C.X.270.XX.23 = 1 TLA Not at Idle for Start ! |
| ! ! Initiation ! |
| ! ! 24 SPARE ! |
| ! ! 25 7C.X.270.XX.25 = 1 Low Sap - (Slow Start) ! |
| ! ! Detected ! |
| ! ! 26 7C.X.275.XX.28 = 1 All Channel Controls Active ! |
| ! ! 27 SPARE ! |
| ! ! 28 SPARE ! |
| ! ! 29 SPARE ! |
| ! ! The 'X' for the System and SDI definition of the ! |
| ! ! engine parameters is as follows: ! |
| ! ! System SDI ! |
| ! ! Engine 1 1 01 ! |
| ! ! Engine 2 2 10 ! |
| !--------------!------------------------------------------------------! |
| ! TAT/ALT/MN/ ! For parameter description see "Standard Header for ! |
| ! BLEED STATUS! Print Reports" ! |
| ! /APU ! Parameter in Report Line C1/CE: Ambient Condition ! |
| ! ! at the time "S1"/"T1" ! |
| ! ! Parameter in Report Line C2: Ambient Condition ! |
| ! ! at the time "V1"/"X1" ! |
| +---------------------------------------------------------------------+ |
(8) Parameter Logic
| +---------------------------------------------------------------------+ |
| ! Param. ! Print Value (Standard Progr.) ! |
| !--------------!------------------------------------------------------! |
| ! ESN ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! EHRS ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! ERT ! Value at moment of trigger ! |
| !--------------! -----------------------------------------------------! |
| ! ECYC ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! AP ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! ECW2 ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! ECW5 ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! EVM ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! N1C ! Snapshot at 1 sec intervals. ! |
| !--------------!------------------------------------------------------! |
| ! N2 ! Snapshot at 1 sec intervals. ! |
| !--------------!------------------------------------------------------! |
| ! EGT ! Snapshot at 1 sec intervals. ! |
| !--------------!------------------------------------------------------! |
| ! FF ! Snapshot at 1 sec intervals. ! |
| !--------------!------------------------------------------------------! |
| ! N1 ! Snapshot at 1 sec intervals. ! |
| !--------------!------------------------------------------------------! |
| ! VN ! Snapshot at 1 sec intervals. ! |
| !--------------!------------------------------------------------------! |
| ! VL ! Snapshot at 1 sec intervals. ! |
| !--------------!------------------------------------------------------! |
| ! VC ! Snapshot at 1 sec intervals. ! |
| !--------------!------------------------------------------------------! |
| ! VH ! Snapshot at 1 sec intervals. ! |
| !--------------!------------------------------------------------------! |
| ! TAT ! Report Line CE at 5 second pre-event ! |
| ! ! Report Line C2 at 5 second post-event ! |
| !--------------!------------------------------------------------------! |
| ! ALT ! Report Line CE at 5 second pre-event ! |
| ! ! Report Line C2 at 5 second post-event ! |
| !--------------!------------------------------------------------------! |
| ! MN ! Report Line CE at 5 second pre-event ! |
| ! ! Report Line C2 at 5 second post-event ! |
| !--------------!------------------------------------------------------! |
| ! BLEED ! Report Line C1 at 5 second pre-event ! |
| ! STATUS ! Report Line C2 at 5 second post-event ! |
| !--------------!------------------------------------------------------! |
| ! APU ! Report Line C1 at 5 second pre-event ! |
| ! ! Report Line C2 at 5 second post-event ! |
| +---------------------------------------------------------------------+ |
(9) Parameter Logic
| +---------------------------------------------------------------------+ |
| ! Param. ! Print Value (Standard Progr.) ! |
| !--------------!------------------------------------------------------! |
| ! ESN ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! EHRS ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! ERT ! Value at moment of trigger ! |
| !--------------! -----------------------------------------------------! |
| ! ECYC ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! AP ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! ECW2 ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! ECW5 ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! EVM ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! TAT ! Report line CE at 5 sec. pre-event ! |
| ! ! Report line C2 at 5 sec. post-event ! |
| !--------------!------------------------------------------------------! |
| ! ALT ! Report line CE at 5 sec. pre-event ! |
| ! ! Report line C2 at 5 sec. post-event ! |
| !--------------!------------------------------------------------------! |
| ! MN ! Report line CE at 5 sec. pre-event ! |
| ! ! Report line C2 at 5 sec. post-event ! |
| !--------------!------------------------------------------------------! |
| ! BLEED ! Report line C1 at 5 sec. pre-event ! |
| ! STATUS ! Report line C2 at 5 sec. post-event ! |
| !--------------!------------------------------------------------------! |
| ! APU ! Report line C1 at 5 sec. pre-event ! |
| ! ! Report line C2 at 5 sec. post-event ! |
| !--------------!------------------------------------------------------! |
| ! N1C ! Snapshot at 1 sec intervals. ! |
| !--------------!------------------------------------------------------! |
| ! N2 ! Snapshot at 1 sec intervals. ! |
| !--------------!------------------------------------------------------! |
| ! EGT ! Snapshot at 1 sec intervals. ! |
| !--------------!------------------------------------------------------! |
| ! FF ! Snapshot at 1 sec intervals. ! |
| !--------------!------------------------------------------------------! |
| ! N1 ! Snapshot at 1 sec intervals. ! |
| !--------------!------------------------------------------------------! |
| ! VN ! Snapshot at 1 sec intervals. ! |
| !--------------!------------------------------------------------------! |
| ! VL ! Snapshot at 1 sec intervals. ! |
| !--------------!------------------------------------------------------! |
| ! VC ! Snapshot at 1 sec intervals. ! |
| !--------------!------------------------------------------------------! |
| ! VH ! Snapshot at 1 sec intervals. ! |
| +---------------------------------------------------------------------+ |
(10) Parameter Logic
| +---------------------------------------------------------------------+ |
| ! Param. ! Print Value (Standard Progr.) ! |
| !--------------!------------------------------------------------------! |
| ! ESN ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! EHRS ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! ERT ! Value at moment of trigger ! |
| !--------------! -----------------------------------------------------! |
| ! ECYC ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! AP ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! ECW2 ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! ECW5 ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! EVM ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! TAT ! Report line CE at 5 sec. pre-event ! |
| ! ! Report line C2 at 5 sec. post-event ! |
| !--------------!------------------------------------------------------! |
| ! ALT ! Report line CE at 5 sec. pre-event ! |
| ! ! Report line C2 at 5 sec. post-event ! |
| !--------------!------------------------------------------------------! |
| ! MN ! Report line CE at 5 sec. pre-event ! |
| ! ! Report line C2 at 5 sec. post-event ! |
| !--------------!------------------------------------------------------! |
| ! BLEED ! Report line C1 at 5 sec. pre-event ! |
| ! STATUS ! Report line C2 at 5 sec. post-event ! |
| !--------------!------------------------------------------------------! |
| ! APU ! Report line C1 at 5 sec. pre-event ! |
| ! ! Report line C2 at 5 sec. post-event ! |
| !--------------!------------------------------------------------------! |
| ! N1 ! Snapshot at 1 sec intervals. ! |
| !--------------!------------------------------------------------------! |
| ! N1C ! Snapshot at 1 sec intervals. ! |
| !--------------!------------------------------------------------------! |
| ! N2 ! Snapshot at 1 sec intervals. ! |
| !--------------!------------------------------------------------------! |
| ! EGT ! Snapshot at 1 sec intervals. ! |
| !--------------!------------------------------------------------------! |
| ! FF ! Snapshot at 1 sec intervals. ! |
| !--------------!------------------------------------------------------! |
| ! VN ! Snapshot at 1 sec intervals. ! |
| !--------------!------------------------------------------------------! |
| ! VL ! Snapshot at 1 sec intervals. ! |
| !--------------!------------------------------------------------------! |
| ! VC ! Snapshot at 1 sec intervals. ! |
| !--------------!------------------------------------------------------! |
| ! VH ! Snapshot at 1 sec intervals. ! |
| +---------------------------------------------------------------------+ |
(11) Engine Report O/R Logic <05> (Engine Type CFMI with Advanced EVMU)
| +----------------------------------------------------------------------+ |
| !Code!Item ! !Progr.!Standard ! |
| ! No.!No. ! Description of Function Item !MCDU !Value or ! |
| ! ! ! !GSE !Table ! |
| !----!------!-----------------------------------------!------!---------! |
| ! !A ! Report Format ! ! ! |
| ! !B ! Parameter Table ! ! ! |
| ! !C ! First three lines of Report ! C ! Blank ! |
| ! !D ! Print-out Rules ! C ! 2 ! |
| ! !E ! Transfer to ACARS MU ! C ! No ! |
| ! !F ! Increment of the report counter if the ! C ! 1 ! |
| ! ! ! report was triggered by a code number ! ! ! |
| ! ! ! > 1000; 1=yes, 0=no ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !1000!1 ! Manual selection via MCDU ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !2000!2 ! Flight phase dependent manual ! ! ! |
| ! ! ! selection via remote print button ! ! ! |
| ! ! ! if programmed. ! ! ! |
| ! !2.1 ! Remote Print Button assignment. ! C ! 4,5,5.1,! |
| ! ! ! ! ! 6,7,7.1,! |
| ! ! ! ! ! 8,9,10 ! |
| !----!------!-----------------------------------------!------!---------! |
| !3000!3 ! Programmable Start Logic ! ! ! |
| ! !3.1 ! Trigger condition ! C ! not ! |
| !----!------!-----------------------------------------!------!---------! |
| !8100!8.1 ! ACARS MU uplink request with IMI 'REQ05'! ! ! |
| ! ! ! The report <05> is immediately generated! ! ! |
| ! ! ! and transmitted to the ACARS MU. ! ! ! |
| !----------------------------------------------------------------------! |
| ! A = Programmable by Airbus ! |
| ! C = Programmable by Customer ! |
| +----------------------------------------------------------------------+ |
(12) Engine Report O/R Logic <05> (Engine Type CFMI with Advanced EVMU)
| +----------------------------------------------------------------------+ |
| !Code!Item ! !Progr.!Standard ! |
| ! No.!No. ! Description of Function Item !MCDU !Value or ! |
| ! ! ! !/GSE !Table TXY! |
| !----!------!-----------------------------------------!------!---------! |
| ! !A ! Report Format ! ! ! |
| ! !B ! Parameter Table ! ! ! |
| ! !C ! First three lines of Report ! C ! Blank ! |
| ! !D ! Print-out Rules ! C ! see ! |
| ! ! ! ! ! separate! |
| ! ! ! ! ! list ! |
| ! !E ! Transfer to ACARS MU ! C ! see ! |
| ! ! ! ! ! separate! |
| ! ! ! ! ! list ! |
| ! !F ! Increment of the report counter if the ! C ! 1 ! |
| ! ! ! report was triggered by a code number ! ! ! |
| ! ! ! > 1000; 1=yes, 0=no ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !1000!1 ! Manual selection via MCDU ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !2000!2 ! Flight phase dependent manual ! ! ! |
| ! ! ! selection via remote print button ! ! ! |
| ! ! ! if programmed. ! ! ! |
| ! !2.1 ! Remote Print Button assignment. ! C ! 4,5,5.1,! |
| ! ! ! ! ! 6,7,7.1,! |
| ! ! ! ! ! 8,9,10 ! |
| !----!------!-----------------------------------------!------!---------! |
| !3000!3 ! Programmable Start Logic ! ! ! |
| ! !3.1 ! Trigger condition ! C ! not ! |
| ! ! ! ! ! progr. ! |
| !----!------!-----------------------------------------!------!---------! |
| !8100!8.1 ! ACARS MU uplink request with IMI 'REQ05'! ! ! |
| ! ! ! The report <05> is immediately generated! ! ! |
| ! ! ! and transmitted to the ACARS MU. ! ! ! |
| !----------------------------------------------------------------------! |
| ! A = Programmable by Airbus ! |
| ! C = Programmable by Customer ! |
| +----------------------------------------------------------------------+ |
(13) Engine Report O/R Logic <05> (Engine Type CFMI with Advanced EVMU)
| +----------------------------------------------------------------------+ |
| !Code!Item ! !Progr.!Standard ! |
| ! No.!No. ! Description of Function Item !MCDU !Value or ! |
| ! ! ! !/GSE !Table TXY! |
| !----!------!-----------------------------------------!------!---------! |
| ! !A ! Report Format ! ! ! |
| ! !B ! Parameter Table ! ! ! |
| ! !C ! First three lines of Report ! C ! Blank ! |
| ! !D ! Print-out Rules ! C ! see ! |
| ! ! ! ! ! separate! |
| ! ! ! ! ! list ! |
| ! !E ! Transfer to ACARS MU ! C ! see ! |
| ! ! ! ! ! separate! |
| ! ! ! ! ! list ! |
| ! !F ! Increment of the report counter if the ! C ! 1 ! |
| ! ! ! report was triggered by a code number ! ! ! |
| ! ! ! > 1000; 1=yes, 0=no ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !1000!1 ! Manual selection via MCDU ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !2000!2 ! Flight phase dependent manual ! ! ! |
| ! ! ! selection via remote print button ! ! ! |
| ! ! ! if programmed. ! ! ! |
| ! !2.1 ! Remote Print Button assignment. ! C ! 4,5,5.1,! |
| ! ! ! ! ! 6,7,7.1,! |
| ! ! ! ! ! 8,9,10 ! |
| !----!------!-----------------------------------------!------!---------! |
| !3000!3 ! Programmable Start Logic ! ! ! |
| ! !3.1 ! Trigger condition ! C ! not ! |
| ! ! ! ! ! progr. ! |
| !----!------!-----------------------------------------!------!---------! |
| !8100!8.1 ! ACARS MU uplink request with IMI 'REQ05'! ! ! |
| ! ! ! The report <05> is immediately generated! ! ! |
| ! ! ! and transmitted to the ACARS MU. ! ! ! |
| !----------------------------------------------------------------------! |
| ! A = Programmable by Airbus ! |
| ! C = Programmable by Customer ! |
| +----------------------------------------------------------------------+ |
(14) Engine Report O/R Logic <05> (Engine Type CFMI with Advanced EVMU)
| +--------------------------------------------------------------------------+ |
| !Code!Item ! !Progr.!Standard ! |
| ! No.!No. ! Description of Function Item !------!Value or ! |
| ! ! ! !MCDU !Table TXY! |
| ! ! ! !GSE ! ! |
| !----!------!-----------------------------------------!------!---------! |
| ! !A ! Report Format ! ! ! |
| ! !A.1 ! "R005RLID" Report Layout Identifier ! ! 01 ! |
| ! ! ! (for ACARS header) ! ! ! |
| ! !A.2 ! "R005RLIS" Report Layout Issue ! ! 01 ! |
| ! ! ! (for ACARS header) ! ! ! |
| ! !B ! Parameter Table ! ! ! |
| ! !C ! First three lines of Report ! C ! Blank ! |
| ! !D ! Print-out Rules ! C ! see ! |
| ! ! ! ! ! separate! |
| ! ! ! ! ! list ! |
| ! !E ! Transfer to ACARS MU ! C ! see ! |
| ! ! ! ! ! separate! |
| ! ! ! ! ! list ! |
| ! !F ! Increment of the report counter if the ! C ! 1 ! |
| ! ! ! report was triggered by a code number ! ! ! |
| ! ! ! > 1000; 1=yes, 0=no ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !1000!1 ! Manual selection through MCDU ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !2000!2 ! Flight phase dependent manual ! ! ! |
| ! ! ! selection through remote print button ! ! ! |
| ! ! ! if programmed. ! ! ! |
| ! !2.1 ! Remote Print Button assignment. ! C ! 4,5,5.1,! |
| ! ! ! ! ! 6,7,7.1,! |
| ! ! ! ! ! 8,9,10 ! |
| !----!------!-----------------------------------------!------!---------! |
| !3000!3 ! Programmable Start Logic ! ! ! |
| ! !3.1 ! Trigger condition ! C ! not ! |
| ! ! ! ! ! progr. ! |
| !----!------!-----------------------------------------!------!---------! |
| !8100!8.1 ! ACARS MU uplink request with IMI 'REQ05'! ! ! |
| ! ! ! The report <05> is immediately generated! ! ! |
| ! ! ! and transmitted to the ACARS MU. ! ! ! |
| !----------------------------------------------------------------------! |
| ! A = Programmable by Airbus ! |
| ! C = Programmable by Customer ! |
| +----------------------------------------------------------------------+ |
H. AIDS Reports Print Rules - Default Values for Report <05>
| +------------------------------------------------+ |
| ! ! ! ! |
| ! Code ! Printer Output ! ACARS-output ! |
| ! ! ! ! |
| !-------!-----------------------!----------------! |
| ! ! ! ! |
| ! 1000 ! Print immediatly ! No ACARS ! |
| ! ! ! ! |
| !-------!-----------------------!----------------! |
| ! ! ! ! |
| ! 2000 ! Print immediatly ! No ACARS ! |
| ! ! ! ! |
| !-------!-----------------------!----------------! |
| ! ! ! ! |
| ! 8100 ! No print ! ACARS VHF ! |
| ! ! ! ! |
| +------------------------------------------------+ |
| +-------------------------------------------------------------------------+ |
| !Trigger! to ACARS ! to printer ! store ! |
| ! Code !------------------------------ -!-----------------!--------------! |
| ! No !Ground ! VHF ! SAT- ! HF ! at ! imme- ! internal& ! |
| ! ! ! ! COM ! !landing ! diate ! external ! |
| ! ! ! ! ! ! ! !(build in RAM&! |
| ! ! ! ! ! ! ! ! PCMCIA) ! |
| !-------!-------!--------!-------!-------!--------!--------!--------------! |
| ! ! ! If ! ! ! ! If !PCMCIA only if! |
| ! 1000 ! NO ! 'SEND' ! NO ! NO ! !'PRINT' ! 'STORE' ! |
| ! ! !selected! ! ! !selected! selected on ! |
| ! ! !on MCDU ! ! ! !on MCDU ! MCDU ! |
| !-------!-------!--------!-------!-------! N !--------!--------------! |
| ! 2000 ! NO ! NO ! NO ! NO ! O ! YES ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 3000 ! NO ! NO ! NO ! NO ! ! NO ! YES ! |
| !-------!-------!--------!------ !-------! !--------!--------------! |
| ! 8100 ! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| +-------------------------------------------------------------------------+ |
| +-------------------------------------------------------------------------+ |
| !Trigger! to ACARS ! to printer ! store ! |
| ! Code !------------------------------ -!-----------------!--------------! |
| ! No !Ground ! VHF ! SAT- ! HF ! at ! imme- ! internal& ! |
| ! ! ! ! COM ! !landing ! diate ! external ! |
| ! ! ! ! ! ! ! !(build in RAM&! |
| ! ! ! ! ! ! ! ! PCMCIA) ! |
| !-------!-------!--------!-------!-------!--------!--------!--------------! |
| ! 1000 ! NO ! NO ! NO ! NO ! NO ! YES ! YES ! |
| !-------!-------!--------!-------!-------!--------!--------!--------------! |
| ! 2000 ! NO ! NO ! NO ! NO ! NO ! YES ! YES ! |
| !-------!-------!--------!-------!-------!--------!--------!--------------! |
| ! 3000 ! NO ! NO ! NO ! NO ! NO ! NO ! YES ! |
| !-------!-------!--------!------ !-------!--------!--------!--------------! |
| ! 8100 ! NO ! YES ! NO ! NO ! NO ! NO ! YES ! |
| +-------------------------------------------------------------------------+ |
I. Engine Gas Path Advisory Report <06>
Engine Gas Path Advisory Report <06> (Engine Type CFMI with Advanced EVMU)
Engine Gas Path Advisory Report <06> (Engine Type CFMI with Advanced EVMU) ** ON A/C NOT FOR ALL
Engine Gas Path Advisory Report <06> (Engine Type CFMI with Advanced EVMU) ** ON A/C NOT FOR ALL
Engine Gas Path Advisory Report <06> (Engine Type CFMI with Advanced EVMU) ** ON A/C NOT FOR ALL
The Engine Gath Path Advisory Report shall be a collection of engine related information when there has been an exceedance of one of the primary engine parameters. In particular STALL, FLAME-OUT, SHUTDOWN, EGT, N1 and N2 shall be monitored for exceedance conditions. The report is generated when one of the logic conditions 1000 to 6000 (for details see Engine Gas Path Advisory Report logic) is present.
Engine Gas Path Advisory Report <06> (Engine Type CFMI with Advanced EVMU) Engine Gas Path Advisory Report <06> (Engine Type CFMI with Advanced EVMU) ** ON A/C NOT FOR ALL Engine Gas Path Advisory Report <06> (Engine Type CFMI with Advanced EVMU) ** ON A/C NOT FOR ALL Engine Gas Path Advisory Report <06> (Engine Type CFMI with Advanced EVMU) ** ON A/C NOT FOR ALL NOTE: For the standard header definition of the report refer to (Ref. AMM D/O 31-36-00-00).
(1) Engine Gas Path Advisory Report Data Field Description <06> (Engine Type CFMI with Advanced EVMU)
NOTE: Reports that are transmitted from the ACARS system do not have report lines without a line identifier.
| +---------------------------------------------------------------------+ |
| ! Value ! Content Description ! |
| !--------------!------------------------------------------------------! |
| ! ESN ! Engine Serial Number ! |
| ! 999999 ! (000000 to 999999) ! |
| ! ! Eng 1 param. 7C.1.046.01 digit 3, 2, 1 ! |
| ! ! 7C.1.047.01 digit 6, 5, 4 ! |
| ! ! Eng 2 param. 7C.2.046.01 digit 3, 2, 1 ! |
| ! ! 7C.2.047.01 digit 6, 5, 4 ! |
| !--------------!------------------------------------------------------! |
| ! EHRS ! Engine Flight Hours ! |
| ! 99999 ! (00000 to 99999 hours) ! |
| ! ! DMU Engine 1 and Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! ERT ! Engine Running Time ! |
| ! 99999 ! (00000 to 65536 hours) ! |
| ! ! Eng 1 param. 7C.1.050.01 ! |
| ! ! Eng 2 param. 7C.2.050.10 ! |
| !--------------!------------------------------------------------------! |
| ! ECYC ! Engine Cycle ! |
| ! 99999 ! (00000 to 99999) ! |
| !--------------!------------------------------------------------------! |
| ! AP ! Auto Pilot Status ! |
| ! 99 ! (00 to G8) ! |
| ! ! FMGC 1 and 2 (FGC part) for Auto Pilot AP1 and AP2 ! |
| ! ! ! |
| ! ! XX Auto Pilot Modes: ! |
| ! ! !! ! |
| ! ! !!__Lateral Modes: 0 = NO MODE ! |
| ! ! ! 1 = HEADING ! |
| ! ! ! 2 = TRACK ! |
| ! ! ! 3 = NAV ! |
| ! ! ! 4 = LOC CAPTURE ! |
| ! ! ! 5 = LOC TRACK ! |
| ! ! ! 6 = LAND TRACK ! |
| ! ! ! 7 = RUNWAY ! |
| ! ! ! 8 = ROLL GO AROUND ! |
| ! ! ! ! |
| ! ! !__Longitudinal Modes: 0 = NO MODE ! |
| ! ! 1 = PITCH G/A ! |
| ! ! 2 = PITCH T/O ! |
| ! ! 3 = G/S TRACK ! |
| ! ! 4 = G/S CAPTURE ! |
| ! ! 5 = V/S ! |
| ! ! 6 = FPA ! |
| ! ! 7 = ALT ! |
| ! ! 8 = ALT ACQ ! |
| ! ! 9 = OPEN CLB ! |
| ! ! A = OPEN DES ! |
| ! ! B = IM CLB ! |
| ! ! C = IM DES ! |
| ! ! D = CLB ! |
| ! ! E = DES ! |
| ! ! F = FINAL DES ! |
| ! ! G = EXPEDITE ! |
| ! ! ! |
| ! ! AP1 ! AP2 ! |
| ! ! Report Line EC: ! Report Line EE: !Difinition: ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! / ! / !No Mode Act. ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.11 = 1 ! 01.2.275.00.11 = 1!RUNWAY Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.12 = 1 ! 01.2.275.00.12 = 1!NAV Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.13 = 1 ! 01.2.275.00.13 = 1!LOC CAPTURE ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.14 = 1 ! 01.2.275.00.14 = 1!LOC TRACK ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.15 = 1 ! 01.2.275.00.15 = 1!Roll GO ! |
| ! ! ! !AROUND Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.16 = 1 ! 01.2.275.00.16 = 1!HEADING Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.17 = 1 ! 01.2.275.00.17 = 1!TRACK Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.15 = 1 ! 01.2.274.00.15 = 1!PITCH TO Mode! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.16 = 1 ! 01.2.274.00.16 = 1!PITCH GA Mode! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.17 = 1 ! 01.2.274.00.17 = 1!V/S Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.18 = 1 ! 01.2.274.00.18 = 1!FPA Mode ! |
| ! ! -------------------!-------------------!-------------! |
| ! ! 01.1.274.00.19 = 1 ! 01.2.274.00.19 = 1!ALT Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.20 = 1 ! 01.2.274.00.20 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.19 = 1 ! 01.2.274.00.19 = 1!ALT ACQ ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.21 = 1 ! 01.2.274.00.21 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.20 = 1 ! 01.2.274.00.20 = 1!G/S TRACK ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.22 = 1 ! 01.2.274.00.22 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.21 = 1 ! 01.2.274.00.21 = 1!G/S CAPTURE ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.22 = 1 ! 01.2.274.00.22 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.23 = 1 ! 01.2.274.00.23 = 1!FINAL DES ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.2.274.00.24 = 1 ! 01.2.274.00.24 = 1!EXPED. Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.146.00.14 = 1 ! 01.2.146.00.14 = 1!LAND TRACK ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!CLB Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.13 = 0 ! 01.2.274.00.13 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.14 = 0 ! 01.2.274.00.14 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.24 = 0 ! 01.2.274.00.24 = 0! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!DES Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.13 = 0 ! 01.2.274.00.13 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.14 = 0 ! 01.2.274.00.14 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.24 = 0 ! 01.2.274.00.24 = 0! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!IM. CLIMB ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.13 = 1 ! 01.2.274.00.13 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!IM. DES Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.13 = 1 ! 01.2.274.00.13 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!OPEN CLB ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.14 = 1 ! 01.2.274.00.14 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!OPEN DES ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.14 = 1 ! 01.2.274.00.14 = 1! ! |
| ! ! ---------------------------------------------------- ! |
| ! ! Auto Pilot Status DMU: ! |
| ! ! AP1 printed in report line EC ! |
| ! ! AP2 printed in report line EE ! |
| !--------------!------------------------------------------------------! |
| ! TR ! Thrust Reverser Position ! |
| ! 11 ! ECU 4 T/R Doors stowd and locked ! |
| ! ! Eng 1 param. 7C.1.273.01.25 ! |
| ! ! Eng 2 param. 7C.2.273.10.25 ! |
| ! ! 4 T/R Doors Deployed ! |
| ! ! Eng 1 param. 7C.1.273.01.26 ! |
| ! ! Eng 2 param. 7C.2.273.01.26 ! |
| !--------------!------------------------------------------------------! |
| ! E ! Exeedance Engine Position ! |
| ! 9 ! ! |
| !--------------!------------------------------------------------------! |
| ! MAX ! Maximal Value of the Exceeded Parameter ! |
| ! 9999 ! ! |
| !--------------!------------------------------------------------------! |
| ! LIM ! Programmable Limit, which was exceeded ! |
| ! 9999 ! ! |
| !--------------!------------------------------------------------------! |
| ! REF ! N2 at Stall Detection ! |
| ! 9999 ! (0.0 to 120.0% rpm) ! |
| !--------------!------------------------------------------------------! |
| ! TOL ! Time Over Limit ! |
| ! 999 ! (Observation time max 60 seconds) ! |
| !--------------!------------------------------------------------------! |
| ! TTP ! Time To Peak ! |
| ! 999 ! ! |
| !--------------!------------------------------------------------------! |
| ! Y1 ! 'Y06.1' Second Programmed Pre-event Intervals ! |
| ! 99 ! (1 to 6 sec) ! |
| !--------------!------------------------------------------------------! |
| ! Y2 ! 'Y06.2' Second Programmed Pre-event Intervals ! |
| ! 99 ! (1 to 60 sec) ! |
| !--------------!------------------------------------------------------! |
| ! PSEL ! Status of different FADEC sensors ! |
| ! XXXX ! X X X X Label: Selected: ! |
| ! ! ! ! ! !___ 211 TAT (Bit 11 --> 15) ! |
| ! ! ! ! ! ____ 344 N2 actual (Bit 11 --> 15) ! |
| ! ! ! !_______ 345 EGT (Bit 11 --> 15) ! |
| ! ! !_________ 346 N1 actual (Bit 11 --> 15) ! |
| ! ! ! |
| ! ! Source: ECU, different labels ! |
| ! ! NOTE: The shown values are coded as follows: ! |
| ! ! Bit: 15 14 13 12 11 ! Shown value ! |
| ! ! --------------------!---------------- ! |
| ! ! 0 0 0 0 0 ! 0 ! |
| ! ! 0 0 0 0 1 ! 1 ! |
| ! ! 0 0 0 1 0 ! 2 ! |
| ! ! 0 0 0 1 1 ! 3 ! |
| ! ! 0 0 1 0 0 ! 4 ! |
| ! ! 0 0 1 0 1 ! 5 ! |
| ! ! 0 0 1 1 0 ! 6 ! |
| ! ! 0 0 1 1 1 ! 7 ! |
| ! ! 0 1 0 0 0 ! 8 ! |
| ! ! 0 1 0 0 1 ! 9 ! |
| ! ! 0 1 0 1 0 ! A ! |
| ! ! 0 1 0 1 1 ! B ! |
| ! ! 0 1 1 0 0 ! C ! |
| ! ! 0 1 1 0 1 ! D ! |
| ! ! 0 1 1 1 0 ! E ! |
| ! ! 0 1 1 1 1 ! F ! |
| ! ! 1 0 0 0 0 ! G ! |
| ! ! 1 0 0 0 1 ! H ! |
| ! ! 1 0 0 1 0 ! I ! |
| ! ! 1 0 0 1 1 ! J ! |
| ! ! 1 0 1 0 0 ! K ! |
| ! ! 1 0 1 0 1 ! L ! |
| ! ! 1 0 1 1 0 ! M ! |
| ! ! 1 0 1 1 1 ! N ! |
| ! ! 1 1 0 0 0 ! O ! |
| ! ! 1 1 0 0 1 ! P ! |
| ! ! 1 1 0 1 0 ! Q ! |
| ! ! 1 1 0 1 1 ! R ! |
| ! ! 1 1 1 0 0 ! S ! |
| ! ! 1 1 1 0 1 ! T ! |
| ! ! 1 1 1 1 0 ! U ! |
| ! ! 1 1 1 1 1 ! V ! |
| ! ! ! |
| !--------------!------------------------------------------------------! |
| ! REASON ! Reason for Exceedance ! |
| ! XXXXXXXXXX ! ! |
| ! XXXXXXXXXX ! Up to 20 Characters ! |
| ! ! Stall Code: 4000 ! |
| ! ! EGT Code: 5100, 5200 and 5300 ! |
| ! ! N1 Code: 5500 ! |
| ! ! N2 Code: 5700 ! |
| ! ! Shut Down Code: 6000 ! |
| !--------------!------------------------------------------------------! |
| ! N1 ! Selected N1 Actual ! |
| ! 9999 ! (0 to 120.0 %rpm) ! |
| ! ! Eng 1 param. 7C.1.346.01 ! |
| ! ! Eng 2 param. 7C.2.346.10 ! |
| !--------------!------------------------------------------------------! |
| ! N1C ! N1 Command ! |
| ! 9999 ! (0 to 120.0 %rpm) ! |
| ! ! Eng 1 param. 7C.1.341.01 ! |
| ! ! Eng 2 param. 7C.2.341.10 ! |
| !--------------!------------------------------------------------------! |
| ! N2 ! Selected N2 Actual ! |
| ! 9999 ! (0 to 120.0 %rpm) ! |
| ! ! Eng 1 param. 7C.1.344.01 ! |
| ! ! Eng 2 param. 7C.2.344.10 ! |
| !--------------!------------------------------------------------------! |
| ! EGT ! Selected T494 (Exhaust Gas Temperature) ! |
| ! X999 ! (-55 to 999.9 C) ! |
| ! ! Eng 1 param. 7C.1.345.01 ! |
| ! ! Eng 2 param. 7C.2.345.10 ! |
| !--------------!------------------------------------------------------! |
| ! FF ! Engine Fuel Flow ! |
| ! 9999 ! ( 0 to 7000 kg/h) ! |
| ! ! Eng 1 param. 7C.1.244.01 ! |
| ! ! Eng 2 param. 7C.2.244.10 ! |
| !--------------!------------------------------------------------------! |
| ! P3 ! Selected PS3 ! |
| ! 9999 ! (0.0 to 450.0 psia) ! |
| ! ! Eng 1 param. 7C.1.264.01 ! |
| ! ! Eng 2 param. 7C.2.264.10 ! |
| !--------------!------------------------------------------------------! |
| ! T3 ! Temperature at Position 3 ! |
| ! X999 ! (-55.0 to 850.0 C) ! |
| ! ! Eng 1 param. 7C.1.265.01 ! |
| ! ! Eng 2 param. 7C.2.265.10 ! |
| !--------------!------------------------------------------------------! |
| ! T5 ! Temperature at Position 5 ! |
| ! X999 ! (-55.0 to 850.0 C) ! |
| ! ! Eng 1 param. 7C.1.260.01 ! |
| ! ! Eng 2 param. 7C.2.260.10 ! |
| !--------------!------------------------------------------------------! |
| ! P25 ! Total Air Pressure at Position 2.5 ! |
| ! 99999 ! (0.0 to 50.000 psia) ! |
| ! ! Eng 1 param. 7C.1.262.01 ! |
| ! ! Eng 2 param. 7C.2.262.10 ! |
| !--------------!------------------------------------------------------! |
| ! T25 ! Selected T25 ! |
| ! X999 ! (-55.0 to 120.0 C) ! |
| ! ! Eng 1 param. 7C.1.263.01 ! |
| ! ! Eng 2 param. 7C.2.263.10 ! |
| !--------------!------------------------------------------------------! |
| ! PT2 ! Total Air Pressure at Position 2 ! |
| ! 99999 ! (o.o to 25.000 psia) ! |
| ! ! Eng 1 param. 7C.1.131.01 ! |
| ! ! Eng 2 param. 7C.2.131.10 ! |
| !--------------!------------------------------------------------------! |
| ! ECW1 ! Engine Control Word 1 ! |
| ! XXXXX ! Each 'X' represents 4 Bits in hexadecimal code of ! |
| ! ! a defined ARINC 429 word: ! |
| ! ! XXXXX Bits HEX ! |
| ! ! !!!!!___________ 14, 13, 12, 11 0...F ! |
| ! ! !!!!____________ 18, 17, 16, 15 0...F ! |
| ! ! !!!_____________ 22, 21, 20, 19 0...F ! |
| ! ! !!______________ 26, 25, 24, 23 0...F ! |
| ! ! !_______________ 29, 28, 27 0...7 ! |
| ! ! -------------------------------------------- ! |
| ! ! Bit Label Parameter Description ! |
| ! ! 11 7C.X.272.XX.19 = 1 Auto Thrust Active ! |
| ! ! 12 7C.X.272.XX.20 = 1 VSV Position Fault ! |
| ! ! 13 SPARE ! |
| ! ! 14 SPARE ! |
| ! ! 15 7C.X.351.XX.29 = 1 Fuel Flow Measurement ! |
| ! ! Invalid ! |
| ! ! 16 7C.X.275.XX.15 = 1 N1/N2 Control ACtive ! |
| ! ! 17 7C.X.275.XX.26 = 1 Channel A Active ! |
| ! ! 18 7C.X.275.XX.27 = 1 Channel B Active ! |
| ! ! 19 SPARE ! |
| ! ! 20 SPARE ! |
| ! ! 21 SPARE ! |
| ! ! 22 SPARE ! |
| ! ! 23 SPARE ! |
| ! ! 24 SPARE ! |
| ! ! 25 SPARE ! |
| ! ! 26 SPARE ! |
| ! ! 27 SPARE ! |
| ! ! 28 SPARE ! |
| ! ! 29 SPARE ! |
| !--------------!------------------------------------------------------! |
| ! VSV ! Variable Statore Vane Position ! |
| ! X99 ! (-5.0 to 45.0 deg) ! |
| ! ! Eng 1 param. 7C.1.072.01 ! |
| ! ! Eng 2 param. 7C.2.072.10 ! |
| !--------------!------------------------------------------------------! |
| ! VBV ! Variable Bleed Valve Position ! |
| ! X99 ! (-9.9 to 40.0 deg) ! |
| ! ! Eng 1 param. 7C.1.071.01 ! |
| ! ! Eng 2 param. 7C.2.071.10 ! |
| +---------------------------------------------------------------------+ |
(2) Engine Gas Path Advisory Report Data Field Description <06> (Engine Type CFMI with Advanced EVMU)
NOTE: Reports that are transmitted from the ACARS system do not have report lines without a line identifier.
NOTE: Only the parts of the ENGINE GAS PATH ADVISORY REPORT <06> which are not included in the ENGINE CRUISE REPORT <01> are given in the subsequent table.
| +---------------------------------------------------------------------+ |
| ! Value ! Content Description ! |
| !--------------!------------------------------------------------------! |
| ! TR ! Thrust Reverser Position ! |
| ! 11 ! ! |
| ! ! 4 T/R Doors stowed and locked = 1 ! |
| ! ! 4 T/R Doors Deployed = 1 ! |
| ! ! ! |
| ! ! ECU 4 T/R Doors stowed and locked ! |
| ! ! Engine 1 7C.1.273.01.25 ! |
| ! ! Engine 2 7C.2.273.10.25 ! |
| ! ! 4 T/R Doors Deployed ! |
| ! ! Engine 1 7C.1.273.01.26 ! |
| ! ! Engine 2 7C.2.273.10.26 ! |
| !--------------!------------------------------------------------------! |
| ! E ! Exceedance Engine Position ! |
| ! 9 ! DMU (Number of Engine where exceedance occurs) ! |
| ! ! NOTE: If the report was not triggered by a limit ! |
| ! ! exceedance then this field contains zeros. ! |
| !--------------!------------------------------------------------------! |
| ! MAX ! Maximal Value of the Exceeded Parameter ! |
| ! 9999 ! NOTE: If the report was not triggered by a limit ! |
| ! ! exceedance then this field contains zeros. ! |
| !--------------! -----------------------------------------------------! |
| ! LIM ! Programmable Limit, which was exceeded ! |
| ! 9999 ! NOTE: If the report was not triggered by a limit ! |
| ! ! exceedance then this field contains zeros. ! |
| !--------------!------------------------------------------------------! |
| ! REF ! N2 at Stall Detection ! |
| ! 9999 ! For all other exceedances 0 are printed. ! |
| ! ! ECU (0.0 to 120.0% rpm) ! |
| ! ! ! |
| ! ! Engine 1 7C.1.344.01 ! |
| ! ! Engine 2 7C.2.344.10 ! |
| !--------------!------------------------------------------------------! |
| ! TOL ! Time Over Limit ! |
| ! 999 ! DMU (Observation time max 60 seconds) ! |
| ! ! NOTE: If the report was not triggered by a limit ! |
| ! ! exceedance then this field contains zeros. ! |
| !--------------!------------------------------------------------------! |
| ! TTP ! Time To Peak ! |
| ! 999 ! (Time to maximum of exceeded value) ! |
| ! ! NOTE: If the report was not triggered by a limit ! |
| ! ! exceedance then this field contains zeros. ! |
| !--------------!------------------------------------------------------! |
| ! Y1 ! 'Y06.1' Seconds Programmed Pre-event Intervals ! |
| ! 99 ! DMU (1 to 6 sec) ! |
| !--------------!------------------------------------------------------! |
| ! Y2 ! 'Y06.2' Seconds Programmed Pre-event Intervals ! |
| ! 99 ! DMU (1 to 60 sec) ! |
| !--------------!------------------------------------------------------! |
| ! PSEL ! Status of different FADEC sensors ! |
| ! XXXX ! X X X X Label: Selected: ! |
| ! ! ! ! ! !___ 211 TAT (Bit 11 --> 15) ! |
| ! ! ! ! !_____ 344 N2 actual (Bit 11 --> 15) ! |
| ! ! ! !_______ 345 EGT (Bit 11 --> 15) ! |
| ! ! !_________ 346 N1 actual (Bit 11 --> 15) ! |
| ! ! ! |
| ! ! Source: ECU, different labels ! |
| ! ! NOTE: The shown values are coded as follows: ! |
| ! ! Bit: 15 14 13 12 11 ! Shown value ! |
| ! ! --------------------!---------------- ! |
| ! ! 0 0 0 0 0 ! 0 ! |
| ! ! 0 0 0 0 1 ! 1 ! |
| ! ! 0 0 0 1 0 ! 2 ! |
| ! ! 0 0 0 1 1 ! 3 ! |
| ! ! 0 0 1 0 0 ! 4 ! |
| ! ! 0 0 1 0 1 ! 5 ! |
| ! ! 0 0 1 1 0 ! 6 ! |
| ! ! 0 0 1 1 1 ! 7 ! |
| ! ! 0 1 0 0 0 ! 8 ! |
| ! ! 0 1 0 0 1 ! 9 ! |
| ! ! 0 1 0 1 0 ! A ! |
| ! ! 0 1 0 1 1 ! B ! |
| ! ! 0 1 1 0 0 ! C ! |
| ! ! 0 1 1 0 1 ! D ! |
| ! ! 0 1 1 1 0 ! E ! |
| ! ! 0 1 1 1 1 ! F ! |
| ! ! 1 0 0 0 0 ! G ! |
| ! ! 1 0 0 0 1 ! H ! |
| ! ! 1 0 0 1 0 ! I ! |
| ! ! 1 0 0 1 1 ! J ! |
| ! ! 1 0 1 0 0 ! K ! |
| ! ! 1 0 1 0 1 ! L ! |
| ! ! 1 0 1 1 0 ! M ! |
| ! ! 1 0 1 1 1 ! N ! |
| ! ! 1 1 0 0 0 ! O ! |
| ! ! 1 1 0 0 1 ! P ! |
| ! ! 1 1 0 1 0 ! Q ! |
| ! ! 1 1 0 1 1 ! R ! |
| ! ! 1 1 1 0 0 ! S ! |
| ! ! 1 1 1 0 1 ! T ! |
| ! ! 1 1 1 1 0 ! U ! |
| ! ! 1 1 1 1 1 ! V ! |
| ! ! ! |
| !--------------!------------------------------------------------------! |
| ! REASON ! Reason for Exceedance ! |
| ! XXXXXXXXXX ! DMU ! |
| ! XXXXXXXXXX ! Up to 20 Characters ! |
| ! ! Stall Code: 4000 ! |
| ! ! EGT Code: 5100, 5200 and 5300 ! |
| ! ! N1 Code: 5400 and 5500 ! |
| ! ! N2 Code: 5600 and 5700 ! |
| ! ! Shut Down Code: 6000 ! |
| ! ! ! |
| ! ! NOTE: If the report was not triggered by a limit ! |
| ! ! exceedance, this field contains blanks. ! |
| +---------------------------------------------------------------------+ |
(3) Engine Gas Path Advisory Report Data Field Description <06> (Engine Type CFMI with Advanced EVMU)
NOTE: Reports that are transmitted from the ACARS system do not have report lines without a line identifier.
| +---------------------------------------------------------------------+ |
| ! Value ! Content Description ! |
| !--------------!------------------------------------------------------! |
| ! ESN ! Engine Serial Number ! |
| ! 999999 ! (000000 to 999999) ! |
| ! ! ECU Engine 1 7C.1.046.01 digit 3, 2, 1 ! |
| ! ! 7C.1.047.01 digit 6, 5, 4 ! |
| ! ! Engine 2 7C.2.046.10 digit 3, 2, 1 ! |
| ! ! 7C.2.047.10 digit 6, 5, 4 ! |
| !--------------!------------------------------------------------------! |
| ! EHRS ! Engine Flight Hours ! |
| ! 99999 ! (00000 to 99999 hours) ! |
| ! ! DMU Engine 1 ! |
| ! ! Engine 2 ! |
| ! ! Remark: Time between "Main (LH and RH) Landing Gear! |
| ! ! Decompressed" and "Main (LH and RH) Landing! |
| ! ! Gear Compressed". The EHRS must be set to ! |
| ! ! zero if a new ESN is recognized by the DMU.! |
| ! ! It is be possible to set the EHRS via the ! |
| ! ! MCDU, e.g. if the DMU is changed on the ! |
| ! ! a/c. ! |
| !--------------!------------------------------------------------------! |
| ! ERT ! Engine Running Time ! |
| ! 99999 ! (00000 to 65536 hours) ! |
| ! ! ECU 7C.1.050.01 Engine 1 ! |
| ! ! 7C.2.050.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! ECYC ! Engine Cycle ! |
| ! 99999 ! (00000 to 99999) ! |
| ! ! DMU Engine 1 ! |
| ! ! Engine 2 ! |
| ! ! Remark: Each time when flight phase 5 (climb) is ! |
| ! ! reached, the counter is incremented by one ! |
| ! ! The ECYC is set to zero if a new ESN is ! |
| ! ! is recognized by the DMU. It is possible to! |
| ! ! set ECYC via the MCDU, if the DMU is ! |
| ! ! changed on the a/c. ! |
| !--------------!------------------------------------------------------! |
| ! AP ! Auto Pilot Status ! |
| ! 99 ! Number of respective status (00 to G8) ! |
| ! ! FMGC 1 and 2 (FGC part) for Auto Pilot AP1 and AP2 ! |
| ! ! ! |
| ! ! Parameter for AP1 ! Parameter for AP2 ! ! |
| ! ! Report Line EC: ! Report Line EE: !Definition: ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! / ! / !No Mode ! |
| ! ! ! !Active ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.11 = 1 ! 01.2.275.00.11 = 1!RUNWAY Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.12 = 1 ! 01.2.275.00.12 = 1!NAV Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.13 = 1 ! 01.2.275.00.13 = 1!LOC CAPTURE ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.14 = 1 ! 01.2.275.00.14 = 1!LOC TRACK ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.15 = 1 ! 01.2.275.00.15 = 1!Roll GO ! |
| ! ! ! !AROUND Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.16 = 1 ! 01.2.275.00.16 = 1!HEADING Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.17 = 1 ! 01.2.275.00.17 = 1!TRACK Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.15 = 1 ! 01.2.274.00.15 = 1!PITCH T/O ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.16 = 1 ! 01.2.274.00.16 = 1!PITCH GA Mode! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.17 = 1 ! 01.2.274.00.17 = 1!V/S Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.18 = 1 ! 01.2.274.00.18 = 1!FPA Mode ! |
| ! ! -------------------!-------------------!-------------! |
| ! ! 01.1.274.00.19 = 1 ! 01.2.274.00.19 = 1!ALT Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.20 = 1 ! 01.2.274.00.20 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.19 = 1 ! 01.2.274.00.19 = 1!ALT ACQ ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.21 = 1 ! 01.2.274.00.21 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.20 = 1 ! 01.2.274.00.20 = 1!G/S TRACK ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.22 = 1 ! 01.2.274.00.22 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.21 = 1 ! 01.2.274.00.21 = 1!G/S CAPTURE ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.22 = 1 ! 01.2.274.00.22 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.23 = 1 ! 01.2.274.00.23 = 1!FINAL DES ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.24 = 1 ! 01.2.274.00.24 = 1!EXPED. Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.146.00.14 = 1 ! 01.2.146.00.14 = 1!LAND TRACK ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!CLB Mode ! |
| ! ! AND ! AND ! ! |
| ! ! ! ! ! ! ! |
| ! ! -------------- ! -------------- ! ! |
| ! ! 01.1.274.00.13 = 0 ! 01.2.274.00.13 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.14 = 0 ! 01.2.274.00.14 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.24 = 0 ! 01.2.274.00.24 = 0! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!DES Mode ! |
| ! ! AND ! AND ! ! |
| ! ! ! ! ! ! ! |
| ! ! -------------- ! -------------- ! ! |
| ! ! 01.1.274.00.13 = 0 ! 01.2.274.00.13 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.14 = 0 ! 01.2.274.00.14 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.24 = 0 ! 01.2.274.00.24 = 0! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!IM. CLIMB ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.13 = 1 ! 01.2.274.00.13 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!IM. DES Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.13 = 1 ! 01.2.274.00.13 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!OPEN CLB ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.14 = 1 ! 01.2.274.00.14 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!OPEN. DES ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.14 = 1 ! 01.2.274.00.14 = 1! ! |
| ! ! ---------------------------------------------------- ! |
| ! ! Auto Pilot Status DMU: ! |
| ! ! Auto Pilot AP1 printed in report line EC ! |
| ! ! Auto Pilot AP2 printed in report line EE ! |
| ! ! Combined Auto Pilot Modes ! |
| ! ! The longitudinal auto pilot mode (1 to G) appears on ! |
| ! ! on the left position for the AP1 and AP2 print ! |
| ! ! format. ! |
| ! ! The lateral auto pilot mode (1 to 8) appears on the ! |
| ! ! right position for the AP1 and AP2 print format. ! |
| ! ! In case of a combined auto pilot mode e.g. DES mode ! |
| ! ! and NAV mode are engaged simultaneously, the 'E3' ! |
| ! ! appears below AP1 and AP2. ! |
| ! ! XX Auto Pilot Modes: ! |
| ! ! !! ! |
| ! ! !!__Lateral Modes: 0 = NO MODE ! |
| ! ! ! 1 = HEADING ! |
| ! ! ! 2 = TRACK ! |
| ! ! ! 3 = NAV ! |
| ! ! ! 4 = LOC CAPTURE ! |
| ! ! ! 5 = LOCK TRACK ! |
| ! ! ! 6 = LAND TRACK ! |
| ! ! ! 7 = RUNWAY ! |
| ! ! ! 8 = ROLL GO AROUND ! |
| ! ! ! ! |
| ! ! !__Longitudinal Modes: 0 = NO MODE ! |
| ! ! 1 = PITCH G/A ! |
| ! ! 2 = PITCH TO ! |
| ! ! 3 = G/S TRACK ! |
| ! ! 4 = G/S CAPTURE ! |
| ! ! 5 = V/S ! |
| ! ! 6 = FPA ! |
| ! ! 7 = ALT ! |
| ! ! 8 = ALT ACQ ! |
| ! ! 9 = OPEN CLB ! |
| ! ! A = OPEN DES ! |
| ! ! B = IM CLB ! |
| ! ! C = IM DES ! |
| ! ! D = CLB ! |
| ! ! E = DES ! |
| ! ! F = FINAL DES ! |
| ! ! G = EXPEDITE ! |
| !--------------!------------------------------------------------------! |
| ! TR ! Thrust Reverser Position ! |
| ! 11 ! 11 ! |
| ! ! 4 T/R Doors stowed and locked = 1___!! ! |
| ! ! 4 T/R Doors Deployed = 1_____________! ! |
| ! ! ! |
| ! ! ECU 4 T/R Doors stowed and locked ! |
| ! ! Engine 1 7C.1.273.01.25 ! |
| ! ! Engine 2 7C.2.273.10.25 ! |
| ! ! 4 T/R Doors Deployed ! |
| ! ! Engine 1 7C.1.273.01.26 ! |
| ! ! Engine 2 7C.2.273.10.26 ! |
| !--------------!------------------------------------------------------! |
| ! E ! Exceedance Engine Position ! |
| ! 9 ! Number of Engine where exceedance occurs ! |
| ! ! Remark: If the report was not triggered by a limit ! |
| ! ! exceedance then this field contains zeros. ! |
| !--------------!------------------------------------------------------! |
| ! MAX ! Maximal Value of the Exceeded Parameter ! |
| ! 9999 ! Depending of exceeded parameter. ! |
| ! ! Remark: If the report was not triggered by a limit ! |
| ! ! exceedance then this field contains zeros. ! |
| !--------------! -----------------------------------------------------! |
| ! LIM ! Programmable Limit, which was exceeded ! |
| ! 9999 ! Depending of exceeded parameter. ! |
| ! ! Remark: If the report was not triggered by a limit ! |
| ! ! exceedance then this field contains zeros. ! |
| !--------------! -----------------------------------------------------! |
| ! REF ! N2 at Stall Detection ! |
| ! 9999 ! For all other exceedances 0 are printed. ! |
| ! ! ECU (0.0 to 120.0% rpm) ! |
| ! ! ! |
| ! ! Engine 1 7C.1.344.01 ! |
| ! ! Engine 2 7C.2.344.10 ! |
| !--------------!------------------------------------------------------! |
| ! TOL ! Time Over Limit ! |
| ! 999 ! (Observation time max 60 seconds) ! |
| ! ! Remark: If the report was not triggered by a limit ! |
| ! ! exceedance then this field contains zeros. ! |
| !--------------!------------------------------------------------------! |
| ! TTP ! Time To Peak ! |
| ! 999 ! (Time to maximum of exceeded value) ! |
| ! ! Remark: If the report was not triggered by a limit ! |
| ! ! exceedance then this field contains zeros. ! |
| !--------------!------------------------------------------------------! |
| ! Y1 ! 'Y06.1' Seconds Programmed Pre-event Intervals ! |
| ! 99 ! DMU (1 to 6 sec) ! |
| !--------------!------------------------------------------------------! |
| ! Y2 ! 'Y06.2' Seconds Programmed Pre-event Intervals ! |
| ! 99 ! DMU (1 to 60 sec) ! |
| !--------------!------------------------------------------------------! |
| ! PSEL ! Status of different FADEC sensors ! |
| ! XXXX ! XXXX Label: Selected: ! |
| ! ! !!!!_ 211 TAT (Bit 11 -> 15)! |
| ! ! !!!__ 344 N2 actual (Bit 11 -> 15)! |
| ! ! !!___ 345 EGT (Bit 11 -> 15)! |
| ! ! !____ 346 N1 actual (Bit 11 -> 15)! |
| ! ! Source: ECU, different labels ! |
| ! ! NOTE: The shown values are coded as follows: ! |
| ! ! Bit: 15 14 13 12 11 ! Shown value ! |
| ! ! --------------------!---------------- ! |
| ! ! 0 0 0 0 0 ! 0 ! |
| ! ! 0 0 0 0 1 ! 1 ! |
| ! ! 0 0 0 1 0 ! 2 ! |
| ! ! 0 0 0 1 1 ! 3 ! |
| ! ! 0 0 1 0 0 ! 4 ! |
| ! ! 0 0 1 0 1 ! 5 ! |
| ! ! 0 0 1 1 0 ! 6 ! |
| ! ! 0 0 1 1 1 ! 7 ! |
| ! ! 0 1 0 0 0 ! 8 ! |
| ! ! 0 1 0 0 1 ! 9 ! |
| ! ! 0 1 0 1 0 ! A ! |
| ! ! 0 1 0 1 1 ! B ! |
| ! ! 0 1 1 0 0 ! C ! |
| ! ! 0 1 1 0 1 ! D ! |
| ! ! 0 1 1 1 0 ! E ! |
| ! ! 0 1 1 1 1 ! F ! |
| ! ! 1 0 0 0 0 ! G ! |
| ! ! 1 0 0 0 1 ! H ! |
| ! ! 1 0 0 1 0 ! I ! |
| ! ! 1 0 0 1 1 ! J ! |
| ! ! 1 0 1 0 0 ! K ! |
| ! ! 1 0 1 0 1 ! L ! |
| ! ! 1 0 1 1 0 ! M ! |
| ! ! 1 0 1 1 1 ! N ! |
| ! ! 1 1 0 0 0 ! O ! |
| ! ! 1 1 0 0 1 ! P ! |
| ! ! 1 1 0 1 0 ! Q ! |
| ! ! 1 1 0 1 1 ! R ! |
| ! ! 1 1 1 0 0 ! S ! |
| ! ! 1 1 1 0 1 ! T ! |
| ! ! 1 1 1 1 0 ! U ! |
| ! ! 1 1 1 1 1 ! V ! |
| !--------------!------------------------------------------------------! |
| ! REASON ! Reason for Exceedance ! |
| ! XXXXXXXXXX ! DMU ! |
| ! XXXXXXXXXX ! Up to 20 Characters ! |
| ! ! Stall Code: 4000 ! |
| ! ! EGT Code: 5100, 5200 and 5300 ! |
| ! ! N1 Code: 5400 and 5500 ! |
| ! ! N2 Code: 5600 and 5700 ! |
| ! ! Shut Down Code: 6000 ! |
| ! ! ! |
| ! ! NOTE: If the report was not triggered by a limit ! |
| ! ! exceedance, this field contains blanks. ! |
| !--------------!------------------------------------------------------! |
| ! N1 ! Selected N1 Actual ! |
| ! 9999 ! (0 to 120.0 %rpm) ! |
| ! ! ECU 7C.1.346.01 Engine 1 ! |
| ! ! 7C.2.346.10 Engine 2 ! |
| ! ! Remark: In the report line V3 and V4 the values ! |
| ! ! from the last stable descent are printed. ! |
| ! ! In the report line V5 and V6 the values ! |
| ! ! from the last stable climb are printed. ! |
| !--------------!------------------------------------------------------! |
| ! N1C ! N1 Command ! |
| ! 9999 ! (0 to 120.0 %rpm) ! |
| ! ! ECU 7C.1.341.01 Engine 1 ! |
| ! ! 7C.2.341.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! N2 ! Selected N2 Actual ! |
| ! 9999 ! (0 to 120.0 %rpm) ! |
| ! ! ECU 7C.1.344.01 Engine 1 ! |
| ! ! 7C.2.344.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! EGT ! Selected T495 (Exhaust Gas Temperature) ! |
| ! X999 ! (-55 to 999.9 [C) ! |
| ! ! Negative values are indicated by '-' on the first ! |
| ! ! position. Otherwise the first position is used for ! |
| ! ! the value. ! |
| ! ! ECU 7C.1.345.01 Engine 1 ! |
| ! ! 7C.2.345.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! FF ! Engine Fuel Flow ! |
| ! 9999 ! 0 to 7000 kg/h (0 to 15000 p/h) ! |
| ! ! ECU 7C.1.244.01 Engine 1 ! |
| ! ! 7C.2.244.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! P3 ! Selected PS3 (Burner Pressure) ! |
| ! 9999 ! (0.0 to 450.0 psia) ! |
| ! ! ECU 7C.1.264.01 Engine 1 ! |
| ! ! 7C.2.264.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! T3 ! Selected T3 ! |
| ! X999 ! (-55.0 to 850.0 deg C) ! |
| ! ! Negative values are indicated by '-' on the first ! |
| ! ! position. Otherwise the first position is used for ! |
| ! ! the value. ! |
| ! ! ECU 7C.1.265.01 Engine 1 ! |
| ! ! 7C.2.265.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! T5 ! T5 Temperature at position T5 ! |
| ! X999 ! (-55.0 to 850.0 [C) ! |
| ! ! Negative values are indicated by '-' on the first ! |
| ! ! position. Otherwise the firt position is used for ! |
| ! ! the value. ! |
| ! ! ECU 7C.1.260.01 Engine 1 ! |
| ! ! 7C.2.260.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! P25 ! P25 Total Air Pressure at Position 2.5 ! |
| ! 99999 ! (0.0 to 50.000 psia) ! |
| ! ! ECU 7C.1.262.01 Engine 1 ! |
| ! ! 7C.2.262.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! T25 ! Selected T25 ! |
| ! X999 ! (-55.0 to 120.0 [C) ! |
| ! ! Negative values are indicated by '-' on the first ! |
| ! ! position. Otherwise the first position is used for ! |
| ! ! the value. ! |
| ! ! ECU 7C.1.263.01 Engine 1 ! |
| ! ! 7C.2.263.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! PT2 ! PT2 Total Air Pressure at Position 2 ! |
| ! 99999 ! (0.0 to 25.000 psia) ! |
| ! ! ECU 7C.1.131.01 Engine 1 ! |
| ! ! 7C.2.131.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! ECW1 ! Engine Control Word 1 ! |
| ! XXXXX ! XXXXX Bits HEX ! |
| ! ! !!!!!________14, 13, 12, 11 0..F ! |
| ! ! !!!!_________18, 17, 16, 15 0..F ! |
| ! ! !!!__________22, 21, 20, 19 0..F ! |
| ! ! !!___________26, 25, 24, 23 0..F ! |
| ! ! !____________ 29, 28, 27 0..F ! |
| ! ! Bit Label Parameter Description ! |
| ! ! 11 7C.X.272.XX.19 = 1 Auto Thrust Active ! |
| ! ! 12 7C.X.275.XX.20 = 1 VSV Position Fault ! |
| ! ! 13 SPARE ! |
| ! ! 14 SPARE ! |
| ! ! 15 7C.X.351.XX.29 = 1 Fuel Flow Measurement ! |
| ! ! Invalid ! |
| ! ! 16 7C.X.275.XX.15 = 1 N1/N2 Control Active ! |
| ! ! 17 7C.X.275.XX.26 = 1 Channel A Active ! |
| ! ! 18 7C.X.275.XX.27 = 1 Channel B Active ! |
| ! ! 19 SPARE ! |
| ! ! 20 SPARE ! |
| ! ! 21 SPARE ! |
| ! ! 22 SPARE ! |
| ! ! 23 SPARE ! |
| ! ! 24 SPARE ! |
| ! ! 25 SPARE ! |
| ! ! 26 SPARE ! |
| ! ! 27 SPARE ! |
| ! ! 28 SPARE ! |
| ! ! 29 SPARE ! |
| ! ! The 'X' for the System and SDI definition of the ! |
| ! ! engine parameters appears as follows: ! |
| ! ! System SDI ! |
| ! ! Engine 1 1 01 ! |
| ! ! Engine 2 2 10 ! |
| !--------------!------------------------------------------------------! |
| ! VSV ! Selected Variable Stator Vane Position ! |
| ! X99 ! (-5.0 to 45.0 deg) ! |
| ! ! Negative values are indicated by '-' on the first ! |
| ! ! position. Otherwise the first position is used for ! |
| ! ! the value. ! |
| ! ! ECU 7C.1.072.01 Engine 1 ! |
| ! ! 7C.2.072.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! VBV ! Variable Bleed Valve Position ! |
| ! X99 ! (-9.9 to 40.0 deg) ! |
| ! ! Negative values are indicated by '-' on the first ! |
| ! ! position. Otherwise the first position is used for ! |
| ! ! the value. ! |
| ! ! ECU 7C.1.071.01 Engine 1 ! |
| ! ! 7C.2.071.10 Engine 2 ! |
| +---------------------------------------------------------------------+ |
(4) Engine Gas Path Advisory Report Data Field Description <06> (Engine Type CFMI with Advanced EVMU)
NOTE: Reports that are transmitted from the ACARS system do not have report lines without a line identifier.
| +---------------------------------------------------------------------+ |
| ! Value ! Content Description ! |
| !--------------!------------------------------------------------------! |
| ! ESN ! Engine Serial Number ! |
| ! 999999 ! (000000 to 999999) ! |
| ! ! ECU Engine 1 7C.1.046.01 digit 3, 2, 1 ! |
| ! ! 7C.1.047.01 digit 6, 5, 4 ! |
| ! ! Engine 2 7C.2.046.10 digit 3, 2, 1 ! |
| ! ! 7C.2.047.10 digit 6, 5, 4 ! |
| !--------------!------------------------------------------------------! |
| ! EHRS ! Engine Flight Hours ! |
| ! 99999 ! (00000 to 99999 hours) ! |
| ! ! DMU Engine 1 ! |
| ! ! Engine 2 ! |
| ! ! Remark: Time between "Main (LH and RH) Landing Gear! |
| ! ! Decompressed" and "Main (LH and RH) Landing! |
| ! ! Gear Compressed". The EHRS shall be set to ! |
| ! ! zero if a new ESN is recognized by the DMU.! |
| ! ! It shall be possible to set the EHRS via ! |
| ! ! the MCDU, e.g. if the DMU is changed on the! |
| ! ! a/c. ! |
| !--------------!------------------------------------------------------! |
| ! ERT ! Engine Running Time ! |
| ! 99999 ! (00000 to 65536 hours) ! |
| ! ! ECU 7C.1.050.01 Engine 1 ! |
| ! ! 7C.2.050.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! ECYC ! Engine Cycle ! |
| ! 99999 ! (00000 to 99999) ! |
| ! ! DMU Engine 1 ! |
| ! ! Engine 2 ! |
| ! ! Remark: Each time when flight phase 5 (climb) is ! |
| ! ! reached, the counter shall be incremented ! |
| ! ! by one. The ECYC is set to zero if a new ! |
| ! ! ESN is recognized by the DMU. It shall be ! |
| ! ! possible to set ECYC via the MCDU, if the ! |
| ! ! DMU is changed on the a/c. ! |
| !--------------!------------------------------------------------------! |
| ! AP ! Auto Pilot Status ! |
| ! 99 ! Number of respective status (00 to G8) ! |
| ! ! FMGC 1 and 2 (FGC part) for Auto Pilot AP1 and AP2 ! |
| ! ! ! |
| ! ! Parameter for AP1 ! Parameter for AP2 ! ! |
| ! ! Report Line EC: ! Report Line EE: !Definition: ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! / ! / !No Mode ! |
| ! ! ! !Active ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.11 = 1 ! 01.2.275.00.11 = 1!RUNWAY Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.12 = 1 ! 01.2.275.00.12 = 1!NAV Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.13 = 1 ! 01.2.275.00.13 = 1!LOC CAPTURE ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.14 = 1 ! 01.2.275.00.14 = 1!LOC TRACK ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.15 = 1 ! 01.2.275.00.15 = 1!Roll GO ! |
| ! ! ! !AROUND Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.16 = 1 ! 01.2.275.00.16 = 1!HEADING Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.17 = 1 ! 01.2.275.00.17 = 1!TRACK Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.15 = 1 ! 01.2.274.00.15 = 1!PITCH T/O ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.16 = 1 ! 01.2.274.00.16 = 1!PITCH GA Mode! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.17 = 1 ! 01.2.274.00.17 = 1!V/S Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.18 = 1 ! 01.2.274.00.18 = 1!FPA Mode ! |
| ! ! -------------------!-------------------!-------------! |
| ! ! 01.1.274.00.19 = 1 ! 01.2.274.00.19 = 1!ALT Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.20 = 1 ! 01.2.274.00.20 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.19 = 1 ! 01.2.274.00.19 = 1!ALT ACQ ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.21 = 1 ! 01.2.274.00.21 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.20 = 1 ! 01.2.274.00.20 = 1!G/S TRACK ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.22 = 1 ! 01.2.274.00.22 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.21 = 1 ! 01.2.274.00.21 = 1!G/S CAPTURE ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.22 = 1 ! 01.2.274.00.22 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.23 = 1 ! 01.2.274.00.23 = 1!FINAL DES ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.24 = 1 ! 01.2.274.00.24 = 1!EXPED. Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.146.00.14 = 1 ! 01.2.146.00.14 = 1!LAND TRACK ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!CLB Mode ! |
| ! ! AND ! AND ! ! |
| ! ! ! ! ! ! ! |
| ! ! -------------- ! -------------- ! ! |
| ! ! 01.1.274.00.13 = 0 ! 01.2.274.00.13 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.14 = 0 ! 01.2.274.00.14 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.24 = 0 ! 01.2.274.00.24 = 0! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!DES Mode ! |
| ! ! AND ! AND ! ! |
| ! ! ! ! ! ! ! |
| ! ! -------------- ! -------------- ! ! |
| ! ! 01.1.274.00.13 = 0 ! 01.2.274.00.13 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.14 = 0 ! 01.2.274.00.14 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.24 = 0 ! 01.2.274.00.24 = 0! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!IM. CLIMB ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.13 = 1 ! 01.2.274.00.13 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!IM. DES Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.13 = 1 ! 01.2.274.00.13 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!OPEN CLB ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.14 = 1 ! 01.2.274.00.14 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!OPEN. DES ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.14 = 1 ! 01.2.274.00.14 = 1! ! |
| ! ! ---------------------------------------------------- ! |
| ! ! Auto Pilot Status DMU: ! |
| ! ! Auto Pilot AP1 printed in report line EC ! |
| ! ! Auto Pilot AP2 printed in report line EE ! |
| ! ! Combined Auto Pilot Modes ! |
| ! ! The longitudinal auto pilot mode (1 to G) shall ! |
| ! ! appear on the left position for the AP1 and AP2 print! |
| ! ! format. ! |
| ! ! The lateral auto pilot mode (1 to 8) shall appear on ! |
| ! ! the right position for the AP1 and AP2 print format. ! |
| ! ! In case of a combined auto pilot mode e.g. DES mode ! |
| ! ! and NAV mode are engaged simultaneously, the 'E3' ! |
| ! ! shall appear below AP1 and AP2. ! |
| ! ! XX Auto Pilot Modes: ! |
| ! ! !! ! |
| ! ! !!__Lateral Modes: 0 = NO MODE ! |
| ! ! ! 1 = HEADING ! |
| ! ! ! 2 = TRACK ! |
| ! ! ! 3 = NAV ! |
| ! ! ! 4 = LOC CAPTURE ! |
| ! ! ! 5 = LOCK TRACK ! |
| ! ! ! 6 = LAND TRACK ! |
| ! ! ! 7 = RUNWAY ! |
| ! ! ! 8 = ROLL GO AROUND ! |
| ! ! ! ! |
| ! ! !__Longitudinal Modes: 0 = NO MODE ! |
| ! ! 1 = PITCH G/A ! |
| ! ! 2 = PITCH TO ! |
| ! ! 3 = G/S TRACK ! |
| ! ! 4 = G/S CAPTURE ! |
| ! ! 5 = V/S ! |
| ! ! 6 = FPA ! |
| ! ! 7 = ALT ! |
| ! ! 8 = ALT ACQ ! |
| ! ! 9 = OPEN CLB ! |
| ! ! A = OPEN DES ! |
| ! ! B = IM CLB ! |
| ! ! C = IM DES ! |
| ! ! D = CLB ! |
| ! ! E = DES ! |
| ! ! F = FINAL DES ! |
| ! ! G = EXPEDITE ! |
| !--------------!------------------------------------------------------! |
| ! TR ! Thrust Reverser Position ! |
| ! 11 ! 11 ! |
| ! ! 4 T/R Doors stowed and locked = 1___!! ! |
| ! ! 4 T/R Doors Deployed = 1_____________! ! |
| ! ! ! |
| ! ! ECU 4 T/R Doors stowed and locked ! |
| ! ! Engine 1 7C.1.273.01.25 ! |
| ! ! Engine 2 7C.2.273.10.25 ! |
| ! ! 4 T/R Doors Deployed ! |
| ! ! Engine 1 7C.1.273.01.26 ! |
| ! ! Engine 2 7C.2.273.10.26 ! |
| !--------------!------------------------------------------------------! |
| ! E ! Exeedance Engine Position ! |
| ! 9 ! Number of Engine where exceedance occurs ! |
| !--------------!------------------------------------------------------! |
| ! MAX ! Maximal Value of the Exceeded Parameter ! |
| ! 9999 ! Depending of exceeded parameter. ! |
| ! ! Remark: If the report was not triggered by a limit ! |
| ! ! exceedance then this field shall contain ! |
| ! ! zeros. ! |
| !--------------! -----------------------------------------------------! |
| ! LIM ! Programmable Limit, which was exceeded ! |
| ! 9999 ! Depending of exceeded parameter. ! |
| ! ! Remark: If the report was not triggered by a limit ! |
| ! ! exceedance then this field shall contain ! |
| ! ! zeros. ! |
| !--------------! -----------------------------------------------------! |
| ! REF ! N2 at Stall Detection ! |
| ! 9999 ! For all other exceedances 0 are printed. ! |
| ! ! ECU (0.0 to 120.0% rpm) ! |
| ! ! ! |
| ! ! Engine 1 7C.1.344.01 ! |
| ! ! Engine 2 7C.2.344.10 ! |
| !--------------!------------------------------------------------------! |
| ! TOL ! Time Over Limit ! |
| ! 999 ! (Observation time max 60 seconds) ! |
| ! ! Remark: If the report was not triggered by a limit ! |
| ! ! exceedance then this field shall contain ! |
| ! ! zeros. ! |
| !--------------!------------------------------------------------------! |
| ! TTP ! Time To Peak ! |
| ! 999 ! (Time to maximum of exceeded value) ! |
| ! ! Remark: If the report was not triggered by a limit ! |
| ! ! exceedance then this field shall contain ! |
| ! ! zeros. ! |
| !--------------!------------------------------------------------------! |
| ! Y1 ! 'Y06.1' Seconds Programmed Pre-event Intervals ! |
| ! 99 ! DMU (1 to 6 sec) ! |
| !--------------!------------------------------------------------------! |
| ! Y2 ! 'Y06.2' Seconds Programmed Pre-event Intervals ! |
| ! 99 ! DMU (1 to 60 sec) ! |
| !--------------!------------------------------------------------------! |
| ! PSEL ! Status of different FADEC sensors ! |
| ! XXXX ! XXXX Label: Selected: ! |
| ! ! !!!!_ 211 TAT (Bit 11 -> 15)! |
| ! ! !!!__ 344 N2 actual (Bit 11 -> 15)! |
| ! ! !!___ 345 EGT (Bit 11 -> 15)! |
| ! ! !____ 346 N1 actual (Bit 11 -> 15)! |
| ! ! Source: ECU, different labels ! |
| ! ! NOTE: The shown values are coded as follows: ! |
| ! ! Bit: 15 14 13 12 11 ! Shown value ! |
| ! ! --------------------!---------------- ! |
| ! ! 0 0 0 0 0 ! 0 ! |
| ! ! 0 0 0 0 1 ! 1 ! |
| ! ! 0 0 0 1 0 ! 2 ! |
| ! ! 0 0 0 1 1 ! 3 ! |
| ! ! 0 0 1 0 0 ! 4 ! |
| ! ! 0 0 1 0 1 ! 5 ! |
| ! ! 0 0 1 1 0 ! 6 ! |
| ! ! 0 0 1 1 1 ! 7 ! |
| ! ! 0 1 0 0 0 ! 8 ! |
| ! ! 0 1 0 0 1 ! 9 ! |
| ! ! 0 1 0 1 0 ! A ! |
| ! ! 0 1 0 1 1 ! B ! |
| ! ! 0 1 1 0 0 ! C ! |
| ! ! 0 1 1 0 1 ! D ! |
| ! ! 0 1 1 1 0 ! E ! |
| ! ! 0 1 1 1 1 ! F ! |
| ! ! 1 0 0 0 0 ! G ! |
| ! ! 1 0 0 0 1 ! H ! |
| ! ! 1 0 0 1 0 ! I ! |
| ! ! 1 0 0 1 1 ! J ! |
| ! ! 1 0 1 0 0 ! K ! |
| ! ! 1 0 1 0 1 ! L ! |
| ! ! 1 0 1 1 0 ! M ! |
| ! ! 1 0 1 1 1 ! N ! |
| ! ! 1 1 0 0 0 ! O ! |
| ! ! 1 1 0 0 1 ! P ! |
| ! ! 1 1 0 1 0 ! Q ! |
| ! ! 1 1 0 1 1 ! R ! |
| ! ! 1 1 1 0 0 ! S ! |
| ! ! 1 1 1 0 1 ! T ! |
| ! ! 1 1 1 1 0 ! U ! |
| ! ! 1 1 1 1 1 ! V ! |
| !--------------!------------------------------------------------------! |
| ! N1 ! Selected N1 Actual ! |
| ! 9999 ! (0 to 120.0 %rpm) ! |
| ! ! ECU 7C.1.346.01 Engine 1 ! |
| ! ! 7C.2.346.10 Engine 2 ! |
| ! ! Remark: In the report line V3 and V4 the values ! |
| ! ! from the last stable descent shall be ! |
| ! ! printed. ! |
| ! ! In the report line V5 and V6 the values ! |
| ! ! from the last stable climb shall be ! |
| ! ! printed. ! |
| !--------------!------------------------------------------------------! |
| ! N1C ! N1 Command ! |
| ! 9999 ! (0 to 120.0 %rpm) ! |
| ! ! ECU 7C.1.341.01 Engine 1 ! |
| ! ! 7C.2.341.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! N2 ! Selected N2 Actual ! |
| ! 9999 ! (0 to 120.0 %rpm) ! |
| ! ! ECU 7C.1.344.01 Engine 1 ! |
| ! ! 7C.2.344.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! EGT ! Selected T495 (Exhaust Gas Temperature) ! |
| ! X999 ! (-55 to 999.9 [C) ! |
| ! ! Negative values are indicated by 'N' on the ! |
| ! ! first position. Otherwise the first position is ! |
| ! ! used for the value. ! |
| ! ! ECU 7C.1.345.01 Engine 1 ! |
| ! ! 7C.2.345.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! FF ! Engine Fuel Flow ! |
| ! 9999 ! 0 to 7000 kg/h (0 to 15000 p/h) ! |
| ! ! ECU 7C.1.244.01 Engine 1 ! |
| ! ! 7C.2.244.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! P3 ! Selected PS3 (Burner Pressure) ! |
| ! 9999 ! (0.0 to 450.0 psia) ! |
| ! ! ECU 7C.1.264.01 Engine 1 ! |
| ! ! 7C.2.264.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! T3 ! Selected T3 ! |
| ! X999 ! (-55.0 to 850.0 deg C) ! |
| ! ! Negative values are indicated by 'N' on the ! |
| ! ! first position. Otherwise the first position is ! |
| ! ! used for the value. ! |
| ! ! ECU 7C.1.265.01 Engine 1 ! |
| ! ! 7C.2.265.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! T5 ! T5 Temperature at position T5 ! |
| ! X999 ! (-55.0 to 850.0 [C) ! |
| ! ! Negative values are indicated by 'N' on the ! |
| ! ! first position. Otherwise the firt position is ! |
| ! ! used for the value. ! |
| ! ! ECU 7C.1.260.01 Engine 1 ! |
| ! ! 7C.2.260.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! P25 ! P25 Total Air Pressure at Position 2.5 ! |
| ! 99999 ! (0.0 to 50.000 psia) ! |
| ! ! ECU 7C.1.262.01 Engine 1 ! |
| ! ! 7C.2.262.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! T25 ! Selected T25 ! |
| ! X999 ! (-55.0 to 120.0 [C) ! |
| ! ! Negative values are indicated by 'N' on the ! |
| ! ! first position. Otherwise the first position is ! |
| ! ! used for the value. ! |
| ! ! ECU 7C.1.263.01 Engine 1 ! |
| ! ! 7C.2.263.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! PT2 ! PT2 Total Air Pressure at Position 2 ! |
| ! 99999 ! (0.0 to 25.000 psia) ! |
| ! ! ECU 7C.1.131.01 Engine 1 ! |
| ! ! 7C.2.131.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! ECW1 ! Engine Control Word 1 ! |
| ! XXXXX ! XXXXX Bits HEX ! |
| ! ! !!!!!________14, 13, 12, 11 0..F ! |
| ! ! !!!!_________18, 17, 16, 15 0..F ! |
| ! ! !!!__________22, 21, 20, 19 0..F ! |
| ! ! !!___________26, 25, 24, 23 0..F ! |
| ! ! !____________ 29, 28, 27 0..F ! |
| ! ! Bit Label Parameter Description ! |
| ! ! 11 7C.X.272.XX.19 = 1 Auto Thrust Active ! |
| ! ! 12 7C.X.275.XX.20 = 1 VSV Position Fault ! |
| ! ! 13 SPARE ! |
| ! ! 14 SPARE ! |
| ! ! 15 7C.X.351.XX.29 = 1 Fuel Flow Measurement ! |
| ! ! Invalid ! |
| ! ! 16 7C.X.275.XX.15 = 1 N1/N2 Control Active ! |
| ! ! 17 7C.X.275.XX.26 = 1 Channel A Active ! |
| ! ! 18 7C.X.275.XX.27 = 1 Channel B Active ! |
| ! ! 19 SPARE ! |
| ! ! 20 SPARE ! |
| ! ! 21 SPARE ! |
| ! ! 22 SPARE ! |
| ! ! 23 SPARE ! |
| ! ! 24 SPARE ! |
| ! ! 25 SPARE ! |
| ! ! 26 SPARE ! |
| ! ! 27 SPARE ! |
| ! ! 28 SPARE ! |
| ! ! 29 SPARE ! |
| ! ! The 'X' for the System and SDI definition of the ! |
| ! ! engine parameters shall be as follows: ! |
| ! ! System SDI ! |
| ! ! Engine 1 1 01 ! |
| ! ! Engine 2 2 10 ! |
| !--------------!------------------------------------------------------! |
| ! VSV ! Selected Variable Stator Vane Position ! |
| ! X99 ! (-5.0 to 45.0 deg) ! |
| ! ! Negative values are indicated by 'N' on the ! |
| ! ! first position. Otherwise the first position is ! |
| ! ! used for the value. ! |
| ! ! ECU 7C.1.072.01 Engine 1 ! |
| ! ! 7C.2.072.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! VBV ! Variable Bleed Valve Position ! |
| ! X99 ! (-9.9 to 40.0 deg) ! |
| ! ! Negative values are indicated by 'N' on the ! |
| ! ! first position. Otherwise the first position is ! |
| ! ! used for the value. ! |
| ! ! ECU 7C.1.071.01 Engine 1 ! |
| ! ! 7C.2.071.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! REASON ! Reason for Exceedance ! |
| ! XXXXXXXXXX ! (Up to 20 characters) ! |
| ! XXXXXXXXXX ! STALL Code: 4000 ! |
| ! ! EGT Code: 5100, 5200 and 5300 ! |
| ! ! N1 Code: 5500 ! |
| ! ! N2U Code: 5700 ! |
| ! ! SHUT DOWN Code: 6000 ! |
| ! ! Remark: If the report was not triggered by a limit ! |
| ! ! exceedance, this field shall contain zeros.! |
| +---------------------------------------------------------------------+ |
(5) Engine Gas Path Advisory Report Data Field Description <06> (Engine Type CFMI with Advanced EVMU)
NOTE: Reports that are transmitted from the ACARS system do not have report lines without a line identifier.
NOTE: Only the parts of the ENGINE GAS PATH ADVISORY REPORT <06> which are not included in the ENGINE CRUISE REPORT <01> are given in the subsequent table.
| +---------------------------------------------------------------------+ |
| ! Value ! Content Description ! |
| !--------------!------------------------------------------------------! |
| ! TR ! Thrust Reverser Position ! |
| ! 11 ! 11 ! |
| ! ! 4 T/R Doors stowed and locked = 1___!! ! |
| ! ! 4 T/R Doors Deployed = 1_____________! ! |
| ! ! ! |
| ! ! ECU 4 T/R Doors stowed and locked ! |
| ! ! Engine 1 7C.1.273.01.25 ! |
| ! ! Engine 2 7C.2.273.10.25 ! |
| ! ! 4 T/R Doors Deployed ! |
| ! ! Engine 1 7C.1.273.01.26 ! |
| ! ! Engine 2 7C.2.273.10.26 ! |
| !--------------!------------------------------------------------------! |
| ! E ! Exceedance Engine Position ! |
| ! 9 ! Number of Engine where exceedance occurs ! |
| ! ! Remark: If the report is not triggered by a limit ! |
| ! ! exceedance, this field contains zeros. ! |
| !--------------!------------------------------------------------------! |
| ! MAX ! Maximal Value of the Exceeded Parameter ! |
| ! 9999 ! Depending of exceeded parameter. ! |
| ! ! Remark: If the report was not triggered by a limit ! |
| ! ! exceedance then this field contains zeros. ! |
| !--------------!------------------------------------------------------! |
| ! LIM ! Programmable Limit, which was exceeded ! |
| ! 9999 ! Depending of exceeded parameter. ! |
| ! ! Remark: If the report was not triggered by a limit ! |
| ! ! exceedance then this field contains zeros. ! |
| !--------------!------------------------------------------------------! |
| ! REF ! N2 at Stall Detection ! |
| ! 9999 ! For all other exceedances zeros are printed. ! |
| ! ! ECU (0.0 to 120.0% rpm) ! |
| ! ! ! |
| ! ! Engine 1 7C.1.344.01 ! |
| ! ! Engine 2 7C.2.344.10 ! |
| !--------------!------------------------------------------------------! |
| ! TOL ! Time Over Limit ! |
| ! 999 ! Time at least 60 seconds ! |
| ! ! Remark: If the report was not triggered by a limit ! |
| ! ! exceedance then this field contains zeros. ! |
| !--------------!------------------------------------------------------! |
| ! TTP ! Time To Peak ! |
| ! 999 ! Time to maximum of exceeded value ! |
| ! ! Remark: If the report was not triggered by a limit ! |
| ! ! exceedance then this field contains zeros. ! |
| !--------------!------------------------------------------------------! |
| ! Y1 ! 'Y06.1' Seconds Programmed Pre-event Intervals ! |
| ! 99 ! DMU (1 to 6 sec) ! |
| !--------------!------------------------------------------------------! |
| ! Y2 ! 'Y06.2' Seconds Programmed Pre-event Intervals ! |
| ! 99 ! DMU (1 to 60 sec) ! |
| !--------------!------------------------------------------------------! |
| ! PSEL ! Status of different FADEC sensors ! |
| ! XXXX ! XXXX Label: Selected: ! |
| ! ! !!!!_ 211 TAT (Bit 11 -> 15)! |
| ! ! !!!__ 344 N2 actual (Bit 11 -> 15)! |
| ! ! !!___ 345 EGT (Bit 11 -> 15)! |
| ! ! !____ 346 N1 actual (Bit 11 -> 15)! |
| ! ! Source: ECU, different labels ! |
| ! ! NOTE: The shown values are coded as follows: ! |
| ! ! Bit: 15 14 13 12 11 ! Shown value ! |
| ! ! --------------------!---------------- ! |
| ! ! 0 0 0 0 0 ! 0 ! |
| ! ! 0 0 0 0 1 ! 1 ! |
| ! ! 0 0 0 1 0 ! 2 ! |
| ! ! 0 0 0 1 1 ! 3 ! |
| ! ! 0 0 1 0 0 ! 4 ! |
| ! ! 0 0 1 0 1 ! 5 ! |
| ! ! 0 0 1 1 0 ! 6 ! |
| ! ! 0 0 1 1 1 ! 7 ! |
| ! ! 0 1 0 0 0 ! 8 ! |
| ! ! 0 1 0 0 1 ! 9 ! |
| ! ! 0 1 0 1 0 ! A ! |
| ! ! 0 1 0 1 1 ! B ! |
| ! ! 0 1 1 0 0 ! C ! |
| ! ! 0 1 1 0 1 ! D ! |
| ! ! 0 1 1 1 0 ! E ! |
| ! ! 0 1 1 1 1 ! F ! |
| ! ! 1 0 0 0 0 ! G ! |
| ! ! 1 0 0 0 1 ! H ! |
| ! ! 1 0 0 1 0 ! I ! |
| ! ! 1 0 0 1 1 ! J ! |
| ! ! 1 0 1 0 0 ! K ! |
| ! ! 1 0 1 0 1 ! L ! |
| ! ! 1 0 1 1 0 ! M ! |
| ! ! 1 0 1 1 1 ! N ! |
| ! ! 1 1 0 0 0 ! O ! |
| ! ! 1 1 0 0 1 ! P ! |
| ! ! 1 1 0 1 0 ! Q ! |
| ! ! 1 1 0 1 1 ! R ! |
| ! ! 1 1 1 0 0 ! S ! |
| ! ! 1 1 1 0 1 ! T ! |
| ! ! 1 1 1 1 0 ! U ! |
| ! ! 1 1 1 1 1 ! V ! |
| +---------------------------------------------------------------------+ |
(6) Engine Gas Path Advisory Report Data Field Description <06> (Engine Type CFMI with Advanced EVMU)
NOTE: Reports that are transmitted from the ACARS system do not have report lines without a line identifier.
NOTE: Only the parts of the ENGINE GAS PATH ADVISORY REPORT <06> which are not included in the ENGINE CRUISE REPORT <01> are given in the subsequent table.
| +---------------------------------------------------------------------+ |
| ! Value ! Content Description ! |
| !--------------!------------------------------------------------------! |
| ! TR ! Thrust Reverser Position ! |
| ! 11 ! 11 ! |
| ! ! 4 T/R Doors stowed and locked = 1___!! ! |
| ! ! 4 T/R Doors Deployed = 1_____________! ! |
| ! ! ! |
| ! ! ECU 4 T/R Doors stowed and locked ! |
| ! ! Engine 1 7C.1.273.01.25 ! |
| ! ! Engine 2 7C.2.273.10.25 ! |
| ! ! 4 T/R Doors Deployed ! |
| ! ! Engine 1 7C.1.273.01.26 ! |
| ! ! Engine 2 7C.2.273.10.26 ! |
| !--------------!------------------------------------------------------! |
| ! E ! Exeedance Engine Position ! |
| ! 9 ! Number of Engine where exceedance occurs ! |
| ! ! DMU ! |
| ! ! ! |
| !--------------!------------------------------------------------------! |
| ! MAX ! Maximal Value of the Exceeded Parameter ! |
| ! 9999 ! Depending of exceeded parameter. ! |
| ! ! Remark: If the report was not triggered by a limit ! |
| ! ! exceedance then this field contains zeros. ! |
| !--------------!------------------------------------------------------! |
| ! LIM ! Programmable Limit, which was exceeded ! |
| ! 9999 ! Depending of exceeded parameter. ! |
| ! ! Remark: If the report was not triggered by a limit ! |
| ! ! exceedance then this field contains zeros. ! |
| !--------------!------------------------------------------------------! |
| ! REF ! N2 at Stall Detection ! |
| ! 9999 ! For all other exceedances zeros are printed. ! |
| ! ! ECU (0.0 to 120.0 %rpm) ! |
| ! ! ! |
| ! ! Engine 1 7C.1.344.01 ! |
| ! ! Engine 2 7C.2.344.10 ! |
| !--------------!------------------------------------------------------! |
| ! TOL ! Time Over Limit ! |
| ! 999 ! Time at least 60 seconds ! |
| ! ! Remark: If the report was not triggered by a limit ! |
| ! ! exceedance then this field contains zeros. ! |
| !--------------!------------------------------------------------------! |
| ! TTP ! Time To Peak ! |
| ! 999 ! Time to maximum of exceeded value ! |
| ! ! Remark: If the report was not triggered by a limit ! |
| ! ! exceedance then this field contains zeros. ! |
| !--------------!------------------------------------------------------! |
| ! Y1 ! 'Y06.1' Seconds Programmed Pre-event Intervals ! |
| ! 99 ! DMU (1 to 6 sec) ! |
| !--------------!------------------------------------------------------! |
| ! Y2 ! 'Y06.2' Seconds Programmed Pre-event Intervals ! |
| ! 99 ! DMU (1 to 60 sec) ! |
| !--------------!------------------------------------------------------! |
| ! PSEL ! Status of different FADEC sensors ! |
| ! XXXX ! ! |
| ! ! XXXX Label: Selected: ! |
| ! ! !!!!_ 211 TAT (Bit 11 -> 15)! |
| ! ! !!!__ 344 N2 actual (Bit 11 -> 15)! |
| ! ! !!___ 345 EGT (Bit 11 -> 15)! |
| ! ! !____ 346 N1 actual (Bit 11 -> 15)! |
| ! ! Source: ECU, different labels ! |
| ! ! NOTE: The shown values are coded as follows: ! |
| ! ! Bit: 15 14 13 12 11 ! Shown value ! |
| ! ! --------------------!---------------- ! |
| ! ! 0 0 0 0 0 ! 0 ! |
| ! ! 0 0 0 0 1 ! 1 ! |
| ! ! 0 0 0 1 0 ! 2 ! |
| ! ! 0 0 0 1 1 ! 3 ! |
| ! ! 0 0 1 0 0 ! 4 ! |
| ! ! 0 0 1 0 1 ! 5 ! |
| ! ! 0 0 1 1 0 ! 6 ! |
| ! ! 0 0 1 1 1 ! 7 ! |
| ! ! 0 1 0 0 0 ! 8 ! |
| ! ! 0 1 0 0 1 ! 9 ! |
| ! ! 0 1 0 1 0 ! A ! |
| ! ! 0 1 0 1 1 ! B ! |
| ! ! 0 1 1 0 0 ! C ! |
| ! ! 0 1 1 0 1 ! D ! |
| ! ! 0 1 1 1 0 ! E ! |
| ! ! 0 1 1 1 1 ! F ! |
| ! ! 1 0 0 0 0 ! G ! |
| ! ! 1 0 0 0 1 ! H ! |
| ! ! 1 0 0 1 0 ! I ! |
| ! ! 1 0 0 1 1 ! J ! |
| ! ! 1 0 1 0 0 ! K ! |
| ! ! 1 0 1 0 1 ! L ! |
| ! ! 1 0 1 1 0 ! M ! |
| ! ! 1 0 1 1 1 ! N ! |
| ! ! 1 1 0 0 0 ! O ! |
| ! ! 1 1 0 0 1 ! P ! |
| ! ! 1 1 0 1 0 ! Q ! |
| ! ! 1 1 0 1 1 ! R ! |
| ! ! 1 1 1 0 0 ! S ! |
| ! ! 1 1 1 0 1 ! T ! |
| ! ! 1 1 1 1 0 ! U ! |
| ! ! 1 1 1 1 1 ! V ! |
| !--------------!------------------------------------------------------! |
| ! REASON ! Reason for Exceedance ! |
| ! XXXXXXXXXX ! DMU (Up to 20 characters) ! |
| ! XXXXXXXXXX ! STALL Code: 4000 ! |
| ! ! EGT Code: 5100, 5200 and 5300 ! |
| ! ! N1 Code: 5500 ! |
| ! ! N2 Code: 5700 ! |
| ! ! SHUT DOWN Code: 6000 ! |
| ! ! ! |
| ! ! NOTE: If the report was not triggered by a limit ! |
| ! ! exceedance, this field contains blanks. ! |
| +---------------------------------------------------------------------+ |
(7) Engine Gas Path Advisory Report Data Field Description <06> (Engine Type CFMI with Advanced EVMU)
NOTE: Reports that are transmitted from the ACARS system do not have report lines without a line identifier.
NOTE: Only the parts of the ENGINE GAS PATH ADVISORY REPORT <06> which are not included in the ENGINE CRUISE REPORT <01> are given in the subsequent table.
| +---------------------------------------------------------------------+ |
| ! Value ! Content Description ! |
| !--------------!------------------------------------------------------! |
| ! TR ! Thrust Reverser Position ! |
| ! 11 ! 11 ! |
| ! ! 4 T/R Doors stowed and locked = 1___!! ! |
| ! ! 4 T/R Doors Deployed = 1_____________! ! |
| ! ! ! |
| ! ! ECU 4 T/R Doors stowed and locked ! |
| ! ! Engine 1 7C.1.273.01.25 ! |
| ! ! Engine 2 7C.2.273.10.25 ! |
| ! ! 4 T/R Doors Deployed ! |
| ! ! Engine 1 7C.1.273.01.26 ! |
| ! ! Engine 2 7C.2.273.10.26 ! |
| !--------------!------------------------------------------------------! |
| ! E ! Exeedance Engine Position ! |
| ! 9 ! Number of Engine where exceedance occurs ! |
| ! ! DMU ! |
| ! ! ! |
| !--------------!------------------------------------------------------! |
| ! MAX ! Maximal Value of the Exceeded Parameter ! |
| ! 9999 ! Depending of exceeded parameter. ! |
| ! ! Remark: If the report was not triggered by a limit ! |
| ! ! exceedance, this field contains zeros. ! |
| !--------------!------------------------------------------------------! |
| ! LIM ! Programmable Limit, which was exceeded ! |
| ! 9999 ! Depending of exceeded parameter. ! |
| ! ! Remark: If the report was not triggered by a limit ! |
| ! ! exceedance, this field contains zeros. ! |
| !--------------!------------------------------------------------------! |
| ! REF ! N2 at Stall Detection ! |
| ! 9999 ! For all other exceedances zeros are printed. ! |
| ! ! ECU (0.0 to 120.0 %rpm) ! |
| ! ! ! |
| ! ! Engine 1 7C.1.344.01 ! |
| ! ! Engine 2 7C.2.344.10 ! |
| !--------------!------------------------------------------------------! |
| ! TOL ! Time Over Limit ! |
| ! 999 ! Time minimum 60 seconds ! |
| ! ! Remark: If the report was not triggered by a limit ! |
| ! ! exceedance, this field contains zeros . ! |
| !--------------!------------------------------------------------------! |
| ! TTP ! Time To Peak ! |
| ! 999 ! Time to maximum of exceeded value ! |
| ! ! Remark: If the report was not triggered by a limit ! |
| ! ! exceedance, this field contains zeros. ! |
| !--------------!------------------------------------------------------! |
| ! Y1 ! 'Y06.1' Seconds Programmed Pre-event Intervals ! |
| ! 99 ! DMU (1 to 6 sec) ! |
| !--------------!------------------------------------------------------! |
| ! Y2 ! 'Y06.2' Seconds Programmed Pre-event Intervals ! |
| ! 99 ! DMU (1 to 60 sec) ! |
| !--------------!------------------------------------------------------! |
| ! PSEL ! Status of different FADEC sensors ! |
| ! XXXX ! ! |
| ! ! XXXX Label: Selected: ! |
| ! ! !!!!_ 211 TAT (Bit 11 -> 15)! |
| ! ! !!!__ 344 N2 actual (Bit 11 -> 15)! |
| ! ! !!___ 345 EGT (Bit 11 -> 15)! |
| ! ! !____ 346 N1 actual (Bit 11 -> 15)! |
| ! ! Source: ECU, different labels ! |
| ! ! NOTE: The shown values are coded as follows: ! |
| ! ! Bit: 15 14 13 12 11 ! Shown value ! |
| ! ! --------------------!---------------- ! |
| ! ! 0 0 0 0 0 ! 0 ! |
| ! ! 0 0 0 0 1 ! 1 ! |
| ! ! 0 0 0 1 0 ! 2 ! |
| ! ! 0 0 0 1 1 ! 3 ! |
| ! ! 0 0 1 0 0 ! 4 ! |
| ! ! 0 0 1 0 1 ! 5 ! |
| ! ! 0 0 1 1 0 ! 6 ! |
| ! ! 0 0 1 1 1 ! 7 ! |
| ! ! 0 1 0 0 0 ! 8 ! |
| ! ! 0 1 0 0 1 ! 9 ! |
| ! ! 0 1 0 1 0 ! A ! |
| ! ! 0 1 0 1 1 ! B ! |
| ! ! 0 1 1 0 0 ! C ! |
| ! ! 0 1 1 0 1 ! D ! |
| ! ! 0 1 1 1 0 ! E ! |
| ! ! 0 1 1 1 1 ! F ! |
| ! ! 1 0 0 0 0 ! G ! |
| ! ! 1 0 0 0 1 ! H ! |
| ! ! 1 0 0 1 0 ! I ! |
| ! ! 1 0 0 1 1 ! J ! |
| ! ! 1 0 1 0 0 ! K ! |
| ! ! 1 0 1 0 1 ! L ! |
| ! ! 1 0 1 1 0 ! M ! |
| ! ! 1 0 1 1 1 ! N ! |
| ! ! 1 1 0 0 0 ! O ! |
| ! ! 1 1 0 0 1 ! P ! |
| ! ! 1 1 0 1 0 ! Q ! |
| ! ! 1 1 0 1 1 ! R ! |
| ! ! 1 1 1 0 0 ! S ! |
| ! ! 1 1 1 0 1 ! T ! |
| ! ! 1 1 1 1 0 ! U ! |
| ! ! 1 1 1 1 1 ! V ! |
| !--------------!------------------------------------------------------! |
| ! REASON ! Reason for Exceedance ! |
| ! XXXXXXXXXX ! DMU (Up to 20 characters) ! |
| ! XXXXXXXXXX ! STALL Code: 4000 ! |
| ! ! EGT Code: 5100, 5200 and 5300 ! |
| ! ! N1 Code: 5500 ! |
| ! ! N2 Code: 5700 ! |
| ! ! SHUT DOWN Code: 6000 ! |
| ! ! ! |
| ! ! NOTE: If the report was not triggered by a limit ! |
| ! ! exceedance, this field contains blanks. ! |
| +---------------------------------------------------------------------+ |
(8) Parameter Logic
| +---------------------------------------------------------------------+ |
| ! Param. ! Print Value (Standard Progr.) ! |
| !--------------!------------------------------------------------------! |
| ! ESN ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! EHRS ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! ERT ! Value at moment of trigger ! |
| !--------------! -----------------------------------------------------! |
| ! ECYC ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! AP ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! TR ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! E ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! MAX ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! LIM ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! REF ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! TOL ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! TTP ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! Y1 ! Programmed 'Y06.1' pre-event intervals ! |
| !--------------!------------------------------------------------------! |
| ! Y2 ! Programmed 'Y06.2' pre-event intervals ! |
| !--------------!------------------------------------------------------! |
| ! PSEL ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! N1 ! Snapshot at Y06.1 and Y06.2 sec. intervals. ! |
| !--------------!------------------------------------------------------! |
| ! N1C ! Snapshot at Y06.1 and Y06.2 sec. intervals. ! |
| !--------------!------------------------------------------------------! |
| ! N2 ! Snapshot at Y06.1 and Y06.2 sec. intervals. ! |
| !--------------!------------------------------------------------------! |
| ! EGT ! Snapshot at Y06.1 and Y06.2 sec. intervals. ! |
| !--------------!------------------------------------------------------! |
| ! FF ! Snapshot at Y06.1 and Y06.2 sec. intervals. ! |
| !--------------!------------------------------------------------------! |
| ! P3 ! Snapshot at Y06.1 and Y06.2 sec. intervals. ! |
| !--------------!------------------------------------------------------! |
| ! T3 ! Snapshot at Y06.1 and Y06.2 sec. intervals. ! |
| !--------------!------------------------------------------------------! |
| ! T5 ! Snapshot at Y06.1 and Y06.2 sec. intervals. ! |
| !--------------!------------------------------------------------------! |
| ! P25 ! Snapshot at Y06.1 and Y06.2 sec. intervals. ! |
| !--------------!------------------------------------------------------! |
| ! T25 ! Snapshot at Y06.1 and Y06.2 sec. intervals. ! |
| !--------------!------------------------------------------------------! |
| ! PT2 ! Snapshot at Y06.1 and Y06.2 sec. intervals. ! |
| !--------------!------------------------------------------------------! |
| ! ECW1 ! Snapshot at Y06.1 and Y06.2 sec. intervals. ! |
| !--------------!------------------------------------------------------! |
| ! VSV ! Snapshot at Y06.1 and Y06.2 sec. intervals. ! |
| !--------------!------------------------------------------------------! |
| ! VBV ! Snapshot at Y06.1 and Y06.2 sec. intervals. ! |
| +---------------------------------------------------------------------+ |
(9) Parameter Logic
| +---------------------------------------------------------------------+ |
| ! Param. ! Print Value (Standard Progr.) ! |
| !--------------!------------------------------------------------------! |
| ! ESN ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! EHRS ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! ERT ! Value at moment of trigger ! |
| !--------------! -----------------------------------------------------! |
| ! ECYC ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! AP ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! TR ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! E ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! MAX ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! LIM ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! REF ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! TOL ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! TTP ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! Y1 ! Programmed 'Y06.1' pre-event intervals ! |
| !--------------!------------------------------------------------------! |
| ! Y2 ! Programmed 'Y06.2' pre-event intervals ! |
| !--------------!------------------------------------------------------! |
| ! PSEL ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! N1 ! Snapshot at Y06.1 and Y06.2 sec. intervals. ! |
| !--------------!------------------------------------------------------! |
| ! N1C ! Snapshot at Y06.1 and Y06.2 sec. intervals. ! |
| !--------------!------------------------------------------------------! |
| ! N2 ! Snapshot at Y06.1 and Y06.2 sec. intervals. ! |
| !--------------!------------------------------------------------------! |
| ! EGT ! Snapshot at Y06.1 and Y06.2 sec. intervals. ! |
| !--------------!------------------------------------------------------! |
| ! FF ! Snapshot at Y06.1 and Y06.2 sec. intervals. ! |
| !--------------!------------------------------------------------------! |
| ! P3 ! Snapshot at Y06.1 and Y06.2 sec. intervals. ! |
| !--------------!------------------------------------------------------! |
| ! T3 ! Snapshot at Y06.1 and Y06.2 sec. intervals. ! |
| !--------------!------------------------------------------------------! |
| ! T5 ! Snapshot at Y06.1 and Y06.2 sec. intervals. ! |
| !--------------!------------------------------------------------------! |
| ! P25 ! Snapshot at Y06.1 and Y06.2 sec. intervals. ! |
| !--------------!------------------------------------------------------! |
| ! T25 ! Snapshot at Y06.1 and Y06.2 sec. intervals. ! |
| !--------------!------------------------------------------------------! |
| ! PT2 ! Snapshot at Y06.1 and Y06.2 sec. intervals. ! |
| !--------------!------------------------------------------------------! |
| ! ECW1 ! Snapshot at Y06.1 and Y06.2 sec. intervals. ! |
| !--------------!------------------------------------------------------! |
| ! VSV ! Snapshot at Y06.1 and Y06.2 sec. intervals. ! |
| !--------------!------------------------------------------------------! |
| ! VBV ! Snapshot at Y06.1 and Y06.2 sec. intervals. ! |
| +---------------------------------------------------------------------+ |
(10) Engine Gas Path Advisory Report Logic <06> (Engine Type CFMI with Advanced EVMU)
| +----------------------------------------------------------------------+ |
| !Code!Item ! !Progr.!Standard ! |
| ! No.!No. ! Description of Function Item !MCDU !Value or ! |
| ! ! ! !GSE !Table ! |
| !----!------!-----------------------------------------!------!---------! |
| ! !A ! Report Format ! ! ! |
| ! !B ! Parameter Table ! ! ! |
| ! !C ! First three lines of Report ! C ! Blank ! |
| ! !D ! Print-out Rules ! C ! 2 ! |
| ! !E ! Transfer to ACARS MU ! C ! No ! |
| ! !F ! Increment of the report counter if the ! C ! 1 ! |
| ! ! ! report was triggered by a code number ! ! ! |
| ! ! ! > 1000; 1=yes, 0=no ! ! ! |
| ! !G ! 'Y06.1' Pre-event print intervals in ! C ! 6 ! |
| ! ! ! seconds. ! ! ! |
| ! !H ! 'Y06.2' Post-event print intervals in ! C ! 5 ! |
| ! ! ! seconds. ! ! ! |
| ! !I ! 'M06.1' Number of Post-event data set ! C ! 5 ! |
| ! ! ! up to 20. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !1000!1 ! Manual selection via MCDU ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !2000!2 ! Flight phase dependent manual ! ! ! |
| ! ! ! selection via remote print button ! ! ! |
| ! ! ! if programmed. ! ! ! |
| ! !2.1 ! Remote Print Button assignment. ! C ! not ! |
| !----!------!-----------------------------------------!------!---------! |
| !3000!3 ! Programmable Start Logic ! ! ! |
| ! !3.1 ! Trigger condition ! C ! not ! |
| !----!------!-----------------------------------------!------!---------! |
| !4000!4 ! Report generation, if Stall bit is set ! ! ! |
| ! ! ! to '1'. ! ! ! |
| ! ! ! Eng.1 param. 7C.1.270.01.18 = 1 ! ! ! |
| ! ! ! Eng.2 param. 7C.2.270.10.18 = 1 ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !5100!5 ! EGT > EGTL1 in Flight Phases 3, 4, 5 ! ! ! |
| ! ! ! or ! ! ! |
| !5200! ! EGT > EGTL2 in all PH except ! ! ! |
| ! ! ! PH 1.1, 3, 4, 5 ! ! ! |
| ! ! ! or ! ! ! |
| !5300! ! EGT > EGTL3 in all PH ! ! ! |
| ! ! ! or ! ! ! |
| !5400! ! N1 > N1L1.1 in all PH ! ! ! |
| ! ! ! or ! ! ! |
| !5500! ! N1 > N1L1.2 in all PH ! ! ! |
| ! ! ! or ! ! ! |
| !5600! ! N2 > N2L1.1 in all PH ! ! ! |
| ! ! ! or ! ! ! |
| !5700! ! N2 > N2L1.2 in all PH ! ! ! |
| ! ! ! ! ! ! |
| ! !5.1 ! EGTL1 limit in C ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.2 ! EGTL2 limit in C (yellow limit) ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.3 ! EGTL3 limit in C (red limit) ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.4 ! N1L1.1 limit in %rpm (yellow limit) ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.5 ! N1L1.2 limit in %rpm (red limit) ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.6 ! N2L1.1 limit in %rpm (yellow limit) ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.7 ! N2L1.2 limit in %rpm (red limit) ! C ! limit- ! |
| ! ! ! ! ! table ! |
| !----!------!-----------------------------------------!------!---------! |
| !6000!6 ! If in PH 5, 5.1, 6, 7, 7.1 the fuel ! ! ! |
| ! ! ! shut off valve is closed. ! ! ! |
| ! ! ! param. 7C.1.270.01.14 = 1 or ! ! ! |
| ! ! ! param. 7C.1.270.10.14 = 1 ! ! ! |
| ! ! ! The report generation is only performed ! ! ! |
| ! ! ! in case that the status of the 'fuel ! ! ! |
| ! ! ! shut off valve' = 1 is stable for least ! ! ! |
| ! ! ! 4 seconds. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| ! !7 ! Report Generation stops when exceedance ! ! ! |
| ! ! ! parameter again within their limits or ! ! ! |
| ! ! ! 'M06.1' is reached. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !8100!8.1 ! ACARS MU uplink request with IMI 'REQ06'! ! ! |
| ! ! ! The report <06> is immediately generated! ! ! |
| ! ! ! and transmitted to the ACARS MU. ! ! ! |
| !----------------------------------------------------------------------! |
| ! A = Programmable by Airbus ! |
| ! C = Programmable by Customer ! |
| +----------------------------------------------------------------------+ |
(11) Engine Gas Path Advisory Report Logic <06> (Engine Type CFMI with Advanced EVMU)
| +----------------------------------------------------------------------+ |
| !Code!Item ! !Progr.!Standard ! |
| ! No.!No. ! Description of Function Item !MCDU !Value or ! |
| ! ! ! !/GSE !Table TXY! |
| !----!------!-----------------------------------------!------!---------! |
| ! !A ! Report Format ! ! ! |
| ! !B ! Parameter Table ! ! ! |
| ! !C ! First three lines of Report ! C ! Blank ! |
| ! !D ! Print-out Rules ! C ! See ! |
| ! ! ! ! ! separate! |
| ! ! ! ! ! list ! |
| ! !E ! Transfer to ACARS MU ! C ! See ! |
| ! ! ! ! ! separate! |
| ! ! ! ! ! list ! |
| ! !F ! Increment of the report counter if the ! C ! 1 ! |
| ! ! ! report was triggered by a code number ! ! ! |
| ! ! ! > 1000; 1=yes, 0=no ! ! ! |
| ! !G ! 'Y06.1' Pre-event print intervals in ! C ! 6 ! |
| ! ! ! seconds. ! ! ! |
| ! ! ! 'Y06.1' shall be programmable in the ! ! ! |
| ! ! ! range from 1 to 7. ! ! ! |
| ! !H ! 'Y06.2' Post-event print intervals in ! C ! 5 ! |
| ! ! ! seconds. ! ! ! |
| ! ! ! 'Y06.2' shall be programmable in the ! ! ! |
| ! ! ! range from 1 to 61. ! ! ! |
| ! !I ! 'M06.1' Number of Post-event data set ! C ! 5 ! |
| ! ! ! up to 20. ! ! ! |
| ! ! ! 'M06.1' shall be programmable in the ! ! ! |
| ! ! ! range from 1 to 11. ! ! ! |
| ! !J ! Max. No. of reports per trigger, engine ! C ! 10 ! |
| ! ! ! and flight leg. ! ! ! |
| ! !K ! Max. No of reports per engine and flight! C ! 50 ! |
| ! ! ! leg. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !1000!1 ! Manual selection via MCDU ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !2000!2 ! Flight phase dependent manual ! ! ! |
| ! ! ! selection via remote print button ! ! ! |
| ! ! ! if programmed. ! ! ! |
| ! !2.1 ! Remote Print Button assignment. ! C ! not ! |
| ! ! ! ! ! assigned! |
| !----!------!-----------------------------------------!------!---------! |
| !3000!3 ! Programmable Start Logic ! ! ! |
| ! !3.1 ! Trigger condition ! C ! not ! |
| ! ! ! ! ! progr. ! |
| !----!------!-----------------------------------------!------!---------! |
| !4000!4 ! Report generation, if Stall bit is set ! ! ! |
| ! ! ! to '1'. ! ! ! |
| ! ! ! Eng.1 param. 7C.1.270.01.18 = 1 ! ! ! |
| ! ! ! Eng.2 param. 7C.2.270.10.18 = 1 ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !5100!5 ! EGT > EGTL1 in Flight Phases 3, 4, 5 ! ! ! |
| ! ! ! or ! ! ! |
| !5200! ! EGT > EGTL2 in all PH except ! ! ! |
| ! ! ! PH 1.1, 3, 4, 5 ! ! ! |
| ! ! ! or ! ! ! |
| !5300! ! EGT > EGTL3 in all PH ! ! ! |
| ! ! ! or ! ! ! |
| !5400! ! N1 > N1L1.1 in all PH ! ! ! |
| ! ! ! or ! ! ! |
| !5500! ! N1 > N1L1.2 in all PH ! ! ! |
| ! ! ! or ! ! ! |
| !5600! ! N2 > N2L1.1 in all PH ! ! ! |
| ! ! ! or ! ! ! |
| !5700! ! N2 > N2L1.2 in all PH ! ! ! |
| ! ! ! ! ! ! |
| ! !5.1 ! EGTL1 limit in C ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.2 ! EGTL2 limit in C (yellow limit) ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.3 ! EGTL3 limit in C (red limit) ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.4 ! N1L1.1 limit in %rpm (yellow limit) ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.5 ! N1L1.2 limit in %rpm (red limit) ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.6 ! N2L1.1 limit in %rpm (yellow limit) ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.7 ! N2L1.2 limit in %rpm (red limit) ! C ! limit- ! |
| ! ! ! ! ! table ! |
| !----!------!-----------------------------------------!------!---------! |
| !6000!6 ! If in PH 5, 5.1, 6, 7, 7.1 the fuel ! ! ! |
| ! ! ! shut off valve is closed. ! ! ! |
| ! ! ! 7C.1.270.01.14 = 1 or ! ! ! |
| ! ! ! 7C.2.270.10.14 = 1 ! ! ! |
| ! ! ! The report generation is only performed ! ! ! |
| ! ! ! in the case that the status of the 'fuel! ! ! |
| ! ! ! shut off valve' = 1 is stable for at ! ! ! |
| ! ! ! least 4 seconds. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| ! !7 ! Report Generation stops when exceedance ! ! ! |
| ! ! ! parameter is again within its limits or ! ! ! |
| ! ! ! 'M06.1' is reached. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !8100!8.1 ! ACARS MU uplink request with IMI 'REQ06'! ! ! |
| ! ! ! The report <06> is immediately generated! ! ! |
| ! ! ! and transmitted to the ACARS MU. ! ! ! |
| !----------------------------------------------------------------------! |
| ! A = Programmable by Airbus ! |
| ! C = Programmable by Customer ! |
| +----------------------------------------------------------------------+ |
(12) Engine Gas Path Advisory Report Logic <06> (Engine Type CFMI with Advanced EVMU)
| +----------------------------------------------------------------------+ |
| !Code!Item ! !Progr.!Standard ! |
| ! No.!No. ! Description of Function Item !MCDU !Value or ! |
| ! ! ! !/GSE !Table TXY! |
| !----!------!-----------------------------------------!------!---------! |
| ! !A ! Report Format ! ! ! |
| ! !B ! Parameter Table ! ! ! |
| ! !C ! First three lines of Report ! C ! Blank ! |
| ! !D ! Print-out Rules ! C ! See ! |
| ! ! ! ! ! separate! |
| ! ! ! ! ! list ! |
| ! !E ! Transfer to ACARS MU ! C ! See ! |
| ! ! ! ! ! separate! |
| ! ! ! ! ! list ! |
| ! !F ! Increment of the report counter if the ! C ! 1 ! |
| ! ! ! report was triggered by a code number ! ! ! |
| ! ! ! > 1000; 1=yes, 0=no ! ! ! |
| ! !G ! 'Y06.1' Pre-event print intervals in ! C ! 6 ! |
| ! ! ! seconds. ! ! ! |
| ! ! ! 'Y06.1' shall be programmable in the ! ! ! |
| ! ! ! range from 1 to 7. ! ! ! |
| ! !H ! 'Y06.2' Post-event print intervals in ! C ! 5 ! |
| ! ! ! seconds. ! ! ! |
| ! ! ! 'Y06.2' shall be programmable in the ! ! ! |
| ! ! ! range from 1 to 61. ! ! ! |
| ! !I ! 'M06.1' Number of Post-event data set ! C ! 5 ! |
| ! ! ! up to 20. ! ! ! |
| ! ! ! 'M06.1' shall be programmable in the ! ! ! |
| ! ! ! range from 1 to 11. ! ! ! |
| ! !J ! Max. No. of reports per trigger, engine ! C ! 10 ! |
| ! ! ! and flight leg. ! ! ! |
| ! !K ! Max. No of reports per engine and flight! C ! 50 ! |
| ! ! ! leg. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !1000!1 ! Manual selection via MCDU ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !2000!2 ! Flight phase dependent manual ! ! ! |
| ! ! ! selection via remote print button ! ! ! |
| ! ! ! if programmed. ! ! ! |
| ! !2.1 ! Remote Print Button assignment. ! C ! not ! |
| ! ! ! ! ! assigned! |
| !----!------!-----------------------------------------!------!---------! |
| !3000!3 ! Programmable Start Logic ! ! ! |
| ! !3.1 ! Trigger condition ! C ! not ! |
| ! ! ! ! ! progr. ! |
| !----!------!-----------------------------------------!------!---------! |
| !4000!4 ! Report generation, if Stall bit is set ! ! ! |
| ! ! ! to '1'. ! ! ! |
| ! ! ! Eng.1 param. 7C.1.270.01.18 = 1 ! ! ! |
| ! ! ! Eng.2 param. 7C.2.270.10.18 = 1 ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !5100!5 ! EGT > EGTL1 in Flight Phases 3, 4, 5 ! ! ! |
| ! ! ! or ! ! ! |
| !5200! ! EGT > EGTL2 in all PH except ! ! ! |
| ! ! ! PH 1.1, 3, 4, 5 ! ! ! |
| ! ! ! or ! ! ! |
| !5300! ! EGT > EGTL3 in all PH ! ! ! |
| ! ! ! or ! ! ! |
| !5400! ! N1 > N1L1.1 in all PH ! ! ! |
| ! ! ! or ! ! ! |
| !5500! ! N1 > N1L1.2 in all PH ! ! ! |
| ! ! ! or ! ! ! |
| !5600! ! N2 > N2L1.1 in all PH ! ! ! |
| ! ! ! or ! ! ! |
| !5700! ! N2 > N2L1.2 in all PH ! ! ! |
| ! ! ! ! ! ! |
| ! !5.1 ! EGTL1 limit in deg C ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.2 ! EGTL2 limit in deg C (yellow limit) ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.3 ! EGTL3 limit in deg C (red limit) ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.4 ! N1L1.1 limit in %rpm (yellow limit) ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.5 ! N1L1.2 limit in %rpm (red limit) ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.6 ! N2L1.1 limit in %rpm (yellow limit) ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.7 ! N2L1.2 limit in %rpm (red limit) ! C ! limit- ! |
| ! ! ! ! ! table ! |
| !----!------!-----------------------------------------!------!---------! |
| !6000!6 ! If in PH 5, 5.1, 6, 7, 7.1 the fuel ! ! ! |
| ! ! ! shut off valve is closed. ! ! ! |
| ! ! ! 7C.1.270.01.14 = 1 or ! ! ! |
| ! ! ! 7C.2.270.10.14 = 1 ! ! ! |
| ! ! ! The report generation is only performed ! ! ! |
| ! ! ! in the case that the status of the 'fuel! ! ! |
| ! ! ! shut off valve' = 1 is stable for at ! ! ! |
| ! ! ! least 4 seconds. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| ! !7 ! Report Generation stops when exceedance ! ! ! |
| ! ! ! parameter is again within its limits or ! ! ! |
| ! ! ! 'M06.1' is reached. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !8100!8.1 ! ACARS MU uplink request with IMI 'REQ06'! ! ! |
| ! ! ! The report <06> is immediately generated! ! ! |
| ! ! ! and transmitted to the ACARS MU. ! ! ! |
| !----------------------------------------------------------------------! |
| ! A = Programmable by Airbus ! |
| ! C = Programmable by Customer ! |
| +----------------------------------------------------------------------+ |
(13) Engine Gas Path Advisory Report Logic <06> (Engine Type CFMI with Advanced EVMU)
| +----------------------------------------------------------------------+ |
| !Code!Item ! !Progr.!Standard ! |
| ! No.!No. ! Description of Function Item !------!Value or ! |
| ! ! ! !MCDU/ !Table TXY! |
| ! ! ! !GSE ! ! |
| !----!------!-----------------------------------------!------!---------! |
| ! !A ! Report Format ! ! ! |
| ! !A.1 ! "R006RLID" Report Layout Identifier ! ! 01 ! |
| ! ! ! (for ACARS header) ! ! ! |
| ! !A.2 ! "R006RLIS" Report Layout Issue ! ! 01 ! |
| ! ! ! (for ACARS header) ! ! ! |
| ! !B ! Parameter Table ! ! ! |
| ! !C ! First three lines of Report ! C ! Blank ! |
| ! !D ! Print-out Rules ! C ! See ! |
| ! ! ! ! ! separate! |
| ! ! ! ! ! list ! |
| ! !E ! Transfer to ACARS MU ! C ! See ! |
| ! ! ! ! ! separate! |
| ! ! ! ! ! list ! |
| ! !F ! Increment of the report counter if the ! C ! 1 ! |
| ! ! ! report was triggered by a code number ! ! ! |
| ! ! ! > 1000; 1=yes, 0=no ! ! ! |
| ! !G ! "Y06.1" Pre-event print intervals in ! C ! 6 ! |
| ! ! ! seconds. ! ! ! |
| ! ! ! "Y06.1" is programmable in the range ! ! ! |
| ! ! ! from 1 to 7. ! ! ! |
| ! !H ! "Y06.2" Post-event print intervals in ! C ! 5 ! |
| ! ! ! seconds. ! ! ! |
| ! ! ! "Y06.2" is programmable in the range ! ! ! |
| ! ! ! from 1 to 61. ! ! ! |
| ! !I ! "M06.1" Number of Post-event data set ! C ! 5 ! |
| ! ! ! up to 20. ! ! ! |
| ! ! ! "M06.1" is programmable in the range ! ! ! |
| ! ! ! from 1 to 11. ! ! ! |
| ! !J ! Max. No. of reports per trigger, engine ! C ! 10 ! |
| ! ! ! and flight leg. ! ! ! |
| ! !K ! Max. No of reports per engine and flight! C ! 50 ! |
| ! ! ! leg. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !1000!1 ! Manual selection through MCDU ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !2000!2 ! Flight phase dependent manual ! ! ! |
| ! ! ! selection through remote print button ! ! ! |
| ! ! ! if programmed. ! ! ! |
| ! !2.1 ! Remote Print Button assignment. ! C ! not ! |
| ! ! ! ! ! assigned! |
| !----!------!-----------------------------------------!------!---------! |
| !3000!3 ! Programmable Start Logic ! ! ! |
| ! !3.1 ! Trigger condition ! C ! not ! |
| ! ! ! ! ! progr. ! |
| !----!------!-----------------------------------------!------!---------! |
| !4000!4 ! Report generation, if Stall bit is set ! ! ! |
| ! ! ! to "1". ! ! ! |
| ! ! ! Eng.1 param. 7C.1.270.01.18 = 1 ! ! ! |
| ! ! ! Eng.2 param. 7C.2.270.10.18 = 1 ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !5100!5 ! (EGT > EGTL1) AND ! ! ! |
| ! ! ! ?? (PH == 3) OR ! ! ! |
| ! ! ! (PH == 4) OR ! ! ! |
| ! ! ! (PH == 5) OR ! ! ! |
| ! ! ! (PH == 6) ! ! ! |
| ! ! ! (Alpha Floor protection active == 1) |! ! ! |
| ! ! ! AND ! ! ! |
| ! ! ! (EGT limit exceedance indicated by ! ! ! |
| ! ! ! FWC == 1) ! ! ! |
| ! ! ! Alpha Floor protection active ! ! ! |
| ! ! ! 7C.1.272.01.21 = 1 Engine 1 ! ! ! |
| ! ! ! 7C.2.272.10.21 = 1 Engine 2 ! ! ! |
| ! ! ! EGT limit exceedance indicated by FWC ! ! ! |
| ! ! ! 26.1.124.00.15 = 1 Engine 1 ! ! ! |
| ! ! ! 26.2.124.00.15 = 1# ! ! ! |
| ! ! ! 26.1.124.00.16 = 1 Engine 2 ! ! ! |
| ! ! ! 26.2.124.00.16 = 1# ! ! ! |
| ! ! ! or ! ! ! |
| !5200! ! (EGT > EGTL2) AND ! ! ! |
| ! ! ! ( (PH != 1.1) AND ! ! ! |
| ! ! ! (PH != 3) AND ! ! ! |
| ! ! ! (PH != 4) AND ! ! ! |
| ! ! ! (PH != 5) ) AND ! ! ! |
| ! ! ! (EGT limit exceedance indicated by ! ! ! |
| ! ! ! FWC == 1) ! ! ! |
| ! ! ! or ! ! ! |
| !5300! ! Not applicable ! ! ! |
| ! ! ! or ! ! ! |
| !5400! ! N1 > N1L1.1 in all PH ! ! ! |
| ! ! ! or ! ! ! |
| !5500! ! N1 > N1L1.2 in all PH ! ! ! |
| ! ! ! or ! ! ! |
| !5600! ! N2 > N2L1.1 in all PH ! ! ! |
| ! ! ! or ! ! ! |
| !5700! ! N2 > N2L1.2 in all PH ! ! ! |
| ! ! ! ! ! ! |
| ! !5.1 ! EGTL1 limit in Degrees C (red limit) ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.2 ! EGTL2 limit in Degrees C (yellow limit) ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.3 ! Not applicable ! ! ! |
| ! ! ! ! ! ! |
| ! !5.4 ! N1L1.1 limit in %rpm (yellow limit) ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.5 ! N1L1.2 limit in %rpm (red limit) ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.6 ! N2L1.1 limit in %rpm (yellow limit) ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.7 ! N2L1.2 limit in %rpm (red limit) ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !5.8 ! If trigger code 5100 is activated ! ! ! |
| ! ! ! and report code 5200 was already acti- ! ! ! |
| ! ! ! vated before but not closed yet, report ! ! ! |
| ! ! ! code 5100 is only generated and code ! ! ! |
| ! ! ! 5200 is discarded. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !6000!6 ! If in PH 5, 5.1, 6, 7, 7.1 the fuel ! ! ! |
| ! ! ! shut off valve is closed. ! ! ! |
| ! ! ! 7C.1.270.01.14 = 1 or ! ! ! |
| ! ! ! 7C.2.270.10.14 = 1 ! ! ! |
| ! ! ! The report generation is only performed ! ! ! |
| ! ! ! in the case that the status of the "fuel! ! ! |
| ! ! ! shut off valve" = 1 is stable for at ! ! ! |
| ! ! ! least 4 seconds. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| ! !7 ! Report Generation stops when exceedance ! ! ! |
| ! ! ! parameter is again within its limits or ! ! ! |
| ! ! ! "M06.1" is reached. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !8100!8.1 ! ACARS MU uplink request with IMI "REQ06"! ! ! |
| ! ! ! The report <06> is immediately generated! ! ! |
| ! ! ! and transmitted to the ACARS MU. ! ! ! |
| !----------------------------------------------------------------------! |
| ! A = Programmable by Airbus ! |
| ! C = Programmable by Customer ! |
| +----------------------------------------------------------------------+ |
J. AIDS Reports Print Rules - Default Values for Report <06>
| +------------------------------------------------+ |
| ! ! ! ! |
| ! Code ! Printer Output ! ACARS-output ! |
| ! ! ! ! |
| !-------!-----------------------!----------------! |
| ! ! ! ! |
| ! 1000 ! Print immediatly ! No ACARS ! |
| ! ! ! ! |
| !-------!-----------------------!----------------! |
| ! ! ! ! |
| ! 2000 ! Print immediatly ! No ACARS ! |
| ! ! ! ! |
| !-------!-----------------------!----------------! |
| ! ! ! ! |
| ! 4000 ! Print at landing ! ACARS VHF ! |
| ! ! ! ! |
| !-------!-----------------------!----------------! |
| ! ! ! ! |
| ! 5100 ! Print at landing ! ACARS VHF ! |
| ! ! ! ! |
| !-------!-----------------------!----------------! |
| ! ! ! ! |
| ! 5200 ! Print at landing ! ACARS VHF ! |
| ! ! ! ! |
| !-------!-----------------------!----------------! |
| ! ! ! ! |
| ! 5300 ! Print at landing ! ACARS VHF ! |
| ! ! ! ! |
| !-------!-----------------------!----------------! |
| ! ! ! ! |
| ! 5400 ! Print at landing ! ACARS VHF ! |
| ! ! ! ! |
| !-------!-----------------------!----------------! |
| ! ! ! ! |
| ! 5500 ! Print at landing ! ACARS VHF ! |
| ! ! ! ! |
| !-------!-----------------------!----------------! |
| ! ! ! ! |
| ! 5600 ! Print at landing ! ACARS VHF ! |
| ! ! ! ! |
| !-------!-----------------------!----------------! |
| ! ! ! ! |
| ! 5700 ! Print at landing ! ACARS VHF ! |
| ! ! ! ! |
| !-------!-----------------------!----------------! |
| ! ! ! ! |
| ! 6000 ! Print at landing ! ACARS VHF ! |
| ! ! ! ! |
| !-------!-----------------------!----------------! |
| ! ! ! ! |
| ! 8100 ! No print ! ACARS VHF ! |
| ! ! ! ! |
| +------------------------------------------------+ |
| +-------------------------------------------------------------------------+ |
| !Trigger! to ACARS ! to printer ! store ! |
| ! Code !------------------------------ -!-----------------!--------------! |
| ! No !Ground ! VHF ! SAT- ! HF ! at ! imme- ! internal& ! |
| ! ! ! ! COM ! !landing ! diate ! external ! |
| ! ! ! ! ! ! ! !(build in RAM&! |
| ! ! ! ! ! ! ! ! PCMCIA) ! |
| !-------!-------!--------!-------!-------!--------!--------!--------------! |
| ! ! ! If ! ! ! ! If !PCMCIA only if! |
| ! 1000 ! NO ! 'SEND' ! NO ! NO ! NO !'PRINT' ! 'STORE' ! |
| ! ! !selected! ! ! !selected! selected on ! |
| ! ! !on MCDU ! ! ! !on MCDU ! MCDU ! |
| !-------!-------!--------!-------!-------!--------!--------!--------------! |
| ! 2000 ! NO ! NO ! NO ! NO ! ! YES ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 3000 ! NO ! NO ! NO ! NO ! Y ! NO ! YES ! |
| !-------!-------!--------!------ !-------! E !--------!--------------! |
| ! 4000 ! NO ! YES ! NO ! NO ! S ! NO ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 5100 ! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 5200 ! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| !-------!-----------------------------------------------------------------! |
| ! 5300 ! Not applicable ! |
| !-------!-----------------------------------------------------------------! |
| ! 5400 ! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 5500 ! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| !-------!-------!--------!-------!-------! Y !--------!--------------! |
| ! 5600 ! NO ! YES ! NO ! NO ! E ! NO ! YES ! |
| !-------!-------!--------!-------!-------! S !--------!--------------! |
| ! 5700 ! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 6000 ! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 8100 ! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| +-------------------------------------------------------------------------+ |
| +-------------------------------------------------------------------------+ |
| !Trigger! to ACARS ! to printer ! store ! |
| ! Code !------------------------------ -!-----------------!--------------! |
| ! No !Ground ! VHF ! SAT- ! HF ! at ! imme- ! internal& ! |
| ! ! ! ! COM ! !landing ! diate ! external ! |
| ! ! ! ! ! ! ! !(build in RAM&! |
| ! ! ! ! ! ! ! ! PCMCIA) ! |
| !-------!-------!--------!-------!-------!--------!--------!--------------! |
| ! 1000 ! NO ! NO ! NO ! NO ! NO ! YES ! YES ! |
| !-------!-------!--------!-------!-------!--------!--------!--------------! |
| ! 2000 ! NO ! NO ! NO ! NO ! NO ! YES ! YES ! |
| !-------!-------!--------!-------!-------!--------!--------!--------------! |
| ! 3000 ! NO ! NO ! NO ! NO ! NO ! NO ! YES ! |
| !-------!-------!--------!------ !-------!--------!--------!--------------! |
| ! 4000 ! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 5100 ! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 5200 ! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 5300 ! NO ! YES ! NO ! NO ! Y ! NO ! YES ! |
| !-------!-------!--------!-------!-------! E !--------!--------------! |
| ! 5400 ! NO ! YES ! NO ! NO ! S ! NO ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 5500 ! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 5600 ! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 5700 ! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 6000 ! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| !-------!-------!--------!-------!-------!--------!--------!--------------! |
| ! 8100 ! NO ! YES ! NO ! NO ! NO ! NO ! YES ! |
| +-------------------------------------------------------------------------+ |
| +-------------------------------------------------------------------------+ |
| !Trigger! to ACARS ! to printer ! store ! |
| ! Code !------------------------------ -!-----------------!--------------! |
| ! No !Ground ! VHF ! SAT- ! HF ! at ! imme- ! internal& ! |
| ! ! ! ! COM ! !landing ! diate ! external ! |
| ! ! ! ! ! ! ! !(build in RAM&! |
| ! ! ! ! ! ! ! ! PCMCIA) ! |
| !-------!-------!--------!-------!-------!--------!--------!--------------! |
| ! 1000 ! NO ! NO ! NO ! NO ! NO ! YES ! YES ! |
| !-------!-------!--------!-------!-------!--------!--------!--------------! |
| ! 2000 ! NO ! NO ! NO ! NO ! NO ! YES ! YES ! |
| !-------!-------!--------!-------!-------!--------!--------!--------------! |
| ! 3000 ! NO ! NO ! NO ! NO ! NO ! NO ! YES ! |
| !-------!-------!--------!------ !-------!--------!--------!--------------! |
| ! 4000 ! NO ! YES ! NO ! NO ! YES ! NO ! YES ! |
| !-------!-------!--------!-------!-------!--------!--------!--------------! |
| ! 5100 ! NO ! YES ! NO ! NO ! YES ! NO ! YES ! |
| !-------!-------!--------!-------!-------!--------!--------!--------------! |
| ! 5200 ! NO ! YES ! NO ! NO ! YES ! NO ! YES ! |
| !-------!-----------------------------------------------------------------! |
| ! 5300 ! NOT APPLICABLE ! |
| !-------!-----------------------------------------------------------------! |
| ! 5400 ! NO ! YES ! NO ! NO ! YES ! NO ! YES ! |
| !-------!-------!--------!-------!-------!--------!--------!--------------! |
| ! 5500 ! NO ! YES ! NO ! NO ! YES ! NO ! YES ! |
| !-------!-------!--------!-------!-------!--------!--------!--------------! |
| ! 5600 ! NO ! YES ! NO ! NO ! YES ! NO ! YES ! |
| !-------!-------!--------!-------!-------!--------!--------!--------------! |
| ! 5700 ! NO ! YES ! NO ! NO ! YES ! NO ! YES ! |
| !-------!-------!--------!-------!-------!--------!--------!--------------! |
| ! 6000 ! NO ! YES ! NO ! NO ! YES ! NO ! YES ! |
| !-------!-------!--------!-------!-------!--------!--------!--------------! |
| ! 8100 ! NO ! YES ! NO ! NO ! NO ! NO ! YES ! |
| +-------------------------------------------------------------------------+ |
K. Engine Mechanical Advisory Report <07>
Engine Mechanical Advisory Report <07> (Engine Type CFMI with Advanced EVMU)
Engine Mechanical Advisory Report <07> (Engine Type CFMI with Advanced EVMU)
Engine Mechanical Advisory Report <07> (Engine Type CFMI with Advanced EVMU) ** ON A/C NOT FOR ALL
Engine Mechanical Advisory Report <07> (Engine Type CFMI with Advanced EVMU) ** ON A/C NOT FOR ALL
Engine Mechanical Advisory Report <07> (Engine Type CFMI with Advanced EVMU) ** ON A/C NOT FOR ALL
The Engine Mechanical Advisory Report shall be a collection of engine related information when there has been an exceedance of one of the secondary engine parameters. In particular engine oil pressure, engine oil temperature, engine oil consumption, engine nacelle temperature and engine vibrations shall be monitored for out of tolerance conditions. The report is generated when one of the logic conditions 1000 to 4400 (for details see the Engine Mechanical Advisory Report logic) is present.
Engine Mechanical Advisory Report <07> (Engine Type CFMI with Advanced EVMU) Engine Mechanical Advisory Report <07> (Engine Type CFMI with Advanced EVMU) Engine Mechanical Advisory Report <07> (Engine Type CFMI with Advanced EVMU) ** ON A/C NOT FOR ALL Engine Mechanical Advisory Report <07> (Engine Type CFMI with Advanced EVMU) ** ON A/C NOT FOR ALL Engine Mechanical Advisory Report <07> (Engine Type CFMI with Advanced EVMU) ** ON A/C NOT FOR ALL NOTE: For the standard header definition of the report refer to (Ref. AMM D/O 31-36-00-00).
(1) Engine Mechanical Advisory Report Data Field Description <07> (Engine Type CFMI with Advanced EVMU)
NOTE: Reports that are transmitted from the ACARS system do not have report lines without a line identifier.
| +---------------------------------------------------------------------+ |
| ! Value ! Content Description ! |
| !--------------!------------------------------------------------------! |
| ! ESN ! Engine Serial Number ! |
| ! 999999 ! (000000 to 999999) ! |
| ! ! Eng 1 param. 7C.1.046.01 digit 3, 2, 1 ! |
| ! ! 7C.1.047.01 digit 6, 5, 4 ! |
| ! ! Eng 2 param. 7C.2.046.01 digit 3, 2, 1 ! |
| ! ! 7C.2.047.01 digit 6, 5, 4 ! |
| !--------------!------------------------------------------------------! |
| ! EHRS ! Engine Flight Hours ! |
| ! 99999 ! (00000 to 99999 hours) ! |
| ! ! DMU Engine 1 and Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! ERT ! Engine Running Time ! |
| ! 99999 ! (00000 to 65536 hours) ! |
| ! ! Eng 1 param. 7C.1.050.01 ! |
| ! ! Eng 2 param. 7C.2.050.10 ! |
| !--------------!------------------------------------------------------! |
| ! ECYC ! Engine Cycle ! |
| ! 99999 ! (00000 to 99999) ! |
| !--------------!------------------------------------------------------! |
| ! AP ! Auto Pilot Status ! |
| ! 99 ! (00 to G8) ! |
| ! ! FMGC 1 and 2 (FGC part) for Auto Pilot AP1 and AP2 ! |
| ! ! ! |
| ! ! XX Auto Pilot Modes: ! |
| ! ! !! ! |
| ! ! !!__Lateral Modes: 0 = NO MODE ! |
| ! ! ! 1 = HEADING ! |
| ! ! ! 2 = TRACK ! |
| ! ! ! 3 = NAV ! |
| ! ! ! 4 = LOC CAPTURE ! |
| ! ! ! 5 = LOC TRACK ! |
| ! ! ! 6 = LAND TRACK ! |
| ! ! ! 7 = RUNWAY ! |
| ! ! ! 8 = ROLL GO AROUND ! |
| ! ! ! ! |
| ! ! !__Longitudinal Modes: 0 = NO MODE ! |
| ! ! 1 = PITCH G/A ! |
| ! ! 2 = PITCH T/O ! |
| ! ! 3 = G/S TRACK ! |
| ! ! 4 = G/S CAPTURE ! |
| ! ! 5 = V/S ! |
| ! ! 6 = FPA ! |
| ! ! 7 = ALT ! |
| ! ! 8 = ALT ACQ ! |
| ! ! 9 = OPEN CLB ! |
| ! ! A = OPEN DES ! |
| ! ! B = IM CLB ! |
| ! ! C = IM DES ! |
| ! ! D = CLB ! |
| ! ! E = DES ! |
| ! ! F = FINAL DES ! |
| ! ! G = EXPEDITE ! |
| ! ! ! |
| ! ! AP1 ! AP2 ! |
| ! ! Report Line EC: ! Report Line EE: !Difinition: ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! / ! / !No Mode Act. ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.11 = 1 ! 01.2.275.00.11 = 1!RUNWAY Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.12 = 1 ! 01.2.275.00.12 = 1!NAV Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.13 = 1 ! 01.2.275.00.13 = 1!LOC CAPTURE ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.14 = 1 ! 01.2.275.00.14 = 1!LOC TRACK ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.15 = 1 ! 01.2.275.00.15 = 1!Roll GO ! |
| ! ! ! !AROUND Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.16 = 1 ! 01.2.275.00.16 = 1!HEADING Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.17 = 1 ! 01.2.275.00.17 = 1!TRACK Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.15 = 1 ! 01.2.274.00.15 = 1!PITCH TO Mode! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.16 = 1 ! 01.2.274.00.16 = 1!PITCH GA Mode! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.17 = 1 ! 01.2.274.00.17 = 1!V/S Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.18 = 1 ! 01.2.274.00.18 = 1!FPA Mode ! |
| ! ! -------------------!-------------------!-------------! |
| ! ! 01.1.274.00.19 = 1 ! 01.2.274.00.19 = 1!ALT Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.20 = 1 ! 01.2.274.00.20 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.19 = 1 ! 01.2.274.00.19 = 1!ALT ACQ ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.21 = 1 ! 01.2.274.00.21 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.20 = 1 ! 01.2.274.00.20 = 1!G/S TRACK ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.22 = 1 ! 01.2.274.00.22 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.21 = 1 ! 01.2.274.00.21 = 1!G/S CAPTURE ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.22 = 1 ! 01.2.274.00.22 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.23 = 1 ! 01.2.274.00.23 = 1!FINAL DES ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.2.274.00.24 = 1 ! 01.2.274.00.24 = 1!EXPED. Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.146.00.14 = 1 ! 01.2.146.00.14 = 1!LAND TRACK ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!CLB Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.13 = 0 ! 01.2.274.00.13 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.14 = 0 ! 01.2.274.00.14 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.24 = 0 ! 01.2.274.00.24 = 0! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!DES Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.13 = 0 ! 01.2.274.00.13 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.14 = 0 ! 01.2.274.00.14 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.24 = 0 ! 01.2.274.00.24 = 0! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!IM. CLIMB ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.13 = 1 ! 01.2.274.00.13 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!IM. DES Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.13 = 1 ! 01.2.274.00.13 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!OPEN CLB ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.14 = 1 ! 01.2.274.00.14 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!OPEN DES ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.14 = 1 ! 01.2.274.00.14 = 1! ! |
| ! ! ---------------------------------------------------- ! |
| ! ! Auto Pilot Status DMU: ! |
| ! ! AP1 printed in report line EC ! |
| ! ! AP2 printed in report line EE ! |
| !--------------!------------------------------------------------------! |
| ! ECW1 ! Engine Control Word 1 ! |
| ! XXXXX ! Each 'X' represents 4 Bits in hexadecimal code of ! |
| ! ! a defined ARINC 429 word: ! |
| ! ! XXXXX Bits HEX ! |
| ! ! !!!!!___________ 14, 13, 12, 11 0...F ! |
| ! ! !!!!____________ 18, 17, 16, 15 0...F ! |
| ! ! !!!_____________ 22, 21, 20, 19 0...F ! |
| ! ! !!______________ 26, 25, 24, 23 0...F ! |
| ! ! !_______________ 29, 28, 27 0...7 ! |
| ! ! -------------------------------------------- ! |
| ! ! Bit Label Parameter Description ! |
| ! ! 11 7C.X.272.XX.19 = 1 Auto Thrust Active ! |
| ! ! 12 7C.X.272.XX.20 = 1 VSV Position Fault ! |
| ! ! 13 SPARE ! |
| ! ! 14 SPARE ! |
| ! ! 15 7C.X.351.XX.29 = 1 Fuel Flow Measurement ! |
| ! ! Invalid ! |
| ! ! 16 7C.X.275.XX.15 = 1 N1/N2 Control ACtive ! |
| ! ! 17 7C.X.275.XX.26 = 1 Channel A Active ! |
| ! ! 18 7C.X.275.XX.27 = 1 Channel B Active ! |
| ! ! 19 SPARE ! |
| ! ! 20 SPARE ! |
| ! ! 21 SPARE ! |
| ! ! 22 SPARE ! |
| ! ! 23 SPARE ! |
| ! ! 24 SPARE ! |
| ! ! 25 SPARE ! |
| ! ! 26 SPARE ! |
| ! ! 27 SPARE ! |
| ! ! 28 SPARE ! |
| ! ! 29 SPARE ! |
| !--------------!------------------------------------------------------! |
| ! E ! Exeedance Engine Position ! |
| ! 9 ! ! |
| !--------------!------------------------------------------------------! |
| ! MAX ! Maximal Value of the Exceeded Parameter ! |
| ! 9999 ! ! |
| !--------------!------------------------------------------------------! |
| ! LIM ! Programmable Limit, which was exceeded ! |
| ! 9999 ! ! |
| !--------------!------------------------------------------------------! |
| ! REF ! N2 at Stall Detection ! |
| ! 9999 ! (0.0 to 120.0% rpm) ! |
| !--------------!------------------------------------------------------! |
| ! TOL ! Time Over Limit ! |
| ! 999 ! (Observation time max 60 seconds) ! |
| !--------------!------------------------------------------------------! |
| ! TTP ! Time To Peak ! |
| ! 999 ! ! |
| !--------------!------------------------------------------------------! |
| ! EVM ! Engine Vibration Status Word ! |
| ! XXXXX ! Eng.1 param. 3D.1.035.01 ! |
| ! ! Eng.2 param. 3D.1.035.10 ! |
| ! ! Each 'X' represents 4 Bits in hexadecimal code of ! |
| ! ! a defined ARINC 429 word: ! |
| ! ! XXXXX Bits HEX ! |
| ! ! !!!!!___________ 14, 13, 12, 11 0...F ! |
| ! ! !!!!____________ 18, 17, 16, 15 0...F ! |
| ! ! !!!_____________ 22, 21, 20, 19 0...F ! |
| ! ! !!______________ 26, 25, 24, 23 0...F ! |
| ! ! !_______________ 29, 28, 27 0...7 ! |
| !--------------!------------------------------------------------------! |
| ! REASON ! Reason for Exceedance ! |
| ! XXXXXXXXXX ! ! |
| ! XXXXXXXXXX ! Up to 20 Characters ! |
| ! ! OIT Code: 4110, 4120 and 4130 ! |
| ! ! OIP Code: 4210, 4220 and 4230 ! |
| ! ! VB1 Code: 4310 ! |
| ! ! VB2 Code: 4320 ! |
| !--------------!------------------------------------------------------! |
| ! N1 ! Selected N1 Actual ! |
| ! 9999 ! (0 to 120.0 %rpm) ! |
| ! ! Eng 1 param. 7C.1.346.01 ! |
| ! ! Eng 2 param. 7C.2.346.10 ! |
| !--------------!------------------------------------------------------! |
| ! N2 ! Selected N2 Actual ! |
| ! 9999 ! (0 to 120.0 %rpm) ! |
| ! ! Eng 1 param. 7C.1.344.01 ! |
| ! ! Eng 2 param. 7C.2.344.10 ! |
| !--------------!------------------------------------------------------! |
| ! VN ! FAN Pick Up N1 Track Vibration ! |
| ! 99 ! (0.0 to 10.0) ! |
| ! ! Eng 1 param. 3D.1.227.01 ! |
| ! ! Eng 2 param. 3D.1.227.10 ! |
| !--------------!------------------------------------------------------! |
| ! VC ! FAN Pick Up N2 Track Vibration ! |
| ! 99 ! (0.0 to 4.0) ! |
| ! ! Eng 1 param. 3D.1.230.01 ! |
| ! ! Eng 2 param. 3D.1.230.10 ! |
| !--------------!------------------------------------------------------! |
| ! VH ! TRF Pick Up N2 Track Vibration ! |
| ! 99 ! (0.0 to 4.0) ! |
| ! ! Eng 1 param. 3D.1.230.11 ! |
| ! ! Eng 2 param. 3D.1.230.00 ! |
| !--------------!------------------------------------------------------! |
| ! VL ! TRF Pick Up N1 Vibration ! |
| ! 99 ! (0.0 to 10.0) ! |
| ! ! Eng 1 param. 3D.1.227.11 ! |
| ! ! Eng 2 param. 3D.1.227.00 ! |
| !--------------!------------------------------------------------------! |
| ! PHA ! FAN Pick Up Phase Angle ! |
| ! 999 ! (0 to 360 deg) ! |
| ! ! Eng 1 param. 3D.1.226.01 ! |
| ! ! Eng 2 param. 3D.1.226.10 ! |
| !--------------!------------------------------------------------------! |
| ! PHT ! TRF Pick Up Phase Angle ! |
| ! 999 ! (0 to 360 deg) ! |
| ! ! Eng 1 param. 3D.1.226.11 ! |
| ! ! Eng 2 param. 3D.1.226.00 ! |
| !--------------!------------------------------------------------------! |
| ! OIT ! Engine Oil Temperature ! |
| ! X99 ! (-60 to 250 C) ! |
| ! ! Eng 1 param. 26.1.316.01 ! |
| ! ! 26.2.316.01 ! |
| ! ! Eng 2 param. 26.1.316.10 ! |
| ! ! 26.2.316.10 ! |
| !--------------!------------------------------------------------------! |
| ! OIP ! Engine Oil Pressure ! |
| ! 999 ! (0 to 400 psia) ! |
| ! ! Eng 1 param. 26.1.317.01 ! |
| ! ! 26.2.317.01 ! |
| ! ! Eng 2 param. 26.1.317.10 ! |
| ! ! 26.2.317.10 ! |
| +---------------------------------------------------------------------+ |
(2) Engine Mechanical Advisory Report Data Field Description <07> (Engine Type CFMI with Advanced EVMU)
NOTE: Reports that are transmitted from the ACARS system do not have report lines without a line identifier.
NOTE: Only the parts of the ENGINE MECHANICAL ADVISORY REPORT <07> which are not included in the ENGINE CRUISE REPORT <01> are given in the subsequent table.
| +---------------------------------------------------------------------+ |
| ! Value ! Content Description ! |
| !--------------!------------------------------------------------------! |
| ! E ! Exeedance Engine Position ! |
| ! 9 ! DMU (No. of engine where the exceedance occurs. ! |
| ! ! If the report was not triggered by a limit ! |
| ! ! exceedance then this field has zero's. ! |
| !--------------!------------------------------------------------------! |
| ! MAX ! Maximal Value of the Exceeded Parameter ! |
| ! 9999 ! If there is OIPL1.1 or OIPL1.2 exceedance the ! |
| ! ! minimal value is printed. If the report was not ! |
| ! ! triggered by a limit exceedance then this field ! |
| ! ! has zero's. ! |
| !--------------!------------------------------------------------------! |
| ! LIM ! Programmable Limit, which was exceeded ! |
| ! 9999 ! ! |
| ! ! If the report was not triggered by a limit ! |
| ! ! exceedance then this field has zero's. ! |
| !--------------!------------------------------------------------------! |
| ! REF ! N2 at Stall Detection ! |
| ! 9999 ! ECU (0.0 to 120.0% rpm) ! |
| ! ! N1 7C.1.346.01 Engine 1 ! |
| ! ! 7C.2.346.10 Engine 2 ! |
| ! ! ! |
| ! ! N2 7C.1.346.01 Engine 1 ! |
| ! ! 7C.2.346.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! TOL ! Time Over Limit ! |
| ! 999 ! DMU (Observation time max 60 seconds) ! |
| ! ! If the report was not triggered by a limit ! |
| ! ! exceedance then this field has zero's. ! |
| !--------------!------------------------------------------------------! |
| ! TTP ! Time To Peak ! |
| ! 999 ! ! |
| ! ! If the report was not triggered by a limit ! |
| ! ! exceedance then this field has zero's. ! |
| !--------------!------------------------------------------------------! |
| ! REASON ! Reason for Exceedance ! |
| ! XXXXXXXXXX ! ! |
| ! XXXXXXXXXX ! Up to 20 Characters ! |
| ! ! OIT Code: 4110, 4120 and 4130 ! |
| ! ! OIP Code: 4210, 4220 and 4230 ! |
| ! ! VB1 Code: 4310 ! |
| ! ! VB2 Code: 4320 ! |
| ! ! If the report was not triggered by a limit ! |
| ! ! exceedance then this field has zero's. ! |
| +---------------------------------------------------------------------+ |
(3) Engine Mechanical Advisory Report Data Field Description <07> (Engine Type CFMI with Advanced EVMU)
NOTE: Reports that are transmitted from the ACARS system do not have report lines without a line identifier.
NOTE: Only the parts of the ENGINE MECHANICAL ADVISORY REPORT <07> which are not included in the ENGINE CRUISE REPORT <01> are given in the subsequent table.
| +---------------------------------------------------------------------+ |
| ! Value ! Content Description ! |
| !--------------!------------------------------------------------------! |
| ! E ! Exceedance Engine Position ! |
| ! 9 ! DMU (No. of engine where the exceedance occurs. ! |
| ! ! NOTE: If the report was not triggered by a limit ! |
| ! ! exceedance then this field has zeros. ! |
| !--------------!------------------------------------------------------! |
| ! MAX ! Maximal Value of the Exceeded Parameter ! |
| ! 9999 ! NOTE: If there is OIPL1.1 or OIPL1.2 exceedance the! |
| ! ! minimal value is printed. If the report was ! |
| ! ! not triggered by a limit exceedance then ! |
| ! ! this field has zeros. ! |
| !--------------!------------------------------------------------------! |
| ! LIM ! Programmable Limit, which was exceeded ! |
| ! 9999 ! ! |
| ! ! NOTE: If the report was not triggered by a limit ! |
| ! ! exceedance then this field has zeros. ! |
| !--------------!------------------------------------------------------! |
| ! REF ! N1 is used when VB1 is exceeded. ! |
| ! 9999 ! For all other exceedance N2 is used. ! |
| ! ! ECU (0.0 to 120.0% rpm) ! |
| ! ! N1 7C.1.346.01 Engine 1 ! |
| ! ! 7C.2.346.10 Engine 2 ! |
| ! ! ! |
| ! ! N2 7C.1.344.01 Engine 1 ! |
| ! ! 7C.2.344.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! TOL ! - Time Over Limit for EGT Exceedance or ! |
| ! 999 ! - Time from SAV = Open to N2 = N2trigger ! |
| ! ! DMU (Time in seconds) ! |
| ! ! Engine1 7C.1.270.01.15 = 1 SAV open ! |
| ! ! Engine2 7C.2.270.10.15 = 1 ! |
| !--------------!------------------------------------------------------! |
| ! TTP ! Time to Peak ! |
| ! 999 ! (Time to maximum of exceeded value) ! |
| ! ! NOTE: If the report was not triggered by a limit ! |
| ! ! exceedance then this field has zeros. ! |
| !--------------!------------------------------------------------------! |
| ! REASON ! Reason for Exceedance ! |
| ! XXXXXXXXXX ! DMU ! |
| ! XXXXXXXXXX ! Up to 20 Characters ! |
| ! ! OIT Code: 4110, 4120 and 4130 ! |
| ! ! OIP Code: 4210, 4220 and 4230 ! |
| ! ! VB1 Code: 4310 ! |
| ! ! VB2 Code: 4320 ! |
| ! ! NOTE: If the report was not triggered by a limit ! |
| ! ! exceedance, this field contains blanks. ! |
| +---------------------------------------------------------------------+ |
(4) Engine Mechanical Advisory Report Data Field Description <07> (Engine Type CFMI with Advanced EVMU)
NOTE: Reports that are transmitted from the ACARS system do not have report lines without a line identifier.
| +---------------------------------------------------------------------+ |
| ! Value ! Content Description ! |
| !--------------!------------------------------------------------------! |
| ! ESN ! Engine Serial Number ! |
| ! 999999 ! (000000 to 999999) ! |
| ! ! ECU Engine 1 7C.1.046.01 digit 3, 2, 1 ! |
| ! ! 7C.1.047.01 digit 6, 5, 4 ! |
| ! ! Engine 2 7C.2.046.10 digit 3, 2, 1 ! |
| ! ! 7C.2.047.10 digit 6, 5, 4 ! |
| !--------------!------------------------------------------------------! |
| ! EHRS ! Engine Flight Hours ! |
| ! 99999 ! (00000 to 99999 hours) ! |
| ! ! DMU Engine 1 ! |
| ! ! Engine 2 ! |
| ! ! Remark: Time between "Main (LH and RH) Landing Gear! |
| ! ! Decompressed" and "Main (LH and RH) Landing! |
| ! ! Gear Compressed". The EHRS is set to zero ! |
| ! ! if a new ESN is recognized by the DMU. ! |
| ! ! It is be possible to set the EHRS via the ! |
| ! ! MCDU, e.g. if the DMU is changed on the a/c! |
| !--------------!------------------------------------------------------! |
| ! ERT ! Engine Running Time ! |
| ! 99999 ! (00000 to 65536 hours) ! |
| ! ! ECU 7C.1.050.01 Engine 1 ! |
| ! ! 7C.2.050.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! ECYC ! Engine Cycle ! |
| ! 99999 ! (00000 to 99999) ! |
| ! ! DMU Engine 1 ! |
| ! ! Engine 2 ! |
| ! ! Remark: Each time when flight phase 5 (climb) is ! |
| ! ! reached, the counter is incremented by one ! |
| ! ! The ECYC is set to zero if a new ESN is ! |
| ! ! recognized by the DMU. It is possible to ! |
| ! ! ECYC via the MCDU, if the DMU is changed on! |
| ! ! the a/c. ! |
| !--------------!------------------------------------------------------! |
| ! AP ! Auto Pilot Status ! |
| ! 99 ! Number of respective status (00 to G8) ! |
| ! ! FMGC 1 and 2 (FGC part) for Auto Pilot AP1 and AP2 ! |
| ! ! ! |
| ! ! Parameter for AP1 ! Parameter for AP2 ! ! |
| ! ! Report Line EC: ! Report Line EE: !Definition: ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! / ! / !No Mode ! |
| ! ! ! !Active ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.11 = 1 ! 01.2.275.00.11 = 1!RUNWAY Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.12 = 1 ! 01.2.275.00.12 = 1!NAV Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.13 = 1 ! 01.2.275.00.13 = 1!LOC CAPTURE ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.14 = 1 ! 01.2.275.00.14 = 1!LOC TRACK ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.15 = 1 ! 01.2.275.00.15 = 1!Roll GO ! |
| ! ! ! !AROUND Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.16 = 1 ! 01.2.275.00.16 = 1!HEADING Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.17 = 1 ! 01.2.275.00.17 = 1!TRACK Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.15 = 1 ! 01.2.274.00.15 = 1!PITCH T/O ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.16 = 1 ! 01.2.274.00.16 = 1!PITCH GA Mode! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.17 = 1 ! 01.2.274.00.17 = 1!V/S Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.18 = 1 ! 01.2.274.00.18 = 1!FPA Mode ! |
| ! ! -------------------!-------------------!-------------! |
| ! ! 01.1.274.00.19 = 1 ! 01.2.274.00.19 = 1!ALT Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.20 = 1 ! 01.2.274.00.20 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.19 = 1 ! 01.2.274.00.19 = 1!ALT ACQ ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.21 = 1 ! 01.2.274.00.21 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.20 = 1 ! 01.2.274.00.20 = 1!G/S TRACK ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.22 = 1 ! 01.2.274.00.22 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.21 = 1 ! 01.2.274.00.21 = 1!G/S CAPTURE ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.22 = 1 ! 01.2.274.00.22 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.23 = 1 ! 01.2.274.00.23 = 1!FINAL DES ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.24 = 1 ! 01.2.274.00.24 = 1!EXPED. Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.146.00.14 = 1 ! 01.2.146.00.14 = 1!LAND TRACK ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!CLB Mode ! |
| ! ! AND ! AND ! ! |
| ! ! ! ! ! ! ! |
| ! ! -------------- ! -------------- ! ! |
| ! ! 01.1.274.00.13 = 0 ! 01.2.274.00.13 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.14 = 0 ! 01.2.274.00.14 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.24 = 0 ! 01.2.274.00.24 = 0! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!DES Mode ! |
| ! ! AND ! AND ! ! |
| ! ! ! ! ! ! ! |
| ! ! -------------- ! -------------- ! ! |
| ! ! 01.1.274.00.13 = 0 ! 01.2.274.00.13 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.14 = 0 ! 01.2.274.00.14 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.24 = 0 ! 01.2.274.00.24 = 0! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!IM. CLIMB ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.13 = 1 ! 01.2.274.00.13 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!IM. DES Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.13 = 1 ! 01.2.274.00.13 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!OPEN CLB ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.14 = 1 ! 01.2.274.00.14 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!OPEN. DES ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.14 = 1 ! 01.2.274.00.14 = 1! ! |
| ! ! ---------------------------------------------------- ! |
| ! ! Auto Pilot Status DMU: ! |
| ! ! Auto Pilot AP1 printed in report line EC ! |
| ! ! Auto Pilot AP2 printed in report line EE ! |
| ! ! Combined Auto Pilot Modes ! |
| ! ! The longitudinal auto pilot mode (1 to G) shall ! |
| ! ! appear on the left position for the AP1 and AP2 print! |
| ! ! format. ! |
| ! ! The lateral auto pilot mode (1 to 8) shall appear on ! |
| ! ! the right position for the AP1 and AP2 print format. ! |
| ! ! In case of a combined auto pilot mode e.g. DES mode ! |
| ! ! and NAV mode are engaged simultaneously, the 'E3' ! |
| ! ! shall appear below AP1 and AP2. ! |
| ! ! XX Auto Pilot Modes: ! |
| ! ! !! ! |
| ! ! !!__Lateral Modes: 0 = NO MODE ! |
| ! ! ! 1 = HEADING ! |
| ! ! ! 2 = TRACK ! |
| ! ! ! 3 = NAV ! |
| ! ! ! 4 = LOC CAPTURE ! |
| ! ! ! 5 = LOCK TRACK ! |
| ! ! ! 6 = LAND TRACK ! |
| ! ! ! 7 = RUNWAY ! |
| ! ! ! 8 = ROLL GO AROUND ! |
| ! ! ! ! |
| ! ! !__Longitudinal Modes: 0 = NO MODE ! |
| ! ! 1 = PITCH G/A ! |
| ! ! 2 = PITCH TO ! |
| ! ! 3 = G/S TRACK ! |
| ! ! 4 = G/S CAPTURE ! |
| ! ! 5 = V/S ! |
| ! ! 6 = FPA ! |
| ! ! 7 = ALT ! |
| ! ! 8 = ALT ACQ ! |
| ! ! 9 = OPEN CLB ! |
| ! ! A = OPEN DES ! |
| ! ! B = IM CLB ! |
| ! ! C = IM DES ! |
| ! ! D = CLB ! |
| ! ! E = DES ! |
| ! ! F = FINAL DES ! |
| ! ! G = EXPEDITE ! |
| !--------------!------------------------------------------------------! |
| ! ECW1 ! Engine Control Word 1 ! |
| ! XXXXX ! XXXXX Bits HEX ! |
| ! ! !!!!!________14, 13, 12, 11 0..F ! |
| ! ! !!!!_________18, 17, 16, 15 0..F ! |
| ! ! !!!__________22, 21, 20, 19 0..F ! |
| ! ! !!___________26, 25, 24, 23 0..F ! |
| ! ! !____________ 29, 28, 27 0..F ! |
| ! ! Bit Label Parameter Description ! |
| ! ! 11 7C.X.272.XX.19 = 1 Auto Thrust Active ! |
| ! ! 12 7C.X.275.XX.20 = 1 VSV Position Fault ! |
| ! ! 13 SPARE ! |
| ! ! 14 SPARE ! |
| ! ! 15 7C.X.351.XX.29 = 1 Fuel Flow Measurement ! |
| ! ! Invalid ! |
| ! ! 16 7C.X.275.XX.15 = 1 N1/N2 Control Active ! |
| ! ! 17 7C.X.275.XX.26 = 1 Channel A Active ! |
| ! ! 18 7C.X.275.XX.27 = 1 Channel B Active ! |
| ! ! 19 SPARE ! |
| ! ! 20 SPARE ! |
| ! ! 21 SPARE ! |
| ! ! 22 SPARE ! |
| ! ! 23 SPARE ! |
| ! ! 24 SPARE ! |
| ! ! 25 SPARE ! |
| ! ! 26 SPARE ! |
| ! ! 27 SPARE ! |
| ! ! 28 SPARE ! |
| ! ! 29 SPARE ! |
| ! ! The 'X' for the System and SDI definition of the ! |
| ! ! engine parameters shall be as follows: ! |
| ! ! System SDI ! |
| ! ! Engine 1 1 01 ! |
| ! ! Engine 2 2 10 ! |
| !--------------!------------------------------------------------------! |
| ! E ! Exceedance Engine Position ! |
| ! 9 ! No. of engine where the exceedance occurs. ! |
| ! ! Remark: If the report was not triggered by a limit ! |
| ! ! exceedance then this field has zeros. ! |
| !--------------!------------------------------------------------------! |
| ! MAX ! Maximal Value of the Exceeded Parameter ! |
| ! 9999 ! Remark: If there is OIPL1.1 or OIPL1.2 exceedance ! |
| ! ! the minimal value is printed. If the ! |
| ! ! report was not triggered by a limit ! |
| ! ! exceedance this field has zeros. ! |
| !--------------!------------------------------------------------------! |
| ! LIM ! Programmable Limit, which was exceeded ! |
| ! 9999 ! ! |
| ! ! Remark: If the report was not triggered by a limit ! |
| ! ! exceedance then this field has zeros. ! |
| !--------------!------------------------------------------------------! |
| ! REF ! N1 is used when VB1 is exceeded. ! |
| ! 9999 ! For all other exceedance N2 is used. ! |
| ! ! ECU (0.0 to 120.0% rpm) ! |
| ! ! N1 7C.1.346.01 Engine 1 ! |
| ! ! 7C.2.346.10 Engine 2 ! |
| ! ! ! |
| ! ! N2 7C.1.344.01 Engine 1 ! |
| ! ! 7C.2.344.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! TOL ! Time Over Limit ! |
| ! 999 ! Observation time max 60 seconds ! |
| ! ! DMU ! |
| ! ! Remark: If the report was not triggered by a limit ! |
| ! ! exceedance, this field contains zeros. ! |
| !--------------!------------------------------------------------------! |
| ! TTP ! Time to Peak ! |
| ! 999 ! (Time to maximum of exceeded value) ! |
| ! ! Remark: If the report was not triggered by a limit ! |
| ! ! exceedance then this field has zeros. ! |
| !--------------!------------------------------------------------------! |
| ! REASON ! Reason for Exceedance ! |
| ! XXXXXXXXXX ! DMU ! |
| ! XXXXXXXXXX ! Up to 20 Characters ! |
| ! ! OIT Code: 4110, 4120 and 4130 ! |
| ! ! OIP Code: 4210, 4220 and 4230 ! |
| ! ! VB1 Code: 4310 ! |
| ! ! VB2 Code: 4320 ! |
| ! ! ! |
| ! ! NOTE: If the report was not triggered by a limit ! |
| ! ! exceedance, this field contains blanks. ! |
| +---------------------------------------------------------------------+ |
| ! N1 ! Selected N1 Actual ! |
| ! 9999 ! (0 to 120.0 %rpm) ! |
| ! ! ECU 7C.1.346.01 Engine 1 ! |
| ! ! 7C.2.346.10 Engine 2 ! |
| ! ! Remark: In the report line V3 and V4 the values ! |
| ! ! from the last stable descent shall be ! |
| ! ! printed. ! |
| ! ! In the report line V5 and V6 the values ! |
| ! ! from the last stable climb shall be ! |
| ! ! printed. ! |
| !--------------!------------------------------------------------------! |
| ! N2 ! Selected N2 Actual ! |
| ! 9999 ! (0 to 120.0 %rpm) ! |
| ! ! ECU 7C.1.344.01 Engine 1 ! |
| ! ! 7C.2.344.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! VN ! FAN Pick Up N1 Track Vibration ! |
| ! 99 ! (0.0 to 10.0) ! |
| ! ! If value is 10.0 then 99 shall be printed. ! |
| ! ! EVM 3D.1.227.01 Engine 1 ! |
| ! ! 3D.1.227.10 Engine 2 ! |
| ! ! Remark: In report line V3 and V4 the values from ! |
| ! ! the last stable descent shall be ! |
| ! ! printed. ! |
| ! ! In report line V5 and V6 the values from ! |
| ! ! the last stable climb shall be printed. ! |
| !--------------!------------------------------------------------------! |
| ! VC ! FAN Pick Up N2 Track Vibration ! |
| ! 99 ! (0.0 to 4.0) ! |
| ! ! EVM 3D.1.230.01 Engine 1 ! |
| ! ! 3D.1.230.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! VH ! TRF Pick Up N2 Track Vibration ! |
| ! 99 ! (0.0 to 4.0) ! |
| ! ! EVM 3D.1.230.11 Engine 1 ! |
| ! ! 3D.1.230.00 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! VL ! TRF Pick Up N1 Vibration ! |
| ! 99 ! (0.0 to 10.0) ! |
| ! ! If value is 10.0 then 99 shall be printed. ! |
| ! ! EVM 3D.1.227.11 Engine 1 ! |
| ! ! 3D.1.227.00 Engine 2 ! |
| ! ! Remark: In report line V3 and V4 the values from ! |
| ! ! the last stable descent are printed. ! |
| ! ! In report line V5 and V6 the values from ! |
| ! ! the last stable climb are printed. ! |
| !--------------!------------------------------------------------------! |
| ! PHA ! FAN Pick Up Phase Angle ! |
| ! 999 ! (0 to 360 deg) ! |
| ! ! EVM 3D.1.226.01 Engine 1 ! |
| ! ! 3D.1.226.10 Engine 2 ! |
| ! ! Remark: In report line V3 and V4 the values from ! |
| ! ! the last stable descent are printed. ! |
| ! ! In report line V5 and V6 the values from ! |
| ! ! the last stable climb are printed . ! |
| !--------------!------------------------------------------------------! |
| ! PHT ! TRF Pick Up Phase Angle ! |
| ! 999 ! (0 to 360 deg) ! |
| ! ! EVM 3D.1.226.11 Engine 1 ! |
| ! ! 3D.1.226.00 Engine 2 ! |
| ! ! Remark: In report line V3 and V4 the values from ! |
| ! ! the last stable descent are printed. ! |
| ! ! In report line V5 and V6 the values from ! |
| ! ! the last stable climb are printed. ! |
| !--------------!------------------------------------------------------! |
| ! EVM ! Engine Vibration Status Word ! |
| ! XXXXX ! EVM 3D.1.035.01 Engine 1 ! |
| ! ! 3D.1.035.10 Engine 2 ! |
| ! ! XXXXX Bits HEX ! |
| ! ! !!!!!________14, 13, 12, 11 0..F ! |
| ! ! !!!!_________18, 17, 16, 15 0..F ! |
| ! ! !!!__________22, 21, 20, 19 0..F ! |
| ! ! !!___________26, 25, 24, 23 0..F ! |
| ! ! !____________ 29, 28, 27 0..F ! |
| !--------------!------------------------------------------------------! |
| ! OIT ! Engine Oil Temperature ! |
| ! X99 ! (-60 to 250 C) ! |
| ! ! Negative values are indicated by '-' on the first ! |
| ! ! position. Otherwise the firt position is used for ! |
| ! ! the value. ! |
| ! ! FWC 26.1.316.01 Engine 1 ! |
| ! ! 26.2.316.01 ! |
| ! ! 26.1.316.10 Engine 2 ! |
| ! ! 26.2.316.10 ! |
| !--------------!------------------------------------------------------! |
| ! OIP ! Engine Oil Pressure ! |
| ! 999 ! (0 to 400 psia) ! |
| ! ! FWC 26.1.317.01 Engine 1 ! |
| ! ! 26.2.317.01 ! |
| ! ! 26.1.317.10 Engine 2 ! |
| ! ! 26.2.317.10 ! |
| +---------------------------------------------------------------------+ |
(5) Engine Mechanical Advisory Report Data Field Description <07> (Engine Type CFMI with Advanced EVMU)
NOTE: Reports that are transmitted from the ACARS system do not have report lines without a line identifier.
| +---------------------------------------------------------------------+ |
| ! Value ! Content Description ! |
| !--------------!------------------------------------------------------! |
| ! ESN ! Engine Serial Number ! |
| ! 999999 ! (000000 to 999999) ! |
| ! ! ECU Engine 1 7C.1.046.01 digit 3, 2, 1 ! |
| ! ! 7C.1.047.01 digit 6, 5, 4 ! |
| ! ! Engine 2 7C.2.046.10 digit 3, 2, 1 ! |
| ! ! 7C.2.047.10 digit 6, 5, 4 ! |
| !--------------!------------------------------------------------------! |
| ! EHRS ! Engine Flight Hours ! |
| ! 99999 ! (00000 to 99999 hours) ! |
| ! ! DMU Engine 1 ! |
| ! ! Engine 2 ! |
| ! ! Remark: Time between "Main (LH and RH) Landing Gear! |
| ! ! Decompressed" and "Main (LH and RH) Landing! |
| ! ! Gear Compressed". The EHRS shall be set to ! |
| ! ! zero if a new ESN is recognized by the DMU.! |
| ! ! It shall be possible to set the EHRS via ! |
| ! ! the MCDU, e.g. if the DMU is changed on the! |
| ! ! a/c. ! |
| !--------------!------------------------------------------------------! |
| ! ERT ! Engine Running Time ! |
| ! 99999 ! (00000 to 65536 hours) ! |
| ! ! ECU 7C.1.050.01 Engine 1 ! |
| ! ! 7C.2.050.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! ECYC ! Engine Cycle ! |
| ! 99999 ! (00000 to 99999) ! |
| ! ! DMU Engine 1 ! |
| ! ! Engine 2 ! |
| ! ! Remark: Each time when flight phase 5 (climb) is ! |
| ! ! reached, the counter shall be incremented ! |
| ! ! by one. The ECYC is set to zero if a new ! |
| ! ! ESN is recognized by the DMU. It shall be ! |
| ! ! possible to set ECYC via the MCDU, if the ! |
| ! ! DMU is changed on the a/c. ! |
| !--------------!------------------------------------------------------! |
| ! AP ! Auto Pilot Status ! |
| ! 99 ! Number of respective status (00 to G8) ! |
| ! ! FMGC 1 and 2 (FGC part) for Auto Pilot AP1 and AP2 ! |
| ! ! ! |
| ! ! Parameter for AP1 ! Parameter for AP2 ! ! |
| ! ! Report Line EC: ! Report Line EE: !Definition: ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! / ! / !No Mode ! |
| ! ! ! !Active ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.11 = 1 ! 01.2.275.00.11 = 1!RUNWAY Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.12 = 1 ! 01.2.275.00.12 = 1!NAV Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.13 = 1 ! 01.2.275.00.13 = 1!LOC CAPTURE ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.14 = 1 ! 01.2.275.00.14 = 1!LOC TRACK ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.15 = 1 ! 01.2.275.00.15 = 1!Roll GO ! |
| ! ! ! !AROUND Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.16 = 1 ! 01.2.275.00.16 = 1!HEADING Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.17 = 1 ! 01.2.275.00.17 = 1!TRACK Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.15 = 1 ! 01.2.274.00.15 = 1!PITCH T/O ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.16 = 1 ! 01.2.274.00.16 = 1!PITCH GA Mode! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.17 = 1 ! 01.2.274.00.17 = 1!V/S Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.18 = 1 ! 01.2.274.00.18 = 1!FPA Mode ! |
| ! ! -------------------!-------------------!-------------! |
| ! ! 01.1.274.00.19 = 1 ! 01.2.274.00.19 = 1!ALT Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.20 = 1 ! 01.2.274.00.20 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.19 = 1 ! 01.2.274.00.19 = 1!ALT ACQ ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.21 = 1 ! 01.2.274.00.21 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.20 = 1 ! 01.2.274.00.20 = 1!G/S TRACK ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.22 = 1 ! 01.2.274.00.22 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.21 = 1 ! 01.2.274.00.21 = 1!G/S CAPTURE ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.22 = 1 ! 01.2.274.00.22 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.23 = 1 ! 01.2.274.00.23 = 1!FINAL DES ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.24 = 1 ! 01.2.274.00.24 = 1!EXPED. Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.146.00.14 = 1 ! 01.2.146.00.14 = 1!LAND TRACK ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!CLB Mode ! |
| ! ! AND ! AND ! ! |
| ! ! ! ! ! ! ! |
| ! ! -------------- ! -------------- ! ! |
| ! ! 01.1.274.00.13 = 0 ! 01.2.274.00.13 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.14 = 0 ! 01.2.274.00.14 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.24 = 0 ! 01.2.274.00.24 = 0! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!DES Mode ! |
| ! ! AND ! AND ! ! |
| ! ! ! ! ! ! ! |
| ! ! -------------- ! -------------- ! ! |
| ! ! 01.1.274.00.13 = 0 ! 01.2.274.00.13 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.14 = 0 ! 01.2.274.00.14 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.24 = 0 ! 01.2.274.00.24 = 0! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!IM. CLIMB ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.13 = 1 ! 01.2.274.00.13 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!IM. DES Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.13 = 1 ! 01.2.274.00.13 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!OPEN CLB ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.14 = 1 ! 01.2.274.00.14 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!OPEN. DES ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.14 = 1 ! 01.2.274.00.14 = 1! ! |
| ! ! ---------------------------------------------------- ! |
| ! ! Auto Pilot Status DMU: ! |
| ! ! Auto Pilot AP1 printed in report line EC ! |
| ! ! Auto Pilot AP2 printed in report line EE ! |
| ! ! Combined Auto Pilot Modes ! |
| ! ! The longitudinal auto pilot mode (1 to G) shall ! |
| ! ! appear on the left position for the AP1 and AP2 print! |
| ! ! format. ! |
| ! ! The lateral auto pilot mode (1 to 8) shall appear on ! |
| ! ! the right position for the AP1 and AP2 print format. ! |
| ! ! In case of a combined auto pilot mode e.g. DES mode ! |
| ! ! and NAV mode are engaged simultaneously, the 'E3' ! |
| ! ! shall appear below AP1 and AP2. ! |
| ! ! XX Auto Pilot Modes: ! |
| ! ! !! ! |
| ! ! !!__Lateral Modes: 0 = NO MODE ! |
| ! ! ! 1 = HEADING ! |
| ! ! ! 2 = TRACK ! |
| ! ! ! 3 = NAV ! |
| ! ! ! 4 = LOC CAPTURE ! |
| ! ! ! 5 = LOCK TRACK ! |
| ! ! ! 6 = LAND TRACK ! |
| ! ! ! 7 = RUNWAY ! |
| ! ! ! 8 = ROLL GO AROUND ! |
| ! ! ! ! |
| ! ! !__Longitudinal Modes: 0 = NO MODE ! |
| ! ! 1 = PITCH G/A ! |
| ! ! 2 = PITCH TO ! |
| ! ! 3 = G/S TRACK ! |
| ! ! 4 = G/S CAPTURE ! |
| ! ! 5 = V/S ! |
| ! ! 6 = FPA ! |
| ! ! 7 = ALT ! |
| ! ! 8 = ALT ACQ ! |
| ! ! 9 = OPEN CLB ! |
| ! ! A = OPEN DES ! |
| ! ! B = IM CLB ! |
| ! ! C = IM DES ! |
| ! ! D = CLB ! |
| ! ! E = DES ! |
| ! ! F = FINAL DES ! |
| ! ! G = EXPEDITE ! |
| !--------------!------------------------------------------------------! |
| ! ECW1 ! Engine Control Word 1 ! |
| ! XXXXX ! XXXXX Bits HEX ! |
| ! ! !!!!!________14, 13, 12, 11 0..F ! |
| ! ! !!!!_________18, 17, 16, 15 0..F ! |
| ! ! !!!__________22, 21, 20, 19 0..F ! |
| ! ! !!___________26, 25, 24, 23 0..F ! |
| ! ! !____________ 29, 28, 27 0..F ! |
| ! ! Bit Label Parameter Description ! |
| ! ! 11 7C.X.272.XX.19 = 1 Auto Thrust Active ! |
| ! ! 12 7C.X.275.XX.20 = 1 VSV Position Fault ! |
| ! ! 13 SPARE ! |
| ! ! 14 SPARE ! |
| ! ! 15 7C.X.351.XX.29 = 1 Fuel Flow Measurement ! |
| ! ! Invalid ! |
| ! ! 16 7C.X.275.XX.15 = 1 N1/N2 Control Active ! |
| ! ! 17 7C.X.275.XX.26 = 1 Channel A Active ! |
| ! ! 18 7C.X.275.XX.27 = 1 Channel B Active ! |
| ! ! 19 SPARE ! |
| ! ! 20 SPARE ! |
| ! ! 21 SPARE ! |
| ! ! 22 SPARE ! |
| ! ! 23 SPARE ! |
| ! ! 24 SPARE ! |
| ! ! 25 SPARE ! |
| ! ! 26 SPARE ! |
| ! ! 27 SPARE ! |
| ! ! 28 SPARE ! |
| ! ! 29 SPARE ! |
| ! ! The 'X' for the System and SDI definition of the ! |
| ! ! engine parameters shall be as follows: ! |
| ! ! System SDI ! |
| ! ! Engine 1 1 01 ! |
| ! ! Engine 2 2 10 ! |
| !--------------!------------------------------------------------------! |
| ! E ! Exeedance Engine Position ! |
| ! 9 ! No. of engine where the exceedance occurs. ! |
| ! ! Remark: If the report was not triggered by a limit ! |
| ! ! exceedance then this field has zeros. ! |
| !--------------!------------------------------------------------------! |
| ! MAX ! Maximal Value of the Exceeded Parameter ! |
| ! 9999 ! Remark: If there is OIPL1.1 or OIPL1.2 exceedance ! |
| ! ! the minimal value is printed. If the ! |
| ! ! report was not triggered by a limit ! |
| ! ! exceedance this field has zeros. ! |
| !--------------!------------------------------------------------------! |
| ! LIM ! Programmable Limit, which was exceeded ! |
| ! 9999 ! ! |
| ! ! Remark: If the report was not triggered by a limit ! |
| ! ! exceedance then this field has zeros. ! |
| !--------------!------------------------------------------------------! |
| ! REF ! N1 is used when VB1 is exceeded. ! |
| ! 9999 ! For all other exceedance N2 is used. ! |
| ! ! ECU (0.0 to 120.0% rpm) ! |
| ! ! N1 7C.1.346.01 Engine 1 ! |
| ! ! 7C.2.346.10 Engine 2 ! |
| ! ! ! |
| ! ! N2 7C.1.344.01 Engine 1 ! |
| ! ! 7C.2.344.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! TOL ! Time Over Limit ! |
| ! 999 ! Observation time max 60 seconds ! |
| ! ! DMU ! |
| ! ! Remark: If the report was not triggered by a limit ! |
| ! ! exceedance, this field shal contain zeros. ! |
| !--------------!------------------------------------------------------! |
| ! TTP ! Time to Peak ! |
| ! 999 ! (Time to maximum of exceeded value) ! |
| ! ! Remark: If the report was not triggered by a limit ! |
| ! ! exceedance then this field has zeros. ! |
| !--------------!------------------------------------------------------! |
| ! N1 ! Selected N1 Actual ! |
| ! 9999 ! (0 to 120.0 %rpm) ! |
| ! ! ECU 7C.1.346.01 Engine 1 ! |
| ! ! 7C.2.346.10 Engine 2 ! |
| ! ! Remark: In the report line V3 and V4 the values ! |
| ! ! from the last stable descent shall be ! |
| ! ! printed. ! |
| ! ! In the report line V5 and V6 the values ! |
| ! ! from the last stable climb shall be ! |
| ! ! printed. ! |
| !--------------!------------------------------------------------------! |
| ! N2 ! Selected N2 Actual ! |
| ! 9999 ! (0 to 120.0 %rpm) ! |
| ! ! ECU 7C.1.344.01 Engine 1 ! |
| ! ! 7C.2.344.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! VN ! FAN Pick Up N1 Track Vibration ! |
| ! 99 ! (0.0 to 10.0) ! |
| ! ! If value is 10.0 then 99 shall be printed. ! |
| ! ! EVM 3D.1.227.01 Engine 1 ! |
| ! ! 3D.1.227.10 Engine 2 ! |
| ! ! Remark: In report line V3 and V4 the values from ! |
| ! ! the last stable descent shall be ! |
| ! ! printed. ! |
| ! ! In report line V5 and V6 the values from ! |
| ! ! the last stable climb shall be printed. ! |
| !--------------!------------------------------------------------------! |
| ! VC ! FAN Pick Up N2 Track Vibration ! |
| ! 99 ! (0.0 to 4.0) ! |
| ! ! EVM 3D.1.230.01 Engine 1 ! |
| ! ! 3D.1.230.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! VH ! TRF Pick Up N2 Track Vibration ! |
| ! 99 ! (0.0 to 4.0) ! |
| ! ! EVM 3D.1.230.11 Engine 1 ! |
| ! ! 3D.1.230.00 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! VL ! TRF Pick Up N1 Vibration ! |
| ! 99 ! (0.0 to 10.0) ! |
| ! ! If value is 10.0 then 99 shall be printed. ! |
| ! ! EVM 3D.1.227.11 Engine 1 ! |
| ! ! 3D.1.227.00 Engine 2 ! |
| ! ! Remark: In report line V3 and V4 the values frome ! |
| ! ! the last stable descent shall be ! |
| ! ! printed. ! |
| ! ! In report line V5 and V6 the values frome ! |
| ! ! the last stable climb shall be printed. ! |
| !--------------!------------------------------------------------------! |
| ! PHA ! FAN Pick Up Phase Angle ! |
| ! 999 ! (0 to 360 deg) ! |
| ! ! EVM 3D.1.226.01 Engine 1 ! |
| ! ! 3D.1.226.10 Engine 2 ! |
| ! ! Remark: In report line V3 and V4 the values frome ! |
| ! ! the last stable descent shall be ! |
| ! ! printed. ! |
| ! ! In report line V5 and V6 the values frome ! |
| ! ! the last stable climb shall be printed. ! |
| !--------------!------------------------------------------------------! |
| ! PHT ! TRF Pick Up Phase Angle ! |
| ! 999 ! (0 to 360 deg) ! |
| ! ! EVM 3D.1.226.11 Engine 1 ! |
| ! ! 3D.1.226.00 Engine 2 ! |
| ! ! Remark: In report line V3 and V4 the values frome ! |
| ! ! the last stable descent shall be ! |
| ! ! printed. ! |
| ! ! In report line V5 and V6 the values frome ! |
| ! ! the last stable climb shall be printed. ! |
| !--------------!------------------------------------------------------! |
| ! EVM ! Engine Vibration Status Word ! |
| ! XXXXX ! EVM 3D.1.035.01 Engine 1 ! |
| ! ! 3D.1.035.10 Engine 2 ! |
| ! ! XXXXX Bits HEX ! |
| ! ! !!!!!________14, 13, 12, 11 0..F ! |
| ! ! !!!!_________18, 17, 16, 15 0..F ! |
| ! ! !!!__________22, 21, 20, 19 0..F ! |
| ! ! !!___________26, 25, 24, 23 0..F ! |
| ! ! !____________ 29, 28, 27 0..F ! |
| !--------------!------------------------------------------------------! |
| ! OIT ! Engine Oil Temperature ! |
| ! X99 ! (-60 to 250 C) ! |
| ! ! Negative values are indicated by 'N' on the ! |
| ! ! first position. Otherwise the firt position are ! |
| ! ! used for the value. ! |
| ! ! FWC 26.1.316.01 Engine 1 ! |
| ! ! 26.2.316.01 ! |
| ! ! 26.1.316.10 Engine 2 ! |
| ! ! 26.2.316.10 ! |
| !--------------!------------------------------------------------------! |
| ! OIP ! Engine Oil Pressure ! |
| ! 999 ! (0 to 400 psia) ! |
| ! ! FWC 26.1.317.01 Engine 1 ! |
| ! ! 26.2.317.01 ! |
| ! ! 26.1.317.10 Engine 2 ! |
| ! ! 26.2.317.10 ! |
| !--------------!------------------------------------------------------! |
| ! REASON ! Reason for Exceedance ! |
| ! XXXXXXXXXX ! (Up to 20 characters) ! |
| ! XXXXXXXXXX ! OIT Code: 4110, 4120 and 4130 ! |
| ! ! OIP Code: 4210, 4220 and 4230 ! |
| ! ! VB1 Code: 4310 ! |
| ! ! VB2 Code: 4320 ! |
| ! ! Remark: If the report was not triggered by a limit ! |
| ! ! of exceedance, this field shall contain ! |
| ! ! blanks. ! |
| +---------------------------------------------------------------------+ |
(6) Engine Mechanical Advisory Report Data Field Description <07> (Engine Type CFMI with Advanced EVMU)
NOTE: Reports that are transmitted from the ACARS system do not have report lines without a line identifier.
NOTE: Only the parts of the ENGINE MECHANICAL ADVISORY REPORT <07> which are not included in the ENGINE CRUISE REPORT <01> are given in the subsequent table.
| +---------------------------------------------------------------------+ |
| ! Value ! Content Description ! |
| !--------------!------------------------------------------------------! |
| ! E ! Exceedance Engine Position ! |
| ! 9 ! DMU (No. of engine where the exceedance occurs or ! |
| ! ! in case of discrete trigger the related No. of ! |
| ! ! engine. ! |
| !--------------!------------------------------------------------------! |
| ! MAX ! Maximal Value of the Exceeded Parameter ! |
| ! X999 ! Depending of exceeded parameter. ! |
| ! ! Remark: If there is OIPL1.1 or OIPL1.2 exceedance ! |
| ! ! the minimal value is printed. If the report was not! |
| ! ! triggered by a limit exceedance but by a discrete ! |
| ! ! signal, the value is calculated indirect. ! |
| !--------------!------------------------------------------------------! |
| ! LIM ! Programmable Limit, which was exceeded ! |
| ! 9999 ! Depending of exceeded parameter. ! |
| ! ! Remark: If the report was not triggered by a limit ! |
| ! ! exceedance then this field has zeros. ! |
| !--------------!------------------------------------------------------! |
| ! REF ! N1 is used when VB1 is exceeded. ! |
| ! 9999 ! For all other exceedance N2 is used. ! |
| ! ! ECU (0.0 to 120.0% rpm) ! |
| ! ! N1 7C.1.346.01 Engine 1 ! |
| ! ! 7C.2.346.10 Engine 2 ! |
| ! ! ! |
| ! ! N2 7C.1.344.01 Engine 1 ! |
| ! ! 7C.2.344.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! TOL ! Time Over Limit ! |
| ! 999 ! Time at least 60 seconds. ! |
| ! ! DMU ! |
| ! ! Remark: If the report was not triggered by a limit ! |
| ! ! exceedance but by a discrete signal, the value is ! |
| ! ! calculated indirect. ! |
| !--------------!------------------------------------------------------! |
| ! TTP ! Time to Peak ! |
| ! 999 ! Time to maximum of exceeded value ! |
| ! ! Remark: If the report was not triggered by a limit ! |
| ! ! exceedance but by a discrete signal, the value ! |
| ! ! is calculated indirect. ! |
| +---------------------------------------------------------------------+ |
| ! REASON ! Reason for Exceedance ! |
| ! XXXXXXXXXX ! (Up to 20 characters) ! |
| ! XXXXXXXXXX ! OIT Code: 4110, 4120 and 4130 ! |
| ! ! OIP Code: 4210, 4220 and 4230 ! |
| ! ! VB1 Code: 4310 ! |
| ! ! VB2 Code: 4320 ! |
| ! ! ! |
| ! ! NOTE: If the report was not triggered by a limit ! |
| ! ! exceedance, this field contains blanks. ! |
| +---------------------------------------------------------------------+ |
(7) Engine Mechanical Advisory Report Data Field Description <07> (Engine Type CFMI with Advanced EVMU)
NOTE: Reports that are transmitted from the ACARS system do not have report lines without a line identifier.
NOTE: Only the parts of the ENGINE MECHANICAL ADVISORY REPORT <07> which are not included in the ENGINE CRUISE REPORT <01> are given in the subsequent table.
| +---------------------------------------------------------------------+ |
| ! Value ! Content Description ! |
| !--------------!------------------------------------------------------! |
| ! E ! Exceedance Engine Position ! |
| ! 9 ! DMU ! |
| ! ! No. of engine where the exceedance occurs ! |
| ! ! Remark: If the report was not triggered by a limit ! |
| ! ! exceedance then this field contains zeros. ! |
| !--------------!------------------------------------------------------! |
| ! MAX ! Maximal Value of the Exceeded Parameter ! |
| ! 9999 ! Depending of exceeded parameter. ! |
| ! ! Remark: If there is OIPL1.1 or OIPL1.2 exceedance ! |
| ! ! the minimal value is printed. If the report was not! |
| ! ! triggered by a limit exceedance, this field ! |
| ! ! contains zeros. ! |
| !--------------!------------------------------------------------------! |
| ! LIM ! Programmable Limit, which was exceeded ! |
| ! 9999 ! Depending of exceeded parameter. ! |
| ! ! Remark: If the report was not triggered by a limit ! |
| ! ! exceedance then this field contains zeros. ! |
| !--------------!------------------------------------------------------! |
| ! REF ! N1 is used when VB1 is exceeded. ! |
| ! 9999 ! For all other exceedance N2 is used. ! |
| ! ! ECU (0.0 to 120.0% rpm) ! |
| ! ! N1 7C.1.346.01 Engine 1 ! |
| ! ! 7C.2.346.10 Engine 2 ! |
| ! ! ! |
| ! ! N2 7C.1.344.01 Engine 1 ! |
| ! ! 7C.2.344.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! TOL ! Time Over Limit ! |
| ! 99 ! Time at least 60 seconds. ! |
| ! ! DMU ! |
| ! ! Remark: If the report was not triggered by a limit ! |
| ! ! exceedance, this field contains zeros. ! |
| !--------------!------------------------------------------------------! |
| ! TTP ! Time to Peak ! |
| ! 999 ! Time to maximum of exceeded value ! |
| ! ! Remark: If the report was not triggered by a limit ! |
| ! ! exceedance, this field contains zeros. ! |
| !--------------!------------------------------------------------------! |
| ! REASON ! Reason for Exceedance ! |
| ! XXXXXXXXXX ! (Up to 20 characters) ! |
| ! XXXXXXXXXX ! OIT Code: 4110, 4120 and 4130 ! |
| ! ! OIP Code: 4210, 4220 and 4230 ! |
| ! ! VB1 Code: 4310 ! |
| ! ! VB2 Code: 4320 ! |
| ! ! ! |
| ! ! NOTE: If the report was not triggered by a limit ! |
| ! ! exceedance, this field contains blanks. ! |
| +---------------------------------------------------------------------+ |
(8) Engine Mechanical Advisory Report Data Field Description <07> (Engine Type CFMI with Advanced EVMU)
NOTE: Reports that are transmitted from the ACARS system do not have report lines without a line identifier.
NOTE: Only the parts of the ENGINE MECHANICAL ADVISORY REPORT <07> which are not included in the ENGINE CRUISE REPORT <01> are given in the subsequent table.
| +---------------------------------------------------------------------+ |
| ! Value ! Content Description ! |
| !--------------!------------------------------------------------------! |
| ! E ! Exceedance Engine Position ! |
| ! 9 ! DMU ! |
| ! ! No. of engine where the exceedance occurs ! |
| ! ! Remark: If the report was not triggered by a limit ! |
| ! ! exceedance, this field contains zeros. ! |
| !--------------!------------------------------------------------------! |
| ! MAX ! Maximal Value of the Exceeded Parameter ! |
| ! 9999 ! Depending of exceeded parameter. ! |
| ! ! For ! |
| ! ! ! HEADER! 01! 02! 04! 05! 06! 07! 09! 10! 11 ! |
| ! ! ------!-------!---!---!---!---!---!---!---!---!---- ! |
| ! ! Report! ! ! ! ! ! ! X ! ! ! ! |
| ! ! ! |
| ! ! Remark: If there is OIPL1.1 or OIPL1.2 exceedance, ! |
| ! ! the minimal value is printed. If the report was not! |
| ! ! triggered by a limit exceedance, but by a discrete ! |
| ! ! signal, the value is calculated indirect. ! |
| !--------------!------------------------------------------------------! |
| ! LIM ! Programmable Limit, which was exceeded ! |
| ! 9999 ! Depending of exceeded parameter. ! |
| ! ! Remark: If the report was not triggered by a limit ! |
| ! ! exceedance then this field contains zeros. ! |
| !--------------!------------------------------------------------------! |
| ! REF ! N1 is used when VB1 is exceeded. ! |
| ! 9999 ! For all other exceedance N2 is used. ! |
| ! ! ECU (0.0 to 120.0% rpm) ! |
| ! ! N1 7C.1.346.01 Engine 1 ! |
| ! ! 7C.2.346.10 Engine 2 ! |
| ! ! ! |
| ! ! N2 7C.1.344.01 Engine 1 ! |
| ! ! 7C.2.344.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! TOL ! Time Over Limit ! |
| ! 999 ! Time minimum 60 seconds. ! |
| ! ! For ! |
| ! ! ! HEADER! 01! 02! 04! 05! 06! 07! 09! 10! 11 ! |
| ! ! ------!-------!---!---!---!---!---!---!---!---!---- ! |
| ! ! Report! ! ! ! ! ! ! X ! ! ! ! |
| ! ! ! |
| ! ! DMU ! |
| ! ! Remark: If the report was not triggered by a limit ! |
| ! ! exceedance, but by a discrete signal, the value is ! |
| ! ! calculated indirect. ! |
| !--------------!------------------------------------------------------! |
| ! TTP ! Time to Peak ! |
| ! 999 ! Time to maximum of exceeded value ! |
| ! ! For ! |
| ! ! ! HEADER! 01! 02! 04! 05! 06! 07! 09! 10! 11 ! |
| ! ! ------!-------!---!---!---!---!---!---!---!---!---- ! |
| ! ! Report! ! ! ! ! ! ! X ! ! ! ! |
| ! ! ! |
| ! ! Remark: If the report was not triggered by a limit ! |
| ! ! exceedance, the value is calculated indirect. ! |
| !--------------!------------------------------------------------------! |
| ! VB1 ! N1 Vibration ! |
| ! 999 ! (0.0 to 10.0) ! |
| ! ! For ! |
| ! ! ! HEADER! 01! 02! 04! 05! 06! 07! 09! 10! 11 ! |
| ! ! ------!-------!---!---!---!---!---!---!---!---!---- ! |
| ! ! Report! ! ! ! ! ! ! X ! ! ! ! |
| ! ! ! |
| ! ! EVM 3D.1.135.01 Engine 1 ! |
| ! ! 3D.1.135.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! VB2 ! N2 Vibration ! |
| ! 999 ! (0.0 to 10.0) ! |
| ! ! For ! |
| ! ! ! HEADER! 01! 02! 04! 05! 06! 07! 09! 10! 11 ! |
| ! ! ------!-------!---!---!---!---!---!---!---!---!---- ! |
| ! ! Report! ! ! ! ! ! ! X ! ! ! ! |
| ! ! ! |
| ! ! EVM 3D.1.136.01 Engine 1 ! |
| ! ! 3D.1.136.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! REASON ! Reason for Exceedance ! |
| ! XXXXXXXXXX ! Format: Up to 20 characters ! |
| ! XXXXXXXXXX ! OIT Code: 4110, 4120 and 4130 ! |
| ! ! OIP Code: 4210, 4220 and 4230 ! |
| ! ! VB1 Code: 4310 ! |
| ! ! VB2 Code: 4320 ! |
| ! ! Source: DMU ! |
| ! ! Remark: If the report was not triggered by a limit ! |
| ! ! exceedance, this field contains blanks. ! |
| +---------------------------------------------------------------------+ |
(9) Parameter Logic
| +---------------------------------------------------------------------+ |
| ! Param. ! Print Value (Standard Progr.) ! |
| !--------------!------------------------------------------------------! |
| ! ESN ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! EHRS ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! ERT ! Value at moment of trigger ! |
| !--------------! -----------------------------------------------------! |
| ! ECYC ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! AP ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! ECW1 ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! E ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! MAX ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! LIM ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! REF ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! TOL ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! TTP ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! EVM ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! N1 ! Snapshot at Y07.1 and Y07.2 sec. intervals ! |
| !--------------!------------------------------------------------------! |
| ! N2 ! Snapshot at Y07.1 and Y07.2 sec. intervals ! |
| !--------------!------------------------------------------------------! |
| ! VN ! Snapshot at Y07.1 and Y07.2 sec. intervals ! |
| !--------------!------------------------------------------------------! |
| ! VC ! Snapshot at Y07.1 and Y07.2 sec. intervals ! |
| !--------------!------------------------------------------------------! |
| ! VH ! Snapshot at Y07.1 and Y07.2 sec. intervals ! |
| !--------------!------------------------------------------------------! |
| ! VL ! Snapshot at Y07.1 and Y07.2 sec. intervals ! |
| !--------------!------------------------------------------------------! |
| ! PHA ! Snapshot at Y07.1 and Y07.2 sec. intervals ! |
| !--------------!------------------------------------------------------! |
| ! PHT ! Snapshot at Y07.1 and Y07.2 sec. intervals ! |
| !--------------!------------------------------------------------------! |
| ! OIT ! Snapshot at Y07.1 and Y07.2 sec. intervals ! |
| !--------------!------------------------------------------------------! |
| ! OIP ! Snapshot at Y07.1 and Y07.2 sec. intervals ! |
| +---------------------------------------------------------------------+ |
(10) Parameter Logic
| +---------------------------------------------------------------------+ |
| ! Param. ! Print Value (Standard Progr.) ! |
| !--------------!------------------------------------------------------! |
| ! ESN ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! EHRS ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! ERT ! Value at moment of trigger ! |
| !--------------! -----------------------------------------------------! |
| ! ECYC ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! AP ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! ECW1 ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! E ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! MAX ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! LIM ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! REF ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! TOL ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! TTP ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! EVM ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! N1 ! Snapshot at Y07.1 and Y07.2 sec. intervals ! |
| !--------------!------------------------------------------------------! |
| ! N2 ! Snapshot at Y07.1 and Y07.2 sec. intervals ! |
| !--------------!------------------------------------------------------! |
| ! VN ! Snapshot at Y07.1 and Y07.2 sec. intervals ! |
| !--------------!------------------------------------------------------! |
| ! VC ! Snapshot at Y07.1 and Y07.2 sec. intervals ! |
| !--------------!------------------------------------------------------! |
| ! VH ! Snapshot at Y07.1 and Y07.2 sec. intervals ! |
| !--------------!------------------------------------------------------! |
| ! VL ! Snapshot at Y07.1 and Y07.2 sec. intervals ! |
| !--------------!------------------------------------------------------! |
| ! PHA ! Snapshot at Y07.1 and Y07.2 sec. intervals ! |
| !--------------!------------------------------------------------------! |
| ! PHT ! Snapshot at Y07.1 and Y07.2 sec. intervals ! |
| !--------------!------------------------------------------------------! |
| ! OIT ! Snapshot at Y07.1 and Y07.2 sec. intervals ! |
| !--------------!------------------------------------------------------! |
| ! OIP ! Snapshot at Y07.1 and Y07.2 sec. intervals ! |
| +---------------------------------------------------------------------+ |
(11) Engine Mechanical Advisory Report Logic <07> (Engine Type CFMI with Advanced EVMU)
| +----------------------------------------------------------------------+ |
| !Code!Item ! !Progr.!Standard ! |
| ! No.!No. ! Description of Function Item !MCDU !Value or ! |
| ! ! ! !GSE !Table ! |
| !----!------!-----------------------------------------!------!---------! |
| ! !A ! Report Format ! ! ! |
| ! !B ! Parameter Table ! ! ! |
| ! !C ! First three lines of Report ! C ! Blank ! |
| ! !D ! Print-out Rules ! C ! 2 ! |
| ! !E ! Transfer to ACARS MU ! C ! No ! |
| ! !F ! Increment of the report counter if the ! C ! 1 ! |
| ! ! ! report was triggered by a code number ! ! ! |
| ! ! ! > 1000; 1=yes, 0=no ! ! ! |
| ! !G ! 'Y07.1' Pre-event print intervals in ! C ! 4 ! |
| ! ! ! seconds. ! ! ! |
| ! !H ! 'Y07.2' Post-event print intervals in ! C ! 5 ! |
| ! ! ! seconds. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !1000!1 ! Manual selection via MCDU ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !2000!2 ! Flight phase dependent manual ! ! ! |
| ! ! ! selection via remote print button ! ! ! |
| ! ! ! if programmed. ! ! ! |
| ! !2.1 ! Remote Print Button assignment. ! C ! not ! |
| !----!------!-----------------------------------------!------!---------! |
| !3000!3 ! Programmable Start Logic ! ! ! |
| ! !3.1 ! Trigger condition ! C ! not ! |
| !----!------!-----------------------------------------!------!---------! |
| !4110!4 ! OIT > OITL1 in all PH ! ! ! |
| !4120! ! OIT > OITL2 in all PH ! ! ! |
| !4130! ! OIT > OITL3 for 'Y07.3' min. in all PH ! ! ! |
| !4210! ! OIP < OIPL1.1 at N2L2.1 in PH 2, 3 and 9! ! ! |
| !4220! ! OIP < OIPL1.2 at N2L2.2 in PH 4 to 8 ! ! ! |
| !4230! ! OIP > OIPL2 in all PH ! ! ! |
| !4310! ! VB1 is above Advisory Level in all PH ! ! ! |
| ! ! ! Eng.1 param. 3D.1.035.01.11 ! ! ! |
| ! ! ! Eng.2 param. 3D.1.035.10.11 ! ! ! |
| !4320! ! VB2 is above Advisory Level in all PH ! ! ! |
| ! ! ! Eng.1 param. 3D.1.035.01.12 ! ! ! |
| ! ! ! Eng.2 param. 3D.1.035.10.12 ! ! ! |
| ! ! ! ! ! ! |
| ! !4.1.1 ! OITL1 limit in C ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.1.2 ! OITL2 limit in C (amber limit) ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.1.3 ! OITL3 limit in C ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.1.4 ! 'Y07.3' time limit in minutes ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.2.1 ! OIPL1.1 limit defined in the following ! A ! limit- ! |
| ! ! ! table: ! ! table ! |
| ! ! ! OIPL1.1 (psia) ! N2L2.1 (%rpm) ! ! ! |
| ! ! ! ________________!_______________ ! ! ! |
| ! ! ! 0 ! 0 ! ! ! |
| ! ! ! 0 ! 54 ! ! ! |
| ! ! ! 13 ! 55 ! ! ! |
| ! ! ! 13 ! 65 ! ! ! |
| ! ! ! 38 ! 105 ! ! ! |
| ! ! ! ! ! ! |
| ! !4.2.2 ! OIPL1.2 limit defined in the following ! A ! limit- ! |
| ! ! ! table: ! ! table ! |
| ! ! ! OIPL1.2 (psia) ! N2L2.2 (%rpm) ! ! ! |
| ! ! ! ________________!_______________ ! ! ! |
| ! ! ! 0 ! 0 ! ! ! |
| ! ! ! 0 ! 54 ! ! ! |
| ! ! ! 13 ! 55 ! ! ! |
| ! ! ! 13 ! 65 ! ! ! |
| ! ! ! 38 ! 105 ! ! ! |
| ! ! ! ! ! ! |
| ! !4.2.3 ! OIPL2 limit in psi ! C ! limit- ! |
| ! ! ! ! ! table ! |
| !----!------!-----------------------------------------!------!---------! |
| ! !5 ! Generation stops when exceedance param. ! ! ! |
| ! ! ! are again within their limits or 10 sets! ! ! |
| ! ! ! of post event data are generated. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !8100!8.1 ! ACARS MU uplink request with IMI 'REQ07'! ! ! |
| ! ! ! The report <07> is immediately generated! ! ! |
| ! ! ! and transmitted to the ACARS MU. ! ! ! |
| !----------------------------------------------------------------------! |
| ! A = Programmable by Airbus ! |
| ! C = Programmable by Customer ! |
| +----------------------------------------------------------------------+ |
(12) Engine Mechanical Advisory Report Logic <07> (Engine Type CFMI with EVMU)
| +----------------------------------------------------------------------+ |
| !Code!Item ! !Progr.!Standard ! |
| ! No.!No. ! Description of Function Item !MCDU !Value or ! |
| ! ! ! !/GSE !Table TXY! |
| !----!------!-----------------------------------------!------!---------! |
| ! !A ! Report Format ! ! ! |
| ! !B ! Parameter Table ! ! ! |
| ! !C ! First three lines of Report ! C ! Blank ! |
| ! !D ! Print-out Rules ! C ! See ! |
| ! ! ! ! ! separate! |
| ! ! ! ! ! list ! |
| ! !E ! Transfer to ACARS MU ! C ! See ! |
| ! ! ! ! ! separate! |
| ! ! ! ! ! list ! |
| ! !F ! Increment of the report counter if the ! C ! 1 ! |
| ! ! ! report was triggered by a code number ! ! ! |
| ! ! ! > 1000; 1=yes, 0=no ! ! ! |
| ! !G ! 'Y07.1' Pre-event intervals in ! C ! 4 ! |
| ! ! ! seconds. ! ! ! |
| ! ! ! 'Y07.1' shall be programmable in the ! ! ! |
| ! ! ! range of 1 to 5 ! ! ! |
| ! !H ! 'Y07.2' Post-event intervals in ! C ! 5 ! |
| ! ! ! seconds. ! ! ! |
| ! ! ! 'Y07.2' shall be programmable in the ! ! ! |
| ! ! ! range of 1 to 61 ! ! ! |
| ! !I ! Max. No. of reports per trigger engine ! C ! 10 ! |
| ! ! ! and flight leg. ! ! ! |
| ! !J ! Max. No. of reports per engine and ! C ! 50 ! |
| ! ! ! flight leg. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !1000!1 ! Manual selection via MCDU ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !2000!2 ! Flight phase dependent manual ! ! ! |
| ! ! ! selection via remote print button ! ! ! |
| ! ! ! if programmed. ! ! ! |
| ! !2.1 ! Remote Print Button assignment. ! C ! not ! |
| ! ! ! ! ! assigned! |
| !----!------!-----------------------------------------!------!---------! |
| !3000!3 ! Programmable Start Logic ! ! ! |
| ! !3.1 ! Trigger condition ! C ! not ! |
| ! ! ! ! ! progr. ! |
| !----!------!-----------------------------------------!------!---------! |
| !4110!4 ! OIT > OITL1 in all flight phases ! ! ! |
| !4120! ! OIT > OITL2 in all flight phases ! ! ! |
| !4130! ! OIT > OITL3 for 'Y07.3' min. in all ! ! ! |
| ! ! ! flight phases ! ! ! |
| !4210! ! OIP < OIPL1.1 at N2L2.1 in flight phases! ! ! |
| ! ! ! 2, 3 and 9 ! ! ! |
| !4220! ! OIP < OIPL1.2 at N2L2.2 in flight phases! ! ! |
| ! ! ! 4 thru 8 ! ! ! |
| !4230! ! OIP > OIPL2 in all flight phases ! ! ! |
| !4310! ! VB1 is above Advisory Level in all ! ! ! |
| ! ! ! flight phases ! ! ! |
| ! ! ! EVMU 3D.1.035.01.11 Engine 1 ! ! ! |
| ! ! ! 3D.1.035.10.11 Engine 2 ! ! ! |
| !4320! ! VB2 is above Advisory Level in all ! ! ! |
| ! ! ! flight phases ! ! ! |
| ! ! ! EVMU 3D.1.035.01.12 Engine 1 ! ! ! |
| ! ! ! 3D.1.035.10.12 Engine 2 ! ! ! |
| ! ! ! ! ! ! |
| ! !4.1.1 ! OITL1 limit in C ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.1.2 ! OITL2 limit in C (amber limit) ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.1.3 ! OITL3 limit in C ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.1.4 ! 'Y07.3' time limit in minutes ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.2.1 ! OIPL1.1 limit defined in the following ! A ! limit- ! |
| ! ! ! table: ! ! table ! |
| ! ! ! (linear interpolation and linear ! ! ! |
| ! ! ! extrapolation below 50% and above 100%)! ! ! |
| ! ! ! OIPL1.1 (psia) ! N2L2.1 (%rpm) ! ! ! |
| ! ! ! ________________!_______________ ! ! ! |
| ! ! ! 0 ! 0 ! ! ! |
| ! ! ! 0 ! 54 ! ! ! |
| ! ! ! 13 ! 55 ! ! ! |
| ! ! ! 13 ! 65 ! ! ! |
| ! ! ! 38 ! 105 ! ! ! |
| ! ! ! ! ! ! |
| ! !4.2.2 ! OIPL1.2 defined in the following table: ! A ! limit- ! |
| ! ! ! (linear interpolation and linear ! ! table ! |
| ! ! ! extrapolation below 50% and above 100%)! ! ! |
| ! ! ! OIPL1.2 (psia) ! N2L2.2 (%rpm) ! ! ! |
| ! ! ! ________________!_______________ ! ! ! |
| ! ! ! 0 ! 0 ! ! ! |
| ! ! ! 0 ! 54 ! ! ! |
| ! ! ! 13 ! 55 ! ! ! |
| ! ! ! 13 ! 65 ! ! ! |
| ! ! ! 38 ! 105 ! ! ! |
| ! ! ! ! ! ! |
| ! !4.2.3 ! OIPL2 limit in psi ! C ! limit- ! |
| ! ! ! ! ! table ! |
| !----!------!-----------------------------------------!------!---------! |
| ! !5 ! Generation stops when exceedance param. ! ! ! |
| ! ! ! are again within their limits or 10 sets! ! ! |
| ! ! ! of post event data are generated. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !8100!8.1 ! ACARS MU uplink request with IMI 'REQ07'! ! ! |
| ! ! ! The report <07> is immediately generated! ! ! |
| ! ! ! and transmitted to the ACARS MU. ! ! ! |
| !----------------------------------------------------------------------! |
| ! A = Programmable by Airbus ! |
| ! C = Programmable by Customer ! |
| +----------------------------------------------------------------------+ |
(13) Engine Mechanical Advisory Report Logic <07> (Engine Type CFMI with EVMU)
| +----------------------------------------------------------------------+ |
| !Code!Item ! !Progr.!Standard ! |
| ! No.!No. ! Description of Function Item !MCDU !Value or ! |
| ! ! ! !/GSE !Table TXY! |
| !----!------!-----------------------------------------!------!---------! |
| ! !A ! Report Format ! ! ! |
| ! !B ! Parameter Table ! ! ! |
| ! !C ! First three lines of Report ! C ! Blank ! |
| ! !D ! Print-out Rules ! C ! See ! |
| ! ! ! ! ! separate! |
| ! ! ! ! ! list ! |
| ! !E ! Transfer to ACARS MU ! C ! See ! |
| ! ! ! ! ! separate! |
| ! ! ! ! ! list ! |
| ! !F ! Increment of the report counter if the ! C ! 1 ! |
| ! ! ! report was triggered by a code number ! ! ! |
| ! ! ! > 1000; 1=yes, 0=no ! ! ! |
| ! !G ! 'Y07.1' Pre-event intervals in ! C ! 4 ! |
| ! ! ! seconds. ! ! ! |
| ! ! ! 'Y07.1' shall be programmable in the ! ! ! |
| ! ! ! range of 1 to 5 ! ! ! |
| ! !H ! 'Y07.2' Post-event intervals in ! C ! 5 ! |
| ! ! ! seconds. ! ! ! |
| ! ! ! 'Y07.2' shall be programmable in the ! ! ! |
| ! ! ! range of 1 to 61 ! ! ! |
| ! !I ! Max. No. of reports per trigger engine ! C ! 10 ! |
| ! ! ! and flight leg. ! ! ! |
| ! !J ! Max. No. of reports per engine and ! C ! 50 ! |
| ! ! ! flight leg. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !1000!1 ! Manual selection via MCDU ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !2000!2 ! Flight phase dependent manual ! ! ! |
| ! ! ! selection via remote print button ! ! ! |
| ! ! ! if programmed. ! ! ! |
| ! !2.1 ! Remote Print Button assignment. ! C ! not ! |
| ! ! ! ! ! assigned! |
| !----!------!-----------------------------------------!------!---------! |
| !3000!3 ! Programmable Start Logic ! ! ! |
| ! !3.1 ! Trigger condition ! C ! not ! |
| ! ! ! ! ! progr. ! |
| !----!------!-----------------------------------------!------!---------! |
| !4110!4 ! OIT > OITL1 in all flight phases ! ! ! |
| !4120! ! OIT > OITL2 in all flight phases ! ! ! |
| !4130! ! OIT > OITL3 for 'Y07.3' min. in all ! ! ! |
| ! ! ! flight phases ! ! ! |
| !4210! ! OIP > OIPL1.1 at N2L2.1 in flight phases! ! ! |
| ! ! ! 2, 3 and 9 ! ! ! |
| !4220! ! OIP > OIPL1.2 at N2L2.2 in flight phases! ! ! |
| ! ! ! 4 to 8 ! ! ! |
| !4230! ! OIP > OIPL2 in all flight phases ! ! ! |
| !4310! ! VB1 is above Advisory Level in all ! ! ! |
| ! ! ! flight phases ! ! ! |
| ! ! ! EVMU 3D.1.035.01.11 Engine 1 ! ! ! |
| ! ! ! 3D.1.035.10.11 Engine 2 ! ! ! |
| !4320! ! VB2 is above Advisory Level in all ! ! ! |
| ! ! ! flight phases ! ! ! |
| ! ! ! EVMU 3D.1.035.01.12 Engine 1 ! ! ! |
| ! ! ! 3D.1.035.10.12 Engine 2 ! ! ! |
| ! ! ! ! ! ! |
| ! !4.1.1 ! OITL1 limit in Degrees C ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.1.2 ! OITL2 limit in Degrees C (amber limit) ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.1.3 ! OITL3 limit in Degrees C ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.1.4 ! 'Y07.3' time limit in minutes ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.2.1 ! OIPL1.1 limit defined in the following ! A ! limit- ! |
| ! ! ! table: ! ! table ! |
| ! ! ! (linear interpolation and linear ! ! ! |
| ! ! ! extrapolation below 50% and above 100%)! ! ! |
| ! ! ! OIPL1.1 (psia) ! N2L2.1 (%rpm) ! ! ! |
| ! ! ! ________________!_______________ ! ! ! |
| ! ! ! 0 ! 0 ! ! ! |
| ! ! ! 0 ! 54 ! ! ! |
| ! ! ! 13 ! 55 ! ! ! |
| ! ! ! 13 ! 65 ! ! ! |
| ! ! ! 38 ! 105 ! ! ! |
| ! ! ! ! ! ! |
| ! !4.2.2 ! OIPL1.2 defined in the following table: ! A ! limit- ! |
| ! ! ! (linear interpolation and linear ! ! table ! |
| ! ! ! extrapolation below 50% and above 100%)! ! ! |
| ! ! ! OIPL1.2 (psia) ! N2L2.2 (%rpm) ! ! ! |
| ! ! ! ________________!_______________ ! ! ! |
| ! ! ! 0 ! 0 ! ! ! |
| ! ! ! 0 ! 54 ! ! ! |
| ! ! ! 13 ! 55 ! ! ! |
| ! ! ! 13 ! 65 ! ! ! |
| ! ! ! 38 ! 105 ! ! ! |
| ! ! ! ! ! ! |
| ! !4.2.3 ! OIPL2 limit in psi ! C ! limit- ! |
| ! ! ! ! ! table ! |
| !----!------!-----------------------------------------!------!---------! |
| ! !5 ! Generation stops when exceedance param. ! ! ! |
| ! ! ! are again within their limits or 10 sets! ! ! |
| ! ! ! of post event data are generated. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !8100!8.1 ! ACARS MU uplink request with IMI 'REQ07'! ! ! |
| ! ! ! The report <07> is immediately generated! ! ! |
| ! ! ! and transmitted to the ACARS MU. ! ! ! |
| !----------------------------------------------------------------------! |
| ! A = Programmable by Airbus ! |
| ! C = Programmable by Customer ! |
| +----------------------------------------------------------------------+ |
(14) Engine Mechanical Advisory Report Logic <07> (Engine Type CFMI with EVMU)
| +----------------------------------------------------------------------+ |
| !Code!Item ! !Progr.!Standard ! |
| ! No.!No. ! Description of Function Item !------!Value or ! |
| ! ! ! !MCDU !Table TXY! |
| ! ! ! !GSE ! ! |
| !----!------!-----------------------------------------!------!---------! |
| ! !A ! Report Format ! ! ! |
| ! !A.1 ! "R007RLID" Report Layout Identifier ! ! 01 ! |
| ! ! ! (for ACARS header) ! ! ! |
| ! !A.2 ! "R007RLIS" Report Layout Issue ! ! 01 ! |
| ! ! ! (for ACARS header) ! ! ! |
| ! !B ! Parameter Table ! ! ! |
| ! !C ! First three lines of Report ! C ! Blank ! |
| ! !D ! Print-out Rules ! C ! See ! |
| ! ! ! ! ! separate! |
| ! ! ! ! ! list ! |
| ! !E ! Transfer to ACARS MU ! C ! See ! |
| ! ! ! ! ! separate! |
| ! ! ! ! ! list ! |
| ! !F ! Increment of the report counter if the ! C ! 1 ! |
| ! ! ! report was triggered by a code number ! ! ! |
| ! ! ! > 1000; 1=yes, 0=no ! ! ! |
| ! !G ! "Y07.1" Pre-event intervals in ! C ! 4 ! |
| ! ! ! seconds. ! ! ! |
| ! ! ! "Y07.1" is programmable in the range ! ! ! |
| ! ! ! of 1 to 5 ! ! ! |
| ! !H ! "Y07.2" Post-event intervals in ! C ! 5 ! |
| ! ! ! seconds. ! ! ! |
| ! ! ! "Y07.2" is programmable in the range ! ! ! |
| ! ! ! of 1 to 61 ! ! ! |
| ! !I ! Max. No. of reports per trigger engine ! C ! 10 ! |
| ! ! ! and flight leg. ! ! ! |
| ! !J ! Max. No. of reports per engine and ! C ! 50 ! |
| ! ! ! flight leg. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !1000!1 ! Manual selection through MCDU ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !2000!2 ! Flight phase dependent manual ! ! ! |
| ! ! ! selection through remote print button ! ! ! |
| ! ! ! if programmed. ! ! ! |
| ! !2.1 ! Remote Print Button assignment. ! C ! not ! |
| ! ! ! ! ! assigned! |
| !----!------!-----------------------------------------!------!---------! |
| !3000!3 ! Programmable Start Logic ! ! ! |
| ! !3.1 ! Trigger condition ! C ! not ! |
| ! ! ! ! ! progr. ! |
| !----!------!-----------------------------------------!------!---------! |
| !4110!4 ! OIT > OITL1 in all flight phases ! ! ! |
| !4120! ! OIT > OITL2 in all flight phases ! ! ! |
| !4130! ! OIT > OITL3 for "Y07.3" min. in all ! ! ! |
| ! ! ! flight phases ! ! ! |
| !4210! ! OIP > OIPL1.1 at N2L2.1 in flight phases! ! ! |
| ! ! ! 2, 3 and 9 ! ! ! |
| !4220! ! OIP > OIPL1.2 at N2L2.2 in flight phases! ! ! |
| ! ! ! 4 to 8 ! ! ! |
| !4230! ! OIP > OIPL2 in all flight phases ! ! ! |
| !4310! ! VB1 is above Advisory Level in all ! ! ! |
| ! ! ! flight phases ! ! ! |
| ! ! ! EVMU 3D.1.035.01.11 Engine 1 ! ! ! |
| ! ! ! 3D.1.035.10.11 Engine 2 ! ! ! |
| ! ! ! Remark: Refer also to item 4.3 ! ! ! |
| !4320! ! VB2 is above Advisory Level in all ! ! ! |
| ! ! ! flight phases ! ! ! |
| ! ! ! EVMU 3D.1.035.01.12 Engine 1 ! ! ! |
| ! ! ! 3D.1.035.10.12 Engine 2 ! ! ! |
| ! ! ! Remark: Refer also to item 4.4 ! ! ! |
| ! ! ! ! ! ! |
| ! !4.1.1 ! OITL1 limit in Degrees C ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.1.2 ! OITL2 limit in Degrees C (amber limit) ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.1.3 ! OITL3 limit in Degrees C ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.1.4 ! 'Y07.3' time limit in minutes ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.2.1 ! OIPL1.1 limit defined in the following ! A ! limit- ! |
| ! ! ! table: ! ! table ! |
| ! ! ! (linear interpolation and linear ! ! ! |
| ! ! ! extrapolation below 50% and above 100%)! ! ! |
| ! ! ! OIPL1.1 (psia) ! N2L2.1 (%rpm) ! ! ! |
| ! ! ! ________________!_______________ ! ! ! |
| ! ! ! 0 ! 0 ! ! ! |
| ! ! ! 0 ! 54 ! ! ! |
| ! ! ! 13 ! 55 ! ! ! |
| ! ! ! 13 ! 65 ! ! ! |
| ! ! ! 38 ! 105 ! ! ! |
| ! ! ! ! ! ! |
| ! !4.2.2 ! OIPL1.2 defined in the following table: ! A ! limit- ! |
| ! ! ! (linear interpolation and linear ! ! table ! |
| ! ! ! extrapolation below 50% and above 100%)! ! ! |
| ! ! ! OIPL1.2 (psia) ! N2L2.2 (%rpm) ! ! ! |
| ! ! ! ________________!_______________ ! ! ! |
| ! ! ! 0 ! 0 ! ! ! |
| ! ! ! 0 ! 54 ! ! ! |
| ! ! ! 13 ! 55 ! ! ! |
| ! ! ! 13 ! 65 ! ! ! |
| ! ! ! 38 ! 105 ! ! ! |
| ! ! ! ! ! ! |
| ! !4.2.3 ! OIPL2 limit in psia ! C ! limit- ! |
| ! ! ! ! ! table ! |
| !----!------!-----------------------------------------!------!---------! |
| ! !4.3 ! For code 4310 the value for Max and TTP ! ! ! |
| ! ! ! is calculated indirectly by observing ! ! ! |
| ! ! ! the value for VB1: ! ! ! |
| ! ! ! EVM 3D.1.135.01 Engine 1 ! ! ! |
| ! ! ! 3D.1.135.10 Engine 2 ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! while the discrete for code 4310 of the ! ! ! |
| ! ! ! related engine is set to "1", the DMU ! ! ! |
| ! ! ! searches for the maximum of VB1 of the ! ! ! |
| ! ! ! related engine. The DMU also counts the ! ! ! |
| ! ! ! seconds while the above named discrete ! ! ! |
| ! ! ! is set to "1" and the Maximum is not ! ! ! |
| ! ! ! reached and use the counted seconds for ! ! ! |
| ! ! ! TTP. ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! The value for TOL is the time while the ! ! ! |
| ! ! ! discrete for code 4310 is set to "1". ! ! ! |
| ! ! ! If the discrete is set to "1" for ! ! ! |
| ! ! ! more than 60 seconds, the calculation ! ! ! |
| ! ! ! of the values TOL, TTP and MAX stops. ! ! ! |
| ! ! ! ! ! ! |
| ! ! 4.4 ! The same algorithm - as described in ! ! ! |
| ! ! ! item 4.3 - is used for TOL, MAX and TTP,! ! ! |
| ! ! ! if code 4320 with the related discrete ! ! ! |
| ! ! ! signal triggers the report. But in this ! ! ! |
| ! ! ! case using VB2: ! ! ! |
| ! ! ! EVM 3D.1.136.01 Engine 1 ! ! ! |
| ! ! ! 3D.1.136.10 Engine 2 ! ! ! |
| ! ! ! and the related discrete for code 4320. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| ! !5 ! Generation stops when exceedance param. ! ! ! |
| ! ! ! are again within their limits or 10 sets! ! ! |
| ! ! ! of post event data are generated. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !8100!8.1 ! ACARS MU uplink request with IMI "REQ07"! ! ! |
| ! ! ! The report <07> is immediately generated! ! ! |
| ! ! ! and transmitted to the ACARS MU. ! ! ! |
| !----------------------------------------------------------------------! |
| ! A = Programmable by Airbus ! |
| ! C = Programmable by Customer ! |
| +----------------------------------------------------------------------+ |
L. AIDS Reports Print Rules - Default Values for Report <07>
| +------------------------------------------------+ |
| ! ! ! ! |
| ! Code ! Printer Output ! ACARS-output ! |
| ! ! ! ! |
| !-------!-----------------------!----------------! |
| ! ! ! ! |
| ! 1000 ! Print immediatly ! No ACARS ! |
| ! ! ! ! |
| !-------!-----------------------!----------------! |
| ! ! ! ! |
| ! 2000 ! Print immediatly ! No ACARS ! |
| ! ! ! ! |
| !-------!-----------------------!----------------! |
| ! ! ! ! |
| ! 4110 ! Print at landing ! ACARS VHF ! |
| ! ! ! ! |
| !-------!-----------------------!----------------! |
| ! ! ! ! |
| ! 4120 ! Print at landing ! ACARS VHF ! |
| ! ! ! ! |
| !-------!-----------------------!----------------! |
| ! ! ! ! |
| ! 4130 ! Print at landing ! ACARS VHF ! |
| ! ! ! ! |
| !-------!-----------------------!----------------! |
| ! ! ! ! |
| ! 4210 ! Print at landing ! ACARS VHF ! |
| ! ! ! ! |
| !-------!-----------------------!----------------! |
| ! ! ! ! |
| ! 4220 ! Print at landing ! ACARS VHF ! |
| ! ! ! ! |
| !-------!-----------------------!----------------! |
| ! ! ! ! |
| ! 4230 ! Print at landing ! ACARS VHF ! |
| ! ! ! ! |
| !-------!-----------------------!----------------! |
| ! ! ! ! |
| ! 4310 ! Print at landing ! ACARS VHF ! |
| ! ! ! ! |
| !-------!-----------------------!----------------! |
| ! ! ! ! |
| ! 4320 ! Print at landing ! ACARS VHF ! |
| ! ! ! ! |
| !-------!-----------------------!----------------! |
| ! ! ! ! |
| ! 8100 ! No print ! ACARS VHF ! |
| ! ! ! ! |
| +------------------------------------------------+ |
| +-------------------------------------------------------------------------+ |
| !Trigger! to ACARS ! to printer ! store ! |
| ! Code !------------------------------ -!-----------------!--------------! |
| ! No !Ground ! VHF ! SAT- ! HF ! at ! imme- ! internal& ! |
| ! ! ! ! COM ! !landing ! diate ! external ! |
| ! ! ! ! ! ! ! !(build in RAM&! |
| ! ! ! ! ! ! ! ! PCMCIA) ! |
| !-------!-------!--------!-------!-------!--------!--------!--------------! |
| ! ! ! If ! ! ! ! If !PCMCIA only if! |
| ! 1000 ! NO ! 'SEND' ! NO ! NO ! NO !'PRINT' ! 'STORE' ! |
| ! ! !selected! ! ! !selected! selected on ! |
| ! ! !on MCDU ! ! ! !on MCDU ! MCDU ! |
| !-------!-------!--------!-------!-------!--------!--------!--------------! |
| ! 2000 ! NO ! NO ! NO ! NO ! ! YES ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 3000 ! NO ! NO ! NO ! NO ! ! NO ! YES ! |
| !-------!-------!--------!------ !-------! !--------!--------------! |
| ! 4110 ! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 4120 ! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 4130 ! NO ! YES ! NO ! NO ! Y ! NO ! YES ! |
| !-------!-------!--------!-------!-------! E !--------!--------------! |
| ! 4210 ! NO ! YES ! NO ! NO ! S ! NO ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 4220 ! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 4230 ! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 4310 ! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 4320 ! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 8100 ! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| +-------------------------------------------------------------------------+ |
| +-------------------------------------------------------------------------+ |
| !Trigger! to ACARS ! to printer ! store ! |
| ! Code !------------------------------ -!-----------------!--------------! |
| ! No !Ground ! VHF ! SAT- ! HF ! at ! imme- ! internal& ! |
| ! ! ! ! COM ! !landing ! diate ! external ! |
| ! ! ! ! ! ! ! !(build in RAM&! |
| ! ! ! ! ! ! ! ! PCMCIA) ! |
| !-------!-------!--------!-------!-------!--------!--------!--------------! |
| ! 1000 ! NO ! NO ! NO ! NO ! NO ! YES ! YES ! |
| !-------!-------!--------!-------!-------!--------!--------!--------------! |
| ! 2000 ! NO ! NO ! NO ! NO ! NO ! YES ! YES ! |
| !-------!-------!--------!-------!-------!--------!--------!--------------! |
| ! 3000 ! NO ! NO ! NO ! NO ! NO ! NO ! YES ! |
| !-------!-------!--------!------ !-------!--------!--------!--------------! |
| ! 4110 ! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 4120 ! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 4130 ! NO ! YES ! NO ! NO ! Y ! NO ! YES ! |
| !-------!-------!--------!-------!-------! E !--------!--------------! |
| ! 4210 ! NO ! YES ! NO ! NO ! S ! NO ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 4220 ! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 4230 ! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 4310 ! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 4320 ! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| !-------!-------!--------!-------!-------!--------!--------!--------------! |
| ! 8100 ! NO ! YES ! NO ! NO ! NO ! NO ! YES ! |
| +-------------------------------------------------------------------------+ |
M. Engine Divergence Report <09>
Engine Divergence Report <09> (Engine Type CFMU with EVMU)
Engine Divergence Report <09> (Engine Type CFMU with EVMU)
Engine Divergence Report <09> (Engine Type CFMU with EVMU) ** ON A/C NOT FOR ALL
Engine Divergence Report <09> (Engine Type CFMU with EVMU) ** ON A/C NOT FOR ALL
Engine Divergence Report <09> (Engine Type CFMU with EVMU) ** ON A/C NOT FOR ALL
The Engine Divergence Report shall be a time series collection of engine related information prior to and after the detection of an engine divergence condition. The engine divergence logic is intended to detect rapid degradation in engine performance over the course of a few hours. The report is generated when one of the logic conditions 1000 to 4180 (for details see the Engine Divergence Report logic) is present.
Engine Divergence Report <09> (Engine Type CFMU with EVMU) Engine Divergence Report <09> (Engine Type CFMU with EVMU) Engine Divergence Report <09> (Engine Type CFMU with EVMU) ** ON A/C NOT FOR ALL Engine Divergence Report <09> (Engine Type CFMU with EVMU) ** ON A/C NOT FOR ALL Engine Divergence Report <09> (Engine Type CFMU with EVMU) ** ON A/C NOT FOR ALL NOTE: For the standard header definition of the report refer to (Ref. AMM D/O 31-36-00-00).
(1) Engine Divergence Report Data Field Description <09>(Engine Type CFMI with Advanced EVMU)
NOTE: Reports that are transmitted from the ACARS system do not have report lines without a line identifier.
| +---------------------------------------------------------------------+ |
| ! Value ! Content Description ! |
| !--------------!------------------------------------------------------! |
| ! ESN ! Engine Serial Number ! |
| ! 999999 ! (000000 to 999999) ! |
| ! ! Eng 1 param. 7C.1.046.01 digit 3, 2, 1 ! |
| ! ! 7C.1.047.01 digit 6, 5, 4 ! |
| ! ! Eng 2 param. 7C.2.046.01 digit 3, 2, 1 ! |
| ! ! 7C.2.047.01 digit 6, 5, 4 ! |
| !--------------!------------------------------------------------------! |
| ! EHRS ! Engine Flight Hours ! |
| ! 99999 ! (00000 to 99999 hours) ! |
| ! ! DMU Engine 1 and Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! ERT ! Engine Running Time ! |
| ! 99999 ! (00000 to 65536 hours) ! |
| ! ! Eng 1 param. 7C.1.050.01 ! |
| ! ! Eng 2 param. 7C.2.050.10 ! |
| !--------------!------------------------------------------------------! |
| ! ECYC ! Engine Cycle ! |
| ! 99999 ! (00000 to 99999) ! |
| !--------------!------------------------------------------------------! |
| ! AP ! Auto Pilot Status ! |
| ! 99 ! (00 to G8) ! |
| ! ! FMGC 1 and 2 (FGC part) for Auto Pilot AP1 and AP2 ! |
| ! ! ! |
| ! ! XX Auto Pilot Modes: ! |
| ! ! !! ! |
| ! ! !!__Lateral Modes: 0 = NO MODE ! |
| ! ! ! 1 = HEADING ! |
| ! ! ! 2 = TRACK ! |
| ! ! ! 3 = NAV ! |
| ! ! ! 4 = LOC CAPTURE ! |
| ! ! ! 5 = LOC TRACK ! |
| ! ! ! 6 = LAND TRACK ! |
| ! ! ! 7 = RUNWAY ! |
| ! ! ! 8 = ROLL GO AROUND ! |
| ! ! ! ! |
| ! ! !__Longitudinal Modes: 0 = NO MODE ! |
| ! ! 1 = PITCH G/A ! |
| ! ! 2 = PITCH T/O ! |
| ! ! 3 = G/S TRACK ! |
| ! ! 4 = G/S CAPTURE ! |
| ! ! 5 = V/S ! |
| ! ! 6 = FPA ! |
| ! ! 7 = ALT ! |
| ! ! 8 = ALT ACQ ! |
| ! ! 9 = OPEN CLB ! |
| ! ! A = OPEN DES ! |
| ! ! B = IM CLB ! |
| ! ! C = IM DES ! |
| ! ! D = CLB ! |
| ! ! E = DES ! |
| ! ! F = FINAL DES ! |
| ! ! G = EXPEDITE ! |
| ! ! ! |
| ! ! AP1 ! AP2 ! |
| ! ! Report Line EC: ! Report Line EE: !Difinition: ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! / ! / !No Mode Act. ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.11 = 1 ! 01.2.275.00.11 = 1!RUNWAY Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.12 = 1 ! 01.2.275.00.12 = 1!NAV Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.13 = 1 ! 01.2.275.00.13 = 1!LOC CAPTURE ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.14 = 1 ! 01.2.275.00.14 = 1!LOC TRACK ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.15 = 1 ! 01.2.275.00.15 = 1!Roll GO ! |
| ! ! ! !AROUND Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.16 = 1 ! 01.2.275.00.16 = 1!HEADING Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.17 = 1 ! 01.2.275.00.17 = 1!TRACK Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.15 = 1 ! 01.2.274.00.15 = 1!PITCH TO Mode! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.16 = 1 ! 01.2.274.00.16 = 1!PITCH GA Mode! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.17 = 1 ! 01.2.274.00.17 = 1!V/S Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.18 = 1 ! 01.2.274.00.18 = 1!FPA Mode ! |
| ! ! -------------------!-------------------!-------------! |
| ! ! 01.1.274.00.19 = 1 ! 01.2.274.00.19 = 1!ALT Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.20 = 1 ! 01.2.274.00.20 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.19 = 1 ! 01.2.274.00.19 = 1!ALT ACQ ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.21 = 1 ! 01.2.274.00.21 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.20 = 1 ! 01.2.274.00.20 = 1!G/S TRACK ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.22 = 1 ! 01.2.274.00.22 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.21 = 1 ! 01.2.274.00.21 = 1!G/S CAPTURE ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.22 = 1 ! 01.2.274.00.22 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.23 = 1 ! 01.2.274.00.23 = 1!FINAL DES ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.2.274.00.24 = 1 ! 01.2.274.00.24 = 1!EXPED. Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.146.00.14 = 1 ! 01.2.146.00.14 = 1!LAND TRACK ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!CLB Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.13 = 0 ! 01.2.274.00.13 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.14 = 0 ! 01.2.274.00.14 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.24 = 0 ! 01.2.274.00.24 = 0! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!DES Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.13 = 0 ! 01.2.274.00.13 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.14 = 0 ! 01.2.274.00.14 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.24 = 0 ! 01.2.274.00.24 = 0! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!IM. CLIMB ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.13 = 1 ! 01.2.274.00.13 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!IM. DES Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.13 = 1 ! 01.2.274.00.13 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!OPEN CLB ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.14 = 1 ! 01.2.274.00.14 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!OPEN DES ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.14 = 1 ! 01.2.274.00.14 = 1! ! |
| ! ! ---------------------------------------------------- ! |
| ! ! Auto Pilot Status DMU: ! |
| ! ! AP1 printed in report line EC ! |
| ! ! AP2 printed in report line EE ! |
| !--------------!------------------------------------------------------! |
| ! VSV ! Variable Statore Vane Position ! |
| ! X99 ! (-5.0 to 45.0 deg) ! |
| ! ! Eng 1 param. 7C.1.072.01 ! |
| ! ! Eng 2 param. 7C.2.072.10 ! |
| !--------------!------------------------------------------------------! |
| ! VBV ! Variable Bleed Valve Position ! |
| ! X99 ! (-9.9 to 40.0 deg) ! |
| ! ! Eng 1 param. 7C.1.071.01 ! |
| ! ! Eng 2 param. 7C.2.071.10 ! |
| !--------------!------------------------------------------------------! |
| ! E ! Exeedance Engine Position ! |
| ! 9 ! ! |
| !--------------!------------------------------------------------------! |
| ! DIV ! Parameter Divergency ! |
| ! 9999 ! ! |
| !--------------!------------------------------------------------------! |
| ! REF ! Actual deltaEGTref or deltaTNref value ! |
| ! X999 ! (-999 to 999 C) ! |
| !--------------!------------------------------------------------------! |
| ! K ! Actual Value of K ! |
| ! 99 ! (0 to 99) ! |
| !--------------!------------------------------------------------------! |
| ! ECW1 ! Engine Control Word 1 ! |
| ! XXXXX ! Each 'X' represents 4 Bits in hexadecimal code of ! |
| ! ! a defined ARINC 429 word: ! |
| ! ! XXXXX Bits HEX ! |
| ! ! !!!!!___________ 14, 13, 12, 11 0...F ! |
| ! ! !!!!____________ 18, 17, 16, 15 0...F ! |
| ! ! !!!_____________ 22, 21, 20, 19 0...F ! |
| ! ! !!______________ 26, 25, 24, 23 0...F ! |
| ! ! !_______________ 29, 28, 27 0...7 ! |
| ! ! -------------------------------------------- ! |
| ! ! Bit Label Parameter Description ! |
| ! ! 11 7C.X.272.XX.19 = 1 Auto Thrust Active ! |
| ! ! 12 7C.X.272.XX.20 = 1 VSV Position Fault ! |
| ! ! 13 SPARE ! |
| ! ! 14 SPARE ! |
| ! ! 15 7C.X.351.XX.29 = 1 Fuel Flow Measurement ! |
| ! ! Invalid ! |
| ! ! 16 7C.X.275.XX.15 = 1 N1/N2 Control ACtive ! |
| ! ! 17 7C.X.275.XX.26 = 1 Channel A Active ! |
| ! ! 18 7C.X.275.XX.27 = 1 Channel B Active ! |
| ! ! 19 SPARE ! |
| ! ! 20 SPARE ! |
| ! ! 21 SPARE ! |
| ! ! 22 SPARE ! |
| ! ! 23 SPARE ! |
| ! ! 24 SPARE ! |
| ! ! 25 SPARE ! |
| ! ! 26 SPARE ! |
| ! ! 27 SPARE ! |
| ! ! 28 SPARE ! |
| ! ! 29 SPARE ! |
| !--------------!------------------------------------------------------! |
| ! ECW2 ! Engine Control Word 2 ! |
| ! XXXXX ! Each 'X' represents 4 Bits in hexadecimal code of ! |
| ! ! a defined ARINC 429 word: ! |
| ! ! XXXXX Bits HEX ! |
| ! ! !!!!!___________ 14, 13, 12, 11 0...F ! |
| ! ! !!!!____________ 18, 17, 16, 15 0...F ! |
| ! ! !!!_____________ 22, 21, 20, 19 0...F ! |
| ! ! !!______________ 26, 25, 24, 23 0...F ! |
| ! ! !_______________ 29, 28, 27 0...7 ! |
| ! ! -------------------------------------------- ! |
| ! ! Bit Label Parameter Description ! |
| ! ! 11 7C.X.272.XX.12 = 1 Bump/Overboost #1 enable ! |
| ! ! 12 7C.X.272.XX.13 = 1 Bump/Overboost #2 enable ! |
| ! ! 13 7C.X.272.XX.14 = 1 Bump/Overboost #3 enable ! |
| ! ! 14 7C.X.272.XX.22 = 1 MTO. GA limit mode select.! |
| ! ! 15 7C.X.272.XX.23 = 1 Flex Take-Off limit mode ! |
| ! ! selected ! |
| ! ! 16 SPARE ! |
| ! ! 17 SPARE ! |
| ! ! 18 SPARE ! |
| ! ! 19 SPARE ! |
| ! ! 20 SPARE ! |
| ! ! 21 SPARE ! |
| ! ! 22 SPARE ! |
| ! ! 23 SPARE ! |
| ! ! 24 SPARE ! |
| ! ! 25 SPARE ! |
| ! ! 26 SPARE ! |
| ! ! 27 SPARE ! |
| ! ! 28 SPARE ! |
| ! ! 29 SPARE ! |
| !--------------!------------------------------------------------------! |
| ! PSEL ! Status of different FADEC sensors ! |
| ! XXXX ! X X X X Label: Selected: ! |
| ! ! ! ! ! !___ 211 TAT (Bit 11 --> 15) ! |
| ! ! ! ! ! ____ 344 N2 actual (Bit 11 --> 15) ! |
| ! ! ! !_______ 345 EGT (Bit 11 --> 15) ! |
| ! ! !_________ 346 N1 actual (Bit 11 --> 15) ! |
| ! ! Source: ECU, different labels ! |
| ! ! NOTE: The shown values are coded as follows: ! |
| ! ! Bit: 15 14 13 12 11 ! Shown value ! |
| ! ! --------------------!---------------- ! |
| ! ! 0 0 0 0 0 ! 0 ! |
| ! ! 0 0 0 0 1 ! 1 ! |
| ! ! 0 0 0 1 0 ! 2 ! |
| ! ! 0 0 0 1 1 ! 3 ! |
| ! ! 0 0 1 0 0 ! 4 ! |
| ! ! 0 0 1 0 1 ! 5 ! |
| ! ! 0 0 1 1 0 ! 6 ! |
| ! ! 0 0 1 1 1 ! 7 ! |
| ! ! 0 1 0 0 0 ! 8 ! |
| ! ! 0 1 0 0 1 ! 9 ! |
| ! ! 0 1 0 1 0 ! A ! |
| ! ! 0 1 0 1 1 ! B ! |
| ! ! 0 1 1 0 0 ! C ! |
| ! ! 0 1 1 0 1 ! D ! |
| ! ! 0 1 1 1 0 ! E ! |
| ! ! 0 1 1 1 1 ! F ! |
| ! ! 1 0 0 0 0 ! G ! |
| ! ! 1 0 0 0 1 ! H ! |
| ! ! 1 0 0 1 0 ! I ! |
| ! ! 1 0 0 1 1 ! J ! |
| ! ! 1 0 1 0 0 ! K ! |
| ! ! 1 0 1 0 1 ! L ! |
| ! ! 1 0 1 1 0 ! M ! |
| ! ! 1 0 1 1 1 ! N ! |
| ! ! 1 1 0 0 0 ! O ! |
| ! ! 1 1 0 0 1 ! P ! |
| ! ! 1 1 0 1 0 ! Q ! |
| ! ! 1 1 0 1 1 ! R ! |
| ! ! 1 1 1 0 0 ! S ! |
| ! ! 1 1 1 0 1 ! T ! |
| ! ! 1 1 1 1 0 ! U ! |
| ! ! 1 1 1 1 1 ! V ! |
| ! ! ! |
| !--------------!------------------------------------------------------! |
| ! REASON ! Reason for Exceedance ! |
| ! XXXXXXXXXX ! ! |
| ! XXXXXXXXXX ! Up to 20 Characters ! |
| ! ! EGT Code: 4110, 4120, 4130 and 4140 ! |
| ! ! TN Code: 4150, 4160, 4170 and 4180 ! |
| !--------------!------------------------------------------------------! |
| ! N1 ! Selected N1 Actual ! |
| ! 9999 ! (0 to 120.0 %rpm) ! |
| ! ! Eng 1 param. 7C.1.346.01 ! |
| ! ! Eng 2 param. 7C.2.346.10 ! |
| !--------------!------------------------------------------------------! |
| ! N1C ! N1 Command ! |
| ! 9999 ! (0 to 120.0 %rpm) ! |
| ! ! Eng 1 param. 7C.1.341.01 ! |
| ! ! Eng 2 param. 7C.2.341.10 ! |
| !--------------!------------------------------------------------------! |
| ! N2 ! Selected N2 Actual ! |
| ! 9999 ! (0 to 120.0 %rpm) ! |
| ! ! Eng 1 param. 7C.1.344.01 ! |
| ! ! Eng 2 param. 7C.2.344.10 ! |
| !--------------!------------------------------------------------------! |
| ! EGT ! Selected T494 (Exhaust Gas Temperature) ! |
| ! X999 ! (-55 to 999.9 C) ! |
| ! ! Eng 1 param. 7C.1.345.01 ! |
| ! ! Eng 2 param. 7C.2.345.10 ! |
| !--------------!------------------------------------------------------! |
| ! FF ! Engine Fuel Flow ! |
| ! 9999 ! ( 0 to 7000 kg/h) ! |
| ! ! Eng 1 param. 7C.1.244.01 ! |
| ! ! Eng 2 param. 7C.2.244.10 ! |
| !--------------!------------------------------------------------------! |
| ! TN ! Nacelle Temperature ! |
| ! X99 ! Eng 1 param. 26.1.322.01 ! |
| ! ! 26.2.322.01 ! |
| ! ! Eng 2 param. 26.1.322.10 ! |
| ! ! 26.2.322.10 ! |
| +---------------------------------------------------------------------+ |
(2) Engine Divergence Report Data Field Description <09> (Engine Type CFMI with Advanced EVMU)
NOTE: Reports that are transmitted from the ACARS system do not have report lines without a line identifier.
NOTE: Only the parts of the ENGINE DIVERGENCE REPORT <09> which are not included in the ENGINE CRUISE REPORT <01> are given in the subsequent table.
| +---------------------------------------------------------------------+ |
| ! Value ! Content Description ! |
| !--------------!------------------------------------------------------! |
| ! E ! Divergent Engine Position ! |
| ! 9 ! DMU (No. of engine which has a divergence) ! |
| !--------------!------------------------------------------------------! |
| ! DIV ! Parameter Divergency ! |
| ! 9999 ! ! |
| !--------------!------------------------------------------------------! |
| ! REF ! Actual deltaEGTref or deltaTNref value ! |
| ! X999 ! DMU (-999 to 999 C) ! |
| ! ! NOTE: Negative values are shown with an 'N' in the ! |
| ! ! first position. ! |
| !--------------!------------------------------------------------------! |
| ! K ! Actual Value of K ! |
| ! 99 ! DMU (0 to 99) ! |
| !--------------!------------------------------------------------------! |
| ! ECW2 ! Engine Control Word 2 ! |
| ! XXXXX ! Each 'X' represents 4 Bits in hexadecimal code of ! |
| ! ! a defined ARINC 429 word: ! |
| ! ! XXXXX Bits HEX ! |
| ! ! !!!!!___________ 14, 13, 12, 11 0...F ! |
| ! ! !!!!____________ 18, 17, 16, 15 0...F ! |
| ! ! !!!_____________ 22, 21, 20, 19 0...F ! |
| ! ! !!______________ 26, 25, 24, 23 0...F ! |
| ! ! !_______________ 29, 28, 27 0...7 ! |
| ! ! -------------------------------------------- ! |
| ! ! Bit Label Parameter Description ! |
| ! ! 11 7C.X.272.XX.12 = 1 Bump/Overboost #1 enable ! |
| ! ! 12 7C.X.272.XX.13 = 1 Bump/Overboost #2 enable ! |
| ! ! 13 7C.X.272.XX.14 = 1 Bump/Overboost #3 enable ! |
| ! ! 14 7C.X.272.XX.22 = 1 MTO. GA limit mode ! |
| ! ! selected ! |
| ! ! 15 7C.X.272.XX.23 = 1 Flex Take-Off limit mode ! |
| ! ! selected ! |
| ! ! 16 SPARE ! |
| ! ! 17 SPARE ! |
| ! ! 18 SPARE ! |
| ! ! 19 SPARE ! |
| ! ! 20 SPARE ! |
| ! ! 21 SPARE ! |
| ! ! 22 SPARE ! |
| ! ! 23 SPARE ! |
| ! ! 24 SPARE ! |
| ! ! 25 SPARE ! |
| ! ! 26 SPARE ! |
| ! ! 27 SPARE ! |
| ! ! 28 SPARE ! |
| ! ! 29 SPARE ! |
| !--------------!------------------------------------------------------! |
| ! PSEL ! Status of different FADEC sensors ! |
| ! XXXX ! X X X X Label: Selected: (Bit 11 --> 15) ! |
| ! ! I I I I___ 211 TAT ! |
| ! ! I I I ____ 344 N2 actual ! |
| ! ! I I_______ 345 EGT ! |
| ! ! I_________ 346 N1 actual ! |
| ! ! (All labels Bit 11 --> 15) ! |
| ! ! Source: ECU, different labels ! |
| ! ! NOTE: The shown values are coded as follows: ! |
| ! ! Bit: 15 14 13 12 11 ! Shown value ! |
| ! ! --------------------!---------------- ! |
| ! ! 0 0 0 0 0 ! 0 ! |
| ! ! 0 0 0 0 1 ! 1 ! |
| ! ! 0 0 0 1 0 ! 2 ! |
| ! ! 0 0 0 1 1 ! 3 ! |
| ! ! 0 0 1 0 0 ! 4 ! |
| ! ! 0 0 1 0 1 ! 5 ! |
| ! ! 0 0 1 1 0 ! 6 ! |
| ! ! 0 0 1 1 1 ! 7 ! |
| ! ! 0 1 0 0 0 ! 8 ! |
| ! ! 0 1 0 0 1 ! 9 ! |
| ! ! 0 1 0 1 0 ! A ! |
| ! ! 0 1 0 1 1 ! B ! |
| ! ! 0 1 1 0 0 ! C ! |
| ! ! 0 1 1 0 1 ! D ! |
| ! ! 0 1 1 1 0 ! E ! |
| ! ! 0 1 1 1 1 ! F ! |
| ! ! 1 0 0 0 0 ! G ! |
| ! ! 1 0 0 0 1 ! H ! |
| ! ! 1 0 0 1 0 ! I ! |
| ! ! 1 0 0 1 1 ! J ! |
| ! ! 1 0 1 0 0 ! K ! |
| ! ! 1 0 1 0 1 ! L ! |
| ! ! 1 0 1 1 0 ! M ! |
| ! ! 1 0 1 1 1 ! N ! |
| ! ! 1 1 0 0 0 ! O ! |
| ! ! 1 1 0 0 1 ! P ! |
| ! ! 1 1 0 1 0 ! Q ! |
| ! ! 1 1 0 1 1 ! R ! |
| ! ! 1 1 1 0 0 ! S ! |
| ! ! 1 1 1 0 1 ! T ! |
| ! ! 1 1 1 1 0 ! U ! |
| ! ! 1 1 1 1 1 ! V ! |
| ! ! ! |
| !--------------!------------------------------------------------------! |
| ! REASON ! Reason for Exceedance ! |
| ! XXXXXXXXXX ! DMU ! |
| ! XXXXXXXXXX ! Up to 20 Characters ! |
| ! ! EGT Code: 4110, 4120, 4130 and 4140 ! |
| ! ! TN Code: 4150, 4160, 4170 and 4180 ! |
| ! ! If the report was not triggered by a limit ! |
| ! ! exceedence then this field contains blanks. ! |
| +---------------------------------------------------------------------+ |
(3) Engine Divergence Report Data Field Description <09> (Engine Type CFMI with Advanced EVMU)
NOTE: Reports that are transmitted from the ACARS system do not have report lines without a line identifier.
NOTE: Only the parts of the ENGINE DIVERGENCE REPORT <09> which are not included in the ENGINE CRUISE REPORT <01> are given in the subsequent table.
| +---------------------------------------------------------------------+ |
| ! Value ! Content Description ! |
| !--------------!------------------------------------------------------! |
| ! E ! Divergent Engine Position ! |
| ! 9 ! DMU (No. of engine which has a divergence) ! |
| !--------------!------------------------------------------------------! |
| ! DIV ! Parameter Divergency ! |
| ! ! ! |
| !--------------!------------------------------------------------------! |
| ! REF ! Actual deltaEGT or deltaTNref value in PH5.1 or PH6! |
| ! X999 ! DMU (-999 to 999 C) ! |
| ! ! NOTE: Negative values are shown with an '-' in the ! |
| ! ! first position. ! |
| !--------------!------------------------------------------------------! |
| ! K ! Actual Value of K in PH5.1 or PH6 ! |
| ! 99 ! DMU (0 to 99) ! |
| !--------------!------------------------------------------------------! |
| ! ECW2 ! Engine Control Word 2 ! |
| ! XXXXX ! Each 'X' represents 4 Bits in hexadecimal code of ! |
| ! ! a defined ARINC 429 word: ! |
| ! ! XXXXX Bits HEX ! |
| ! ! !!!!!___________ 14, 13, 12, 11 0...F ! |
| ! ! !!!!____________ 18, 17, 16, 15 0...F ! |
| ! ! !!!_____________ 22, 21, 20, 19 0...F ! |
| ! ! !!______________ 26, 25, 24, 23 0...F ! |
| ! ! !_______________ 29, 28, 27 0...7 ! |
| ! ! Source DMU, got from several ECU labels as given ! |
| ! ! below. For engine 1 and engine 2. ! |
| ! ! The 'X' for the System and SDI definition of the ! |
| ! ! engine parameters: ! |
| ! ! System SDI ! |
| ! ! Engine 1 1 01 ! |
| ! ! Engine 2 2 10 ! |
| ! ! -------------------------------------------- ! |
| ! ! Bit Label Parameter Description ! |
| ! ! 11 7C.X.272.XX.12 = 1 Bump/Overboost #1 enable ! |
| ! ! 12 7C.X.272.XX.13 = 1 Bump/Overboost #2 enable ! |
| ! ! 13 7C.X.272.XX.14 = 1 Bump/Overboost #3 enable ! |
| ! ! 14 7C.X.272.XX.22 = 1 MTO. GA limit mode ! |
| ! ! selected ! |
| ! ! 15 7C.X.272.XX.23 = 1 Flex Take-Off limit mode ! |
| ! ! selected ! |
| ! ! 16 SPARE ! |
| ! ! 17 SPARE ! |
| ! ! 18 SPARE ! |
| ! ! 19 SPARE ! |
| ! ! 20 SPARE ! |
| ! ! 21 SPARE ! |
| ! ! 22 SPARE ! |
| ! ! 23 SPARE ! |
| ! ! 24 SPARE ! |
| ! ! 25 SPARE ! |
| ! ! 26 SPARE ! |
| ! ! 27 SPARE ! |
| ! ! 28 SPARE ! |
| ! ! 29 SPARE ! |
| !--------------!------------------------------------------------------! |
| ! PSEL ! Status of different FADEC sensors ! |
| ! XXXX ! X X X X Label: Selected: (Bit 11 --> 15) ! |
| ! ! ! ! ! !___ 211 TAT ! |
| ! ! ! ! !_____ 344 N2 actual ! |
| ! ! ! !_______ 345 EGT ! |
| ! ! !_________ 346 N1 actual ! |
| ! ! (All labels Bit 11 --> 15) ! |
| ! ! Source: ECU, different labels ! |
| ! ! NOTE: The shown values are coded as follows: ! |
| ! ! Bit: 15 14 13 12 11 ! Shown value ! |
| ! ! --------------------!---------------- ! |
| ! ! 0 0 0 0 0 ! 0 ! |
| ! ! 0 0 0 0 1 ! 1 ! |
| ! ! 0 0 0 1 0 ! 2 ! |
| ! ! 0 0 0 1 1 ! 3 ! |
| ! ! 0 0 1 0 0 ! 4 ! |
| ! ! 0 0 1 0 1 ! 5 ! |
| ! ! 0 0 1 1 0 ! 6 ! |
| ! ! 0 0 1 1 1 ! 7 ! |
| ! ! 0 1 0 0 0 ! 8 ! |
| ! ! 0 1 0 0 1 ! 9 ! |
| ! ! 0 1 0 1 0 ! A ! |
| ! ! 0 1 0 1 1 ! B ! |
| ! ! 0 1 1 0 0 ! C ! |
| ! ! 0 1 1 0 1 ! D ! |
| ! ! 0 1 1 1 0 ! E ! |
| ! ! 0 1 1 1 1 ! F ! |
| ! ! 1 0 0 0 0 ! G ! |
| ! ! 1 0 0 0 1 ! H ! |
| ! ! 1 0 0 1 0 ! I ! |
| ! ! 1 0 0 1 1 ! J ! |
| ! ! 1 0 1 0 0 ! K ! |
| ! ! 1 0 1 0 1 ! L ! |
| ! ! 1 0 1 1 0 ! M ! |
| ! ! 1 0 1 1 1 ! N ! |
| ! ! 1 1 0 0 0 ! O ! |
| ! ! 1 1 0 0 1 ! P ! |
| ! ! 1 1 0 1 0 ! Q ! |
| ! ! 1 1 0 1 1 ! R ! |
| ! ! 1 1 1 0 0 ! S ! |
| ! ! 1 1 1 0 1 ! T ! |
| ! ! 1 1 1 1 0 ! U ! |
| ! ! 1 1 1 1 1 ! V ! |
| ! ! ! |
| !--------------!------------------------------------------------------! |
| ! REASON ! Reason for Exceedance ! |
| ! XXXXXXXXXX ! DMU ! |
| ! XXXXXXXXXX ! Up to 20 Characters ! |
| ! ! EGT Code: 4110, 4120, 4130 and 4140 ! |
| ! ! TN Code: 4150, 4160, 4170 and 4180 ! |
| ! ! ! |
| ! ! NOTE: If the report was not triggered by a limit ! |
| ! ! exceedence, this field contains blanks. ! |
| +---------------------------------------------------------------------+ |
(4) Engine Divergence Report Data Field Description <09> (Engine Type CFMI with Advanced EVMU)
NOTE: Reports that are transmitted from the ACARS system do not have report lines without a line identifier.
| +---------------------------------------------------------------------+ |
| ! Value ! Content Description ! |
| !--------------!------------------------------------------------------! |
| ! ESN ! Engine Serial Number ! |
| ! 999999 ! (000000 to 999999) ! |
| ! ! ECU Engine 1 7C.1.046.01 digit 3, 2, 1 ! |
| ! ! 7C.1.047.01 digit 6, 5, 4 ! |
| ! ! Engine 2 7C.2.046.10 digit 3, 2, 1 ! |
| ! ! 7C.2.047.10 digit 6, 5, 4 ! |
| !--------------!------------------------------------------------------! |
| ! EHRS ! Engine Flight Hours ! |
| ! 99999 ! (00000 to 99999 hours) ! |
| ! ! DMU Engine 1 ! |
| ! ! Engine 2 ! |
| ! ! Remark: Time between "Main (LH and RH) Landing Gear! |
| ! ! Decompressed" and "Main (LH and RH) Landing! |
| ! ! Gear Compressed". The EHRS is set to zero ! |
| ! ! if a new ESN is recognized by the DMU. ! |
| ! ! It is possible to set the EHRS via the ! |
| ! ! MCDU, e.g. if the DMU is changed on the ! |
| ! ! a/c. ! |
| !--------------!------------------------------------------------------! |
| ! ERT ! Engine Running Time ! |
| ! 99999 ! (00000 to 65536 hours) ! |
| ! ! ECU 7C.1.050.01 Engine 1 ! |
| ! ! 7C.2.050.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! ECYC ! Engine Cycle ! |
| ! 99999 ! (00000 to 99999) ! |
| ! ! DMU Engine 1 ! |
| ! ! Engine 2 ! |
| ! ! Remark: Each time when flight phase 5 (climb) is ! |
| ! ! reached, the counter is incremented by one ! |
| ! ! The ECYC is set to zero if a new ESN is ! |
| ! ! recognized by the DMU. It is possible to ! |
| ! ! set ECYC via the MCDU, if the DMU is ! |
| ! ! changed on the a/c. ! |
| !--------------!------------------------------------------------------! |
| ! AP ! Auto Pilot Status ! |
| ! 99 ! Number of respective status (00 to G8) ! |
| ! ! FMGC 1 and 2 (FGC part) for Auto Pilot AP1 and AP2 ! |
| ! ! ! |
| ! ! Parameter for AP1 ! Parameter for AP2 ! ! |
| ! ! Report Line EC: ! Report Line EE: !Definition: ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! / ! / !No Mode ! |
| ! ! ! !Active ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.11 = 1 ! 01.2.275.00.11 = 1!RUNWAY Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.12 = 1 ! 01.2.275.00.12 = 1!NAV Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.13 = 1 ! 01.2.275.00.13 = 1!LOC CAPTURE ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.14 = 1 ! 01.2.275.00.14 = 1!LOC TRACK ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.15 = 1 ! 01.2.275.00.15 = 1!Roll GO ! |
| ! ! ! !AROUND Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.16 = 1 ! 01.2.275.00.16 = 1!HEADING Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.17 = 1 ! 01.2.275.00.17 = 1!TRACK Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.15 = 1 ! 01.2.274.00.15 = 1!PITCH T/O ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.16 = 1 ! 01.2.274.00.16 = 1!PITCH GA Mode! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.17 = 1 ! 01.2.274.00.17 = 1!V/S Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.18 = 1 ! 01.2.274.00.18 = 1!FPA Mode ! |
| ! ! -------------------!-------------------!-------------! |
| ! ! 01.1.274.00.19 = 1 ! 01.2.274.00.19 = 1!ALT Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.20 = 1 ! 01.2.274.00.20 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.19 = 1 ! 01.2.274.00.19 = 1!ALT ACQ ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.21 = 1 ! 01.2.274.00.21 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.20 = 1 ! 01.2.274.00.20 = 1!G/S TRACK ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.22 = 1 ! 01.2.274.00.22 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.21 = 1 ! 01.2.274.00.21 = 1!G/S CAPTURE ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.22 = 1 ! 01.2.274.00.22 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.23 = 1 ! 01.2.274.00.23 = 1!FINAL DES ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.24 = 1 ! 01.2.274.00.24 = 1!EXPED. Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.146.00.14 = 1 ! 01.2.146.00.14 = 1!LAND TRACK ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!CLB Mode ! |
| ! ! AND ! AND ! ! |
| ! ! ! ! ! ! ! |
| ! ! -------------- ! -------------- ! ! |
| ! ! 01.1.274.00.13 = 0 ! 01.2.274.00.13 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.14 = 0 ! 01.2.274.00.14 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.24 = 0 ! 01.2.274.00.24 = 0! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!DES Mode ! |
| ! ! AND ! AND ! ! |
| ! ! ! ! ! ! ! |
| ! ! -------------- ! -------------- ! ! |
| ! ! 01.1.274.00.13 = 0 ! 01.2.274.00.13 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.14 = 0 ! 01.2.274.00.14 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.24 = 0 ! 01.2.274.00.24 = 0! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!IM. CLIMB ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.13 = 1 ! 01.2.274.00.13 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!IM. DES Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.13 = 1 ! 01.2.274.00.13 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!OPEN CLB ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.14 = 1 ! 01.2.274.00.14 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!OPEN. DES ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.14 = 1 ! 01.2.274.00.14 = 1! ! |
| ! ! ---------------------------------------------------- ! |
| ! ! Auto Pilot Status DMU: ! |
| ! ! Auto Pilot AP1 printed in report line EC ! |
| ! ! Auto Pilot AP2 printed in report line EE ! |
| ! ! Combined Auto Pilot Modes ! |
| ! ! The longitudinal auto pilot mode (1 to G) shall ! |
| ! ! appear on the left position for the AP1 and AP2 print! |
| ! ! format. ! |
| ! ! The lateral auto pilot mode (1 to 8) shall appear on ! |
| ! ! the right position for the AP1 and AP2 print format. ! |
| ! ! In case of a combined auto pilot mode e.g. DES mode ! |
| ! ! and NAV mode are engaged simultaneously, the 'E3' ! |
| ! ! shall appear below AP1 and AP2. ! |
| ! ! XX Auto Pilot Modes: ! |
| ! ! !! ! |
| ! ! !!__Lateral Modes: 0 = NO MODE ! |
| ! ! ! 1 = HEADING ! |
| ! ! ! 2 = TRACK ! |
| ! ! ! 3 = NAV ! |
| ! ! ! 4 = LOC CAPTURE ! |
| ! ! ! 5 = LOCK TRACK ! |
| ! ! ! 6 = LAND TRACK ! |
| ! ! ! 7 = RUNWAY ! |
| ! ! ! 8 = ROLL GO AROUND ! |
| ! ! ! ! |
| ! ! !__Longitudinal Modes: 0 = NO MODE ! |
| ! ! 1 = PITCH G/A ! |
| ! ! 2 = PITCH TO ! |
| ! ! 3 = G/S TRACK ! |
| ! ! 4 = G/S CAPTURE ! |
| ! ! 5 = V/S ! |
| ! ! 6 = FPA ! |
| ! ! 7 = ALT ! |
| ! ! 8 = ALT ACQ ! |
| ! ! 9 = OPEN CLB ! |
| ! ! A = OPEN DES ! |
| ! ! B = IM CLB ! |
| ! ! C = IM DES ! |
| ! ! D = CLB ! |
| ! ! E = DES ! |
| ! ! F = FINAL DES ! |
| ! ! G = EXPEDITE ! |
| !--------------!------------------------------------------------------! |
| ! VSV ! Selected Variable Stator Vane Position ! |
| ! X99 ! (-5.0 to 45.0 deg) ! |
| ! ! Negative values are indicated by '-' on the first ! |
| ! ! position. Otherwise the first position is used for ! |
| ! ! the value. ! |
| ! ! ECU 7C.1.072.01 Engine 1 ! |
| ! ! 7C.2.072.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! VBV ! Variable Bleed Valve Position ! |
| ! X99 ! (-9.9 to 40.0 deg) ! |
| ! ! Negative values are indicated by '-' on the first ! |
| ! ! position. Otherwise the first position is used for ! |
| ! ! the value. ! |
| ! ! ECU 7C.1.071.01 Engine 1 ! |
| ! ! 7C.2.071.10 Engine 2 ! |
| !--------------! -----------------------------------------------------! |
| ! E ! Exceedance Engine Position ! |
| ! 9 ! Number of engine which has a divergence. ! |
| ! ! DMU ! |
| !--------------!------------------------------------------------------! |
| ! DIV ! Parameter Divergency ! |
| ! ! Depending on divergent parameter ! |
| !--------------!------------------------------------------------------! |
| ! REF ! Actual deltaEGT or deltaTNref value of PH5.1 or PH6! |
| ! X999 ! -999 to 999 deg C ! |
| ! ! Negative values are indicated by '-' on the first ! |
| ! ! position. ! |
| !--------------!------------------------------------------------------! |
| ! K ! Actual Value of K in Ph5.1 or PH6 ! |
| ! 99 ! 0 to 99 ! |
| ! ! DMU ! |
| !--------------!------------------------------------------------------! |
| ! ECW1 ! Engine Control Word 1 ! |
| ! XXXXX ! XXXXX Bits HEX ! |
| ! ! !!!!!________14, 13, 12, 11 0..F ! |
| ! ! !!!!_________18, 17, 16, 15 0..F ! |
| ! ! !!!__________22, 21, 20, 19 0..F ! |
| ! ! !!___________26, 25, 24, 23 0..F ! |
| ! ! !____________ 29, 28, 27 0..F ! |
| ! ! Bit Label Parameter Description ! |
| ! ! 11 7C.X.272.XX.19 = 1 Auto Thrust Active ! |
| ! ! 12 7C.X.275.XX.20 = 1 VSV Position Fault ! |
| ! ! 13 SPARE ! |
| ! ! 14 SPARE ! |
| ! ! 15 7C.X.351.XX.29 = 1 Fuel Flow Measurement ! |
| ! ! Invalid ! |
| ! ! 16 7C.X.275.XX.15 = 1 N1/N2 Control Active ! |
| ! ! 17 7C.X.275.XX.26 = 1 Channel A Active ! |
| ! ! 18 7C.X.275.XX.27 = 1 Channel B Active ! |
| ! ! 19 SPARE ! |
| ! ! 20 SPARE ! |
| ! ! 21 SPARE ! |
| ! ! 22 SPARE ! |
| ! ! 23 SPARE ! |
| ! ! 24 SPARE ! |
| ! ! 25 SPARE ! |
| ! ! 26 SPARE ! |
| ! ! 27 SPARE ! |
| ! ! 28 SPARE ! |
| ! ! 29 SPARE ! |
| ! ! The 'X' for the System and SDI definition of the ! |
| ! ! engine parameters are as follows: ! |
| ! ! System SDI ! |
| ! ! Engine 1 1 01 ! |
| ! ! Engine 2 2 10 ! |
| !--------------!------------------------------------------------------! |
| ! ECW2 ! Engine Control Word 2 ! |
| ! XXXXX ! XXXXX Bits HEX ! |
| ! ! !!!!!________14, 13, 12, 11 0..F ! |
| ! ! !!!!_________18, 17, 16, 15 0..F ! |
| ! ! !!!__________22, 21, 20, 19 0..F ! |
| ! ! !!___________26, 25, 24, 23 0..F ! |
| ! ! !____________ 29, 28, 27 0..F ! |
| ! ! Bit Label Parameter Description ! |
| ! ! 11 7C.X.272.XX.12 = 1 Bump/Overboost #1 Enable ! |
| ! ! 12 7C.X.272.XX.13 = 1 Bump/Overboost #2 Enable ! |
| ! ! 13 7C.X.272.XX.14 = 1 Bump/Overboost #3 Enable ! |
| ! ! 14 7C.X.272.XX.22 = 1 MTO. GA Limit Mode Select.! |
| ! ! 15 7C.X.272.XX.23 = 1 Flex Take Off Limit Mode ! |
| ! ! Selected ! |
| ! ! 16 SPARE ! |
| ! ! 17 SPARE ! |
| ! ! 18 SPARE ! |
| ! ! 19 SPARE ! |
| ! ! 20 SPARE ! |
| ! ! 21 SPARE ! |
| ! ! 22 SPARE ! |
| ! ! 23 SPARE ! |
| ! ! 24 SPARE ! |
| ! ! 25 SPARE ! |
| ! ! 26 SPARE ! |
| ! ! 27 SPARE ! |
| ! ! 28 SPARE ! |
| ! ! 29 SPARE ! |
| ! ! The 'X' for the System and SDI definition of the ! |
| ! ! engine parameters are be as follows: ! |
| ! ! System SDI ! |
| ! ! Engine 1 1 01 ! |
| ! ! Engine 2 2 10 ! |
| !--------------!------------------------------------------------------! |
| ! PSEL ! Status of different FADEC sensors ! |
| ! XXXX ! XXXX Label: Selected: ! |
| ! ! !!!!_ 211 TAT (Bit 11 -> 15)! |
| ! ! !!!__ 344 N2 actual (Bit 11 -> 15)! |
| ! ! !!___ 345 EGT (Bit 11 -> 15)! |
| ! ! !____ 346 N1 actual (Bit 11 -> 15)! |
| ! ! Source: ECU, different labels ! |
| ! ! NOTE: The shown values are coded as follows: ! |
| ! ! Bit: 15 14 13 12 11 ! Shown value ! |
| ! ! --------------------!---------------- ! |
| ! ! 0 0 0 0 0 ! 0 ! |
| ! ! 0 0 0 0 1 ! 1 ! |
| ! ! 0 0 0 1 0 ! 2 ! |
| ! ! 0 0 0 1 1 ! 3 ! |
| ! ! 0 0 1 0 0 ! 4 ! |
| ! ! 0 0 1 0 1 ! 5 ! |
| ! ! 0 0 1 1 0 ! 6 ! |
| ! ! 0 0 1 1 1 ! 7 ! |
| ! ! 0 1 0 0 0 ! 8 ! |
| ! ! 0 1 0 0 1 ! 9 ! |
| ! ! 0 1 0 1 0 ! A ! |
| ! ! 0 1 0 1 1 ! B ! |
| ! ! 0 1 1 0 0 ! C ! |
| ! ! 0 1 1 0 1 ! D ! |
| ! ! 0 1 1 1 0 ! E ! |
| ! ! 0 1 1 1 1 ! F ! |
| ! ! 1 0 0 0 0 ! G ! |
| ! ! 1 0 0 0 1 ! H ! |
| ! ! 1 0 0 1 0 ! I ! |
| ! ! 1 0 0 1 1 ! J ! |
| ! ! 1 0 1 0 0 ! K ! |
| ! ! 1 0 1 0 1 ! L ! |
| ! ! 1 0 1 1 0 ! M ! |
| ! ! 1 0 1 1 1 ! N ! |
| ! ! 1 1 0 0 0 ! O ! |
| ! ! 1 1 0 0 1 ! P ! |
| ! ! 1 1 0 1 0 ! Q ! |
| ! ! 1 1 0 1 1 ! R ! |
| ! ! 1 1 1 0 0 ! S ! |
| ! ! 1 1 1 0 1 ! T ! |
| ! ! 1 1 1 1 0 ! U ! |
| ! ! 1 1 1 1 1 ! V ! |
| !--------------!------------------------------------------------------! |
| ! REASON ! Reason for Exceedance ! |
| ! XXXXXXXXXX ! DMU ! |
| ! XXXXXXXXXX ! Up to 20 Characters ! |
| ! ! EGT Code: 4110, 4120, 4130 and 4140 ! |
| ! ! TN Code: 4150, 4160, 4170 and 4180 ! |
| ! ! ! |
| ! ! NOTE: If the report was not triggered by a limit ! |
| ! ! exceedance, this field contains blanks. ! |
| !--------------!------------------------------------------------------! |
| ! N1 ! Selected N1 Actual ! |
| ! 9999 ! (0 to 120.0 %rpm) ! |
| ! ! ECU 7C.1.346.01 Engine 1 ! |
| ! ! 7C.2.346.10 Engine 2 ! |
| ! ! Remark: In the report line V3 and V4 the values ! |
| ! ! from the last stable descent are printed. ! |
| ! ! In the report line V5 and V6 the values ! |
| ! ! from the last stable climb are printed. ! |
| !--------------!------------------------------------------------------! |
| ! N1C ! N1 Command ! |
| ! 9999 ! (0 to 120.0 %rpm) ! |
| ! ! ECU 7C.1.341.01 Engine 1 ! |
| ! ! 7C.2.341.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! N2 ! Selected N2 Actual ! |
| ! 9999 ! (0 to 120.0 %rpm) ! |
| ! ! ECU 7C.1.344.01 Engine 1 ! |
| ! ! 7C.2.344.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! EGT ! Selected T495 (Exhaust Gas Temperature) ! |
| ! X999 ! (-55 to 999.9 [C) ! |
| ! ! Negative values are indicated by '-' on the first ! |
| ! ! position. Otherwise the first position is used for ! |
| ! ! the value. ! |
| ! ! ECU 7C.1.345.01 Engine 1 ! |
| ! ! 7C.2.345.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! FF ! Engine Fuel Flow ! |
| ! 9999 ! 0 to 7000 kg/h (0 to 15000 p/h) ! |
| ! ! ECU 7C.1.244.01 Engine 1 ! |
| ! ! 7C.2.244.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! TN ! Nacelle Temperature ! |
| ! X99 ! -55 to 300 degC ! |
| ! ! FWC 26.1.322.01 Engine 1 ! |
| ! ! 26.2.322.01 ! |
| ! ! 26.1.322.10 Engine 2 ! |
| ! ! 26.2.322.10 ! |
| ! ! Negative values are indicated by '-' on the first ! |
| ! ! position. Otherwise the first position is used for ! |
| ! ! the value. ! |
| +---------------------------------------------------------------------+ |
(5) Engine Divergence Report Data Field Description <09> (Engine Type CFMI with Advanced EVMU)
NOTE: Reports that are transmitted from the ACARS system do not have report lines without a line identifier.
| +---------------------------------------------------------------------+ |
| ! Value ! Content Description ! |
| !--------------!------------------------------------------------------! |
| ! ESN ! Engine Serial Number ! |
| ! 999999 ! (000000 to 999999) ! |
| ! ! ECU Engine 1 7C.1.046.01 digit 3, 2, 1 ! |
| ! ! 7C.1.047.01 digit 6, 5, 4 ! |
| ! ! Engine 2 7C.2.046.10 digit 3, 2, 1 ! |
| ! ! 7C.2.047.10 digit 6, 5, 4 ! |
| !--------------!------------------------------------------------------! |
| ! EHRS ! Engine Flight Hours ! |
| ! 99999 ! (00000 to 99999 hours) ! |
| ! ! DMU Engine 1 ! |
| ! ! Engine 2 ! |
| ! ! Remark: Time between "Main (LH and RH) Landing Gear! |
| ! ! Decompressed" and "Main (LH and RH) Landing! |
| ! ! Gear Compressed". The EHRS shall be set to ! |
| ! ! zero if a new ESN is recognized by the DMU.! |
| ! ! It shall be possible to set the EHRS via ! |
| ! ! the MCDU, e.g. if the DMU is changed on the! |
| ! ! a/c. ! |
| !--------------!------------------------------------------------------! |
| ! ERT ! Engine Running Time ! |
| ! 99999 ! (00000 to 65536 hours) ! |
| ! ! ECU 7C.1.050.01 Engine 1 ! |
| ! ! 7C.2.050.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! ECYC ! Engine Cycle ! |
| ! 99999 ! (00000 to 99999) ! |
| ! ! DMU Engine 1 ! |
| ! ! Engine 2 ! |
| ! ! Remark: Each time when flight phase 5 (climb) is ! |
| ! ! reached, the counter shall be incremented ! |
| ! ! by one. The ECYC is set to zero if a new ! |
| ! ! ESN is recognized by the DMU. It shall be ! |
| ! ! possible to set ECYC via the MCDU, if the ! |
| ! ! DMU is changed on the a/c. ! |
| !--------------!------------------------------------------------------! |
| ! AP ! Auto Pilot Status ! |
| ! 99 ! Number of respective status (00 to G8) ! |
| ! ! FMGC 1 and 2 (FGC part) for Auto Pilot AP1 and AP2 ! |
| ! ! ! |
| ! ! Parameter for AP1 ! Parameter for AP2 ! ! |
| ! ! Report Line EC: ! Report Line EE: !Definition: ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! / ! / !No Mode ! |
| ! ! ! !Active ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.11 = 1 ! 01.2.275.00.11 = 1!RUNWAY Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.12 = 1 ! 01.2.275.00.12 = 1!NAV Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.13 = 1 ! 01.2.275.00.13 = 1!LOC CAPTURE ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.14 = 1 ! 01.2.275.00.14 = 1!LOC TRACK ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.15 = 1 ! 01.2.275.00.15 = 1!Roll GO ! |
| ! ! ! !AROUND Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.16 = 1 ! 01.2.275.00.16 = 1!HEADING Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.17 = 1 ! 01.2.275.00.17 = 1!TRACK Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.15 = 1 ! 01.2.274.00.15 = 1!PITCH T/O ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.16 = 1 ! 01.2.274.00.16 = 1!PITCH GA Mode! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.17 = 1 ! 01.2.274.00.17 = 1!V/S Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.18 = 1 ! 01.2.274.00.18 = 1!FPA Mode ! |
| ! ! -------------------!-------------------!-------------! |
| ! ! 01.1.274.00.19 = 1 ! 01.2.274.00.19 = 1!ALT Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.20 = 1 ! 01.2.274.00.20 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.19 = 1 ! 01.2.274.00.19 = 1!ALT ACQ ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.21 = 1 ! 01.2.274.00.21 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.20 = 1 ! 01.2.274.00.20 = 1!G/S TRACK ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.22 = 1 ! 01.2.274.00.22 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.21 = 1 ! 01.2.274.00.21 = 1!G/S CAPTURE ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.22 = 1 ! 01.2.274.00.22 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.23 = 1 ! 01.2.274.00.23 = 1!FINAL DES ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.24 = 1 ! 01.2.274.00.24 = 1!EXPED. Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.146.00.14 = 1 ! 01.2.146.00.14 = 1!LAND TRACK ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!CLB Mode ! |
| ! ! AND ! AND ! ! |
| ! ! ! ! ! ! ! |
| ! ! -------------- ! -------------- ! ! |
| ! ! 01.1.274.00.13 = 0 ! 01.2.274.00.13 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.14 = 0 ! 01.2.274.00.14 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.24 = 0 ! 01.2.274.00.24 = 0! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!DES Mode ! |
| ! ! AND ! AND ! ! |
| ! ! ! ! ! ! ! |
| ! ! -------------- ! -------------- ! ! |
| ! ! 01.1.274.00.13 = 0 ! 01.2.274.00.13 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.14 = 0 ! 01.2.274.00.14 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.24 = 0 ! 01.2.274.00.24 = 0! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!IM. CLIMB ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.13 = 1 ! 01.2.274.00.13 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!IM. DES Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.13 = 1 ! 01.2.274.00.13 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!OPEN CLB ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.14 = 1 ! 01.2.274.00.14 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!OPEN. DES ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.14 = 1 ! 01.2.274.00.14 = 1! ! |
| ! ! ---------------------------------------------------- ! |
| ! ! Auto Pilot Status DMU: ! |
| ! ! Auto Pilot AP1 printed in report line EC ! |
| ! ! Auto Pilot AP2 printed in report line EE ! |
| ! ! Combined Auto Pilot Modes ! |
| ! ! The longitudinal auto pilot mode (1 to G) shall ! |
| ! ! appear on the left position for the AP1 and AP2 print! |
| ! ! format. ! |
| ! ! The lateral auto pilot mode (1 to 8) shall appear on ! |
| ! ! the right position for the AP1 and AP2 print format. ! |
| ! ! In case of a combined auto pilot mode e.g. DES mode ! |
| ! ! and NAV mode are engaged simultaneously, the 'E3' ! |
| ! ! shall appear below AP1 and AP2. ! |
| ! ! XX Auto Pilot Modes: ! |
| ! ! !! ! |
| ! ! !!__Lateral Modes: 0 = NO MODE ! |
| ! ! ! 1 = HEADING ! |
| ! ! ! 2 = TRACK ! |
| ! ! ! 3 = NAV ! |
| ! ! ! 4 = LOC CAPTURE ! |
| ! ! ! 5 = LOCK TRACK ! |
| ! ! ! 6 = LAND TRACK ! |
| ! ! ! 7 = RUNWAY ! |
| ! ! ! 8 = ROLL GO AROUND ! |
| ! ! ! ! |
| ! ! !__Longitudinal Modes: 0 = NO MODE ! |
| ! ! 1 = PITCH G/A ! |
| ! ! 2 = PITCH TO ! |
| ! ! 3 = G/S TRACK ! |
| ! ! 4 = G/S CAPTURE ! |
| ! ! 5 = V/S ! |
| ! ! 6 = FPA ! |
| ! ! 7 = ALT ! |
| ! ! 8 = ALT ACQ ! |
| ! ! 9 = OPEN CLB ! |
| ! ! A = OPEN DES ! |
| ! ! B = IM CLB ! |
| ! ! C = IM DES ! |
| ! ! D = CLB ! |
| ! ! E = DES ! |
| ! ! F = FINAL DES ! |
| ! ! G = EXPEDITE ! |
| !--------------!------------------------------------------------------! |
| ! VSV ! Selected Variable Stator Vane Position ! |
| ! X99 ! (-5.0 to 45.0 deg) ! |
| ! ! Negative values shall be indicated by 'N' on the ! |
| ! ! first position. Otherwise the first position shall ! |
| ! ! be used for the value. ! |
| ! ! ECU 7C.1.072.01 Engine 1 ! |
| ! ! 7C.2.072.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! VBV ! Variable Bleed Valve Position ! |
| ! X99 ! (-9.9 to 40.0 deg) ! |
| ! ! Negative values shall be indicated by 'N' on the ! |
| ! ! first position. Otherwise the first position shall ! |
| ! ! be used for the value. ! |
| ! ! ECU 7C.1.071.01 Engine 1 ! |
| ! ! 7C.2.071.10 Engine 2 ! |
| !--------------! -----------------------------------------------------! |
| ! E ! Divergent Engine Position ! |
| ! 9 ! Number of Engine which has a divergence ! |
| !--------------!------------------------------------------------------! |
| ! DIV ! Parameter Divergency ! |
| ! ! Depending on divergent parameter ! |
| !--------------!------------------------------------------------------! |
| ! REF ! Actual deltaEGT or deltaTNref value of PH5.1 or PH6! |
| ! X999 ! -999 to 999 deg C ! |
| ! ! Negative values shall be indicated by 'N' on the ! |
| ! ! first position. ! |
| !--------------!------------------------------------------------------! |
| ! K ! Actual Value of K in Ph5.1 or PH6 ! |
| ! 99 ! 0 to 99 ! |
| ! ! DMU ! |
| !--------------!------------------------------------------------------! |
| ! ECW1 ! Engine Control Word 1 ! |
| ! XXXXX ! XXXXX Bits HEX ! |
| ! ! !!!!!________14, 13, 12, 11 0..F ! |
| ! ! !!!!_________18, 17, 16, 15 0..F ! |
| ! ! !!!__________22, 21, 20, 19 0..F ! |
| ! ! !!___________26, 25, 24, 23 0..F ! |
| ! ! !____________ 29, 28, 27 0..F ! |
| ! ! Bit Label Parameter Description ! |
| ! ! 11 7C.X.272.XX.19 = 1 Auto Thrust Active ! |
| ! ! 12 7C.X.275.XX.20 = 1 VSV Position Fault ! |
| ! ! 13 SPARE ! |
| ! ! 14 SPARE ! |
| ! ! 15 7C.X.351.XX.29 = 1 Fuel Flow Measurement ! |
| ! ! Invalid ! |
| ! ! 16 7C.X.275.XX.15 = 1 N1/N2 Control Active ! |
| ! ! 17 7C.X.275.XX.26 = 1 Channel A Active ! |
| ! ! 18 7C.X.275.XX.27 = 1 Channel B Active ! |
| ! ! 19 SPARE ! |
| ! ! 20 SPARE ! |
| ! ! 21 SPARE ! |
| ! ! 22 SPARE ! |
| ! ! 23 SPARE ! |
| ! ! 24 SPARE ! |
| ! ! 25 SPARE ! |
| ! ! 26 SPARE ! |
| ! ! 27 SPARE ! |
| ! ! 28 SPARE ! |
| ! ! 29 SPARE ! |
| ! ! The 'X' for the System and SDI definition of the ! |
| ! ! engine parameters shall be as follows: ! |
| ! ! System SDI ! |
| ! ! Engine 1 1 01 ! |
| ! ! Engine 2 2 10 ! |
| !--------------!------------------------------------------------------! |
| ! ECW2 ! Engine Control Word 2 ! |
| ! XXXXX ! XXXXX Bits HEX ! |
| ! ! !!!!!________14, 13, 12, 11 0..F ! |
| ! ! !!!!_________18, 17, 16, 15 0..F ! |
| ! ! !!!__________22, 21, 20, 19 0..F ! |
| ! ! !!___________26, 25, 24, 23 0..F ! |
| ! ! !____________ 29, 28, 27 0..F ! |
| ! ! Bit Label Parameter Description ! |
| ! ! 11 7C.X.272.XX.12 = 1 Bump/Overboost #1 Enable ! |
| ! ! 12 7C.X.272.XX.13 = 1 Bump/Overboost #2 Enable ! |
| ! ! 13 7C.X.272.XX.14 = 1 Bump/Overboost #3 Enable ! |
| ! ! 14 7C.X.272.XX.22 = 1 MTO. GA Limit Mode Select.! |
| ! ! 15 7C.X.272.XX.23 = 1 Flex Take Off Limit Mode ! |
| ! ! Selected ! |
| ! ! 16 SPARE ! |
| ! ! 17 SPARE ! |
| ! ! 18 SPARE ! |
| ! ! 19 SPARE ! |
| ! ! 20 SPARE ! |
| ! ! 21 SPARE ! |
| ! ! 22 SPARE ! |
| ! ! 23 SPARE ! |
| ! ! 24 SPARE ! |
| ! ! 25 SPARE ! |
| ! ! 26 SPARE ! |
| ! ! 27 SPARE ! |
| ! ! 28 SPARE ! |
| ! ! 29 SPARE ! |
| ! ! The 'X' for the System and SDI definition of the ! |
| ! ! engine parameters shall be as follows: ! |
| ! ! System SDI ! |
| ! ! Engine 1 1 01 ! |
| ! ! Engine 2 2 10 ! |
| !--------------!------------------------------------------------------! |
| ! PSEL ! Status of different FADEC sensors ! |
| ! XXXX ! XXXX Label: Selected: ! |
| ! ! !!!!_ 211 TAT (Bit 11 -> 15)! |
| ! ! !!!__ 344 N2 actual (Bit 11 -> 15)! |
| ! ! !!___ 345 EGT (Bit 11 -> 15)! |
| ! ! !____ 346 N1 actual (Bit 11 -> 15)! |
| ! ! Source: ECU, different labels ! |
| ! ! NOTE: The shown values are coded as follows: ! |
| ! ! Bit: 15 14 13 12 11 ! Shown value ! |
| ! ! --------------------!---------------- ! |
| ! ! 0 0 0 0 0 ! 0 ! |
| ! ! 0 0 0 0 1 ! 1 ! |
| ! ! 0 0 0 1 0 ! 2 ! |
| ! ! 0 0 0 1 1 ! 3 ! |
| ! ! 0 0 1 0 0 ! 4 ! |
| ! ! 0 0 1 0 1 ! 5 ! |
| ! ! 0 0 1 1 0 ! 6 ! |
| ! ! 0 0 1 1 1 ! 7 ! |
| ! ! 0 1 0 0 0 ! 8 ! |
| ! ! 0 1 0 0 1 ! 9 ! |
| ! ! 0 1 0 1 0 ! A ! |
| ! ! 0 1 0 1 1 ! B ! |
| ! ! 0 1 1 0 0 ! C ! |
| ! ! 0 1 1 0 1 ! D ! |
| ! ! 0 1 1 1 0 ! E ! |
| ! ! 0 1 1 1 1 ! F ! |
| ! ! 1 0 0 0 0 ! G ! |
| ! ! 1 0 0 0 1 ! H ! |
| ! ! 1 0 0 1 0 ! I ! |
| ! ! 1 0 0 1 1 ! J ! |
| ! ! 1 0 1 0 0 ! K ! |
| ! ! 1 0 1 0 1 ! L ! |
| ! ! 1 0 1 1 0 ! M ! |
| ! ! 1 0 1 1 1 ! N ! |
| ! ! 1 1 0 0 0 ! O ! |
| ! ! 1 1 0 0 1 ! P ! |
| ! ! 1 1 0 1 0 ! Q ! |
| ! ! 1 1 0 1 1 ! R ! |
| ! ! 1 1 1 0 0 ! S ! |
| ! ! 1 1 1 0 1 ! T ! |
| ! ! 1 1 1 1 0 ! U ! |
| ! ! 1 1 1 1 1 ! V ! |
| !--------------!------------------------------------------------------! |
| ! N1 ! Selected N1 Actual ! |
| ! 9999 ! (0 to 120.0 %rpm) ! |
| ! ! ECU 7C.1.346.01 Engine 1 ! |
| ! ! 7C.2.346.10 Engine 2 ! |
| ! ! Remark: In the report line V3 and V4 the values ! |
| ! ! from the last stable descent shall be ! |
| ! ! printed. ! |
| ! ! In the report line V5 and V6 the values ! |
| ! ! from the last stable climb shall be ! |
| ! ! printed. ! |
| !--------------!------------------------------------------------------! |
| ! N1C ! N1 Command ! |
| ! 9999 ! (0 to 120.0 %rpm) ! |
| ! ! ECU 7C.1.341.01 Engine 1 ! |
| ! ! 7C.2.341.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! N2 ! Selected N2 Actual ! |
| ! 9999 ! (0 to 120.0 %rpm) ! |
| ! ! ECU 7C.1.344.01 Engine 1 ! |
| ! ! 7C.2.344.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! EGT ! Selected T495 (Exhaust Gas Temperature) ! |
| ! X999 ! (-55 to 999.9 [C) ! |
| ! ! Negative values shall be indicated by 'N' on the ! |
| ! ! first position. Otherwise the first position shall ! |
| ! ! be used for the value. ! |
| ! ! ECU 7C.1.345.01 Engine 1 ! |
| ! ! 7C.2.345.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! FF ! Engine Fuel Flow ! |
| ! 9999 ! 0 to 7000 kg/h (0 to 15000 p/h) ! |
| ! ! ECU 7C.1.244.01 Engine 1 ! |
| ! ! 7C.2.244.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! TN ! Nacelle Temperature ! |
| ! X99 ! -55 to 300 degC ! |
| ! ! FWC 26.1.322.01 Engine 1 ! |
| ! ! 26.2.322.01 ! |
| ! ! 26.1.322.10 Engine 2 ! |
| ! ! 26.2.322.10 ! |
| ! ! Negative values shall be indicated by 'N' on the ! |
| ! ! first position. Otherwise the first position shall ! |
| ! ! be used for the value. ! |
| !--------------!------------------------------------------------------! |
| ! REASON ! Reason for Exceedance ! |
| ! XXXXXXXXXX ! (Up to 20 characters) ! |
| ! XXXXXXXXXX ! EGT Code: 4110, 4120, 4130 and 4140 ! |
| ! ! TN Code: 4150, 4160, 4170 and 4180 ! |
| ! ! Remark: If the report was not triggered by a limit ! |
| ! ! exceedance this field contain blanks. ! |
| +---------------------------------------------------------------------+ |
(6) Engine Divergence Report Data Field Description <09> (Engine Type CFMI with Advanced EVMU)
NOTE: Reports that are transmitted from the ACARS system do not have report lines without a line identifier.
NOTE: Only the parts of the ENGINE DIVERGENCE REPORT <09> which are not included in the ENGINE CRUISE REPORT <01> are given in the subsequent table.
| +---------------------------------------------------------------------+ |
| ! Value ! Content Description ! |
| !--------------!------------------------------------------------------! |
| ! E ! Divergent Engine Position ! |
| ! 9 ! DMU (No. of engine which has divergence) ! |
| !--------------!------------------------------------------------------! |
| ! DIV ! Parameter Divergency ! |
| ! ! Depending of divergent parameter ! |
| !--------------!------------------------------------------------------! |
| ! REF ! Actual deltaEGT or deltaTNref value of PH5.1 or PH6! |
| ! X999 ! DMU (-999 to 999 deg. C) ! |
| ! ! NOTE: Negative values are shown with an '-' in the ! |
| ! ! first position. ! |
| !--------------!------------------------------------------------------! |
| ! K ! Actual Value of K in PH5.1 or PH6 ! |
| ! 99 ! DMU (0 to 99) ! |
| !--------------!------------------------------------------------------! |
| ! ECW2 ! Engine Control Word 2 ! |
| ! XXXXX ! Each 'X' represents 4 Bits in hexadecimal code of ! |
| ! ! a defined ARINC 429 word: ! |
| ! ! XXXXX Bits HEX ! |
| ! ! !!!!!___________ 14, 13, 12, 11 0...F ! |
| ! ! !!!!____________ 18, 17, 16, 15 0...F ! |
| ! ! !!!_____________ 22, 21, 20, 19 0...F ! |
| ! ! !!______________ 26, 25, 24, 23 0...F ! |
| ! ! !_______________ 29, 28, 27 0...7 ! |
| ! ! Source DMU, got from several ECU labels as given ! |
| ! ! below. For engine 1 and engine 2. ! |
| ! ! The 'X' for the System and SDI definition of the ! |
| ! ! engine parameters: ! |
| ! ! System SDI ! |
| ! ! Engine 1 1 01 ! |
| ! ! Engine 2 2 10 ! |
| ! ! -------------------------------------------- ! |
| ! ! Bit Label Parameter Description ! |
| ! ! 11 7C.X.272.XX.12 = 1 Bump/Overboost #1 enable ! |
| ! ! 12 7C.X.272.XX.13 = 1 Bump/Overboost #2 enable ! |
| ! ! 13 7C.X.272.XX.14 = 1 Bump/Overboost #3 enable ! |
| ! ! 14 7C.X.272.XX.22 = 1 MTO. GA limit mode ! |
| ! ! selected ! |
| ! ! 15 7C.X.272.XX.23 = 1 Flex Take-Off limit mode ! |
| ! ! selected ! |
| ! ! 16 SPARE ! |
| ! ! 17 SPARE ! |
| ! ! 18 SPARE ! |
| ! ! 19 SPARE ! |
| ! ! 20 SPARE ! |
| ! ! 21 SPARE ! |
| ! ! 22 SPARE ! |
| ! ! 23 SPARE ! |
| ! ! 24 SPARE ! |
| ! ! 25 SPARE ! |
| ! ! 26 SPARE ! |
| ! ! 27 SPARE ! |
| ! ! 28 SPARE ! |
| ! ! 29 SPARE ! |
| !--------------!------------------------------------------------------! |
| ! PSEL ! Status of different FADEC sensors ! |
| ! XXXX ! X X X X Label: Selected: (Bit 11 --> 15) ! |
| ! ! ! ! ! !___ 211 TAT ! |
| ! ! ! ! !_____ 344 N2 actual ! |
| ! ! ! !_______ 345 EGT ! |
| ! ! !_________ 346 N1 actual ! |
| ! ! (All labels Bit 11 --> 15) ! |
| ! ! Source: ECU, different labels ! |
| ! ! NOTE: The shown values are coded as follows: ! |
| ! ! Bit: 15 14 13 12 11 ! Shown value ! |
| ! ! --------------------!---------------- ! |
| ! ! 0 0 0 0 0 ! 0 ! |
| ! ! 0 0 0 0 1 ! 1 ! |
| ! ! 0 0 0 1 0 ! 2 ! |
| ! ! 0 0 0 1 1 ! 3 ! |
| ! ! 0 0 1 0 0 ! 4 ! |
| ! ! 0 0 1 0 1 ! 5 ! |
| ! ! 0 0 1 1 0 ! 6 ! |
| ! ! 0 0 1 1 1 ! 7 ! |
| ! ! 0 1 0 0 0 ! 8 ! |
| ! ! 0 1 0 0 1 ! 9 ! |
| ! ! 0 1 0 1 0 ! A ! |
| ! ! 0 1 0 1 1 ! B ! |
| ! ! 0 1 1 0 0 ! C ! |
| ! ! 0 1 1 0 1 ! D ! |
| ! ! 0 1 1 1 0 ! E ! |
| ! ! 0 1 1 1 1 ! F ! |
| ! ! 1 0 0 0 0 ! G ! |
| ! ! 1 0 0 0 1 ! H ! |
| ! ! 1 0 0 1 0 ! I ! |
| ! ! 1 0 0 1 1 ! J ! |
| ! ! 1 0 1 0 0 ! K ! |
| ! ! 1 0 1 0 1 ! L ! |
| ! ! 1 0 1 1 0 ! M ! |
| ! ! 1 0 1 1 1 ! N ! |
| ! ! 1 1 0 0 0 ! O ! |
| ! ! 1 1 0 0 1 ! P ! |
| ! ! 1 1 0 1 0 ! Q ! |
| ! ! 1 1 0 1 1 ! R ! |
| ! ! 1 1 1 0 0 ! S ! |
| ! ! 1 1 1 0 1 ! T ! |
| ! ! 1 1 1 1 0 ! U ! |
| ! ! 1 1 1 1 1 ! V ! |
| ! ! ! |
| !--------------!------------------------------------------------------! |
| ! REASON ! Reason for Exceedance ! |
| ! XXXXXXXXXX ! (Up to 20 characters) ! |
| ! XXXXXXXXXX ! EGT Code: 4110, 4120, 4130 and 4140 ! |
| ! ! TN Code: 4150, 4160, 4170 and 4180 ! |
| ! ! ! |
| ! ! NOTE: If the report was not triggered by a limit ! |
| ! ! exceedance, this field contain blanks. ! |
| +---------------------------------------------------------------------+ |
(7) Engine Divergence Report Data Field Description <09> (Engine Type CFMI with Advanced EVMU)
NOTE: Reports that are transmitted from the ACARS system do not have report lines without a line identifier.
NOTE: Only the parts of the ENGINE DIVERGENCE REPORT <09> which are not included in the ENGINE CRUISE REPORT <01> are given in the subsequent table.
| +---------------------------------------------------------------------+ |
| ! Value ! Content Description ! |
| !--------------!------------------------------------------------------! |
| ! E ! Divergent Engine Position ! |
| ! 9 ! DMU (No. of engine which has divergence) ! |
| !--------------!------------------------------------------------------! |
| ! DIV ! Parameter Divergency ! |
| ! 9999 ! Depending of divergent parameter ! |
| !--------------!------------------------------------------------------! |
| ! REF ! Actual deltaEGTref or deltaTNref value ! |
| ! X999 ! DMU (-999 to 999 °C) ! |
| ! ! NOTE: Negative values are shown with an "N" in the ! |
| ! ! first position. ! |
| !--------------!------------------------------------------------------! |
| ! K ! Actual Value of K ! |
| ! 99 ! DMU (0 to 99) ! |
| !--------------!------------------------------------------------------! |
| ! ECW2 ! Engine Control Word 2 ! |
| ! XXXXX ! Each "X" represents 4 Bits in hexadecimal code of ! |
| ! ! a defined ARINC 429 word: ! |
| ! ! XXXXX Bits HEX ! |
| ! ! !!!!!___________ 14, 13, 12, 11 0...F ! |
| ! ! !!!!____________ 18, 17, 16, 15 0...F ! |
| ! ! !!!_____________ 22, 21, 20, 19 0...F ! |
| ! ! !!______________ 26, 25, 24, 23 0...F ! |
| ! ! !_______________ 29, 28, 27 0...7 ! |
| ! ! Source DMU, got from several ECU labels as given ! |
| ! ! below. For engine 1 and engine 2. ! |
| ! ! The "X" for the System and SDI definition of the ! |
| ! ! engine parameters: ! |
| ! ! System SDI ! |
| ! ! Engine 1 1 01 ! |
| ! ! Engine 2 2 10 ! |
| ! ! ---------------------------------------------- ! |
| ! ! Bit Label Parameter Description ! |
| ! ! 11 7C.X.272.XX.12 = 1 Bump/Overboost #1 Enable ! |
| ! ! 12 7C.X.272.XX.13 = 1 Bump/Overboost #2 Enable ! |
| ! ! 13 7C.X.272.XX.14 = 1 Bump/Overboost #3 Enable ! |
| ! ! 14 7C.X.272.XX.22 = 1 MTO. GA Limit Mode ! |
| ! ! Selected ! |
| ! ! 15 7C.X.272.XX.23 = 1 Flex Take Off Limit Mode ! |
| ! ! Selected ! |
| ! ! 16 SPARE ! |
| ! ! 17 SPARE ! |
| ! ! 18 SPARE ! |
| ! ! 19 SPARE ! |
| ! ! 20 SPARE ! |
| ! ! 21 SPARE ! |
| ! ! 22 SPARE ! |
| ! ! 23 SPARE ! |
| ! ! 24 SPARE ! |
| ! ! 25 SPARE ! |
| ! ! 26 SPARE ! |
| ! ! 27 SPARE ! |
| ! ! 28 SPARE ! |
| ! ! 29 SPARE ! |
| !--------------!------------------------------------------------------! |
| ! PSEL ! Status of different FADEC sensors ! |
| ! XXXX ! X X X X Label: Selected: ! |
| ! ! ! ! ! !___ 211 TAT ! |
| ! ! ! ! !_____ 344 N2 actual ! |
| ! ! ! !_______ 345 EGT ! |
| ! ! !_________ 346 N1 actual ! |
| ! ! (All labels Bit 11 --> 15) ! |
| ! ! Source: ECU, different labels ! |
| ! ! NOTE: The shown values are coded as follows: ! |
| ! ! Bit: 15 14 13 12 11 ! Shown value ! |
| ! ! --------------------!---------------- ! |
| ! ! 0 0 0 0 0 ! 0 ! |
| ! ! 0 0 0 0 1 ! 1 ! |
| ! ! 0 0 0 1 0 ! 2 ! |
| ! ! 0 0 0 1 1 ! 3 ! |
| ! ! 0 0 1 0 0 ! 4 ! |
| ! ! 0 0 1 0 1 ! 5 ! |
| ! ! 0 0 1 1 0 ! 6 ! |
| ! ! 0 0 1 1 1 ! 7 ! |
| ! ! 0 1 0 0 0 ! 8 ! |
| ! ! 0 1 0 0 1 ! 9 ! |
| ! ! 0 1 0 1 0 ! A ! |
| ! ! 0 1 0 1 1 ! B ! |
| ! ! 0 1 1 0 0 ! C ! |
| ! ! 0 1 1 0 1 ! D ! |
| ! ! 0 1 1 1 0 ! E ! |
| ! ! 0 1 1 1 1 ! F ! |
| ! ! 1 0 0 0 0 ! G ! |
| ! ! 1 0 0 0 1 ! H ! |
| ! ! 1 0 0 1 0 ! I ! |
| ! ! 1 0 0 1 1 ! J ! |
| ! ! 1 0 1 0 0 ! K ! |
| ! ! 1 0 1 0 1 ! L ! |
| ! ! 1 0 1 1 0 ! M ! |
| ! ! 1 0 1 1 1 ! N ! |
| ! ! 1 1 0 0 0 ! O ! |
| ! ! 1 1 0 0 1 ! P ! |
| ! ! 1 1 0 1 0 ! Q ! |
| ! ! 1 1 0 1 1 ! R ! |
| ! ! 1 1 1 0 0 ! S ! |
| ! ! 1 1 1 0 1 ! T ! |
| ! ! 1 1 1 1 0 ! U ! |
| ! ! 1 1 1 1 1 ! V ! |
| +---------------------------------------------------------------------+ |
(8) Parameter Logic
| +---------------------------------------------------------------------+ |
| ! Param. ! Print Value (Standard Progr.) ! |
| !--------------!------------------------------------------------------! |
| ! ESN ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! EHRS ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! ERT ! Value at moment of trigger ! |
| !--------------! -----------------------------------------------------! |
| ! ECYC ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! AP ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! E ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! DIV ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! REF ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! K ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! ECW1 ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! ECW2 ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! PSEL ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! N1 ! Snapshot at 2 seconds interval ! |
| !--------------!------------------------------------------------------! |
| ! N1C ! Snapshot at 2 seconds interval ! |
| !--------------!------------------------------------------------------! |
| ! N2 ! Snapshot at 2 seconds interval ! |
| !--------------!------------------------------------------------------! |
| ! EGT ! Snapshot at 2 seconds interval ! |
| !--------------!------------------------------------------------------! |
| ! FF ! Snapshot at 2 seconds interval ! |
| !--------------!------------------------------------------------------! |
| ! TN ! Snapshot at 2 seconds interval ! |
| +---------------------------------------------------------------------+ |
(9) Parameter Logic
| +---------------------------------------------------------------------+ |
| ! Param. ! Print Value (Standard Progr.) ! |
| !--------------!------------------------------------------------------! |
| ! ESN ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! EHRS ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! ERT ! Value at moment of trigger ! |
| !--------------! -----------------------------------------------------! |
| ! ECYC ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! AP ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! VSV ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! VBV ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! E ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! DIV ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! REF ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! K ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! ECW1 ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! ECW2 ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! PSEL ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! N1 ! Snapshot at 2 seconds interval ! |
| !--------------!------------------------------------------------------! |
| ! N1C ! Snapshot at 2 seconds interval ! |
| !--------------!------------------------------------------------------! |
| ! N2 ! Snapshot at 2 seconds interval ! |
| !--------------!------------------------------------------------------! |
| ! EGT ! Snapshot at 2 seconds interval ! |
| !--------------!------------------------------------------------------! |
| ! FF ! Snapshot at 2 seconds interval ! |
| !--------------!------------------------------------------------------! |
| ! TN ! Snapshot at 2 seconds interval ! |
| +---------------------------------------------------------------------+ |
(10) Parameter Logic
| +---------------------------------------------------------------------+ |
| ! Param. ! Print Value (Standard Progr.) ! |
| !--------------!------------------------------------------------------! |
| ! ESN ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! EHRS ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! ERT ! Value at moment of trigger ! |
| !--------------! -----------------------------------------------------! |
| ! ECYC ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! AP ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! VSV ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! VBV ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! E ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! DIV ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! REF ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! K ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! ECW1 ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! ECW2 ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! PSEL ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! N1 ! Snapshot at 2 seconds interval ! |
| !--------------!------------------------------------------------------! |
| ! N1C ! Snapshot at 2 seconds interval ! |
| !--------------!------------------------------------------------------! |
| ! N2 ! Snapshot at 2 seconds interval ! |
| !--------------!------------------------------------------------------! |
| ! EGT ! Snapshot at 2 seconds interval ! |
| !--------------!------------------------------------------------------! |
| ! FF ! Snapshot at 2 seconds interval ! |
| !--------------!------------------------------------------------------! |
| ! TN ! Snapshot at 2 seconds interval ! |
| +---------------------------------------------------------------------+ |
(11) Engine Divergence Report Logic <09> (Engine Type CFMI with Advanced EVMU)
| +----------------------------------------------------------------------+ |
| !Code!Item ! !Progr.!Standard ! |
| ! No.!No. ! Description of Function Item !MCDU !Value or ! |
| ! ! ! !GSE !Table ! |
| !----!------!-----------------------------------------!------!---------! |
| ! !A ! Report Format ! ! ! |
| ! !B ! Parameter Table ! ! ! |
| ! !C ! First three lines of Report ! C ! Blank ! |
| ! !D ! Print-out Rules ! C ! 2 ! |
| ! !E ! Transfer to ACARS MU ! C ! No ! |
| ! !F ! Increment of the report counter if the ! C ! 1 ! |
| ! ! ! report was triggered by a code number ! ! ! |
| ! ! ! > 1000; 1=yes, 0=no ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !1000!1 ! Manual selection via MCDU ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !2000!2 ! Flight phase dependent manual ! ! ! |
| ! ! ! selection via remote print button ! ! ! |
| ! ! ! if programmed. ! ! ! |
| ! !2.1 ! Remote Print Button assignment. ! C ! not ! |
| !----!------!-----------------------------------------!------!---------! |
| !3000!3 ! Programmable Start Logic ! ! ! |
| ! !3.1 ! Trigger condition ! C ! not ! |
| !----!------!-----------------------------------------!------!---------! |
| ! !4 ! If during flight phase climb and cruise ! ! ! |
| ! ! ! (5.1 and 6) the condition as defined ! ! ! |
| ! ! ! under item 4.2 are met the EGT Divergen-! ! ! |
| ! ! ! ce and TN Divergence monitoring ! ! ! |
| ! ! ! functions are performed as defined under! ! ! |
| ! ! ! item 4.3 to 4.4. ! ! ! |
| ! ! ! A divergence report is generated at each! ! ! |
| ! ! ! time when the value of EGTdiv or TNdiv ! ! ! |
| ! ! ! exceeds the defined threshold values ! ! ! |
| ! ! ! defined below. ! ! ! |
| ! !4.1 ! Threshold values: ! ! ! |
| !4110!4.1.1 ! EGTdivT1 limit in C ! C ! limit- ! |
| ! ! ! ! ! table ! |
| !4120!4.1.2 ! EGTdivT2 limit in C ! C ! limit- ! |
| ! ! ! ! ! table ! |
| !4130!4.1.3 ! EGTdivT3 limit in C ! C ! limit- ! |
| ! ! ! ! ! table ! |
| !4140!4.1.4 ! EGTdivT4 limit in C ! C ! limit- ! |
| ! ! ! ! ! table ! |
| !4150!4.1.5 ! TNdivT1 limit in C ! C ! limit- ! |
| ! ! ! ! ! table ! |
| !4160!4.1.6 ! TNdivT2 limit in C ! C ! limit- ! |
| ! ! ! ! ! table ! |
| !4170!4.1.7 ! TNdivT3 limit in C ! C ! limit- ! |
| ! ! ! ! ! table ! |
| !4180!4.1.8 ! TNdivT4 limit in C ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.2 ! Divergence Monitoring Condiitons ! ! ! |
| ! ! ! 1. N1 actual of both engines > N1L1 ! ! ! |
| ! ! ! 2. N1 actual of both engines < N1L2 ! ! ! |
| ! ! ! 3. N1 actual of both engines is within ! ! ! |
| ! ! ! N1L3 of each other. ! ! ! |
| ! ! ! 4. Bleed loads for both engines are ! ! ! |
| ! ! ! symmetrical and crossfeed valve is ! ! ! |
| ! ! ! closed. ! ! ! |
| ! ! ! 5. IVV stable within IVVL, only valid ! ! ! |
| ! ! ! during PH 6. ! ! ! |
| ! ! ! 6. ALT < ALTL, only valid during PH 5.1.! ! ! |
| ! ! ! 7. Delta TAT within TATL. ! ! ! |
| ! ! ! 8. N1rate within N1RL ! ! ! |
| ! ! ! 9. SSM's valid during the whole 'Y09' ! ! ! |
| ! ! ! seconds interval. ! ! ! |
| ! ! !10. Conditions 1-9 TRUE for > 'Y09' sec. ! ! ! |
| ! ! ! ! ! ! |
| ! !4.2.1 ! N1L1 limit in %rpm ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.2.2 ! N1L2 limit in %rpm ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.2.3 ! N1L3 limit in %rpm ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.2.4 ! Symmetrical bleed load: ! ! ! |
| ! ! ! Valve positions LH and RH are identical ! ! ! |
| ! ! ! (mirror image), cross feed valve is ! ! ! |
| ! ! ! closed, APU valve is closed or APU ! ! ! |
| ! ! ! Master Switch is off and Pack Flow is ! ! ! |
| ! ! ! within PFLdelta. ! ! ! |
| ! ! ! APU Master Switch off: ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! param. 29.1.003.11.16 = 0 ! ! ! |
| ! ! ! param. 29.2.003.11.16 = 0 ! ! ! |
| ! ! ! ! ! ! |
| ! !4.2.5 ! IVVL limit in f/min ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.2.6 ! ALTL limit in feet ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.2.7 ! TATL limit in C ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.2.8 ! N1RL limit in %rpm/sec ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.2.9 ! 'Y09' time interval in seconds ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.2.10! PFLdelta limit in kg/sec ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.3 ! EGT Divergence Calculation ! ! ! |
| ! ! ! ! ! ! |
| ! !4.3.1 ! EGTdiv = EGTdiff - deltaEGTref ! ! ! |
| ! ! ! deltaEGTref is calculated if the A/C has! ! ! |
| ! ! ! entered PH 5.1 and PH6 from each flight ! ! ! |
| ! ! ! leg. ! ! ! |
| ! ! ! deltaEGTref PH 5.1 ! ! ! |
| ! ! ! DMU ! ! ! |
| ! ! ! deltaEGTref PH 6 ! ! ! |
| ! ! ! DMU ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! The deltaEGTref is represented in mathe-! ! ! |
| ! ! ! matical form as below: ! ! ! |
| ! !4.3.2 ! CEGT#1 = EGT#1 + (N1#2 - N1#1) * C09.1 ! ! ! |
| ! !4.3.3 ! EGTdiff = CEGT#1 - EGT#2 ! ! ! |
| ! !4.3.4 ! this calculation is done 'M' consecutive! ! ! |
| ! ! ! times once per second i.e. during ! ! ! |
| ! ! ! 10 seconds. ! ! ! |
| ! ! ! ! ! ! |
| ! !4.3.5 ! deltaEGTref = deltaEGTref-1 + 1/K+1 * ! ! ! |
| ! ! ! (deltaEGTm - deltaEGTref-1)! ! ! |
| ! ! ! The calculation deltaEGTref is stored ! ! ! |
| ! ! ! and used for the EGTdiv calculation ! ! ! |
| ! ! ! (item 4.3.1). ! ! ! |
| ! ! ! deltaEGTref-1 is the deltaEGTref value ! ! ! |
| ! ! ! from previous flight. ! ! ! |
| ! ! ! After the deltaEGTref calculation the ! ! ! |
| ! ! ! following EGTdiff calculation is per- ! ! ! |
| ! ! ! formed. ! ! ! |
| ! ! ! CEGT#1 = EGT#1 + (N1#2 - N1#1) * C09.1 ! ! ! |
| ! ! ! EGTdiff= CEGT#1 - EGT#2 ! ! ! |
| ! ! ! EGTdiff is calculated from the actual ! ! ! |
| ! ! ! valve of EGTdiff and the stored delta ! ! ! |
| ! ! ! EGTref value. ! ! ! |
| ! ! ! ! ! ! |
| ! !4.3.6 ! KL limit ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.3.7 ! C09.1 limit for climb PH5 in C/%N1 ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.3.8 ! C09.2 limit for cruise PH6 in C/%N1 ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.3.9 ! M programmed limit ! C ! limit- ! |
| ! ! ! - deltaEGTref is calculated twice per ! ! table ! |
| ! ! ! flight leg independently after enter- ! ! ! |
| ! ! ! ing the PH 5.1 and 6, when conditions ! ! ! |
| ! ! ! 1-10 are met. ! ! ! |
| ! ! ! - deltaEGTref-1 is the deltaEGTref cal- ! ! ! |
| ! ! ! culated in the last flight. ! ! ! |
| ! ! ! - K is incremented by one for each ! ! ! |
| ! ! ! flight leg until KL is reached. Then ! ! ! |
| ! ! ! K = KL is remained as long as: ! ! ! |
| ! ! ! - Engine S/N is not changed ! ! ! |
| ! ! ! - A/C-ID is not changed ! ! ! |
| ! ! ! - The defined values of KL, C09.1,! ! ! |
| ! ! ! C09.2 and the threshold values ! ! ! |
| ! ! ! under item 4.1.1 and 4.1.10 are ! ! ! |
| ! ! ! not changed. ! ! ! |
| ! ! ! - If there is a change as a.m. items ! ! ! |
| ! ! ! then the K and deltaEGTref-1 are set ! ! ! |
| ! ! ! to 0. ! ! ! |
| ! ! ! - K and deltaEGTref-1 values can be ! ! ! |
| ! ! ! reset via MCDU menu. ! ! ! |
| ! ! ! ! ! ! |
| ! !4.3.10! actual K value printed in AIDS report ! ! ! |
| ! ! ! limit list ! ! ! |
| ! !4.3.11! actual EGT ref value for PH 5.1 printed ! ! ! |
| ! ! ! in AIDS report limit list ! ! ! |
| ! !4.3.12! actual EGT ref value for PH 6 printed ! ! ! |
| ! ! ! in AIDS report limit list ! ! ! |
| ! !4.3.13! actual TN ref value for PH 5.1 printed ! ! ! |
| ! ! ! in AIDS report limit list ! ! ! |
| ! !4.3.14! actual TN ref value for PH 6 printed ! ! ! |
| ! ! ! in AIDS report limit list ! ! ! |
| ! !4.4 ! TN Divergence Calculation ! ! ! |
| ! !4.4.1 ! TNdiv = deltaTNdiff - deltaTNref ! ! ! |
| ! ! ! The deltaTNref calculation is represen- ! ! ! |
| ! ! ! ted in mathematical form as below: ! ! ! |
| ! !4.4.2 ! deltaTNdiff = TN#1 - TN#2 ! ! ! |
| ! !4.4.3 ! This calculation is done 'M' consecutive! ! ! |
| ! ! ! times once per socond i.e. during 10 ! ! ! |
| ! ! ! seconds. ! ! ! |
| ! !4.4.4 ! deltaTNdef = deltaTNref-1 + 1/K+1 * ! ! ! |
| ! ! ! (deltaTNm - deltaTNref-1) ! ! ! |
| ! ! ! deltaTNref-1 = deltaTNref from the ! ! ! |
| ! ! ! previous flight leg. ! ! ! |
| ! !4.4.5 ! After the deltaTNref calculation the ! ! ! |
| ! ! ! following TNdiff calculation is perform-! ! ! |
| ! ! ! ed. ! ! ! |
| ! !4.4.6 ! deltaTN = TN#1 - TN#2 ! ! ! |
| ! ! ! deltaTNref PH 5.1 ! ! ! |
| ! ! ! DMU ! ! ! |
| ! ! ! deltaTNref PH 6 ! ! ! |
| ! ! ! DMU ! ! ! |
| ! ! ! The same rules as for EGT divergence are! ! ! |
| ! ! ! applied, except TN#1 is not corrected ! ! ! |
| ! ! ! for deviations in N1. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| ! !5 ! In case of divergence detection and ! ! ! |
| ! ! ! report generation, the search logic for ! ! ! |
| ! ! ! the engine cruise report <01> CODE 7000 ! ! ! |
| ! ! ! for stable frame is started at once. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !8100!8.1 ! ACARS MU uplink request with IMI 'REQ09'! ! ! |
| ! ! ! The report <09> is immediately generated! ! ! |
| ! ! ! and transmitted to the ACARS MU. ! ! ! |
| !----------------------------------------------------------------------! |
| ! A = Programmable by Airbus ! |
| ! C = Programmable by Customer ! |
| +----------------------------------------------------------------------+ |
(12) Engine Divergence Report Logic <09> (Engine Type CFMI with Advanced EVMU)
| +----------------------------------------------------------------------+ |
| !Code!Item ! !Progr.!Standard ! |
| ! No.!No. ! Description of Function Item !MCDU !Value or ! |
| ! ! ! !/GSE !Table TXY! |
| !----!------!-----------------------------------------!------!---------! |
| ! !A ! Report Format ! ! ! |
| ! !B ! Parameter Table ! ! ! |
| ! !C ! First three lines of Report ! C ! Blank ! |
| ! !D ! Print-out Rules ! C ! See ! |
| ! ! ! ! ! separate! |
| ! ! ! ! ! list ! |
| ! !E ! Transfer to ACARS MU ! C ! See ! |
| ! ! ! ! ! separate! |
| ! ! ! ! ! list ! |
| ! !F ! Increment of the report counter if the ! C ! 1 ! |
| ! ! ! report was triggered by a code number ! ! ! |
| ! ! ! > 1000; 1=yes, 0=no ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !1000!1 ! Manual selection via MCDU ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !2000!2 ! Flight phase dependent manual ! ! ! |
| ! ! ! selection via remote print button ! ! ! |
| ! ! ! if programmed. ! ! ! |
| ! !2.1 ! Remote Print Button assignment. ! C ! not ! |
| ! ! ! ! ! assigned! |
| !----!------!-----------------------------------------!------!---------! |
| !3000!3 ! Programmable Start Logic ! ! ! |
| ! !3.1 ! Trigger condition ! C ! not ! |
| ! ! ! ! ! progr. ! |
| !----!------!-----------------------------------------!------!---------! |
| ! !4 ! If during flight phase climb and cruise ! ! ! |
| ! ! ! (5.1 and 6) the conditions as defined ! ! ! |
| ! ! ! under item 4.2 are met the EGT Divergen-! ! ! |
| ! ! ! ce (EGTdiv) and TN Divergence (TNdiv) ! ! ! |
| ! ! ! monitoring functions are performed as ! ! ! |
| ! ! ! defined under item 4.3 to 4.4. ! ! ! |
| ! ! ! A divergence report is generated each ! ! ! |
| ! ! ! time when the value of EGTdiv or TNdiv ! ! ! |
| ! ! ! exceeds the defined threshold values ! ! ! |
| ! ! ! defined below. ! ! ! |
| ! !4.1 ! Threshold values: ! ! ! |
| !4110!4.1.1 ! EGTdivT1 limit in deg C ! C ! limit- ! |
| ! ! ! ! ! table ! |
| !4120!4.1.2 ! EGTdivT2 limit in deg C ! C ! limit- ! |
| ! ! ! ! ! table ! |
| !4130!4.1.3 ! EGTdivT3 limit in deg C ! C ! limit- ! |
| ! ! ! ! ! table ! |
| !4140!4.1.4 ! EGTdivT4 limit in deg C ! C ! limit- ! |
| ! ! ! ! ! table ! |
| !4150!4.1.5 ! TNdivT1 limit in deg C ! C ! limit- ! |
| ! ! ! ! ! table ! |
| !4160!4.1.6 ! TNdivT2 limit in deg C ! C ! limit- ! |
| ! ! ! ! ! table ! |
| !4170!4.1.7 ! TNdivT3 limit in deg C ! C ! limit- ! |
| ! ! ! ! ! table ! |
| !4180!4.1.8 ! TNdivT4 limit in deg C ! C ! limit- ! |
| ! ! ! ! ! table ! |
| !----!------!-----------------------------------------!------!---------! |
| ! !4.2 ! Divergence Monitoring Conditions ! ! ! |
| ! ! ! 1. N1 actual of both engines > N1L1 ! ! ! |
| ! ! ! 2. N1 actual of both engines < N1L2 ! ! ! |
| ! ! ! 3. N1 actual of both engines is within ! ! ! |
| ! ! ! N1L3 of each other. ! ! ! |
| ! ! ! 4. Bleed loads for both engines are ! ! ! |
| ! ! ! symmetrical and cross feed valve is ! ! ! |
| ! ! ! closed. ! ! ! |
| ! ! ! 5. IVV stable within IVVL, only valid ! ! ! |
| ! ! ! during flight phase 6. ! ! ! |
| ! ! ! 6. ALT < ALTL, only valid during flight ! ! ! |
| ! ! ! pahse 5.1. ! ! ! |
| ! ! ! 7. Delta TAT within TATL. ! ! ! |
| ! ! ! 8. N1rate within N1RL ! ! ! |
| ! ! ! 9. SSM's valid during the whole 'Y09' ! ! ! |
| ! ! ! seconds interval. ! ! ! |
| ! ! !10. Conditions 1-9 TRUE for > 'Y09' sec. ! ! ! |
| ! ! ! ! ! ! |
| ! !4.2.1 ! N1L1 limit in %rpm ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.2.2 ! N1L2 limit in %rpm ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.2.3 ! N1L3 limit in %rpm ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.2.4 ! Symmetrical bleed load: ! ! ! |
| ! ! ! Valve positions LH and RH are identical ! ! ! |
| ! ! ! (mirror image), cross feed valve is ! ! ! |
| ! ! ! closed, APU valve is closed or APU ! ! ! |
| ! ! ! Master Switch is off and Pack Flow is ! ! ! |
| ! ! ! within PFLdelta. ! ! ! |
| ! ! ! ! ! ! |
| ! ! !99 1111 1 1111 99 ! ! ! |
| ! ! !__ ____ _ ____ __ ! ! ! |
| ! ! ! ! ! ! ! !____LH Pack Flow ! ! ! |
| ! ! ! ! ! ! !_______RH Valve pos. ! ! ! |
| ! ! ! ! ! !___________Cross feed Valve pos.! ! ! |
| ! ! ! ! !______________LH Valve pos. ! ! ! |
| ! ! ! !__________________LH Pack Flow ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! APU Master Switch off: ! ! ! |
| ! ! ! param. 29.1.003.11.16 = 0 ! ! ! |
| ! ! ! param. 29.2.003.11.16 = 0 ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! PFLdelta =< abs (LH Pack Flow - RH Pack ! ! ! |
| ! ! ! Flow) ! ! ! |
| ! ! ! ! ! ! |
| ! !4.2.5 ! IVVL limit in f/min ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.2.6 ! ALTL limit in feet ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.2.7 ! TATL limit in deg C ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.2.8 ! N1RL limit in %rpm/sec ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.2.9 ! 'Y09' time interval in seconds ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.2.10! PFLdelta limit in kg sec ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.3 ! EGT Divergence Calculation ! ! ! |
| ! ! ! ! ! ! |
| ! !4.3.1 ! EGTdiv = EGTdiff - deltaEGTrefX ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! In PH5.1 deltaEGTrefX is deltaEGTref5. ! ! ! |
| ! ! ! In PH6 deltaEGTrefX is deltaEGTref6. ! ! ! |
| ! ! ! ! ! ! |
| ! !4.3.2 ! CEGT#1 = EGT#1 + (N1#2 - N1#1) * C09.1 ! ! ! |
| ! ! ! (or C09.2).! ! ! |
| ! !4.3.3 ! EGTdiff = CEGT#1 - EGT#2 ! ! ! |
| ! !4.3.4 ! M ! ! ! |
| ! ! ! SIGMA EGTdiff (n) ! ! ! |
| ! ! ! n=1 ! ! ! |
| ! ! ! deltaEGTm = ------------------- ! ! ! |
| ! ! ! M ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! This calculation is done 'M' consecutive! ! ! |
| ! ! ! times once per second i.e. during 10 ! ! ! |
| ! ! ! seconds. ! ! ! |
| ! ! ! ! ! ! |
| ! !4.3.5 ! The calculations 4.3.5.1 and 4.3.5.2 are! ! ! |
| ! ! ! performed when the Divergence Monitoring! ! ! |
| ! ! ! Conditions (Item 4.2) are met. ! ! ! |
| ! ! ! ! ! ! |
| ! !4.3.5.! ! ! ! |
| ! !1 ! deltaEGTref5 is calculated if the A/C ! ! ! |
| ! ! ! has entered flight phase 5.1: ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! deltaEGTref5 = deltaEGTref5old + ! ! ! |
| ! ! ! (deltaEGTm - deltaEGTref5old) ! ! ! |
| ! ! ! ----------------------------- ! ! ! |
| ! ! ! K5 + 1 ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! deltaEGTref5old is the deltaEGTref5 ! ! ! |
| ! ! ! value from previous flight. ! ! ! |
| ! ! ! ! ! ! |
| ! !4.3.5.! ! ! ! |
| ! !2 ! deltaEGTref6 is calculated if the A/C ! ! ! |
| ! ! ! has entered flight phase 6: ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! deltaEGTref6 = deltaEGTref6old + ! ! ! |
| ! ! ! (deltaEGTm - deltaEGTref6old) ! ! ! |
| ! ! ! ----------------------------- ! ! ! |
| ! ! ! K6 + 1 ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! deltaEGTref6old is the deltaEGTref6 ! ! ! |
| ! ! ! value from previous flight. ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! Once the calculation (4.3.5) is ! ! ! |
| ! ! ! performed deltaEGTref5 and deltaEGTref6 ! ! ! |
| ! ! ! are stored and used for the EGTdiv ! ! ! |
| ! ! ! calculation (Item 4.3.1). ! ! ! |
| ! ! ! ! ! ! |
| ! !4.3.6 ! KL limit ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.3.7 ! C09.1 limit for climb PH5.1 in degC/%N1 ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.3.8 ! C09.2 limit for cruise PH6 in degC/%N1 ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.3.9 ! M programmed limit ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! ! ! - K5 and K6 are incremented by one for ! ! ! |
| ! ! ! each flight leg until KL is reached. ! ! ! |
| ! ! ! Then K = KL remains as long as: ! ! ! |
| ! ! ! - Engine S/N is not changed ! ! ! |
| ! ! ! - A/C is not changed ! ! ! |
| ! ! ! - The defined values of KL, C09.1,! ! ! |
| ! ! ! C09.2 and the threshold values ! ! ! |
| ! ! ! under item 4.1.1 and 4.1.1.10 ! ! ! |
| ! ! ! are not changed. ! ! ! |
| ! ! ! - If there is a change as a.m. items ! ! ! |
| ! ! ! then the K5/K6 and deltaEGTref5old and! ! ! |
| ! ! ! deltaEGTref6old will be set to 0. ! ! ! |
| ! ! ! - K5/K6 ,deltaEGTref5old and ! ! ! |
| ! ! ! deltaEGTref6old values can be reset ! ! ! |
| ! ! ! via MCDU menu. ! ! ! |
| ! ! !The K5 value is valid for reference ! ! ! |
| ! ! !calculations in flight phase 5.1., the K6! ! ! |
| ! ! !value is valid for reference calculations! ! ! |
| ! ! !in flight phase 6 during the entire ! ! ! |
| ! ! !flight. ! ! ! |
| ! !4.3.10! actual K5 value printed in AIDS report ! ! ! |
| ! ! ! limit list ! ! ! |
| ! !4.3.11! actual K6 value for PH 6 printed in AIDS! ! ! |
| ! ! ! report limit list ! ! ! |
| ! !4.3.12! actual EGT ref value for PH 5.1 printed ! ! ! |
| ! ! ! in AIDS report limit list ! ! ! |
| ! !4.3.13! actual EGT ref value for PH 6 printed in! ! ! |
| ! ! ! AIDS report limit list ! ! ! |
| ! !4.3.14! actual TN ref value for PH 5.1 printed ! ! ! |
| ! ! ! in AIDS report limit list ! ! ! |
| ! !4.3.15! actual TN ref value for PH 6 printed in ! ! ! |
| ! ! ! AIDS report limit list ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| ! !4.4 ! TN Divergence Calculation ! ! ! |
| ! !4.4.1 ! TNdiv = deltaTNdiff - deltaTNrefX ! ! ! |
| ! ! ! In PH5.1 deltaTNrefX is deltaTNref5 ! ! ! |
| ! ! ! In PH6 deltaTNrefX is deltaTNref6 ! ! ! |
| ! !4.4.2 ! deltaTNdiff = TN#1 - TN#2 ! ! ! |
| ! !4.4.3 ! M ! ! ! |
| ! ! ! SIGMA TNdiff (n) ! ! ! |
| ! ! ! n=1 ! ! ! |
| ! ! ! deltaTNm = ------------------- ! ! ! |
| ! ! ! M ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! This calculation is done 'M' consecutive! ! ! |
| ! ! ! times once per second i.e. during 10 ! ! ! |
| ! ! ! seconds. ! ! ! |
| ! !4.4.4 ! The claculations 4.4.4.1 and 4.4.4.2 are! ! ! |
| ! ! ! performed when the Divergence Monitoring! ! ! |
| ! ! ! Conditions (Item 4.2) are met. ! ! ! |
| ! !4.4.4.! deltaTNref5 is calculated if the A/C has! ! ! |
| ! !1 ! entered flight phase 5.1: ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! deltaTNref5 = deltaTNref5old + ! ! ! |
| ! ! ! (deltaTNm - deltaTNref5old)! ! ! |
| ! ! ! ---------------------------! ! ! |
| ! ! ! K5 + 1 ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! deltaTNref5old = deltaTNref5 from the ! ! ! |
| ! ! ! previous flight leg. ! ! ! |
| ! ! ! ! ! ! |
| ! !4.4.4.! deltaTNref6 is calculated if the A/C has! ! ! |
| ! !1 ! entered flight phase 6: ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! deltaTNref6 = deltaTNref6old + ! ! ! |
| ! ! ! (deltaTNm - deltaTNref6old)! ! ! |
| ! ! ! ---------------------------! ! ! |
| ! ! ! K6 + 1 ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! deltaTNref6old = deltaTNref6 from the ! ! ! |
| ! ! previous flight leg. ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! Once the calculation (4.4.4.) is ! ! ! |
| ! ! ! performed deltaTNref5 and deltaTNref6 ! ! ! |
| ! ! ! are stored and used for the TNdiv ! ! ! |
| ! ! ! calculation (Item 4.4.1): ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! The same rules (analog to 4.3) as for ! ! ! |
| ! ! ! EGT divergence apply except TN#1 is ! ! ! |
| ! ! ! not corrected for deviations in N1. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| ! !5 ! In case of divergence detection and ! ! ! |
| ! ! ! report generation, the search logic for ! ! ! |
| ! ! ! the engine cruise report <01> CODE 7000 ! ! ! |
| ! ! ! for stable frame is started at once. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !8100!8.1 ! ACARS MU uplink request with IMI 'REQ09'! ! ! |
| ! ! ! The report <09> is immediately generated! ! ! |
| ! ! ! and transmitted to the ACARS MU. ! ! ! |
| !----------------------------------------------------------------------! |
| ! A = Programmable by Airbus ! |
| ! C = Programmable by Customer ! |
| +----------------------------------------------------------------------+ |
(13) Engine Divergence Report Logic <09> (Engine Type CFMI with Advanced EVMU)
| +----------------------------------------------------------------------+ |
| !Code!Item ! !Progr.!Standard ! |
| ! No.!No. ! Description of Function Item !MCDU !Value or ! |
| ! ! ! !/GSE !Table TXY! |
| !----!------!-----------------------------------------!------!---------! |
| ! !A ! Report Format ! ! ! |
| ! !B ! Parameter Table ! ! ! |
| ! !C ! First three lines of Report ! C ! Blank ! |
| ! !D ! Print-out Rules ! C ! See ! |
| ! ! ! ! ! separate! |
| ! ! ! ! ! list ! |
| ! !E ! Transfer to ACARS MU ! C ! See ! |
| ! ! ! ! ! separate! |
| ! ! ! ! ! list ! |
| ! !F ! Increment of the report counter if the ! C ! 1 ! |
| ! ! ! report was triggered by a code number ! ! ! |
| ! ! ! > 1000; 1=yes, 0=no ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !1000!1 ! Manual selection via MCDU ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !2000!2 ! Flight phase dependent manual ! ! ! |
| ! ! ! selection via remote print button ! ! ! |
| ! ! ! if programmed. ! ! ! |
| ! !2.1 ! Remote Print Button assignment. ! C ! not ! |
| ! ! ! ! ! assigned! |
| !----!------!-----------------------------------------!------!---------! |
| !3000!3 ! Programmable Start Logic ! ! ! |
| ! !3.1 ! Trigger condition ! C ! not ! |
| ! ! ! ! ! progr. ! |
| !----!------!-----------------------------------------!------!---------! |
| ! !4 ! If during flight phase climb and cruise ! ! ! |
| ! ! ! (5.1 and 6) the conditions as defined ! ! ! |
| ! ! ! under item 4.2 are met the EGT Divergen-! ! ! |
| ! ! ! ce (EGTdiv) and TN Divergence (TNdiv) ! ! ! |
| ! ! ! monitoring functions are performed as ! ! ! |
| ! ! ! defined under item 4.3 to 4.4. ! ! ! |
| ! ! ! A divergence report is generated each ! ! ! |
| ! ! ! time when the value of EGTdiv or TNdiv ! ! ! |
| ! ! ! exceeds the defined threshold values ! ! ! |
| ! ! ! defined below. ! ! ! |
| ! !4.1 ! Threshold values: ! ! ! |
| !4110!4.1.1 ! EGTdivT1 limit in deg C ! C ! limit- ! |
| ! ! ! ! ! table ! |
| !4120!4.1.2 ! EGTdivT2 limit in deg C ! C ! limit- ! |
| ! ! ! ! ! table ! |
| !4130!4.1.3 ! EGTdivT3 limit in deg C ! C ! limit- ! |
| ! ! ! ! ! table ! |
| !4140!4.1.4 ! EGTdivT4 limit in deg C ! C ! limit- ! |
| ! ! ! ! ! table ! |
| !4150!4.1.5 ! TNdivT1 limit in deg C ! C ! limit- ! |
| ! ! ! ! ! table ! |
| !4160!4.1.6 ! TNdivT2 limit in deg C ! C ! limit- ! |
| ! ! ! ! ! table ! |
| !4170!4.1.7 ! TNdivT3 limit in deg C ! C ! limit- ! |
| ! ! ! ! ! table ! |
| !4180!4.1.8 ! TNdivT4 limit in deg C ! C ! limit- ! |
| ! ! ! ! ! table ! |
| !----!------!-----------------------------------------!------!---------! |
| ! !4.2 ! Divergence Monitoring Conditions ! ! ! |
| ! ! ! 1. N1 actual of both engines > N1L1 ! ! ! |
| ! ! ! 2. N1 actual of both engines < N1L2 ! ! ! |
| ! ! ! 3. N1 actual of both engines is within ! ! ! |
| ! ! ! N1L3 of each other. ! ! ! |
| ! ! ! 4. Bleed loads for both engines are ! ! ! |
| ! ! ! symmetrical and cross feed valve is ! ! ! |
| ! ! ! closed. ! ! ! |
| ! ! ! 5. IVV stable within IVVL, only valid ! ! ! |
| ! ! ! during flight phase 6. ! ! ! |
| ! ! ! 6. ALT < ALTL, only valid during flight ! ! ! |
| ! ! ! pahse 5.1. ! ! ! |
| ! ! ! 7. Delta TAT within TATL. ! ! ! |
| ! ! ! 8. N1rate within N1RL ! ! ! |
| ! ! ! 9. SSM's valid during the whole 'Y09' ! ! ! |
| ! ! ! seconds interval. ! ! ! |
| ! ! !10. Conditions 1-9 TRUE for > 'Y09' sec. ! ! ! |
| ! ! ! ! ! ! |
| ! !4.2.1 ! N1L1 limit in %rpm ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.2.2 ! N1L2 limit in %rpm ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.2.3 ! N1L3 limit in %rpm ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.2.4 ! Symmetrical bleed load: ! ! ! |
| ! ! ! Valve positions LH and RH are identical ! ! ! |
| ! ! ! (mirror image), cross feed valve is ! ! ! |
| ! ! ! closed, APU valve is closed or APU ! ! ! |
| ! ! ! Master Switch is off and Pack Flow is ! ! ! |
| ! ! ! within PFLdelta. ! ! ! |
| ! ! ! ! ! ! |
| ! ! !99 1111 1 1111 99 ! ! ! |
| ! ! !__ ____ _ ____ __ ! ! ! |
| ! ! ! ! ! ! ! !____LH Pack Flow ! ! ! |
| ! ! ! ! ! ! !_______RH Valve pos. ! ! ! |
| ! ! ! ! ! !___________Cross feed Valve pos.! ! ! |
| ! ! ! ! !______________LH Valve pos. ! ! ! |
| ! ! ! !__________________LH Pack Flow ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! APU Master Switch off: ! ! ! |
| ! ! ! param. 29.1.003.11.16 = 0 ! ! ! |
| ! ! ! param. 29.2.003.11.16 = 0 ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! PFLdelta =< abs (LH Pack Flow - RH Pack ! ! ! |
| ! ! ! Flow) ! ! ! |
| ! ! ! ! ! ! |
| ! !4.2.5 ! IVVL limit in f/min ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.2.6 ! ALTL limit in feet ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.2.7 ! TATL limit in deg C ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.2.8 ! N1RL limit in %rpm/sec ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.2.9 ! 'Y09' time interval in seconds ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.2.10! PFLdelta limit in kg sec ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.3 ! EGT Divergence Calculation ! ! ! |
| ! ! ! ! ! ! |
| ! !4.3.1 ! EGTdiv = EGTdiff - deltaEGTrefX ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! In PH5.1 deltaEGTrefX is deltaEGTref5. ! ! ! |
| ! ! ! In PH6 deltaEGTrefX is deltaEGTref6. ! ! ! |
| ! ! ! ! ! ! |
| ! !4.3.2 ! CEGT#1 = EGT#1 + (N1#2 - N1#1) * C09.1 ! ! ! |
| ! ! ! (or C09.2).! ! ! |
| ! !4.3.3 ! EGTdiff = CEGT#1 - EGT#2 ! ! ! |
| ! !4.3.4 ! M ! ! ! |
| ! ! ! SIGMA EGTdiff (n) ! ! ! |
| ! ! ! n=1 ! ! ! |
| ! ! ! deltaEGTm = ------------------- ! ! ! |
| ! ! ! M ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! This calculation is done 'M' consecutive! ! ! |
| ! ! ! times once per second i.e. during 10 ! ! ! |
| ! ! ! seconds. ! ! ! |
| ! ! ! ! ! ! |
| ! !4.3.5 ! The calculations 4.3.5.1 and 4.3.5.2 are! ! ! |
| ! ! ! performed when the Divergence Monitoring! ! ! |
| ! ! ! Conditions (Item 4.2) are met. ! ! ! |
| ! ! ! ! ! ! |
| ! !4.3.5.! ! ! ! |
| ! !1 ! deltaEGTref5 is calculated if the A/C ! ! ! |
| ! ! ! has entered flight phase 5.1: ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! deltaEGTref5 = deltaEGTref5old + ! ! ! |
| ! ! ! (deltaEGTm - deltaEGTref5old) ! ! ! |
| ! ! ! ----------------------------- ! ! ! |
| ! ! ! K5 + 1 ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! deltaEGTref5old is the deltaEGTref5 ! ! ! |
| ! ! ! value from previous flight. ! ! ! |
| ! ! ! ! ! ! |
| ! !4.3.5.! ! ! ! |
| ! !2 ! deltaEGTref6 is calculated if the A/C ! ! ! |
| ! ! ! has entered flight phase 6: ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! deltaEGTref6 = deltaEGTref6old + ! ! ! |
| ! ! ! (deltaEGTm - deltaEGTref6old) ! ! ! |
| ! ! ! ----------------------------- ! ! ! |
| ! ! ! K6 + 1 ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! deltaEGTref6old is the deltaEGTref6 ! ! ! |
| ! ! ! value from previous flight. ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! Once the calculation (4.3.5) is ! ! ! |
| ! ! ! performed deltaEGTref5 and deltaEGTref6 ! ! ! |
| ! ! ! are stored and used for the EGTdiv ! ! ! |
| ! ! ! calculation (Item 4.3.1). ! ! ! |
| ! ! ! ! ! ! |
| ! !4.3.6 ! KL limit ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.3.7 ! C09.1 limit for climb PH5.1 in degC/%N1 ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.3.8 ! C09.2 limit for cruise PH6 in degC/%N1 ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.3.9 ! M programmed limit ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! ! ! - K5 and K6 are incremented by one for ! ! ! |
| ! ! ! each flight leg until KL is reached. ! ! ! |
| ! ! ! Then K = KL remains as long as: ! ! ! |
| ! ! ! - Engine S/N is not changed ! ! ! |
| ! ! ! - A/C is not changed ! ! ! |
| ! ! ! - The defined values of KL, C09.1,! ! ! |
| ! ! ! C09.2 and the threshold values ! ! ! |
| ! ! ! under item 4.1.1 and 4.1.1.10 ! ! ! |
| ! ! ! are not changed. ! ! ! |
| ! ! ! - If there is a change as a.m. items ! ! ! |
| ! ! ! then the K5/K6 and deltaEGTref5old and! ! ! |
| ! ! ! deltaEGTref6old will be set to 0. ! ! ! |
| ! ! ! - K5/K6 ,deltaEGTref5old and ! ! ! |
| ! ! ! deltaEGTref6old values can be reset ! ! ! |
| ! ! ! via MCDU menu. ! ! ! |
| ! ! !The K5 value is valid for reference ! ! ! |
| ! ! !calculations in flight phase 5.1., the K6! ! ! |
| ! ! !value is valid for reference calculations! ! ! |
| ! ! !in flight phase 6 during the entire ! ! ! |
| ! ! !flight. ! ! ! |
| ! !4.3.10! actual K5 value for PH5.1 printed in ! ! ! |
| ! ! ! AIDS report limit list ! ! ! |
| ! !4.3.11! actual K6 value for PH 6 printed in AIDS! ! ! |
| ! ! ! report limit list ! ! ! |
| ! !4.3.12! actual EGT ref value for PH 5.1 printed ! ! ! |
| ! ! ! in AIDS report limit list ! ! ! |
| ! !4.3.13! actual EGT ref value for PH 6 printed in! ! ! |
| ! ! ! AIDS report limit list ! ! ! |
| ! !4.3.14! actual TN ref value for PH 5.1 printed ! ! ! |
| ! ! ! in AIDS report limit list ! ! ! |
| ! !4.3.15! actual TN ref value for PH 6 printed in ! ! ! |
| ! ! ! AIDS report limit list ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| ! !4.4 ! TN Divergence Calculation ! ! ! |
| ! !4.4.1 ! TNdiv = deltaTNdiff - deltaTNrefX ! ! ! |
| ! ! ! In PH5.1 deltaTNrefX is deltaTNref5 ! ! ! |
| ! ! ! In PH6 deltaTNrefX is deltaTNref6 ! ! ! |
| ! !4.4.2 ! deltaTNdiff = TN#1 - TN#2 ! ! ! |
| ! !4.4.3 ! M ! ! ! |
| ! ! ! SIGMA TNdiff (n) ! ! ! |
| ! ! ! n=1 ! ! ! |
| ! ! ! deltaTNm = ------------------- ! ! ! |
| ! ! ! M ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! This calculation is done 'M' consecutive! ! ! |
| ! ! ! times once per second i.e. during 10 ! ! ! |
| ! ! ! seconds. ! ! ! |
| ! !4.4.4 ! The claculations 4.4.4.1 and 4.4.4.2 are! ! ! |
| ! ! ! performed when the Divergence Monitoring! ! ! |
| ! ! ! Conditions (Item 4.2) are met. ! ! ! |
| ! !4.4.4.! deltaTNref5 is calculated if the A/C has! ! ! |
| ! !1 ! entered flight phase 5.1: ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! deltaTNref5 = deltaTNref5old + ! ! ! |
| ! ! ! (deltaTNm - deltaTNref5old)! ! ! |
| ! ! ! ---------------------------! ! ! |
| ! ! ! K5 + 1 ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! deltaTNref5old = deltaTNref5 from the ! ! ! |
| ! ! ! previous flight leg. ! ! ! |
| ! ! ! ! ! ! |
| ! !4.4.4.! deltaTNref6 is calculated if the A/C has! ! ! |
| ! !1 ! entered flight phase 6: ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! deltaTNref6 = deltaTNref6old + ! ! ! |
| ! ! ! (deltaTNm - deltaTNref6old)! ! ! |
| ! ! ! ---------------------------! ! ! |
| ! ! ! K6 + 1 ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! deltaTNref6old = deltaTNref6 from the ! ! ! |
| ! ! ! previous flight leg. ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! Once the calculation (4.4.4.) is ! ! ! |
| ! ! ! performed deltaTNref5 and deltaTNref6 ! ! ! |
| ! ! ! are stored and used for the TNdiv ! ! ! |
| ! ! ! calculation (Item 4.4.1): ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! The same rules (analog to 4.3) as for ! ! ! |
| ! ! ! EGT divergence apply except TN#1 is ! ! ! |
| ! ! ! not corrected for deviations in N1. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| ! !5 ! In case of divergence detection and ! ! ! |
| ! ! ! report generation, the search logic for ! ! ! |
| ! ! ! the engine cruise report <01> CODE 7000 ! ! ! |
| ! ! ! for stable frame is started at once. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !8100!8.1 ! ACARS MU uplink request with IMI 'REQ09'! ! ! |
| ! ! ! The report <09> is immediately generated! ! ! |
| ! ! ! and transmitted to the ACARS MU. ! ! ! |
| !----------------------------------------------------------------------! |
| ! A = Programmable by Airbus ! |
| ! C = Programmable by Customer ! |
| +----------------------------------------------------------------------+ |
(14) Engine Divergence Report Logic <09> (Engine Type CFMI with Advanced EVMU)
| +----------------------------------------------------------------------+ |
| !Code!Item ! !Progr.!Standard ! |
| ! No.!No. ! Description of Function Item !------!Value or ! |
| ! ! ! !MCDU /!Table TXY! |
| ! ! ! !GSE ! ! |
| !----!------!-----------------------------------------!------!---------! |
| ! !A ! Report Format ! ! ! |
| ! !A.1 ! "R009RLID" Report Layout Identifier ! ! 01 ! |
| ! ! ! (for ACARS header) ! ! ! |
| ! !A.2 ! "R009RLIS" Report Layout Issue ! ! 01 ! |
| ! ! ! (for acars header) ! ! ! |
| ! !B ! Parameter Table ! ! ! |
| ! !C ! First three lines of Report ! C ! Blank ! |
| ! !D ! Print-out Rules ! C ! See ! |
| ! ! ! ! ! separate! |
| ! ! ! ! ! list ! |
| ! !E ! Transfer to ACARS MU ! C ! See ! |
| ! ! ! ! ! separate! |
| ! ! ! ! ! list ! |
| ! !F ! Increment of the report counter if the ! C ! 1 ! |
| ! ! ! report was triggered by a code number ! ! ! |
| ! ! ! > 1000; 1=yes, 0=no ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !1000!1 ! Manual selection through MCDU ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !2000!2 ! Flight phase dependent manual ! C ! ! |
| ! ! ! selection through remote print button ! ! ! |
| ! ! ! if programmed. ! ! ! |
| ! !2.1 ! Remote Print Button assignment. ! C ! not ! |
| ! ! ! ! ! assigned! |
| !----!------!-----------------------------------------!------!---------! |
| !3000!3 ! Programmable Start Logic ! ! ! |
| ! !3.1 ! Trigger condition ! C ! not ! |
| ! ! ! ! ! progr. ! |
| !----!------!-----------------------------------------!------!---------! |
| ! !4 ! If during flight phase climb and cruise ! ! ! |
| ! ! ! (5.1 and 6) the conditions as defined ! ! ! |
| ! ! ! under item 4.2 are met the EGT Divergen-! ! ! |
| ! ! ! ce (EGTdiv) and TN Divergence (TNdiv) ! ! ! |
| ! ! ! monitoring functions are performed as ! ! ! |
| ! ! ! defined under item 4.3 to 4.4. ! ! ! |
| ! ! ! A divergence report is generated each ! ! ! |
| ! ! ! time when the value of EGTdiv or TNdiv ! ! ! |
| ! ! ! exceeds the defined threshold values ! ! ! |
| ! ! ! defined below. ! ! ! |
| ! !4.1 ! Threshold values: ! ! ! |
| !4110!4.1.1 ! EGTdivT1 limit in Degrees C ! C ! limit- ! |
| ! ! ! ! ! table ! |
| !4120!4.1.2 ! EGTdivT2 limit in Degrees C ! C ! limit- ! |
| ! ! ! ! ! table ! |
| !4130!4.1.3 ! EGTdivT3 limit in Degrees C ! C ! limit- ! |
| ! ! ! ! ! table ! |
| !4140!4.1.4 ! EGTdivT4 limit in Degrees C ! C ! limit- ! |
| ! ! ! ! ! table ! |
| !4150!4.1.5 ! TNdivT1 limit in Degrees C ! C ! limit- ! |
| ! ! ! ! ! table ! |
| !4160!4.1.6 ! TNdivT2 limit in Degrees C ! C ! limit- ! |
| ! ! ! ! ! table ! |
| !4170!4.1.7 ! TNdivT3 limit in Degrees C ! C ! limit- ! |
| ! ! ! ! ! table ! |
| !4180!4.1.8 ! TNdivT4 limit in Degrees C ! C ! limit- ! |
| ! ! ! ! ! table ! |
| !----!------!-----------------------------------------!------!---------! |
| ! !4.2 ! Divergence Monitoring Conditions ! ! ! |
| ! ! ! 1. N1 actual of both engines > N1L1 ! ! ! |
| ! ! ! 2. N1 actual of both engines < N1L2 ! ! ! |
| ! ! ! 3. N1 actual of both engines is within ! ! ! |
| ! ! ! N1L3 of each other. ! ! ! |
| ! ! ! 4. Bleed loads for both engines are ! ! ! |
| ! ! ! symmetrical and cross feed valve is ! ! ! |
| ! ! ! closed. ! ! ! |
| ! ! ! 5. IVV stable within IVVL, only valid ! ! ! |
| ! ! ! during flight phase 6. ! ! ! |
| ! ! ! 6. ALT < ALTL, only valid during flight ! ! ! |
| ! ! ! pahse 5.1. ! ! ! |
| ! ! ! 7. Delta TAT within TATL. ! ! ! |
| ! ! ! The Delta TAT is the difference of ! ! ! |
| ! ! ! TATmin (during last Y09 seconds) and the! ! ! |
| ! ! ! TATmax (during the last Y09 seconds). ! ! ! |
| ! ! ! 8. N1rate within N1RL ! ! ! |
| ! ! ! The N1rate is computed by checking the ! ! ! |
| ! ! ! difference between two samples at 1Hz. ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! 9. SSM's valid during the whole "Y09" ! ! ! |
| ! ! ! seconds interval. ! ! ! |
| ! ! !10. Conditions 1-9 TRUE for > "Y09" sec. ! ! ! |
| ! ! ! ! ! ! |
| ! !4.2.1 ! N1L1 limit in %rpm ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.2.2 ! N1L2 limit in %rpm ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.2.3 ! N1L3 limit in %rpm ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.2.4 ! Symmetrical bleed load: ! ! ! |
| ! ! ! ( (Valve positions LH and RH are identi-! ! ! |
| ! ! ! cal(mirror image)) ! ! ! |
| ! ! ! AND ! ! ! |
| ! ! ! cross feed valve closed ! ! ! |
| ! ! ! AND ! ! ! |
| ! ! ! (APU valve is closed OR APU Master ! ! ! |
| ! ! ! Switch off) ! ! ! |
| ! ! ! AND ! ! ! |
| ! ! ! Pack Flow within PFLdelta) ! ! ! |
| ! ! ! ! ! ! |
| ! ! !99 1111 1 1111 99 ! ! ! |
| ! ! !__ ____ _ ____ __ ! ! ! |
| ! ! ! ! ! ! ! !____RH Pack Flow ! ! ! |
| ! ! ! ! ! ! !_______RH Valve pos. ! ! ! |
| ! ! ! ! ! !___________Cross feed Valve pos.! ! ! |
| ! ! ! ! !______________LH Valve pos. ! ! ! |
| ! ! ! !__________________LH Pack Flow ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! APU Master Switch off: ! ! ! |
| ! ! ! param. 29.1.002.11.16 = 0 ! ! ! |
| ! ! ! param. 29.2.002.11.16 = 0# ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! PFLdelta =< abs (LH Pack Flow - RH Pack ! ! ! |
| ! ! ! Flow) ! ! ! |
| ! ! ! ! ! ! |
| ! !4.2.5 ! IVVL limit in f/min ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.2.6 ! ALTL limit in feet ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.2.7 ! TATL limit in Degrees C ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.2.8 ! N1RL limit in %rpm/sec ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.2.9 ! "Y09" time interval in seconds ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.2.10! PFLdelta limit in kg sec ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.3 ! EGT Divergence Calculation ! ! ! |
| ! ! ! ! ! ! |
| ! !4.3.1 ! EGTdiv = EGTdiff - deltaEGTrefX ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! In PH5.1 deltaEGTrefX is deltaEGTref5. ! ! ! |
| ! ! ! In PH6 deltaEGTrefX is deltaEGTref6. ! ! ! |
| ! ! ! ! ! ! |
| ! !4.3.2 ! CEGT#1 = EGT#1 + (N1#2 - N1#1) * C09.1 ! ! ! |
| ! ! ! (or C09.2).! ! ! |
| ! !4.3.3 ! EGTdiff = CEGT#1 - EGT#2 ! ! ! |
| ! !4.3.4 ! M ! ! ! |
| ! ! ! SIGMA EGTdiff (n) ! ! ! |
| ! ! ! n=1 ! ! ! |
| ! ! ! deltaEGTm = ------------------- ! ! ! |
| ! ! ! M ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! This calculation is done "M" consecutive! ! ! |
| ! ! ! times once per second i.e. during 10 ! ! ! |
| ! ! ! seconds. ! ! ! |
| ! ! ! ! ! ! |
| ! !4.3.5 ! The calculations 4.3.5.1 and 4.3.5.2 are! ! ! |
| ! ! ! performed when the Divergence Monitoring! ! ! |
| ! ! ! Conditions (Item 4.2) are met. ! ! ! |
| ! ! ! ! ! ! |
| ! !4.3.5.! ! ! ! |
| ! !1 ! deltaEGTref5 is calculated if the A/C ! ! ! |
| ! ! ! has entered flight phase 5.1: ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! deltaEGTref5 = deltaEGTref5old + ! ! ! |
| ! ! ! (deltaEGTm - deltaEGTref5old) ! ! ! |
| ! ! ! ----------------------------- ! ! ! |
| ! ! ! K5 + 1 ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! deltaEGTref5old is the deltaEGTref5 ! ! ! |
| ! ! ! value from previous flight. ! ! ! |
| ! ! ! ! ! ! |
| ! !4.3.5.! ! ! ! |
| ! !2 ! deltaEGTref6 is calculated if the A/C ! ! ! |
| ! ! ! has entered flight phase 6: ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! deltaEGTref6 = deltaEGTref6old + ! ! ! |
| ! ! ! (deltaEGTm - deltaEGTref6old) ! ! ! |
| ! ! ! ----------------------------- ! ! ! |
| ! ! ! K6 + 1 ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! deltaEGTref6old is the deltaEGTref6 ! ! ! |
| ! ! ! value from previous flight. ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! Once the calculation (4.3.5) is ! ! ! |
| ! ! ! performed deltaEGTref5 and deltaEGTref6 ! ! ! |
| ! ! ! are stored and used for the EGTdiv ! ! ! |
| ! ! ! calculation (Item 4.3.1). ! ! ! |
| ! ! ! ! ! ! |
| ! !4.3.6 ! KL limit ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.3.7 ! C09.1 limit for climb PH5.1 in degC/%N1 ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.3.8 ! C09.2 limit for cruise PH6 in degC/%N1 ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.3.9 ! M programmed limit ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! ! ! - K5 and K6 are incremented by one for ! ! ! |
| ! ! ! each flight leg until KL is reached. ! ! ! |
| ! ! ! Then K = KL remains as long as: ! ! ! |
| ! ! ! - Engine S/N is not changed ! ! ! |
| ! ! ! - A/C is not changed ! ! ! |
| ! ! ! - The defined values of KL, C09.1,! ! ! |
| ! ! ! C09.2 and the threshold values ! ! ! |
| ! ! ! under item 4.1.1 and 4.1.1.10 ! ! ! |
| ! ! ! are not changed. ! ! ! |
| ! ! ! - If there is a change as a.m. items ! ! ! |
| ! ! ! then the K5/K6 and deltaEGTref5old and! ! ! |
| ! ! ! deltaEGTref6old will be set to 0. ! ! ! |
| ! ! ! - K5/K6 ,deltaEGTref5old and ! ! ! |
| ! ! ! deltaEGTref6old values can be reset ! ! ! |
| ! ! ! through MCDU menu. ! ! ! |
| ! ! !The K5 value is valid for reference ! ! ! |
| ! ! !calculations in flight phase 5.1., the K6! ! ! |
| ! ! !value is valid for reference calculations! ! ! |
| ! ! !in flight phase 6 during the entire ! ! ! |
| ! ! !flight. ! ! ! |
| ! !4.3.10! actual K5 value for PH5.1 printed in ! ! ! |
| ! ! ! AIDS report limit list ! ! ! |
| ! !4.3.11! actual K6 value for PH 6 printed in AIDS! ! ! |
| ! ! ! report limit list ! ! ! |
| ! !4.3.12! actual EGT ref value for PH 5.1 printed ! ! ! |
| ! ! ! in AIDS report limit list ! ! ! |
| ! !4.3.13! actual EGT ref value for PH 6 printed in! ! ! |
| ! ! ! AIDS report limit list ! ! ! |
| ! !4.3.14! actual TN ref value for PH 5.1 printed ! ! ! |
| ! ! ! in AIDS report limit list ! ! ! |
| ! !4.3.15! actual TN ref value for PH 6 printed in ! ! ! |
| ! ! ! AIDS report limit list ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| ! !4.4 ! TN Divergence Calculation ! ! ! |
| ! !4.4.1 ! TNdiv = deltaTNdiff - deltaTNrefX ! ! ! |
| ! ! ! In PH5.1 deltaTNrefX is deltaTNref5 ! ! ! |
| ! ! ! In PH6 deltaTNrefX is deltaTNref6 ! ! ! |
| ! !4.4.2 ! deltaTNdiff = TN#1 - TN#2 ! ! ! |
| ! !4.4.3 ! M ! ! ! |
| ! ! ! SIGMA TNdiff (n) ! ! ! |
| ! ! ! n=1 ! ! ! |
| ! ! ! deltaTNm = ------------------- ! ! ! |
| ! ! ! M ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! This calculation is done 'M' consecutive! ! ! |
| ! ! ! times once per second i.e. during 10 ! ! ! |
| ! ! ! seconds. ! ! ! |
| ! !4.4.4 ! The calculations 4.4.4.1 and 4.4.4.2 are! ! ! |
| ! ! ! performed when the Divergence Monitoring! ! ! |
| ! ! ! Conditions (Item 4.2) are met. ! ! ! |
| ! !4.4.4.! deltaTNref5 is calculated if the A/C has! ! ! |
| ! !1 ! entered flight phase 5.1: ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! deltaTNref5 = deltaTNref5old + ! ! ! |
| ! ! ! (deltaTNm - deltaTNref5old)! ! ! |
| ! ! ! ---------------------------! ! ! |
| ! ! ! K5 + 1 ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! deltaTNref5old = deltaTNref5 from the ! ! ! |
| ! ! ! previous flight leg. ! ! ! |
| ! ! ! ! ! ! |
| ! !4.4.4.! deltaTNref6 is calculated if the A/C has! ! ! |
| ! !2 ! entered flight phase 6: ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! deltaTNref6 = deltaTNref6old + ! ! ! |
| ! ! ! (deltaTNm - deltaTNref6old)! ! ! |
| ! ! ! ---------------------------! ! ! |
| ! ! ! K6 + 1 ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! deltaTNref6old = deltaTNref6 from the ! ! ! |
| ! ! ! previous flight leg. ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! Once the calculation (4.4.4.) is ! ! ! |
| ! ! ! performed deltaTNref5 and deltaTNref6 ! ! ! |
| ! ! ! are stored and used for the TNdiv ! ! ! |
| ! ! ! calculation (Item 4.4.1): ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! The same rules (analog to 4.3) as for ! ! ! |
| ! ! ! EGT divergence apply except TN#1 is ! ! ! |
| ! ! ! not corrected for deviations in N1. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| ! !5 ! In case of divergence detection and ! ! ! |
| ! ! ! report generation, the search logic for ! ! ! |
| ! ! ! the engine cruise report <01> CODE 7000 ! ! ! |
| ! ! ! for stable frame is started at once. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !8100!8.1 ! ACARS MU uplink request with IMI "REQ09"! ! ! |
| ! ! ! The report <09> is immediately generated! ! ! |
| ! ! ! and transmitted to the ACARS MU. ! ! ! |
| !----------------------------------------------------------------------! |
| ! A = Programmable by Airbus ! |
| ! C = Programmable by Customer ! |
| +----------------------------------------------------------------------+ |
(15) Engine Divergence Report Logic <09> (Engine Type CFMI with Advanced EVMU)
| +----------------------------------------------------------------------+ |
| !Code!Item ! !Progr.!Standard ! |
| ! No.!No. ! Description of Function Item !MCDU !Value or ! |
| ! ! ! !/GSE !Table TXY! |
| !----!------!-----------------------------------------!------!---------! |
| ! !A ! Report Format ! ! ! |
| ! !B ! Parameter Table ! ! ! |
| ! !C ! First three lines of Report ! C ! Blank ! |
| ! !D ! Print-out Rules ! C ! See ! |
| ! ! ! ! ! separate! |
| ! ! ! ! ! list ! |
| ! !E ! Transfer to ACARS MU ! C ! See ! |
| ! ! ! ! ! separate! |
| ! ! ! ! ! list ! |
| ! !F ! Increment of the report counter if the ! C ! 1 ! |
| ! ! ! report was triggered by a code number ! ! ! |
| ! ! ! > 1000; 1=yes, 0=no ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !1000!1 ! Manual selection via MCDU ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !2000!2 ! Flight phase dependent manual ! ! ! |
| ! ! ! selection via remote print button ! ! ! |
| ! ! ! if programmed. ! ! ! |
| ! !2.1 ! Remote Print Button assignment. ! C ! not ! |
| ! ! ! ! ! assigned! |
| !----!------!-----------------------------------------!------!---------! |
| !3000!3 ! Programmable Start Logic ! ! ! |
| ! !3.1 ! Trigger condition ! C ! not ! |
| ! ! ! ! ! progr. ! |
| !----!------!-----------------------------------------!------!---------! |
| ! !4 ! If during flight phase climb and cruise ! ! ! |
| ! ! ! (5.1 and 6) the conditions as defined ! ! ! |
| ! ! ! under item 4.2 are met the EGT Divergen-! ! ! |
| ! ! ! ce (EGTdiv) and TN Divergence (TNdiv) ! ! ! |
| ! ! ! monitoring functions are performed as ! ! ! |
| ! ! ! defined under item 4.3 to 4.4. ! ! ! |
| ! ! ! A divergence report is generated each ! ! ! |
| ! ! ! time when the value of EGTdiv or TNdiv ! ! ! |
| ! ! ! exceeds the defined threshold values ! ! ! |
| ! ! ! defined below. ! ! ! |
| ! !4.1 ! Threshold values: ! ! ! |
| !4110!4.1.1 ! EGTdivT1 limit in deg C ! C ! limit- ! |
| ! ! ! ! ! table ! |
| !4120!4.1.2 ! EGTdivT2 limit in deg C ! C ! limit- ! |
| ! ! ! ! ! table ! |
| !4130!4.1.3 ! EGTdivT3 limit in deg C ! C ! limit- ! |
| ! ! ! ! ! table ! |
| !4140!4.1.4 ! EGTdivT4 limit in deg C ! C ! limit- ! |
| ! ! ! ! ! table ! |
| !4150!4.1.5 ! TNdivT1 limit in deg C ! C ! limit- ! |
| ! ! ! ! ! table ! |
| !4160!4.1.6 ! TNdivT2 limit in deg C ! C ! limit- ! |
| ! ! ! ! ! table ! |
| !4170!4.1.7 ! TNdivT3 limit in deg C ! C ! limit- ! |
| ! ! ! ! ! table ! |
| !4180!4.1.8 ! TNdivT4 limit in deg C ! C ! limit- ! |
| ! ! ! ! ! table ! |
| !----!------!-----------------------------------------!------!---------! |
| ! !4.2 ! Divergence Monitoring Conditions ! ! ! |
| ! ! ! 1. N1 actual of both engines > N1L1 ! ! ! |
| ! ! ! 2. N1 actual of both engines < N1L2 ! ! ! |
| ! ! ! 3. N1 actual of both engines is within ! ! ! |
| ! ! ! N1L3 of each other. ! ! ! |
| ! ! ! 4. Bleed loads for both engines are ! ! ! |
| ! ! ! symmetrical and cross feed valve is ! ! ! |
| ! ! ! closed. ! ! ! |
| ! ! ! 5. IVV stable within IVVL, only valid ! ! ! |
| ! ! ! during flight phase 6. ! ! ! |
| ! ! ! 6. ALT < ALTL, only valid during flight ! ! ! |
| ! ! ! pahse 5.1. ! ! ! |
| ! ! ! 7. Delta TAT within TATL. ! ! ! |
| ! ! ! 8. N1rate within N1RL ! ! ! |
| ! ! ! The N1 rate is computed by checking the ! ! ! |
| ! ! ! difference between two saples at 1Hz. ! ! ! |
| ! ! ! 9. SSM's valid during the whole 'Y09' ! ! ! |
| ! ! ! seconds interval. ! ! ! |
| ! ! !10. Conditions 1-9 TRUE for > 'Y09' sec. ! ! ! |
| ! ! ! ! ! ! |
| ! !4.2.1 ! N1L1 limit in %rpm ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.2.2 ! N1L2 limit in %rpm ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.2.3 ! N1L3 limit in %rpm ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.2.4 ! Symmetrical bleed load: ! ! ! |
| ! ! ! Valve positions LH and RH are identical ! ! ! |
| ! ! ! (mirror image), cross feed valve is ! ! ! |
| ! ! ! closed, APU valve is closed or APU ! ! ! |
| ! ! ! Master Switch is off and Pack Flow is ! ! ! |
| ! ! ! within PFLdelta. ! ! ! |
| ! ! ! ! ! ! |
| ! ! !99 1111 1 1111 99 ! ! ! |
| ! ! !__ ____ _ ____ __ ! ! ! |
| ! ! ! ! ! ! ! !____RH Pack Flow ! ! ! |
| ! ! ! ! ! ! !_______RH Valve pos. ! ! ! |
| ! ! ! ! ! !___________Cross feed Valve pos.! ! ! |
| ! ! ! ! !______________LH Valve pos. ! ! ! |
| ! ! ! !__________________LH Pack Flow ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! APU Master Switch off: ! ! ! |
| ! ! ! param. 29.1.002.11.16 = 0 ! ! ! |
| ! ! ! param. 29.2.002.11.16 = 0 ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! PFLdelta =< abs (LH Pack Flow - RH Pack ! ! ! |
| ! ! ! Flow) ! ! ! |
| ! ! ! ! ! ! |
| ! !4.2.5 ! IVVL limit in f/min ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.2.6 ! ALTL limit in feet ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.2.7 ! TATL limit in deg C ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.2.8 ! N1RL limit in %rpm/sec ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.2.9 ! 'Y09' time interval in seconds ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.2.10! PFLdelta limit in kg sec. ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.3 ! EGT Divergence Calculation ! ! ! |
| ! ! ! ! ! ! |
| ! !4.3.1 ! EGTdiv = EGTdiff - deltaEGTrefX ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! In PH5.1 deltaEGTrefX is deltaEGTref5. ! ! ! |
| ! ! ! In PH6 deltaEGTrefX is deltaEGTref6. ! ! ! |
| ! ! ! ! ! ! |
| ! !4.3.2 ! CEGT#1 = EGT#1 + (N1#2 - N1#1) * C09.1 ! ! ! |
| ! ! ! (or C09.2).! ! ! |
| ! !4.3.3 ! EGTdiff = CEGT#1 - EGT#2 ! ! ! |
| ! !4.3.4 ! M ! ! ! |
| ! ! ! SIGMA EGTdiff (n) ! ! ! |
| ! ! ! n=1 ! ! ! |
| ! ! ! deltaEGTm = ------------------- ! ! ! |
| ! ! ! M ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! This calculation is done 'M' consecutive! ! ! |
| ! ! ! times once per second i.e. during 10 ! ! ! |
| ! ! ! seconds. ! ! ! |
| ! ! ! ! ! ! |
| ! !4.3.5 ! The calculations 4.3.5.1 and 4.3.5.2 are! ! ! |
| ! ! ! performed when the Divergence Monitoring! ! ! |
| ! ! ! Conditions (Item 4.2) are met. ! ! ! |
| ! ! ! ! ! ! |
| ! !4.3.5.! ! ! ! |
| ! !1 ! deltaEGTref5 is calculated if the A/C ! ! ! |
| ! ! ! has entered flight phase 5.1: ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! deltaEGTref5 = deltaEGTref5old + ! ! ! |
| ! ! ! (deltaEGTm - deltaEGTref5old) ! ! ! |
| ! ! ! + ----------------------------- ! ! ! |
| ! ! ! K5 + 1 ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! deltaEGTref5old is the deltaEGTref5 ! ! ! |
| ! ! ! value from previous flight. ! ! ! |
| ! ! ! ! ! ! |
| ! !4.3.5.! ! ! ! |
| ! !2 ! deltaEGTref6 is calculated if the A/C ! ! ! |
| ! ! ! has entered flight phase 6: ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! deltaEGTref6 = deltaEGTref6old + ! ! ! |
| ! ! ! (deltaEGTm - deltaEGTref6old) ! ! ! |
| ! ! ! + ----------------------------- ! ! ! |
| ! ! ! K6 + 1 ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! deltaEGTref6old is the deltaEGTref6 ! ! ! |
| ! ! ! value from previous flight. ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! Once the calculation (4.3.5) is ! ! ! |
| ! ! ! performed deltaEGTref5 and deltaEGTref6 ! ! ! |
| ! ! ! are stored and used for the EGTdiv ! ! ! |
| ! ! ! calculation (Item 4.3.1). ! ! ! |
| ! ! ! ! ! ! |
| ! !4.3.6 ! KL limit ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.3.7 ! C09.1 limit for climb PH5.1 in degC/%N1 ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.3.8 ! C09.2 limit for cruise PH6 in degC/%N1 ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !4.3.9 ! M programmed limit ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! ! ! - K5 and K6 are incremented by one for ! ! ! |
| ! ! ! each flight leg until KL is reached. ! ! ! |
| ! ! ! Then K = KL remains as long as: ! ! ! |
| ! ! ! - Engine S/N is not changed ! ! ! |
| ! ! ! - A/C is not changed ! ! ! |
| ! ! ! - The defined values of KL, C09.1,! ! ! |
| ! ! ! C09.2 and the threshold values ! ! ! |
| ! ! ! under item 4.1.1 and 4.1.1.10 ! ! ! |
| ! ! ! are not changed. ! ! ! |
| ! ! ! - If there is a change as a.m. items ! ! ! |
| ! ! ! then the K5/K6 and deltaEGTref5old and! ! ! |
| ! ! ! deltaEGTref6old will be set to 0. ! ! ! |
| ! ! ! - K5/K6 ,deltaEGTref5old and ! ! ! |
| ! ! ! deltaEGTref6old values can be reset ! ! ! |
| ! ! ! via MCDU menu. ! ! ! |
| ! ! !The K5 value is valid for reference ! ! ! |
| ! ! !calculations in flight phase 5.1., the K6! ! ! |
| ! ! !value is valid for reference calculations! ! ! |
| ! ! !in flight phase 6 during the entire ! ! ! |
| ! ! !flight. ! ! ! |
| ! !4.3.10! actual K5 value for PH5.1 printed in ! ! ! |
| ! ! ! AIDS report limit list ! ! ! |
| ! !4.3.11! actual K6 value for PH 6 printed in AIDS! ! ! |
| ! ! ! report limit list ! ! ! |
| ! !4.3.12! actual EGT ref value for PH 5.1 printed ! ! ! |
| ! ! ! in AIDS report limit list ! ! ! |
| ! !4.3.13! actual EGT ref value for PH 6 printed in! ! ! |
| ! ! ! AIDS report limit list ! ! ! |
| ! !4.3.14! actual TN ref value for PH 5.1 printed ! ! ! |
| ! ! ! in AIDS report limit list ! ! ! |
| ! !4.3.15! actual TN ref value for PH 6 printed in ! ! ! |
| ! ! ! AIDS report limit list ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| ! !4.4 ! TN Divergence Calculation ! ! ! |
| ! !4.4.1 ! TNdiv = deltaTNdiff - deltaTNrefX ! ! ! |
| ! ! ! In PH5.1 deltaTNrefX is deltaTNref5 ! ! ! |
| ! ! ! In PH6 deltaTNrefX is deltaTNref6. ! ! ! |
| ! !4.4.2 ! deltaTNdiff = TN#1 - TN#2 ! ! ! |
| ! !4.4.3 ! M ! ! ! |
| ! ! ! SIGMA TNdiff (n) ! ! ! |
| ! ! ! n=1 ! ! ! |
| ! ! ! deltaTNm = ------------------- ! ! ! |
| ! ! ! M ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! This calculation is done 'M' consecutive! ! ! |
| ! ! ! times once per second i.e. during 10 ! ! ! |
| ! ! ! seconds. ! ! ! |
| ! !4.4.4 ! The claculations 4.4.4.1 and 4.4.4.2 are! ! ! |
| ! ! ! performed when the Divergence Monitoring! ! ! |
| ! ! ! Conditions (Item 4.2) are met. ! ! ! |
| ! !4.4.4.! deltaTNref5 is calculated if the A/C has! ! ! |
| ! !1 ! entered flight phase 5.1: ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! deltaTNref5 = deltaTNref5old + ! ! ! |
| ! ! ! (deltaTNm - deltaTNref5old)! ! ! |
| ! ! ! + ---------------------------! ! ! |
| ! ! ! K5 + 1 ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! deltaTNref5old = deltaTNref5 from the ! ! ! |
| ! ! ! previous flight leg. ! ! ! |
| ! ! ! ! ! ! |
| ! !4.4.4.! deltaTNref6 is calculated if the A/C has! ! ! |
| ! !2 ! entered flight phase 6: ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! deltaTNref6 = deltaTNref6old + ! ! ! |
| ! ! ! (deltaTNm - deltaTNref6old)! ! ! |
| ! ! ! ---------------------------! ! ! |
| ! ! ! K6 + 1 ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! deltaTNref6old = deltaTNref6 from the ! ! ! |
| ! ! ! previous flight leg. ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! Once the calculation (4.4.4.) is ! ! ! |
| ! ! ! performed deltaTNref5 and deltaTNref6 ! ! ! |
| ! ! ! are stored and used for the TNdiv ! ! ! |
| ! ! ! calculation (Item 4.4.1). ! ! ! |
| ! ! ! ! ! ! |
| ! ! ! The same rules (analog to 4.3) as for ! ! ! |
| ! ! ! EGT divergence apply except TN#1 is ! ! ! |
| ! ! ! not corrected for deviations in N1. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| ! !5 ! In case of divergence detection and ! ! ! |
| ! ! ! report generation, the search logic for ! ! ! |
| ! ! ! the engine cruise report <01> CODE 7000 ! ! ! |
| ! ! ! for stable frame is started at once. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !8100!8.1 ! ACARS MU uplink request with IMI 'REQ09'! ! ! |
| ! ! ! The report <09> is immediately generated! ! ! |
| ! ! ! and transmitted to the ACARS MU. ! ! ! |
| !----------------------------------------------------------------------! |
| ! A = Programmable by Airbus ! |
| ! C = Programmable by Customer ! |
| +----------------------------------------------------------------------+ |
N. AIDS Reports Print Rules - Default Values for Report <09>
| +------------------------------------------------+ |
| ! ! ! ! |
| ! Code ! Printer Output ! ACARS-output ! |
| ! ! ! ! |
| !-------!-----------------------!----------------! |
| ! ! ! ! |
| ! 1000 ! Print immediatly ! No ACARS ! |
| ! ! ! ! |
| !-------!-----------------------!----------------! |
| ! ! ! ! |
| ! 2000 ! Print immediatly ! No ACARS ! |
| ! ! ! ! |
| !-------!-----------------------!----------------! |
| ! ! ! ! |
| ! 4110 ! Print at landing ! ACARS VHF ! |
| ! ! ! ! |
| !-------!-----------------------!----------------! |
| ! ! ! ! |
| ! 4120 ! Print at landing ! ACARS VHF ! |
| ! ! ! ! |
| !-------!-----------------------!----------------! |
| ! ! ! ! |
| ! 4130 ! Print at landing ! ACARS VHF ! |
| ! ! ! ! |
| !-------!-----------------------!----------------! |
| ! ! ! ! |
| ! 4140 ! Print at landing ! ACARS VHF ! |
| ! ! ! ! |
| !-------!-----------------------!----------------! |
| ! ! ! ! |
| ! 4150 ! Print at landing ! ACARS VHF ! |
| ! ! ! ! |
| !-------!-----------------------!----------------! |
| ! ! ! ! |
| ! 4160 ! Print at landing ! ACARS VHF ! |
| ! ! ! ! |
| !-------!-----------------------!----------------! |
| ! ! ! ! |
| ! 4170 ! Print at landing ! ACARS VHF ! |
| ! ! ! ! |
| !-------!-----------------------!----------------! |
| ! ! ! ! |
| ! 4180 ! Print at landing ! ACARS VHF ! |
| ! ! ! ! |
| !-------!-----------------------!----------------! |
| ! ! ! ! |
| ! 8100 ! No print ! ACARS VHF ! |
| ! ! ! ! |
| +------------------------------------------------+ |
| +-------------------------------------------------------------------------+ |
| !Trigger! to ACARS ! to printer ! store ! |
| ! Code !------------------------------ -!-----------------!--------------! |
| ! No !Ground ! VHF ! SAT- ! HF ! at ! imme- ! internal& ! |
| ! ! ! ! COM ! !landing ! diate ! external ! |
| ! ! ! ! ! ! ! !(build in RAM&! |
| ! ! ! ! ! ! ! ! PCMCIA) ! |
| !-------!-------!--------!-------!-------!--------!--------!--------------! |
| ! ! ! If ! ! ! ! If !PCMCIA only if! |
| ! 1000 ! NO ! 'SEND' ! NO ! NO ! !'PRINT' ! 'STORE' ! |
| ! ! !selected! ! ! !selected! selected on ! |
| ! ! !on MCDU ! ! ! !on MCDU ! MCDU ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 2000 ! NO ! NO ! NO ! NO ! ! YES ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 3000 ! NO ! NO ! NO ! NO ! ! NO ! YES ! |
| !-------!-------!--------!------ !-------! !--------!--------------! |
| ! 4110 ! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 4120 ! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| !-------!-------!--------!-------!-------! N !--------!--------------! |
| ! 4130 ! NO ! YES ! NO ! NO ! O ! NO ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 4140 ! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 4150 ! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 4160 ! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 4170 ! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 4180 ! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 8100 ! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| +-------------------------------------------------------------------------+ |
| +-------------------------------------------------------------------------+ |
| !Trigger! to ACARS ! to printer ! store ! |
| ! Code !------------------------------ -!-----------------!--------------! |
| ! No !Ground ! VHF ! SAT- ! HF ! at ! imme- ! internal& ! |
| ! ! ! ! COM ! !landing ! diate ! external ! |
| ! ! ! ! ! ! ! !(build in RAM&! |
| ! ! ! ! ! ! ! ! PCMCIA) ! |
| !-------!-------!--------!-------!-------!--------!--------!--------------! |
| ! 1000 ! NO ! NO ! NO ! NO ! ! YES ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 2000 ! NO ! NO ! NO ! NO ! ! YES ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 3000 ! NO ! NO ! NO ! NO ! ! NO ! YES ! |
| !-------!-------!--------!------ !-------! !--------!--------------! |
| ! 4110 ! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 4120 ! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| !-------!-------!--------!-------!-------! N !--------!--------------! |
| ! 4130 ! NO ! YES ! NO ! NO ! O ! NO ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 4140 ! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 4150 ! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 4160 ! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 4170 ! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 4180 ! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 8100 ! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| +-------------------------------------------------------------------------+ |
O. Engine Start Report <10>
Engine Start Report <10> (Engine Type CFMI with Advanced EVMU)
Engine Start Report <10> (Engine Type CFMI with Advanced EVMU)
Engine Start Report <10> (Engine Type CFMI with Advanced EVMU) ** ON A/C NOT FOR ALL
Engine Start Report <10> (Engine Type CFMI with Advanced EVMU) ** ON A/C NOT FOR ALL
Engine Start Report <10> (Engine Type CFMI with Advanced EVMU) ** ON A/C NOT FOR ALL
The Engine Start Report shall be a time series collection of engine related information as a function of number of flights and when an abnormal condition has been detected during a main engine start. The report is generated when one of the logic conditions 1000 to 7009 (for details see Engine Start report logic) is present.
Engine Start Report <10> (Engine Type CFMI with Advanced EVMU) Engine Start Report <10> (Engine Type CFMI with Advanced EVMU) Engine Start Report <10> (Engine Type CFMI with Advanced EVMU) ** ON A/C NOT FOR ALL Engine Start Report <10> (Engine Type CFMI with Advanced EVMU) ** ON A/C NOT FOR ALL Engine Start Report <10> (Engine Type CFMI with Advanced EVMU) ** ON A/C NOT FOR ALL NOTE: For the standard header definition of the report refer to (Ref. AMM D/O 31-36-00-00).
(1) Engine Start Report Data Field Description <10> (Engine Type CFMI with Advanced EVMU)
NOTE: Reports that are transmitted from the ACARS system do not have report lines without a line identifier.
| +---------------------------------------------------------------------+ |
| ! Value ! Content Description ! |
| !--------------!------------------------------------------------------! |
| ! ESN ! Engine Serial Number ! |
| ! 999999 ! (000000 to 999999) ! |
| ! ! Eng 1 param. 7C.1.046.01 digit 3, 2, 1 ! |
| ! ! 7C.1.047.01 digit 6, 5, 4 ! |
| ! ! Eng 2 param. 7C.2.046.01 digit 3, 2, 1 ! |
| ! ! 7C.2.047.01 digit 6, 5, 4 ! |
| !--------------!------------------------------------------------------! |
| ! EHRS ! Engine Flight Hours ! |
| ! 99999 ! (00000 to 99999 hours) ! |
| ! ! DMU Engine 1 and Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! ERT ! Engine Running Time ! |
| ! 99999 ! (00000 to 65536 hours) ! |
| ! ! Eng 1 param. 7C.1.050.01 ! |
| ! ! Eng 2 param. 7C.2.050.10 ! |
| !--------------!------------------------------------------------------! |
| ! ECYC ! Engine Cycle ! |
| ! 99999 ! (00000 to 99999) ! |
| !--------------!------------------------------------------------------! |
| ! AP ! Auto Pilot Status ! |
| ! 99 ! (00 to G8) ! |
| ! ! FMGC 1 and 2 (FGC part) for Auto Pilot AP1 and AP2 ! |
| ! ! ! |
| ! ! XX Auto Pilot Modes: ! |
| ! ! !! ! |
| ! ! !!__Lateral Modes: 0 = NO MODE ! |
| ! ! ! 1 = HEADING ! |
| ! ! ! 2 = TRACK ! |
| ! ! ! 3 = NAV ! |
| ! ! ! 4 = LOC CAPTURE ! |
| ! ! ! 5 = LOC TRACK ! |
| ! ! ! 6 = LAND TRACK ! |
| ! ! ! 7 = RUNWAY ! |
| ! ! ! 8 = ROLL GO AROUND ! |
| ! ! ! ! |
| ! ! !__Longitudinal Modes: 0 = NO MODE ! |
| ! ! 1 = PITCH G/A ! |
| ! ! 2 = PITCH T/O ! |
| ! ! 3 = G/S TRACK ! |
| ! ! 4 = G/S CAPTURE ! |
| ! ! 5 = V/S ! |
| ! ! 6 = FPA ! |
| ! ! 7 = ALT ! |
| ! ! 8 = ALT ACQ ! |
| ! ! 9 = OPEN CLB ! |
| ! ! A = OPEN DES ! |
| ! ! B = IM CLB ! |
| ! ! C = IM DES ! |
| ! ! D = CLB ! |
| ! ! E = DES ! |
| ! ! F = FINAL DES ! |
| ! ! G = EXPEDITE ! |
| ! ! ! |
| ! ! AP1 ! AP2 ! |
| ! ! Report Line EC: ! Report Line EE: !Definition: ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! / ! / !No Mode Act. ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.11 = 1 ! 01.2.275.00.11 = 1!RUNWAY Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.12 = 1 ! 01.2.275.00.12 = 1!NAV Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.13 = 1 ! 01.2.275.00.13 = 1!LOC CAPTURE ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.14 = 1 ! 01.2.275.00.14 = 1!LOC TRACK ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.15 = 1 ! 01.2.275.00.15 = 1!Roll GO ! |
| ! ! ! !AROUND Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.16 = 1 ! 01.2.275.00.16 = 1!HEADING Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.17 = 1 ! 01.2.275.00.17 = 1!TRACK Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.15 = 1 ! 01.2.274.00.15 = 1!PITCH TO Mode! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.16 = 1 ! 01.2.274.00.16 = 1!PITCH GA Mode! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.17 = 1 ! 01.2.274.00.17 = 1!V/S Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.18 = 1 ! 01.2.274.00.18 = 1!FPA Mode ! |
| ! ! -------------------!-------------------!-------------! |
| ! ! 01.1.274.00.19 = 1 ! 01.2.274.00.19 = 1!ALT Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.20 = 1 ! 01.2.274.00.20 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.19 = 1 ! 01.2.274.00.19 = 1!ALT ACQ ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.21 = 1 ! 01.2.274.00.21 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.20 = 1 ! 01.2.274.00.20 = 1!G/S TRACK ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.22 = 1 ! 01.2.274.00.22 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.21 = 1 ! 01.2.274.00.21 = 1!G/S CAPTURE ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.22 = 1 ! 01.2.274.00.22 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.23 = 1 ! 01.2.274.00.23 = 1!FINAL DES ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.2.274.00.24 = 1 ! 01.2.274.00.24 = 1!EXPED. Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.146.00.14 = 1 ! 01.2.146.00.14 = 1!LAND TRACK ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!CLB Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.13 = 0 ! 01.2.274.00.13 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.14 = 0 ! 01.2.274.00.14 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.24 = 0 ! 01.2.274.00.24 = 0! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!DES Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.13 = 0 ! 01.2.274.00.13 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.14 = 0 ! 01.2.274.00.14 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.24 = 0 ! 01.2.274.00.24 = 0! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!IM. CLIMB ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.13 = 1 ! 01.2.274.00.13 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!IM. DES Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.13 = 1 ! 01.2.274.00.13 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!OPEN CLB ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.14 = 1 ! 01.2.274.00.14 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!OPEN DES ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.14 = 1 ! 01.2.274.00.14 = 1! ! |
| ! ! ---------------------------------------------------- ! |
| ! ! Auto Pilot Status DMU: ! |
| ! ! AP1 printed in report line EC ! |
| ! ! AP2 printed in report line EE ! |
| !--------------!------------------------------------------------------! |
| ! Y1 ! 'Y10.1' seconds programmed Pre-event Intervals ! |
| ! 99 ! (1 to 6 sec.) ! |
| !--------------!------------------------------------------------------! |
| ! Y2 ! 'Y10.2' seconds programmed Post-event Intervals ! |
| ! 99 ! (1 to 60 sec.) ! |
| !--------------!------------------------------------------------------! |
| ! E ! Engine Position ! |
| ! 9 ! ! |
| !--------------!------------------------------------------------------! |
| ! MAX ! Maximal EGT During Engine Start Phase ! |
| ! X999 ! (-55 to 999.9 C) ! |
| ! ! param. Eng.1 7C.1.345.01 ! |
| ! ! param. Eng.1 7C.2.345.10 ! |
| !--------------!------------------------------------------------------! |
| ! LIM ! Programmed EGT limit ! |
| ! X999 ! (-55 to 999.9 C) ! |
| ! ! param. Eng.1 7C.1.345.01 ! |
| ! ! param. Eng.1 7C.2.345.10 ! |
| !--------------!------------------------------------------------------! |
| ! TOL ! - Time Over Limit for EGT Exceedance or ! |
| ! 999 ! - Time from SAV = open to N2 = N2 trigger ! |
| ! ! param. Eng.1 7C.1.270.01.13 = 1 ! |
| ! ! param. Eng.1 7C.2.270.10.13 = 1 ! |
| !--------------!------------------------------------------------------! |
| ! TTP ! Time from SAV open to max EGT or to start abort ! |
| ! 999 ! ! |
| ! ! param. Eng.1 7C.1.270.01.13 = 1 ! |
| ! ! param. Eng.1 7C.2.270.10.13 = 1 ! |
| !--------------!------------------------------------------------------! |
| ! TTF ! Time from SAV open to Fuel Shut-Off Valve = open ! |
| ! 999 ! ! |
| ! ! param. Eng.1 7C.1.270.01.13 = 1 = SAV open ! |
| ! ! param. Eng.1 7C.2.270.10.13 = 1 ! |
| ! ! param. Eng.1 7C.1.270.01.14 = 1 = Fuel Shut-Off ! |
| ! ! param. Eng.1 7C.2.270.10.14 = 1 VAlve open ! |
| !--------------!------------------------------------------------------! |
| ! FF ! Report Line N1: Fuel Flow 'Y3' seconds after ! |
| ! 9999 ! SAV = open ! |
| ! ! Report Line SX: Fuel Flow (see parameter logic) ! |
| ! ! (0 to 7000 kg/h) ! |
| ! ! Eng.1 param. 7C.1.345.01 ! |
| ! ! Eng.2 param. 7C.2.345.10 ! |
| !--------------!------------------------------------------------------! |
| ! PD ! Report Line N1: Precooler Inlet Pressure at ! |
| ! 99 ! SAV = open ! |
| ! ! Report Line SX: Precooler Inlet Pressure ! |
| ! ! (see parameter logic) ! |
| ! ! (0 to 50 psi) ! |
| ! ! Eng.1 param. 6F.1.143.01 ! |
| ! ! 6F.2.143.10 ! |
| ! ! Eng.2 param. 6F.1.142.01 ! |
| ! ! 6F.2.142.10 ! |
| !--------------!------------------------------------------------------! |
| ! SM ! Start Mode ! |
| ! 1 ! ! |
| ! ! Eng.1 param. 7C.1.273.01.19 ! |
| ! ! Eng.1 param. 7C.2.273.10.19 ! |
| !--------------!------------------------------------------------------! |
| ! Reason ! Reason for Exceedance ! |
| ! XXXXXXXXXX ! Up to 20 characters ! |
| ! XXXXXXXXXX ! SAV CODE: 4410 ! |
| ! ! HPSOV CODE: 4420 ! |
| ! ! EGT CODE: 4430 and 5000 ! |
| ! ! STALL CODE: 4440 ! |
| ! ! No Light off CODE: 4440 ! |
| ! ! Hung CODE: 4460 ! |
| ! ! Start Fail CODE: 4470 ! |
| ! ! Slow CODE: 4480 ! |
| !--------------!------------------------------------------------------! |
| ! N1 ! Selected N1 Actual ! |
| ! 9999 ! (0 to 120.0 %rpm) ! |
| ! ! Eng 1 param. 7C.1.346.01 ! |
| ! ! Eng 2 param. 7C.2.346.10 ! |
| !--------------!------------------------------------------------------! |
| ! N2 ! Selected N2 Actual ! |
| ! 9999 ! (0 to 120.0 %rpm) ! |
| ! ! Eng 1 param. 7C.1.344.01 ! |
| ! ! Eng 2 param. 7C.2.344.10 ! |
| !--------------!------------------------------------------------------! |
| ! EGT ! Selected T494 (Exhaust Gas Temperature) ! |
| ! X999 ! (-55 to 999.9 C) ! |
| ! ! Eng 1 param. 7C.1.345.01 ! |
| ! ! Eng 2 param. 7C.2.345.10 ! |
| !--------------!------------------------------------------------------! |
| ! FF ! Engine Fuel Flow ! |
| ! 9999 ! ( 0 to 7000 kg/h) ! |
| ! ! Eng 1 param. 7C.1.244.01 ! |
| ! ! Eng 2 param. 7C.2.244.10 ! |
| !--------------!------------------------------------------------------! |
| ! FMV ! T.B.D. ! |
| ! 999 ! ! |
| !--------------!------------------------------------------------------! |
| ! T25 ! Selected T25 ! |
| ! X999 ! (-55.0 to 120.0 C) ! |
| ! ! Eng 1 param. 7C.1.263.01 ! |
| ! ! Eng 2 param. 7C.2.263.10 ! |
| !--------------!------------------------------------------------------! |
| ! PD ! Precooler Inlet Pressure ! |
| ! 99 ! (0 to 50 psi) ! |
| ! ! Eng 1 param. 06F.1.143.01 ! |
| ! ! 06F.1.143.10 ! |
| ! ! Eng 2 param. 06F.2.142.10 ! |
| ! ! 06F.2.142.01 ! |
| !--------------!------------------------------------------------------! |
| ! P3 ! Selected PS3 ! |
| ! 9999 ! (0.0 to 450.0 psia) ! |
| ! ! Eng 1 param. 7C.1.264.01 ! |
| ! ! Eng 2 param. 7C.2.264.10 ! |
| !--------------!------------------------------------------------------! |
| ! T3 ! Temperature at Position 3 ! |
| ! X999 ! (-55.0 to 850.0 C) ! |
| ! ! Eng 1 param. 7C.1.265.01 ! |
| ! ! Eng 2 param. 7C.2.265.10 ! |
| !--------------!------------------------------------------------------! |
| ! VSV ! Variable Statore Vane Position ! |
| ! X99 ! (-5.0 to 45.0 deg) ! |
| ! ! Eng 1 param. 7C.1.072.01 ! |
| ! ! Eng 2 param. 7C.2.072.10 ! |
| !--------------!------------------------------------------------------! |
| ! VBV ! Variable Bleed Valve Position ! |
| ! X99 ! (-9.9 to 40.0 deg) ! |
| ! ! Eng 1 param. 7C.1.071.01 ! |
| ! ! Eng 2 param. 7C.2.071.10 ! |
| !--------------!------------------------------------------------------! |
| ! T5 ! Temperature at Position 5 ! |
| ! X999 ! (-55.0 to 850.0 C) ! |
| ! ! Eng 1 param. 7C.1.260.01 ! |
| ! ! Eng 2 param. 7C.2.260.10 ! |
| !--------------!------------------------------------------------------! |
| ! OIT ! Engine Oil Temperature ! |
| ! X99 ! (-60 to 250 C) ! |
| ! ! Eng 1 param. 26.1.316.01 ! |
| ! ! 26.2.316.01 ! |
| ! ! Eng 2 param. 26.1.316.10 ! |
| ! ! 26.2.316.10 ! |
| !--------------!------------------------------------------------------! |
| ! ECW5 ! Engine Control Word 5 ! |
| ! XXXXX ! Each 'X' represents 4 Bits in hexadecimal code of ! |
| ! ! a defined ARINC 429 word: ! |
| ! ! XXXXX Bits HEX ! |
| ! ! !!!!!___________ 14, 13, 12, 11 0...F ! |
| ! ! !!!!____________ 18, 17, 16, 15 0...F ! |
| ! ! !!!_____________ 22, 21, 20, 19 0...F ! |
| ! ! !!______________ 26, 25, 24, 23 0...F ! |
| ! ! !_______________ 29, 28, 27 0...7 ! |
| ! ! -------------------------------------------- ! |
| ! ! ! |
| ! ! Bit Label Parameter Description ! |
| ! ! 11 7C.X.270.XX.11 = 1 Ignition 1 Primary Selected! |
| ! ! 12 SPARE ! |
| ! ! 13 7C.X.270.XX.13 = 1 Starter Air Valve Open ! |
| ! ! Local Switch ! |
| ! ! 14 7C.X.270.XX.14 = 1 HP Fuel Valve Closed Local ! |
| ! ! 15 7C.X.270.XX.15 = 1 SAV Demand/Position ! |
| ! ! Disagree ! |
| ! ! 16 7C.X.270.XX.16 = 1 HPSOV Demand/Position ! |
| ! ! Disagree ! |
| ! ! 17 7C.X.270.XX.17 = 1 Start EGT Overtemp Detected! |
| ! ! 18 7C.X.270.XX.18 = 1 Start Stall Detected ! |
| ! ! 19 7C.X.270.XX.19 = 1 No/Low Fan Speed for Core ! |
| ! ! Speed ! |
| ! ! 20 7C.X.270.XX.20 = 1 No Eng. Light Off Detecetd ! |
| ! ! 21 7C.X.270.XX.21 = 1 Starter Time Limit Exceeded! |
| ! ! 22 7C.X.270.XX.22 = 1 Fuel Schedule Derich Active! |
| ! ! 23 7C.X.270.XX.23 = 1 TLA Not at Idle for Start ! |
| ! ! Initiation ! |
| ! ! 24 SPARE ! |
| ! ! 25 7C.X.270.XX.25 = 1 Low Sap - Deteceted ! |
| ! ! 26 7C.X.270.XX.26 = 1 All Channel Controls Active! |
| ! ! 27 SPARE ! |
| ! ! 28 SPARE ! |
| ! ! 29 SPARE ! |
| +---------------------------------------------------------------------+ |
(2) Engine Start Report Data Field Description <10> (Engine Type CFMI with Advanced EVMU)
NOTE: Reports that are transmitted from the ACARS system do not have report lines without a line identifier.
NOTE: Only the parts of the ENGINE START REPORT <10> which are not included in the ENGINE CRUISE REPORT <01> are given in the subsequent table.
| +---------------------------------------------------------------------+ |
| ! Value ! Content Description ! |
| !--------------!------------------------------------------------------! |
| ! Y1 ! 'Y10.1' seconds programmed Pre-event Intervals ! |
| ! 99 ! DMU (1 to 6 sec.) ! |
| !--------------!------------------------------------------------------! |
| ! Y2 ! 'Y10.2' seconds programmed Post-event Intervals ! |
| ! 99 ! DMU (1 to 60 sec.) ! |
| !--------------!------------------------------------------------------! |
| ! E ! Engine Position ! |
| ! 9 ! DMU ! |
| ! ! No. 1 or 2 engine for which the report is valid ! |
| !--------------!------------------------------------------------------! |
| ! MAX ! Maximal EGT During Engine Start Phase ! |
| ! X999 ! (-55 to 999.9 C) ! |
| ! ! Engine 1 7C.1.345.01 ! |
| ! ! Engine 2 7C.2.345.10 ! |
| ! ! Negative values are shown with an N in the first ! |
| ! ! position. Otherwise the first position is used for ! |
| ! ! the value. ! |
| !--------------!------------------------------------------------------! |
| ! LIM ! Programmed EGT limit ! |
| ! X999 ! ECU (-55 to 999.9 C) ! |
| ! ! Engine 1 7C.1.345.01 ! |
| ! ! Engine 2 7C.2.345.10 ! |
| ! ! Negative values are shown with an N in the first ! |
| ! ! position. Otherwise the first position is used for ! |
| ! ! the value. ! |
| !--------------!------------------------------------------------------! |
| ! TOL ! - Time Over Limit for EGT Exceedance or ! |
| ! 999 ! - Time from SAV = open to N2 = N2 trigger ! |
| ! ! DMU ! |
| ! ! Engine 1 7C.1.270.01.13 = 1 SAV open ! |
| ! ! Engine 2 7C.2.270.10.13 = 1 ! |
| ! ! Time in seconds. ! |
| !--------------!------------------------------------------------------! |
| ! TTP ! Time from SAV open to max EGT or to start abort ! |
| ! 999 ! DMU ! |
| ! ! Engine 1 7C.1.270.01.13 = 1 SAV open ! |
| ! ! Engine 2 7C.2.270.10.13 = 1 ! |
| !--------------!------------------------------------------------------! |
| ! TTF ! Time from SAV open to Fuel Shut-Off Valve = open ! |
| ! 999 ! ! |
| ! ! Engine 1 7C.1.270.01.13 = 1 = SAV open ! |
| ! ! Engine 2 7C.2.270.10.13 = 1 ! |
| ! ! Engine 1 7C.1.270.01.14 = 0 = Fuel Shut-Off ! |
| ! ! Engine 2 7C.2.270.10.14 = 0 Valve open ! |
| !--------------!------------------------------------------------------! |
| ! FF ! Report Line N1: Fuel Flow 'Y3' seconds after ! |
| ! 9999 ! SAV = open ! |
| ! ! Report Line SX: Fuel Flow (see parameter logic) ! |
| ! ! ECU 0 to 7000 kg/h (0 to 15000p/h) ! |
| ! ! Engine 1 7C.1.345.01 ! |
| ! ! Engine 2 7C.2.345.10 ! |
| !--------------!------------------------------------------------------! |
| ! PD ! Report Line N1: Precooler Inlet Pressure at ! |
| ! 99 ! SAV = open ! |
| ! ! Report Line SX: Precooler Inlet Pressure ! |
| ! ! (see parameter logic) ! |
| ! ! BMC (0 to 50 psi) ! |
| ! ! Engine 1 6F.1.143.01 ! |
| ! ! 6F.2.143.10 ! |
| ! ! Engine 2 6F.1.142.01 ! |
| ! ! 6F.2.142.10 ! |
| !--------------!------------------------------------------------------! |
| ! SM ! Start Mode ! |
| ! 1 ! ECU ! |
| ! ! Auto start sequence in progress = 1 ! |
| ! ! Engine 1 7C.1.273.01.19 ! |
| ! ! Engine 2 7C.2.273.10.19 ! |
| !--------------!------------------------------------------------------! |
| ! Reason ! Reason for Exceedance ! |
| ! XXXXXXXXXX ! Up to 20 characters ! |
| ! XXXXXXXXXX ! SAV CODE: 4410 ! |
| ! ! HPSOV CODE: 4420 ! |
| ! ! EGT CODE: 4430 and 5000 ! |
| ! ! STALL CODE: 4440 ! |
| ! ! No Light off CODE: 4450 ! |
| ! ! Hung CODE: 4460 ! |
| ! ! Start Fail CODE: 4470 ! |
| ! ! Slow CODE: 4480 ! |
| !--------------!------------------------------------------------------! |
| ! ECW5 ! Engine Control Word 5 ! |
| ! XXXXX ! Each 'X' represents 4 Bits in hexadecimal code of ! |
| ! ! a defined ARINC 429 word: ! |
| ! ! XXXXX Bits HEX ! |
| ! ! !!!!!___________ 14, 13, 12, 11 0...F ! |
| ! ! !!!!____________ 18, 17, 16, 15 0...F ! |
| ! ! !!!_____________ 22, 21, 20, 19 0...F ! |
| ! ! !!______________ 26, 25, 24, 23 0...F ! |
| ! ! !_______________ 29, 28, 27 0...7 ! |
| ! ! -------------------------------------------- ! |
| ! ! ! |
| ! ! Bit Label Parameter Description ! |
| ! ! 11 7C.X.270.XX.11 = 1 Ignition 1 Primary Selected! |
| ! ! 12 SPARE ! |
| ! ! 13 7C.X.270.XX.13 = 1 Starter Air Valve Open ! |
| ! ! Local Switch ! |
| ! ! 14 7C.X.270.XX.14 = 1 HP Fuel Valve Closed Local ! |
| ! ! 15 7C.X.270.XX.15 = 1 SAV Demand/Position ! |
| ! ! Disagree ! |
| ! ! 16 7C.X.270.XX.16 = 1 HPSOV Demand/Position ! |
| ! ! Disagree ! |
| ! ! 17 7C.X.270.XX.17 = 1 Start EGT Overtemp Detected! |
| ! ! 18 7C.X.270.XX.18 = 1 Start Stall Detected ! |
| ! ! 19 7C.X.270.XX.19 = 1 No/Low Fan Speed for Core ! |
| ! ! Speed ! |
| ! ! 20 7C.X.270.XX.20 = 1 No Eng. Light Off Detecetd ! |
| ! ! 21 7C.X.270.XX.21 = 1 Starter Time Limit Exceeded! |
| ! ! 22 7C.X.270.XX.22 = 1 Fuel Schedule Derich Active! |
| ! ! 23 7C.X.270.XX.23 = 1 TLA Not at Idle for Start ! |
| ! ! Initiation ! |
| ! ! 24 SPARE ! |
| ! ! 25 7C.X.270.XX.25 = 1 Low Sap - Deteceted ! |
| ! ! 26 7C.X.275.XX.26 = 1 All Channel Controls Active! |
| ! ! 27 SPARE ! |
| ! ! 28 SPARE ! |
| ! ! 29 SPARE ! |
| +---------------------------------------------------------------------+ |
(3) Engine Start Report Data Field Description <10> (Engine Type CFMI with Advanced EVMU)
NOTE: Reports that are transmitted from the ACARS system do not have report lines without a line identifier.
NOTE: Only the parts of the ENGINE START REPORT <10> which are not included in the ENGINE CRUISE REPORT <01> are given in the subsequent table.
| +---------------------------------------------------------------------+ |
| ! Value ! Content Description ! |
| !--------------!------------------------------------------------------! |
| ! Y1 ! 'Y10.1' seconds programmed Pre-event Intervals ! |
| ! 99 ! DMU (1 to 6 sec.) ! |
| !--------------!------------------------------------------------------! |
| ! Y2 ! 'Y10.2' seconds programmed Post-event Intervals ! |
| ! 99 ! DMU (1 to 60 sec.) ! |
| !--------------!------------------------------------------------------! |
| ! E ! Engine Position ! |
| ! 9 ! DMU ! |
| ! ! No. 1 or 2 of engine for which the report is valid ! |
| !--------------!------------------------------------------------------! |
| ! MAX ! Maximal EGT During Engine Start Phase ! |
| ! X999 ! (-55 to 999.9 C) ! |
| ! ! Engine 1 7C.1.345.01 ! |
| ! ! Engine 2 7C.2.345.10 ! |
| ! ! NOTE: Negative values are shown with an '-' at the ! |
| ! ! first position. Otherwise the first position ! |
| ! ! is used for the value. ! |
| !--------------!------------------------------------------------------! |
| ! LIM ! Programmed EGT limit ! |
| ! X999 ! ECU (-55 to 999.9 C) ! |
| ! ! Engine 1 7C.1.345.01 ! |
| ! ! Engine 2 7C.2.345.10 ! |
| ! ! NOTE: Negative values are shown with an '-' at the ! |
| ! ! first position. Otherwise the first position ! |
| ! ! is used for the value. ! |
| !--------------!------------------------------------------------------! |
| ! TOL ! - Time Over Limit for EGT Exceedance or ! |
| ! 999 ! - Time from SAV = open to N2 = N2 trigger ! |
| ! ! DMU Time in seconds ! |
| ! ! Engine 1 7C.1.270.01.13 = 1 SAV open ! |
| ! ! Engine 2 7C.2.270.10.13 = 1 ! |
| !--------------!------------------------------------------------------! |
| ! TTP ! Time from SAV open to max EGT or to start abort ! |
| ! 999 ! DMU ! |
| ! ! Engine 1 7C.1.270.01.13 = 1 SAV open ! |
| ! ! Engine 2 7C.2.270.10.13 = 1 ! |
| !--------------!------------------------------------------------------! |
| ! TTF ! Time from SAV open to Fuel Shut-Off Valve = open ! |
| ! 999 ! DMU Time in seconds ! |
| ! ! Engine 1 7C.1.270.01.13 = 1 = SAV open ! |
| ! ! Engine 2 7C.2.270.10.13 = 1 ! |
| ! ! Engine 1 7C.1.270.01.14 = 0 = Fuel Shut-Off ! |
| ! ! Engine 2 7C.2.270.10.14 = 0 Valve open ! |
| !--------------!------------------------------------------------------! |
| ! FF ! Report Line N1: Fuel Flow 'Y3' seconds after ! |
| ! 9999 ! SAV = open ! |
| ! ! Report Line SX: Fuel Flow (see parameter logic) ! |
| ! ! ECU 0 to 7000 kg/h (0 to 15000p/h) ! |
| ! ! Engine 1 7C.1.244.01 ! |
| ! ! Engine 2 7C.2.244.10 ! |
| !--------------!------------------------------------------------------! |
| ! PD ! Report Line N1: Precooler Inlet Pressure at ! |
| ! 99 ! SAV = open ! |
| ! ! Report Line SX: Precooler Inlet Pressure ! |
| ! ! (see parameter logic) ! |
| ! ! BMC (0 to 50 psi) ! |
| ! ! Engine 1 6F.1.143.01 ! |
| ! ! 6F.2.143.10 ! |
| ! ! Engine 2 6F.1.142.01 ! |
| ! ! 6F.2.142.10 ! |
| !--------------!------------------------------------------------------! |
| ! SM ! Start Mode ! |
| ! 1 ! ECU ! |
| ! ! Auto start sequence in progress = 1 ! |
| ! ! Engine 1 7C.1.273.01.19 ! |
| ! ! Engine 2 7C.2.273.10.19 ! |
| !--------------!------------------------------------------------------! |
| ! Reason ! Reason for Exceedance ! |
| ! XXXXXXXXXX ! DMU Up to 20 characters ! |
| ! XXXXXXXXXX ! ! |
| ! ! SAV CODE: 4410 ! |
| ! ! HPSOV CODE: 4420 ! |
| ! ! EGT CODE: 4430 and 5000 ! |
| ! ! STALL CODE: 4440 ! |
| ! ! No Light off CODE: 4450 ! |
| ! ! Hung CODE: 4460 ! |
| ! ! Start Fail CODE: 4470 ! |
| ! ! Slow CODE: 4480 ! |
| ! ! ! |
| ! ! NOTE: If the report was not triggered by a limit ! |
| ! ! exceedance, this field contains blanks. ! |
| !--------------!------------------------------------------------------! |
| ! ECW5 ! Engine Control Word 5 ! |
| ! XXXXX ! Each 'X' represents 4 Bits in hexadecimal code of ! |
| ! ! a defined ARINC 429 word: ! |
| ! ! XXXXX Bits HEX ! |
| ! ! !!!!!___________ 14, 13, 12, 11 0...F ! |
| ! ! !!!!____________ 18, 17, 16, 15 0...F ! |
| ! ! !!!_____________ 22, 21, 20, 19 0...F ! |
| ! ! !!______________ 26, 25, 24, 23 0...F ! |
| ! ! !_______________ 29, 28, 27 0...7 ! |
| ! ! ! |
| ! ! DMU, composed of serveral ECU discrete labels as ! |
| ! ! defined below. For engine 1 and engine 2. ! |
| ! ! The 'X' for the System and SDI definition of the ! |
| ! ! engine parameters are given as follows. ! |
| ! ! ! |
| ! ! System SDI ! |
| ! ! Engine 1 1 01 ! |
| ! ! Engine 2 2 10 ! |
| ! ! --------------------------------------------- ! |
| ! ! Bit Label Parameter Description ! |
| ! ! 11 7C.X.270.XX.11 = 1 Ignition 1 Primary Selected! |
| ! ! 12 SPARE ! |
| ! ! 13 7C.X.270.XX.13 = 1 Starter Air Valve Open ! |
| ! ! Local Switch ! |
| ! ! 14 7C.X.270.XX.14 = 1 HP Fuel Valve Closed Local ! |
| ! ! 15 7C.X.270.XX.15 = 1 SAV Demand/Position ! |
| ! ! Disagree ! |
| ! ! 16 7C.X.270.XX.16 = 1 HPSOV Demand/Position ! |
| ! ! Disagree ! |
| ! ! 17 7C.X.270.XX.17 = 1 Start EGT Overtemp Detected! |
| ! ! 18 7C.X.270.XX.18 = 1 Start Stall Detected ! |
| ! ! 19 7C.X.270.XX.19 = 1 No/Low Fan Speed for Core ! |
| ! ! Speed ! |
| ! ! 20 7C.X.270.XX.20 = 1 No Eng. Light Off Detecetd ! |
| ! ! 21 7C.X.270.XX.21 = 1 Starter Time Limit Exceeded! |
| ! ! 22 7C.X.270.XX.22 = 1 Fuel Schedule Derich Active! |
| ! ! 23 7C.X.270.XX.23 = 1 TLA Not at Idle for Start ! |
| ! ! Initiation ! |
| ! ! 24 SPARE ! |
| ! ! 25 7C.X.270.XX.25 = 1 Low Sap - (Slow Start) ! |
| ! ! Detected ! |
| ! ! 26 7C.X.275.XX.28 = 1 All Channel Controls Active! |
| ! ! 27 SPARE ! |
| ! ! 28 SPARE ! |
| ! ! 29 SPARE ! |
| +---------------------------------------------------------------------+ |
(4) Engine Start Report Data Field Description <10> (Engine Type CFMI with Advanced EVMU)
NOTE: Reports that are transmitted from the ACARS system do not have report lines without a line identifier.
| +---------------------------------------------------------------------+ |
| ! Value ! Content Description ! |
| !--------------!------------------------------------------------------! |
| ! ESN ! Engine Serial Number ! |
| ! 999999 ! (000000 to 999999) ! |
| ! ! ECU Engine 1 7C.1.046.01 digit 3, 2, 1 ! |
| ! ! 7C.1.047.01 digit 6, 5, 4 ! |
| ! ! Engine 2 7C.2.046.10 digit 3, 2, 1 ! |
| ! ! 7C.2.047.10 digit 6, 5, 4 ! |
| !--------------!------------------------------------------------------! |
| ! EHRS ! Engine Flight Hours ! |
| ! 99999 ! (00000 to 99999 hours) ! |
| ! ! DMU Engine 1 ! |
| ! ! Engine 2 ! |
| ! ! Remark: Time between "Main (LH and RH) Landing Gear! |
| ! ! Decompressed" and "Main (LH and RH) Landing! |
| ! ! Gear Compressed". The EHRS is set to zero ! |
| ! ! if a new ESN is recognized by the DMU. ! |
| ! ! It is possible to set the EHRS via the MCDU! |
| ! ! e.g. if the DMU is changed on the a/c. ! |
| !--------------!------------------------------------------------------! |
| ! ERT ! Engine Running Time ! |
| ! 99999 ! (00000 to 65536 hours) ! |
| ! ! ECU 7C.1.050.01 Engine 1 ! |
| ! ! 7C.2.050.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! ECYC ! Engine Cycle ! |
| ! 99999 ! (00000 to 99999) ! |
| ! ! DMU Engine 1 ! |
| ! ! Engine 2 ! |
| ! ! Remark: Each time when flight phase 5 (climb) is ! |
| ! ! reached, the counter is incremented by one.! |
| ! ! The ECYC is set to zero if a new ESN is ! |
| ! ! is recognized by the DMU. It is possible to! |
| ! ! set ECYC via the MCDU, if the DMU is ! |
| ! ! changed on the a/c. ! |
| !--------------!------------------------------------------------------! |
| ! AP ! Auto Pilot Status ! |
| ! 99 ! Number of respective status (00 to G8) ! |
| ! ! FMGC 1 and 2 (FGC part) for Auto Pilot AP1 and AP2 ! |
| ! ! ! |
| ! ! Parameter for AP1 ! Parameter for AP2 ! ! |
| ! ! Report Line EC: ! Report Line EE: !Definition: ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! / ! / !No Mode ! |
| ! ! ! !Active ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.11 = 1 ! 01.2.275.00.11 = 1!RUNWAY Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.12 = 1 ! 01.2.275.00.12 = 1!NAV Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.13 = 1 ! 01.2.275.00.13 = 1!LOC CAPTURE ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.14 = 1 ! 01.2.275.00.14 = 1!LOC TRACK ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.15 = 1 ! 01.2.275.00.15 = 1!Roll GO ! |
| ! ! ! !AROUND Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.16 = 1 ! 01.2.275.00.16 = 1!HEADING Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.17 = 1 ! 01.2.275.00.17 = 1!TRACK Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.15 = 1 ! 01.2.274.00.15 = 1!PITCH T/O ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.16 = 1 ! 01.2.274.00.16 = 1!PITCH GA Mode! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.17 = 1 ! 01.2.274.00.17 = 1!V/S Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.18 = 1 ! 01.2.274.00.18 = 1!FPA Mode ! |
| ! ! -------------------!-------------------!-------------! |
| ! ! 01.1.274.00.19 = 1 ! 01.2.274.00.19 = 1!ALT Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.20 = 1 ! 01.2.274.00.20 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.19 = 1 ! 01.2.274.00.19 = 1!ALT ACQ ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.21 = 1 ! 01.2.274.00.21 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.20 = 1 ! 01.2.274.00.20 = 1!G/S TRACK ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.22 = 1 ! 01.2.274.00.22 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.21 = 1 ! 01.2.274.00.21 = 1!G/S CAPTURE ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.22 = 1 ! 01.2.274.00.22 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.23 = 1 ! 01.2.274.00.23 = 1!FINAL DES ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.24 = 1 ! 01.2.274.00.24 = 1!EXPED. Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.146.00.14 = 1 ! 01.2.146.00.14 = 1!LAND TRACK ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!CLB Mode ! |
| ! ! AND ! AND ! ! |
| ! ! ! ! ! ! ! |
| ! ! -------------- ! -------------- ! ! |
| ! ! 01.1.274.00.13 = 0 ! 01.2.274.00.13 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.14 = 0 ! 01.2.274.00.14 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.24 = 0 ! 01.2.274.00.24 = 0! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!DES Mode ! |
| ! ! AND ! AND ! ! |
| ! ! ! ! ! ! ! |
| ! ! -------------- ! -------------- ! ! |
| ! ! 01.1.274.00.13 = 0 ! 01.2.274.00.13 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.14 = 0 ! 01.2.274.00.14 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.24 = 0 ! 01.2.274.00.24 = 0! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!IM. CLIMB ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.13 = 1 ! 01.2.274.00.13 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!IM. DES Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.13 = 1 ! 01.2.274.00.13 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!OPEN CLB ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.14 = 1 ! 01.2.274.00.14 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!OPEN. DES ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.14 = 1 ! 01.2.274.00.14 = 1! ! |
| ! ! ---------------------------------------------------- ! |
| ! ! Auto Pilot Status DMU: ! |
| ! ! Auto Pilot AP1 printed in report line EC ! |
| ! ! Auto Pilot AP2 printed in report line EE ! |
| ! ! Combined Auto Pilot Modes ! |
| ! ! The longitudinal auto pilot mode (1 to G) shall ! |
| ! ! appear on the left position for the AP1 and AP2 print! |
| ! ! format. ! |
| ! ! The lateral auto pilot mode (1 to 8) shall appear on ! |
| ! ! the right position for the AP1 and AP2 print format. ! |
| ! ! In case of a combined auto pilot mode e.g. DES mode ! |
| ! ! and NAV mode are engaged simultaneously, the 'E3' ! |
| ! ! shall appear below AP1 and AP2. ! |
| ! ! XX Auto Pilot Modes: ! |
| ! ! !! ! |
| ! ! !!__Lateral Modes: 0 = NO MODE ! |
| ! ! ! 1 = HEADING ! |
| ! ! ! 2 = TRACK ! |
| ! ! ! 3 = NAV ! |
| ! ! ! 4 = LOC CAPTURE ! |
| ! ! ! 5 = LOCK TRACK ! |
| ! ! ! 6 = LAND TRACK ! |
| ! ! ! 7 = RUNWAY ! |
| ! ! ! 8 = ROLL GO AROUND ! |
| ! ! ! ! |
| ! ! !__Longitudinal Modes: 0 = NO MODE ! |
| ! ! 1 = PITCH G/A ! |
| ! ! 2 = PITCH TO ! |
| ! ! 3 = G/S TRACK ! |
| ! ! 4 = G/S CAPTURE ! |
| ! ! 5 = V/S ! |
| ! ! 6 = FPA ! |
| ! ! 7 = ALT ! |
| ! ! 8 = ALT ACQ ! |
| ! ! 9 = OPEN CLB ! |
| ! ! A = OPEN DES ! |
| ! ! B = IM CLB ! |
| ! ! C = IM DES ! |
| ! ! D = CLB ! |
| ! ! E = DES ! |
| ! ! F = FINAL DES ! |
| ! ! G = EXPEDITE ! |
| !--------------!------------------------------------------------------! |
| ! Y1 ! 'Y10.1' Seconds Programmed Pre-event Intervals ! |
| ! 99 ! DMU (1 to 6 sec) ! |
| !--------------!------------------------------------------------------! |
| ! Y2 ! 'Y10.2' Seconds Programmed Pre-event Intervals ! |
| ! 99 ! DMU (1 to 60 sec) ! |
| !--------------!------------------------------------------------------! |
| ! E ! Engine Position ! |
| ! 9 ! No. 1 or 2 for which the report is valid ! |
| !--------------!------------------------------------------------------! |
| ! MAX ! Maximal EGT during Engine Start Phase ! |
| ! X999 ! -55 to 999.9 deg C ! |
| ! ! Negative values are indicated by '-' on the first ! |
| ! ! position. Otherwise the first position is used for ! |
| ! ! the value. ! |
| ! ! ECU 7C.1.345.01 Engine 1 ! |
| ! ! 7C.2.345.10 Engine 2 ! |
| !--------------! -----------------------------------------------------! |
| ! LIM ! Limit ! |
| ! 9999 ! (-55 to 999.9 [C) ! |
| ! ! Negative values are indicated by '-' on the first ! |
| ! ! position. Otherwise the first position is used for ! |
| ! ! the value. ! |
| ! ! ECU 7C.1.345.01 Engine 1 ! |
| ! ! 7C.2.345.10 Engine 2 ! |
| !--------------! -----------------------------------------------------! |
| ! TOL ! - Time Over Limit for EGT Exceedance or ! |
| ! 999 ! - Time from SAV = Open to N2 = N2 trigger ! |
| ! ! Time in seconds ! |
| ! ! SAV open 7C.1.270.01.13 = 1 Engine 1 ! |
| ! ! 7C.2.270.10.13 = 1 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! TTP ! Time from SAV open to max EGT or to start abort ! |
| ! 999 ! Time in seconds ! |
| ! ! SAV open 7C.1.270.01.13 = 1 Engine 1 ! |
| ! ! 7C.2.270.10.13 = 1 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! TTF ! Time from SAV = open to fuel shut-of-valve = open ! |
| ! 999 ! Time in seconds ! |
| ! ! SAV open 7C.1.270.01.13 = 1 Engine 1 ! |
| ! ! 7C.2.270.10.13 = 1 Engine 2 ! |
| ! ! SAV open 7C.1.270.01.14 = 1 Engine 1 ! |
| ! ! 7C.2.270.10.14 = 1 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! PD ! Precooler Inlet Pressure ! |
| ! 99 ! 0 to 50 psi ! |
| ! ! BMC 6F.1.143.01 Engine 1 ! |
| ! ! 6F.2.143.10 ! |
| ! ! 6F.1.142.01 Engine 2 ! |
| ! ! 6F.2.142.10 ! |
| ! ! Remark: Report line N1: Precooler Inlet Pressure ! |
| ! ! at SAV = open ! |
| ! ! Report line SX: Precooler Inlet Pressure ! |
| ! ! (see parameter logic) ! |
| !--------------!------------------------------------------------------! |
| ! SM ! Start Mode ! |
| ! 1 ! Auto Start Sequence in Progress = 1 ! |
| ! ! ECU 7C.1.273.01.19 Engine 1 ! |
| ! ! 7C.1.273.10.19 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! Reason ! Reason for Exceedance ! |
| ! XXXXXXXXXX ! DMU Up to 20 characters ! |
| ! XXXXXXXXXX ! ! |
| ! ! SAV CODE: 4410 ! |
| ! ! HPSOV CODE: 4420 ! |
| ! ! EGT CODE: 4430 and 5000 ! |
| ! ! STALL CODE: 4440 ! |
| ! ! No Light off CODE: 4450 ! |
| ! ! Hung CODE: 4460 ! |
| ! ! Start Fail CODE: 4470 ! |
| ! ! Slow CODE: 4480 ! |
| ! ! ! |
| ! ! NOTE: If the report was not triggered by a limit ! |
| ! ! exceedance, this field contains blanks. ! |
| !--------------!------------------------------------------------------! |
| ! N1 ! Selected N1 Actual ! |
| ! 9999 ! (0 to 120.0 %rpm) ! |
| ! ! ECU 7C.1.346.01 Engine 1 ! |
| ! ! 7C.2.346.10 Engine 2 ! |
| ! ! Remark: In the report line V3 and V4 the values ! |
| ! ! from the last stable descent are printed. ! |
| ! ! In the report line V5 and V6 the values ! |
| ! ! from the last stable climb are printed. ! |
| !--------------!------------------------------------------------------! |
| ! N2 ! Selected N2 Actual ! |
| ! 9999 ! (0 to 120.0 %rpm) ! |
| ! ! ECU 7C.1.344.01 Engine 1 ! |
| ! ! 7C.2.344.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! EGT ! Selected T495 (Exhaust Gas Temperature) ! |
| ! X999 ! (-55 to 999.9 [C) ! |
| ! ! Negative values are indicated by '-' on the first ! |
| ! ! position. Otherwise the first position is used for ! |
| ! ! the value. ! |
| ! ! ECU 7C.1.345.01 Engine 1 ! |
| ! ! 7C.2.345.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! FF ! Engine Fuel Flow ! |
| ! 9999 ! 0 to 7000 kg/h (0 to 15000 p/h) ! |
| ! ! Report line N1: Fuel Flow 'Y3' seconds after ! |
| ! ! SAV = open ! |
| ! ! Report line SX: Fuel see parameter logic ! |
| ! ! ECU 7C.1.244.01 Engine 1 ! |
| ! ! 7C.2.244.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! FMV ! Selected Fuel Metering Valve Position ! |
| ! 999 ! 0 to 100% ! |
| ! ! ECU 7C.1.347.01 Engine 1 ! |
| ! ! 7C.1.347.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! T25 ! Selected T25 ! |
| ! X999 ! (-55.0 to 120.0 [C) ! |
| ! ! Negative values are indicated by '-' on the first ! |
| ! ! position. Otherwise the first position is used for ! |
| ! ! the value. ! |
| ! ! ECU 7C.1.263.01 Engine 1 ! |
| ! ! 7C.2.263.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! P3 ! Selected PS3 (Burner Pressure) ! |
| ! 9999 ! (0.0 to 450.0 psia) ! |
| ! ! ECU 7C.1.264.01 Engine 1 ! |
| ! ! 7C.2.264.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! T3 ! Selected T3 ! |
| ! X999 ! (-55.0 to 850.0 deg C) ! |
| ! ! Negative values are indicated by '-' on the first ! |
| ! ! position. Otherwise the first position is used for ! |
| ! ! the value. ! |
| ! ! ECU 7C.1.265.01 Engine 1 ! |
| ! ! 7C.2.265.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! VSV ! Selected Variable Stator Vane Position ! |
| ! X99 ! (-5.0 to 45.0 deg) ! |
| ! ! Negative values are indicated by '-' on the first ! |
| ! ! position. Otherwise the first position is used for ! |
| ! ! the value. ! |
| ! ! ECU 7C.1.072.01 Engine 1 ! |
| ! ! 7C.2.072.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! VBV ! Variable Bleed Valve Position ! |
| ! X99 ! (-9.9 to 40.0 deg) ! |
| ! ! Negative values are indicated by '-' on the first ! |
| ! ! position. Otherwise the first position is used for ! |
| ! ! the value. ! |
| ! ! ECU 7C.1.071.01 Engine 1 ! |
| ! ! 7C.2.071.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! T5 ! T5 Temperature at position T5 ! |
| ! X999 ! (-55.0 to 850.0 [C) ! |
| ! ! Negative values are indicated by '-' on the first ! |
| ! ! position. Otherwise the first position is used for ! |
| ! ! the value. ! |
| ! ! ECU 7C.1.260.01 Engine 1 ! |
| ! ! 7C.2.260.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! OIT ! Engine Oil Temperature ! |
| ! X99 ! (-60 to 250 deg C) ! |
| ! ! Negative values are indicated by '-' on the first ! |
| ! ! position. Otherwise the first position is used for ! |
| ! ! the value. ! |
| ! ! FWC 26.1.316.01 Engine 1 ! |
| ! ! 26.2.316.01 ! |
| ! ! 26.1.316.10 Engine 2 ! |
| ! ! 26.2.316.10 ! |
| !--------------!------------------------------------------------------! |
| ! ECW5 ! Engine Control Word 5 ! |
| ! XXXXX ! XXXXX Bits HEX ! |
| ! ! !!!!!________14, 13, 12, 11 0..F ! |
| ! ! !!!!_________18, 17, 16, 15 0..F ! |
| ! ! !!!__________22, 21, 20, 19 0..F ! |
| ! ! !!___________26, 25, 24, 23 0..F ! |
| ! ! !____________ 29, 28, 27 0..F ! |
| ! ! Bit Label Parameter Description ! |
| ! ! 11 7C.X.270.XX.11 = 1 Ignition 1 Primary Selected ! |
| ! ! 12 SPARE ! |
| ! ! 13 7C.X.270.XX.13 = 1 Starter Air Valve Open ! |
| ! ! Local Switch ! |
| ! ! 14 7C.X.270.XX.14 = 1 HP Fuel Valve Closed Local ! |
| ! ! 15 7C.X.270.XX.15 = 1 SAV Demand/Position Disagree! |
| ! ! 16 7C.X.270.XX.16 = 1 HPSOV Demand/Position ! |
| ! ! Disagree ! |
| ! ! 17 7C.X.270.XX.17 = 1 Start EGT Overtemp-Detected ! |
| ! ! 18 7C.X.270.XX.18 = 1 Start Stall Detected ! |
| ! ! 19 7C.X.270.XX.19 = 1 No/Low Fan Speed for Core ! |
| ! ! Speed ! |
| ! ! 20 7C.X.270.XX.20 = 1 No Engine Light Off Detected! |
| ! ! 21 7C.X.270.XX.21 = 1 Starter Time Limit Exceeded ! |
| ! ! 22 7C.X.270.XX.22 = 1 Fuel Schedule Derich Active ! |
| ! ! 23 7C.X.270.XX.23 = 1 TLA Not at Idle for Start ! |
| ! ! Initiation ! |
| ! ! 24 SPARE ! |
| ! ! 25 7C.X.270.XX.25 = 1 Low Sap-(Slow Start) ! |
| ! ! Detected ! |
| ! ! 26 7C.X.270.XX.28 = 1 50% Thrust Limit Active ! |
| ! ! 27 SPARE ! |
| ! ! 28 SPARE ! |
| ! ! 29 SPARE ! |
| ! ! The 'X' for the System and SDI definition of the ! |
| ! ! engine parameters shall be as follows: ! |
| ! ! System SDI ! |
| ! ! Engine 1 1 01 ! |
| ! ! Engine 2 2 10 ! |
| +---------------------------------------------------------------------+ |
(5) Engine Start Report Data Field Description <10> (Engine Type CFMI with Advanced EVMU)
NOTE: Reports that are transmitted from the ACARS system do not have report lines without a line identifier.
| +---------------------------------------------------------------------+ |
| ! Value ! Content Description ! |
| !--------------!------------------------------------------------------! |
| ! ESN ! Engine Serial Number ! |
| ! 999999 ! (000000 to 999999) ! |
| ! ! ECU Engine 1 7C.1.046.01 digit 3, 2, 1 ! |
| ! ! 7C.1.047.01 digit 6, 5, 4 ! |
| ! ! Engine 2 7C.2.046.10 digit 3, 2, 1 ! |
| ! ! 7C.2.047.10 digit 6, 5, 4 ! |
| !--------------!------------------------------------------------------! |
| ! EHRS ! Engine Flight Hours ! |
| ! 99999 ! (00000 to 99999 hours) ! |
| ! ! DMU Engine 1 ! |
| ! ! Engine 2 ! |
| ! ! Remark: Time between "Main (LH and RH) Landing Gear! |
| ! ! Decompressed" and "Main (LH and RH) Landing! |
| ! ! Gear Compressed". The EHRS shall be set to ! |
| ! ! zero if a new ESN is recognized by the DMU.! |
| ! ! It shall be possible to set the EHRS via ! |
| ! ! the MCDU, e.g. if the DMU is changed on the! |
| ! ! a/c. ! |
| !--------------!------------------------------------------------------! |
| ! ERT ! Engine Running Time ! |
| ! 99999 ! (00000 to 65536 hours) ! |
| ! ! ECU 7C.1.050.01 Engine 1 ! |
| ! ! 7C.2.050.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! ECYC ! Engine Cycle ! |
| ! 99999 ! (00000 to 99999) ! |
| ! ! DMU Engine 1 ! |
| ! ! Engine 2 ! |
| ! ! Remark: Each time when flight phase 5 (climb) is ! |
| ! ! reached, the counter shall be incremented ! |
| ! ! by one. The ECYC is set to zero if a new ! |
| ! ! ESN is recognized by the DMU. It shall be ! |
| ! ! possible to set ECYC via the MCDU, if the ! |
| ! ! DMU is changed on the a/c. ! |
| !--------------!------------------------------------------------------! |
| ! AP ! Auto Pilot Status ! |
| ! 99 ! Number of respective status (00 to G8) ! |
| ! ! FMGC 1 and 2 (FGC part) for Auto Pilot AP1 and AP2 ! |
| ! ! ! |
| ! ! Parameter for AP1 ! Parameter for AP2 ! ! |
| ! ! Report Line EC: ! Report Line EE: !Definition: ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! / ! / !No Mode ! |
| ! ! ! !Active ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.11 = 1 ! 01.2.275.00.11 = 1!RUNWAY Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.12 = 1 ! 01.2.275.00.12 = 1!NAV Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.13 = 1 ! 01.2.275.00.13 = 1!LOC CAPTURE ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.14 = 1 ! 01.2.275.00.14 = 1!LOC TRACK ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.15 = 1 ! 01.2.275.00.15 = 1!Roll GO ! |
| ! ! ! !AROUND Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.16 = 1 ! 01.2.275.00.16 = 1!HEADING Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.17 = 1 ! 01.2.275.00.17 = 1!TRACK Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.15 = 1 ! 01.2.274.00.15 = 1!PITCH T/O ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.16 = 1 ! 01.2.274.00.16 = 1!PITCH GA Mode! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.17 = 1 ! 01.2.274.00.17 = 1!V/S Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.18 = 1 ! 01.2.274.00.18 = 1!FPA Mode ! |
| ! ! -------------------!-------------------!-------------! |
| ! ! 01.1.274.00.19 = 1 ! 01.2.274.00.19 = 1!ALT Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.20 = 1 ! 01.2.274.00.20 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.19 = 1 ! 01.2.274.00.19 = 1!ALT ACQ ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.21 = 1 ! 01.2.274.00.21 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.20 = 1 ! 01.2.274.00.20 = 1!G/S TRACK ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.22 = 1 ! 01.2.274.00.22 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.21 = 1 ! 01.2.274.00.21 = 1!G/S CAPTURE ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.22 = 1 ! 01.2.274.00.22 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.23 = 1 ! 01.2.274.00.23 = 1!FINAL DES ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.24 = 1 ! 01.2.274.00.24 = 1!EXPED. Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.146.00.14 = 1 ! 01.2.146.00.14 = 1!LAND TRACK ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!CLB Mode ! |
| ! ! AND ! AND ! ! |
| ! ! ! ! ! ! ! |
| ! ! -------------- ! -------------- ! ! |
| ! ! 01.1.274.00.13 = 0 ! 01.2.274.00.13 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.14 = 0 ! 01.2.274.00.14 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.24 = 0 ! 01.2.274.00.24 = 0! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!DES Mode ! |
| ! ! AND ! AND ! ! |
| ! ! ! ! ! ! ! |
| ! ! -------------- ! -------------- ! ! |
| ! ! 01.1.274.00.13 = 0 ! 01.2.274.00.13 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.14 = 0 ! 01.2.274.00.14 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.24 = 0 ! 01.2.274.00.24 = 0! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!IM. CLIMB ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.13 = 1 ! 01.2.274.00.13 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!IM. DES Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.13 = 1 ! 01.2.274.00.13 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!OPEN CLB ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.14 = 1 ! 01.2.274.00.14 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!OPEN. DES ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.14 = 1 ! 01.2.274.00.14 = 1! ! |
| ! ! ---------------------------------------------------- ! |
| ! ! Auto Pilot Status DMU: ! |
| ! ! Auto Pilot AP1 printed in report line EC ! |
| ! ! Auto Pilot AP2 printed in report line EE ! |
| ! ! Combined Auto Pilot Modes ! |
| ! ! The longitudinal auto pilot mode (1 to G) shall ! |
| ! ! appear on the left position for the AP1 and AP2 print! |
| ! ! format. ! |
| ! ! The lateral auto pilot mode (1 to 8) shall appear on ! |
| ! ! the right position for the AP1 and AP2 print format. ! |
| ! ! In case of a combined auto pilot mode e.g. DES mode ! |
| ! ! and NAV mode are engaged simultaneously, the 'E3' ! |
| ! ! shall appear below AP1 and AP2. ! |
| ! ! XX Auto Pilot Modes: ! |
| ! ! !! ! |
| ! ! !!__Lateral Modes: 0 = NO MODE ! |
| ! ! ! 1 = HEADING ! |
| ! ! ! 2 = TRACK ! |
| ! ! ! 3 = NAV ! |
| ! ! ! 4 = LOC CAPTURE ! |
| ! ! ! 5 = LOCK TRACK ! |
| ! ! ! 6 = LAND TRACK ! |
| ! ! ! 7 = RUNWAY ! |
| ! ! ! 8 = ROLL GO AROUND ! |
| ! ! ! ! |
| ! ! !__Longitudinal Modes: 0 = NO MODE ! |
| ! ! 1 = PITCH G/A ! |
| ! ! 2 = PITCH TO ! |
| ! ! 3 = G/S TRACK ! |
| ! ! 4 = G/S CAPTURE ! |
| ! ! 5 = V/S ! |
| ! ! 6 = FPA ! |
| ! ! 7 = ALT ! |
| ! ! 8 = ALT ACQ ! |
| ! ! 9 = OPEN CLB ! |
| ! ! A = OPEN DES ! |
| ! ! B = IM CLB ! |
| ! ! C = IM DES ! |
| ! ! D = CLB ! |
| ! ! E = DES ! |
| ! ! F = FINAL DES ! |
| ! ! G = EXPEDITE ! |
| !--------------!------------------------------------------------------! |
| ! Y1 ! 'Y10.1' Seconds Programmed Pre-event Intervals ! |
| ! 99 ! DMU (1 to 6 sec) ! |
| !--------------!------------------------------------------------------! |
| ! Y2 ! 'Y10.2' Seconds Programmed Pre-event Intervals ! |
| ! 99 ! DMU (1 to 60 sec) ! |
| !--------------!------------------------------------------------------! |
| ! E ! Engine Position ! |
| ! 9 ! No. 1 or 2 for wich the report is valid ! |
| !--------------!------------------------------------------------------! |
| ! MAX ! Maximal EGT during Engine Start Phase ! |
| ! X999 ! -55 to 999.9 deg C ! |
| ! ! Negative values are indicated by 'N' on the ! |
| ! ! first position. Otherwise the first position is ! |
| ! ! used for the value. ! |
| ! ! ECU 7C.1.345.01 Engine 1 ! |
| ! ! 7C.2.345.10 Engine 2 ! |
| !--------------! -----------------------------------------------------! |
| ! LIM ! Programmable EGT Limit ! |
| ! 9999 ! (-55 to 999.9 degC) ! |
| ! ! Negative values are indicated by 'N' on the ! |
| ! ! first position. Otherwise the first position is ! |
| ! ! used for the value. ! |
| ! ! ECU 7C.1.345.01 Engine 1 ! |
| ! ! 7C.2.345.10 Engine 2 ! |
| !--------------! -----------------------------------------------------! |
| ! TOL ! - Time Over Limit for EGT Exceedance or ! |
| ! 999 ! - Time from SAV = Open to N2 = N2 trigger ! |
| ! ! Time in seconds ! |
| ! ! SAV open 7C.1.270.01.13 = 1 Engine 1 ! |
| ! ! 7C.2.270.10.13 = 1 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! TTP ! Time from SAV open to max EGT or to start about ! |
| ! 999 ! Time in seconds ! |
| ! ! SAV open 7C.1.270.01.13 = 1 Engine 1 ! |
| ! ! 7C.2.270.10.13 = 1 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! TTF ! Time from SAV = open to fuel shut-of-valve = open ! |
| ! 999 ! Time in seconds ! |
| ! ! SAV open 7C.1.270.01.13 = 1 Engine 1 ! |
| ! ! 7C.2.270.10.13 = 1 Engine 2 ! |
| ! ! SAV open 7C.1.270.01.14 = 1 Engine 1 ! |
| ! ! 7C.2.270.10.14 = 1 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! PD ! Precooler Inlet Pressure ! |
| ! 99 ! 0 to 50 psi ! |
| ! ! BMC 6F.1.143.01 Engine 1 ! |
| ! ! 6F.2.143.10 ! |
| ! ! 6F.1.142.01 Engine 2 ! |
| ! ! 6F.2.142.10 ! |
| ! ! Remark: Report line N1: Precooler Inlet Pressure ! |
| ! ! at SAV = open ! |
| ! ! Report line SX: Precooler Inlet Pressure ! |
| ! ! (see parameter logic) ! |
| !--------------!------------------------------------------------------! |
| ! SM ! Start Mode ! |
| ! 1 ! Auto Start Sequence in Progress = 1 ! |
| ! ! ECU 7C.1.273.01.19 Engine 1 ! |
| ! ! 7C.2.273.01.19 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! N1 ! Selected N1 Actual ! |
| ! 9999 ! (0 to 120.0 %rpm) ! |
| ! ! ECU 7C.1.346.01 Engine 1 ! |
| ! ! 7C.2.346.10 Engine 2 ! |
| ! ! Remark: In the report line V3 and V4 the values ! |
| ! ! from the last stable descent shall be ! |
| ! ! printed. ! |
| ! ! In the report line V5 and V6 the values ! |
| ! ! from the last stable climb shall be ! |
| ! ! printed. ! |
| !--------------!------------------------------------------------------! |
| ! N2 ! Selected N2 Actual ! |
| ! 9999 ! (0 to 120.0 %rpm) ! |
| ! ! ECU 7C.1.344.01 Engine 1 ! |
| ! ! 7C.2.344.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! EGT ! Selected T495 (Exhaust Gas Temperature) ! |
| ! X999 ! (-55 to 999.9 [C) ! |
| ! ! Negative values are indicated by 'N' on the ! |
| ! ! first position. Otherwise the first position is ! |
| ! ! used for the value. ! |
| ! ! ECU 7C.1.345.01 Engine 1 ! |
| ! ! 7C.2.345.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! FF ! Engine Fuel Flow ! |
| ! 9999 ! 0 to 7000 kg/h (0 to 15000 p/h) ! |
| ! ! Report line N1: Fuel Flow 'Y3' seconds after ! |
| ! ! SAV = open ! |
| ! ! Report line SX: Fuel see parameter logic ! |
| ! ! ECU 7C.1.244.01 Engine 1 ! |
| ! ! 7C.2.244.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! FMV ! Selected Fuel Metering Valve Position ! |
| ! 999 ! 0 to 100% ! |
| ! ! ECU 7C.1.347.01 Engine 1 ! |
| ! ! 7C.1.347.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! T25 ! Selected T25 ! |
| ! X999 ! (-55.0 to 120.0 [C) ! |
| ! ! Negative values are indicated by 'N' on the ! |
| ! ! first position. Otherwise the first position is ! |
| ! ! used for the value. ! |
| ! ! ECU 7C.1.263.01 Engine 1 ! |
| ! ! 7C.2.263.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! P3 ! Selected PS3 (Burner Pressure) ! |
| ! 9999 ! (0.0 to 450.0 psia) ! |
| ! ! ECU 7C.1.264.01 Engine 1 ! |
| ! ! 7C.2.264.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! T3 ! Selected T3 ! |
| ! X999 ! (-55.0 to 850.0 deg C) ! |
| ! ! Negative values are indicated by 'N' on the ! |
| ! ! first position. Otherwise the first position is ! |
| ! ! used for the value. ! |
| ! ! ECU 7C.1.265.01 Engine 1 ! |
| ! ! 7C.2.265.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! VSV ! Selected Variable Stator Vane Position ! |
| ! X99 ! (-5.0 to 45.0 deg) ! |
| ! ! Negative values are indicated by 'N' on the ! |
| ! ! first position. Otherwise the first position is ! |
| ! ! used for the value. ! |
| ! ! ECU 7C.1.072.01 Engine 1 ! |
| ! ! 7C.2.072.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! VBV ! Variable Bleed Valve Position ! |
| ! X99 ! (-9.9 to 40.0 deg) ! |
| ! ! Negative values are indicated by 'N' on the ! |
| ! ! first position. Otherwise the first position is ! |
| ! ! used for the value. ! |
| ! ! ECU 7C.1.071.01 Engine 1 ! |
| ! ! 7C.2.071.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! T5 ! T5 Temperature at position T5 ! |
| ! X999 ! (-55.0 to 850.0 [C) ! |
| ! ! Negative values are indicated by 'N' on the ! |
| ! ! first position. Otherwise the firt position is ! |
| ! ! used for the value. ! |
| ! ! ECU 7C.1.260.01 Engine 1 ! |
| ! ! 7C.2.260.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! OIT ! Engine Oil Temperature ! |
| ! X99 ! (-60 to 250 deg C) ! |
| ! ! Negative values are indicated by 'N' on the ! |
| ! ! first position. Otherwise the firt position is ! |
| ! ! used for the value. ! |
| ! ! FWC 26.1.316.01 Engine 1 ! |
| ! ! 26.2.316.01 ! |
| ! ! 26.1.316.10 Engine 2 ! |
| ! ! 26.2.316.10 ! |
| !--------------!------------------------------------------------------! |
| ! ECW5 ! Engine Control Word 5 ! |
| ! XXXXX ! XXXXX Bits HEX ! |
| ! ! !!!!!________14, 13, 12, 11 0..F ! |
| ! ! !!!!_________18, 17, 16, 15 0..F ! |
| ! ! !!!__________22, 21, 20, 19 0..F ! |
| ! ! !!___________26, 25, 24, 23 0..F ! |
| ! ! !____________ 29, 28, 27 0..F ! |
| ! ! Bit Label Parameter Description ! |
| ! ! 11 7C.X.270.XX.11 = 1 Ignition 1 Primary Selected ! |
| ! ! 12 SPARE ! |
| ! ! 13 7C.X.270.XX.13 = 1 Starter Air Valve Open ! |
| ! ! Local Switch ! |
| ! ! 14 7C.X.270.XX.14 = 1 HP Fuel Valve Closed Local ! |
| ! ! 15 7C.X.270.XX.15 = 1 SAV Demand/Position Disagree! |
| ! ! 16 7C.X.270.XX.16 = 1 HPSOV Demand/Position ! |
| ! ! Disagree ! |
| ! ! 17 7C.X.270.XX.17 = 1 Start EGT Overtemp-Detected ! |
| ! ! 18 7C.X.270.XX.18 = 1 Start Stall Detected ! |
| ! ! 19 7C.X.270.XX.19 = 1 No/Low Fan Speed for Core ! |
| ! ! Speed ! |
| ! ! 20 7C.X.270.XX.20 = 1 No Engine Light Off Detected! |
| ! ! 21 7C.X.270.XX.21 = 1 Starter Time Limit Exceeded ! |
| ! ! 22 7C.X.270.XX.22 = 1 Fuel Schedule Derich Active ! |
| ! ! 23 7C.X.270.XX.23 = 1 TLA Not at Idle for Start ! |
| ! ! Initiation ! |
| ! ! 24 SPARE ! |
| ! ! 25 7C.X.270.XX.25 = 1 Low Sap-(Slow Start) ! |
| ! ! Detected ! |
| ! ! 26 7C.X.270.XX.28 = 1 50% Thrust Limit Active ! |
| ! ! 27 SPARE ! |
| ! ! 28 SPARE ! |
| ! ! 29 SPARE ! |
| ! ! The 'X' for the System and SDI definition of the ! |
| ! ! engine parameters shall be as follows: ! |
| ! ! System SDI ! |
| ! ! Engine 1 1 01 ! |
| ! ! Engine 2 2 10 ! |
| +---------------------------------------------------------------------+ |
(6) Engine Start Report Data Field Description <10> (Engine Type CFMI with Advanced EVMU)
NOTE: Reports that are transmitted from the ACARS system do not have report lines without a line identifier.
NOTE: Only the parts of the ENGINE START REPORT <10> which are not included in the ENGINE CRUISE REPORT <01> are given in the subsequent table.
| +---------------------------------------------------------------------+ |
| ! Value ! Content Description ! |
| !--------------!------------------------------------------------------! |
| ! Y1 ! 'Y10.1' seconds programmed Pre-event Intervals ! |
| ! 99 ! DMU (1 to 6 sec.) ! |
| !--------------!------------------------------------------------------! |
| ! Y2 ! 'Y10.2' seconds programmed Post-event Intervals ! |
| ! 99 ! DMU (1 to 60 sec.) ! |
| !--------------!------------------------------------------------------! |
| ! E ! Engine Position ! |
| ! 9 ! DMU ! |
| ! ! No. 1 or 2 of engine for which the report is valid ! |
| !--------------!------------------------------------------------------! |
| ! MAX ! Maximal EGT During Engine Start Phase ! |
| ! X999 ! (-55 to 999.9 deg. C) ! |
| ! ! Engine 1 7C.1.345.01 ! |
| ! ! Engine 2 7C.2.345.10 ! |
| ! ! Negative values are shown with '-' at the first ! |
| ! ! position. Otherwise the first position is used ! |
| ! ! for the value. ! |
| !--------------!------------------------------------------------------! |
| ! LIM ! Programmed EGT limit ! |
| ! X999 ! ECU (-55 to 999.9 deg. C) ! |
| ! ! Engine 1 7C.1.345.01 ! |
| ! ! Engine 2 7C.2.345.10 ! |
| ! ! Negative values are shown with '-' at the first ! |
| ! ! position. Otherwise the first position is used ! |
| ! ! for the value. ! |
| !--------------!------------------------------------------------------! |
| ! TOL ! - Time Over Limit for EGT Exceedance or ! |
| ! 999 ! - Time from SAV = open to N2 = N2 trigger ! |
| ! ! DMU Time in seconds ! |
| ! ! Engine 1 7C.1.270.01.13 = 1 SAV open ! |
| ! ! Engine 2 7C.2.270.10.13 = 1 ! |
| !--------------!------------------------------------------------------! |
| ! TTP ! Time from SAV open to max EGT or to start abort ! |
| ! 999 ! DMU Time in seconds ! |
| ! ! Engine 1 7C.1.270.01.13 = 1 SAV open ! |
| ! ! Engine 2 7C.2.270.10.13 = 1 ! |
| !--------------!------------------------------------------------------! |
| ! TTF ! Time from SAV open to Fuel Shut-Off Valve = open ! |
| ! 999 ! DMU Time in seconds ! |
| ! ! Engine 1 7C.1.270.01.13 = 1 = SAV open ! |
| ! ! Engine 2 7C.2.270.10.13 = 1 ! |
| ! ! Engine 1 7C.1.270.01.14 = 0 = Fuel Shut-Off ! |
| ! ! Engine 2 7C.2.270.10.14 = 0 Valve open ! |
| !--------------!------------------------------------------------------! |
| ! FF ! Report Line N1: Fuel Flow 'Y3' seconds after ! |
| ! 9999 ! SAV = open ! |
| ! ! Report Line SX: Fuel Flow (see parameter logic) ! |
| ! ! ECU 0 to 7000 kg/h (0 to 15000p/h) ! |
| ! ! Engine 1 7C.1.244.01 ! |
| ! ! Engine 2 7C.2.244.10 ! |
| !--------------!------------------------------------------------------! |
| ! PD ! Precooler Inlet Pressure ! |
| ! 99 ! Report Line N1: Precooler Inlet Pressure at ! |
| ! ! SAV = open ! |
| ! ! Report Line SX: Precooler Inlet Pressure ! |
| ! ! (see parameter logic) ! |
| ! ! BMC (0 to 50 psi) ! |
| ! ! Engine 1 6F.1.143.01 ! |
| ! ! 6F.2.143.10 ! |
| ! ! Engine 2 6F.1.142.01 ! |
| ! ! 6F.2.142.10 ! |
| !--------------!------------------------------------------------------! |
| ! SM ! Start Mode ! |
| ! 1 ! ECU ! |
| ! ! Auto start sequence in progress = 1 ! |
| ! ! Engine 1 7C.1.273.01.19 ! |
| ! ! Engine 2 7C.2.273.10.19 ! |
| !--------------!------------------------------------------------------! |
| ! Reason ! Reason for Exceedance ! |
| ! XXXXXXXXXX ! DMU Up to 20 characters ! |
| ! XXXXXXXXXX ! ! |
| ! ! SAV CODE: 4410 ! |
| ! ! HPSOV CODE: 4420 ! |
| ! ! EGT CODE: 4430 and 5000 ! |
| ! ! STALL CODE: 4440 ! |
| ! ! No Light off CODE: 4450 ! |
| ! ! Hung CODE: 4460 ! |
| ! ! Start Fail CODE: 4470 ! |
| ! ! Slow CODE: 4480 ! |
| ! ! ! |
| ! ! NOTE: If the report was not triggered by one of the! |
| ! ! above codes, this field contains blanks. ! |
| !--------------!------------------------------------------------------! |
| ! ECW5 ! Engine Control Word 5 ! |
| ! XXXXX ! Each 'X' represents 4 Bits in hexadecimal code of ! |
| ! ! a defined ARINC 429 word: ! |
| ! ! XXXXX Bits HEX ! |
| ! ! !!!!!___________ 14, 13, 12, 11 0...F ! |
| ! ! !!!!____________ 18, 17, 16, 15 0...F ! |
| ! ! !!!_____________ 22, 21, 20, 19 0...F ! |
| ! ! !!______________ 26, 25, 24, 23 0...F ! |
| ! ! !_______________ 29, 28, 27 0...7 ! |
| ! ! ! |
| ! ! DMU, composed of several ECU discrete labels as ! |
| ! ! defined below. For engine 1 and engine 2. ! |
| ! ! The 'X' for the System and SDI definition of the ! |
| ! ! engine parameters are given as follows. ! |
| ! ! ! |
| ! ! System SDI ! |
| ! ! Engine 1 1 01 ! |
| ! ! Engine 2 2 10 ! |
| ! ! --------------------------------------------- ! |
| ! ! Bit Label Parameter Description ! |
| ! ! 11 7C.X.270.XX.11 = 1 Ignition 1 Primary Selected! |
| ! ! 12 SPARE ! |
| ! ! 13 7C.X.270.XX.13 = 1 Starter Air Valve Open ! |
| ! ! Local Switch ! |
| ! ! 14 7C.X.270.XX.14 = 1 HP Fuel Valve Closed Local ! |
| ! ! 15 7C.X.270.XX.15 = 1 SAV Demand/Position ! |
| ! ! Disagree ! |
| ! ! 16 7C.X.270.XX.16 = 1 HPSOV Demand/Position ! |
| ! ! Disagree ! |
| ! ! 17 7C.X.270.XX.17 = 1 Start EGT Overtemp Detected! |
| ! ! 18 7C.X.270.XX.18 = 1 Start Stall Detected ! |
| ! ! 19 7C.X.270.XX.19 = 1 No/Low Fan Speed for Core ! |
| ! ! Speed ! |
| ! ! 20 7C.X.270.XX.20 = 1 No Eng. Light Off Detecetd ! |
| ! ! 21 7C.X.270.XX.21 = 1 Starter Time Limit Exceeded! |
| ! ! 22 7C.X.270.XX.22 = 1 Fuel Schedule Derich Active! |
| ! ! 23 7C.X.270.XX.23 = 1 TLA Not at Idle for Start ! |
| ! ! Initiation ! |
| ! ! 24 SPARE ! |
| ! ! 25 7C.X.270.XX.25 = 1 Low Sap - (Slow Start) ! |
| ! ! Detected ! |
| ! ! 26 7C.X.275.XX.28 = 1 All Channel Controls Active! |
| ! ! 27 SPARE ! |
| ! ! 28 SPARE ! |
| ! ! 29 SPARE ! |
| +---------------------------------------------------------------------+ |
(7) Engine Start Report Data Field Description <10> (Engine Type CFMI with Advanced EVMU)
NOTE: Reports that are transmitted from the ACARS system do not have report lines without a line identifier.
NOTE: Only the parts of the ENGINE START REPORT <10> which are not included in the ENGINE CRUISE REPORT <01> are given in the subsequent table.
| +---------------------------------------------------------------------+ |
| ! Value ! Content Description ! |
| !--------------!------------------------------------------------------! |
| ! Y1 ! 'Y10.1' seconds programmed Pre-event Intervals ! |
| ! 99 ! DMU (1 to 6 sec.) ! |
| !--------------!------------------------------------------------------! |
| ! Y2 ! 'Y10.2' seconds programmed Post-event Intervals ! |
| ! 99 ! DMU (1 to 60 sec.) ! |
| !--------------!------------------------------------------------------! |
| ! E ! Engine Position ! |
| ! 9 ! DMU ! |
| ! ! No. 1 or 2 of engine for which the report is valid ! |
| !--------------!------------------------------------------------------! |
| ! MAX ! Maximal EGT During Engine Start Phase ! |
| ! X999 ! (-55 to 999.9 deg. C) ! |
| ! ! ECU Engine 1 7C.1.345.01 ! |
| ! ! Engine 2 7C.2.345.10 ! |
| ! ! Negative values are shown with 'N' at the first ! |
| ! ! position. Otherwise the first position is used ! |
| ! ! for the value. ! |
| !--------------!------------------------------------------------------! |
| ! FMV ! Selected Fuel Metering Valve Position ! |
| ! 999 ! (0 to 100%) ! |
| ! ! ECU Engine 1 7C.1.347.01 ! |
| ! ! Engine 2 7C.2.347.10 ! |
| !--------------!------------------------------------------------------! |
| ! LIM ! Programmed EGT limit ! |
| ! X999 ! (-55 to 999.9 °C) ! |
| ! ! ECU Engine 1 7C.1.345.01 ! |
| ! ! Engine 2 7C.2.345.10 ! |
| ! ! Negative values are shown with 'N' at the first ! |
| ! ! position. Otherwise the first position is used ! |
| ! ! for the value. ! |
| !--------------!------------------------------------------------------! |
| ! TOL ! - Time Over Limit for EGT Exceedance or ! |
| ! 999 ! - Time from SAV = Open to N2 = N2 trigger ! |
| ! ! DMU Time in seconds ! |
| ! ! Engine 1 7C.1.270.01.13 = 1 SAV open ! |
| ! ! Engine 2 7C.2.270.10.13 = 1 ! |
| !--------------!------------------------------------------------------! |
| ! TTP ! Time from SAV open to max EGT or to start abort ! |
| ! 999 ! DMU Time in seconds ! |
| ! ! Engine 1 7C.1.270.01.13 = 1 SAV open ! |
| ! ! Engine 2 7C.2.270.10.13 = 1 ! |
| !--------------!------------------------------------------------------! |
| ! TTF ! Time from SAV = open to fuel shut-off-valve = open ! |
| ! 999 ! DMU Time in seconds ! |
| ! ! Engine 1 7C.1.270.01.13 = 1 SAV open ! |
| ! ! Engine 2 7C.2.270.10.13 = 1 ! |
| ! ! Fuel shut-off-valve open ! |
| ! ! Engine 1 7C.1.270.01.14 = 0 ! |
| ! ! Engine 2 7C.2.270.10.14 = 0 ! |
| !--------------!------------------------------------------------------! |
| ! FF ! Report Line N1: Fuel Flow 'Y3' seconds after ! |
| ! 9999 ! SAV = open ! |
| ! ! Report Line SX: Fuel Flow (see parameter logic) ! |
| ! ! ECU 0 to 7000 kg/h (0 to 15000p/h) ! |
| ! ! Engine 1 7C.1.345.01 ! |
| ! ! Engine 2 7C.2.345.10 ! |
| !--------------!------------------------------------------------------! |
| ! PD ! Report Line N1: Precooler Inlet Pressure at ! |
| ! 9999 ! SAV = open ! |
| ! ! Report Line SX: Precooler Inlet Pressure ! |
| ! ! (see parameter logic) ! |
| ! ! BMC (0 to 50 psi) ! |
| ! ! Engine 1 6F.1.143.01 ! |
| ! ! 6F.2.143.10 ! |
| ! ! Engine 2 6F.1.142.01 ! |
| ! ! 6F.2.142.10 ! |
| !--------------!------------------------------------------------------! |
| ! SM ! Start Mode ! |
| ! 1 ! Auto Start Sequence in Progress = 1 ! |
| ! ! ECU Engine 1 7C.1.273.01.19 ! |
| ! ! Engine 2 7C.2.273.10.19 ! |
| !--------------!------------------------------------------------------! |
| ! REASON ! Reason for Exceedance ! |
| ! XXXXXXXXXX ! DMU (Up to 20 characters) ! |
| ! XXXXXXXXXX ! SAV Code: 4410 ! |
| ! ! HPSOV Code: 4420 ! |
| ! ! EGT Code: 4430 and 5000 ! |
| ! ! STALL Code: 4440 ! |
| ! ! NO LIGHT OFF Code: 4450 ! |
| ! ! HUNG Code: 4460 ! |
| ! ! START FAIL Code: 4470 ! |
| ! ! SLOW Code: 4480 ! |
| ! ! ! |
| ! ! NOTE: If the report was not triggered by a limit ! |
| ! ! exceedance, this field contains blanks. ! |
| !--------------!------------------------------------------------------! |
| ! ECW5 ! Engine Control Word 5 ! |
| ! XXXXX ! Each 'X' represents 4 Bits in hexadecimal code of ! |
| ! ! a defined ARINC 429 word: ! |
| ! ! XXXXX Bits HEX ! |
| ! ! !!!!!___________ 14, 13, 12, 11 0...F ! |
| ! ! !!!!____________ 18, 17, 16, 15 0...F ! |
| ! ! !!!_____________ 22, 21, 20, 19 0...F ! |
| ! ! !!______________ 26, 25, 24, 23 0...F ! |
| ! ! !_______________ 29, 28, 27 0...7 ! |
| ! ! ! |
| ! ! DMU, composed of several ECU discrete labels as ! |
| ! ! defined below for engine 1 and engine 2. ! |
| ! ! The 'X' for the System and SDI definition of the ! |
| ! ! engine parameters are given as follows. ! |
| ! ! ! |
| ! ! System SDI ! |
| ! ! Engine 1 1 01 ! |
| ! ! Engine 2 2 10 ! |
| ! ! --------------------------------------------- ! |
| ! ! Bit Label Parameter Description ! |
| ! ! 11 7C.X.270.XX.11 = 1 Ignition 1 Primary Selected! |
| ! ! 12 SPARE ! |
| ! ! 13 7C.X.270.XX.13 = 1 Starter Air Valve Open ! |
| ! ! Local Switch ! |
| ! ! 14 7C.X.270.XX.14 = 1 HP Fuel Valve Closed Local ! |
| ! ! 15 7C.X.270.XX.15 = 1 SAV Demand/Position ! |
| ! ! Disagree ! |
| ! ! 16 7C.X.270.XX.16 = 1 HPSOV Demand/Position ! |
| ! ! Disagree ! |
| ! ! 17 7C.X.270.XX.17 = 1 Start EGT Overtemp Detected! |
| ! ! 18 7C.X.270.XX.18 = 1 Start Stall Detected ! |
| ! ! 19 7C.X.270.XX.19 = 1 No/Low Fan Speed for Core ! |
| ! ! Speed ! |
| ! ! 20 7C.X.270.XX.20 = 1 No Eng. LightOff Detecetd ! |
| ! ! 21 7C.X.270.XX.21 = 1 Starter Time Limit Exceeded! |
| ! ! 22 7C.X.270.XX.22 = 1 Fuel Schedule Derich Active! |
| ! ! 23 7C.X.270.XX.23 = 1 TLA Not at Idle for Start ! |
| ! ! Initiation ! |
| ! ! 24 SPARE ! |
| ! ! 25 7C.X.270.XX.25 = 1 Low Sap - (Slow Start) ! |
| ! ! Detected ! |
| ! ! 26 7C.X.275.XX.28 = 1 All Channel Controls Active! |
| ! ! 27 SPARE ! |
| ! ! 28 SPARE ! |
| ! ! 29 SPARE ! |
| +---------------------------------------------------------------------+ |
(8) Parameter Logic
| +---------------------------------------------------------------------+ |
| ! Param. ! Print Value (Standard Progr.) ! |
| !--------------!------------------------------------------------------! |
| ! ESN ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! EHRS ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! ERT ! Value at moment of trigger ! |
| !--------------! -----------------------------------------------------! |
| ! ECYC ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! AP ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! Y1 ! Programmed 'Y10.1' pre-event intervals ! |
| !--------------!------------------------------------------------------! |
| ! Y2 ! Programmed 'Y10.2' post-event intervals ! |
| !--------------!------------------------------------------------------! |
| ! E ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! MAX ! Highest value during observing time ! |
| !--------------!------------------------------------------------------! |
| ! LIM ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! TOL ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! TTP ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! TTF ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! FF ! Report line N1: value 'Y10.3' sec. after SAV = open! |
| !--------------!------------------------------------------------------! |
| ! PD ! Report line N1: value at moment of SAV = open ! |
| !--------------!------------------------------------------------------! |
| ! SM ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! N1 ! Snapshot at 'Y10.1' and 'Y10.2' seconds intervals. ! |
| !--------------!------------------------------------------------------! |
| ! N2 ! Snapshot at 'Y10.1' and 'Y10.2' seconds intervals. ! |
| !--------------!------------------------------------------------------! |
| ! EGT ! Snapshot at 'Y10.1' and 'Y10.2' seconds intervals. ! |
| !--------------!------------------------------------------------------! |
| ! FF ! Snapshot at 'Y10.1' and 'Y10.2' seconds intervals. ! |
| !--------------!------------------------------------------------------! |
| ! FMV ! Snapshot at 'Y10.1' and 'Y10.2' seconds intervals. ! |
| !--------------!------------------------------------------------------! |
| ! T25 ! Snapshot at 'Y10.1' and 'Y10.2' seconds intervals. ! |
| !--------------!------------------------------------------------------! |
| ! PD ! Snapshot at 'Y10.1' and 'Y10.2' seconds intervals. ! |
| !--------------!------------------------------------------------------! |
| ! P3 ! Snapshot at 'Y10.1' and 'Y10.2' seconds intervals. ! |
| !--------------!------------------------------------------------------! |
| ! T3 ! Snapshot at 'Y10.1' and 'Y10.2' seconds intervals. ! |
| !--------------!------------------------------------------------------! |
| ! VSV ! Snapshot at 'Y10.1' and 'Y10.2' seconds intervals. ! |
| !--------------!------------------------------------------------------! |
| ! VBV ! Snapshot at 'Y10.1' and 'Y10.2' seconds intervals. ! |
| !--------------!------------------------------------------------------! |
| ! T5 ! Snapshot at 'Y10.1' and 'Y10.2' seconds intervals. ! |
| !--------------!------------------------------------------------------! |
| ! OIT ! Snapshot at 'Y10.1' and 'Y10.2' seconds intervals. ! |
| !--------------!------------------------------------------------------! |
| ! ECW5 ! Snapshot at 'Y10.1' and 'Y10.2' seconds intervals. ! |
| +---------------------------------------------------------------------+ |
(9) Parameter Logic
| +---------------------------------------------------------------------+ |
| ! Param. ! Print Value (Standard Progr.) ! |
| !--------------!------------------------------------------------------! |
| ! ESN ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! EHRS ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! ERT ! Value at moment of trigger ! |
| !--------------! -----------------------------------------------------! |
| ! ECYC ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! AP ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! Y1 ! Programmed 'Y10.1' pre-event intervals ! |
| !--------------!------------------------------------------------------! |
| ! Y2 ! Programmed 'Y10.2' post-event intervals ! |
| !--------------!------------------------------------------------------! |
| ! E ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! MAX ! Highest value during observing time ! |
| !--------------!------------------------------------------------------! |
| ! LIM ! programmed value ! |
| !--------------!------------------------------------------------------! |
| ! TOL ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! TTP ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! TTF ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! FF ! Report line N1: value 'Y10.3' sec. after SAV = open! |
| !--------------!------------------------------------------------------! |
| ! PD ! Report line N1: value at moment of SAV = open ! |
| !--------------!------------------------------------------------------! |
| ! SM ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! N1 ! Snapshot at 'Y10.1' and 'Y10.2' seconds intervals. ! |
| !--------------!------------------------------------------------------! |
| ! N2 ! Snapshot at 'Y10.1' and 'Y10.2' seconds intervals. ! |
| !--------------!------------------------------------------------------! |
| ! EGT ! Snapshot at 'Y10.1' and 'Y10.2' seconds intervals. ! |
| !--------------!------------------------------------------------------! |
| ! FF ! Snapshot at 'Y10.1' and 'Y10.2' seconds intervals. ! |
| !--------------!------------------------------------------------------! |
| ! FMV ! Snapshot at 'Y10.1' and 'Y10.2' seconds intervals. ! |
| !--------------!------------------------------------------------------! |
| ! T25 ! Snapshot at 'Y10.1' and 'Y10.2' seconds intervals. ! |
| !--------------!------------------------------------------------------! |
| ! PD ! Snapshot at 'Y10.1' and 'Y10.2' seconds intervals. ! |
| !--------------!------------------------------------------------------! |
| ! P3 ! Snapshot at 'Y10.1' and 'Y10.2' seconds intervals. ! |
| !--------------!------------------------------------------------------! |
| ! T3 ! Snapshot at 'Y10.1' and 'Y10.2' seconds intervals. ! |
| !--------------!------------------------------------------------------! |
| ! VSV ! Snapshot at 'Y10.1' and 'Y10.2' seconds intervals. ! |
| !--------------!------------------------------------------------------! |
| ! VBV ! Snapshot at 'Y10.1' and 'Y10.2' seconds intervals. ! |
| !--------------!------------------------------------------------------! |
| ! T5 ! Snapshot at 'Y10.1' and 'Y10.2' seconds intervals. ! |
| !--------------!------------------------------------------------------! |
| ! OIT ! Snapshot at 'Y10.1' and 'Y10.2' seconds intervals. ! |
| !--------------!------------------------------------------------------! |
| ! ECW5 ! Snapshot at 'Y10.1' and 'Y10.2' seconds intervals. ! |
| +---------------------------------------------------------------------+ |
(10) Engine Start Report Logic <10> (Engine Type CFMI with Advanced EVMU)
| +----------------------------------------------------------------------+ |
| !Code!Item ! !Progr.!Standard ! |
| ! No.!No. ! Description of Function Item !MCDU !Value or ! |
| ! ! ! !GSE !Table ! |
| !----!------!-----------------------------------------!------!---------! |
| ! !A ! Report Format ! ! ! |
| ! !B ! Parameter Table ! ! ! |
| ! !C ! First three lines of Report ! C ! Blank ! |
| ! !D ! Print-out Rules ! C ! 2 ! |
| ! !E ! Transfer to ACARS MU ! C ! No ! |
| ! !F ! Increment of the report counter if the ! C ! 1 ! |
| ! ! ! report was triggered by a code number ! ! ! |
| ! ! ! > 1000; 1=yes, 0=no ! ! ! |
| ! !G ! 'Y10.1' Pre-event print interval in sec.! C ! 5 ! |
| ! !H ! 'Y10.2'Post-event print interval in sec.! C ! 2 ! |
| ! !I ! 'Y10.3' time in seconds when Fuel Flow ! A ! 20 ! |
| ! ! ! is measured after SAV = open ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !1000!1 ! Manual selection via MCDU ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !2000!2 ! Flight phase dependent manual ! ! ! |
| ! ! ! selection via remote print button ! ! ! |
| ! ! ! if programmed. ! ! ! |
| ! !2.1 ! Remote Print Button assignment. ! C ! 1.1 ! |
| !----!------!-----------------------------------------!------!---------! |
| !3000!3 ! Programmable Start Logic ! ! ! |
| ! !3.1 ! Trigger condition ! C ! not ! |
| !----!------!-----------------------------------------!------!---------! |
| ! !4 ! Aborted engine 1 or 2 start detecetd ! ! ! |
| ! ! ! by FADEC: ! ! ! |
| ! ! ! Start Abort Active ! ! ! |
| ! ! ! Eng.1 param. 7C.1.270.01.26 = 1 ! ! ! |
| ! ! ! Eng.2 param. 7C.2.270.10.26 = 1 ! ! ! |
| ! ! ! ! ! ! |
| ! !4.1 ! Logic algorithm ! ! ! |
| ! ! ! The report is generated if the a.m. ! ! ! |
| ! ! ! Start Abort Active bit and one of the ! ! ! |
| ! ! ! following bits (item 4.1.1 to 4.1.8) of ! ! ! |
| ! ! ! the same engine are set to '1'. ! ! ! |
| ! ! ! ! ! ! |
| !4410!4.1.1 ! Start Abort = SAV Demand/Position ! ! ! |
| ! ! ! Disagree ! ! ! |
| ! ! ! Eng.1 param. 7C.1.270.01.15 = 1 ! ! ! |
| ! ! ! Eng.2 param. 7C.2.270.10.15 = 1 ! ! ! |
| !4420!4.1.2 ! Start Abort = HPSOV Demand/Position ! ! ! |
| ! ! ! Disagree ! ! ! |
| ! ! ! Eng.1 param. 7C.1.270.01.16 = 1 ! ! ! |
| ! ! ! Eng.2 param. 7C.2.270.10.16 = 1 ! ! ! |
| !4430!4.1.3 ! Start Abort = EGT Overtemperature ! ! ! |
| ! ! ! Deteceted ! ! ! |
| ! ! ! Eng.1 param. 7C.1.270.01.17 = 1 ! ! ! |
| ! ! ! Eng.2 param. 7C.2.270.10.17 = 1 ! ! ! |
| !4440!4.1.4 ! Start Abort = Stall Deteceted ! ! ! |
| ! ! ! Eng.1 param. 7C.1.270.01.18 = 1 ! ! ! |
| ! ! ! Eng.2 param. 7C.2.270.10.18 = 1 ! ! ! |
| !4450!4.1.5 ! Start Abort = No Engine Lightoff ! ! ! |
| ! ! ! Deteceted ! ! ! |
| ! ! ! Eng.1 param. 7C.1.270.01.20 = 1 ! ! ! |
| ! ! ! Eng.2 param. 7C.2.270.10.20 = 1 ! ! ! |
| !4460!4.1.6 ! Hung Start ! ! ! |
| ! ! ! Eng.1 param. 7C.1.270.01.21 = 1 ! ! ! |
| ! ! ! Eng.2 param. 7C.2.270.10.21 = 1 ! ! ! |
| ! ! ! or ! ! ! |
| ! ! ! Eng.1 param. 7C.1.270.01.22 = 1 ! ! ! |
| ! ! ! Eng.2 param. 7C.2.270.10.22 = 1 ! ! ! |
| !4470!4.1.7 ! Start Abort = Illegal Start Sequence ! ! ! |
| ! ! ! Eng.1 param. 7C.1.270.01.24 = 1 ! ! ! |
| ! ! ! Eng.2 param. 7C.2.270.10.24 = 1 ! ! ! |
| !4480!4.1.8 ! Slow Start Deteceted ! ! ! |
| ! ! ! Eng.1 param. 7C.1.270.01.25 = 1 ! ! ! |
| ! ! ! Eng.2 param. 7C.2.270.10.25 = 1 ! ! ! |
| ! ! ! ! ! ! |
| ! !4.2 ! It is possible to suppress each logic ! ! ! |
| ! ! ! item individually via MCDU. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !5000!5 ! In case of exceedance of EGTL during ! ! ! |
| ! ! ! appropriate engine start. ! ! ! |
| ! !5.1 ! EGTL limit in C ! C ! limit- ! |
| ! ! ! ! ! table ! |
| !----!------!-----------------------------------------!------!---------! |
| !6000!6 ! Every 'F10.1'th cycle at the moment when! ! ! |
| ! ! ! N2 =/> N2 trigger during engine start. ! ! ! |
| ! ! ! Eng.1 param. 7C.1.344.01 ! ! ! |
| ! ! ! Eng.2 param. 7C.2.344.10 ! ! ! |
| ! !6.1 ! 'F10.1' cycle ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !6.2 ! N2 trigger value in %rpm ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !6.3 ! In case 7 post-event data sets are ! C ! limit- ! |
| ! ! ! printed out. ! ! table ! |
| !----!------!-----------------------------------------!------!---------! |
| !7001!7 ! A programmable number 'X10' of consecu- ! ! ! |
| !7002! ! tive legs. ! ! ! |
| !7003! ! This means: During the next 'X10' legs ! ! ! |
| !7004! ! the engine start report is automatically! ! ! |
| !7005! ! generated when N2 = N2trigger during ! ! ! |
| ! . ! ! appropriate engine start. ! ! ! |
| ! . ! ! ! ! ! |
| !700X!7.1 ! Number 'X10' for consecutive legs ! C ! limit- ! |
| ! ! ! programmable up to 9. ! ! table ! |
| !----!------!-----------------------------------------!------!---------! |
| !8100!8.1 ! ACARS MU uplink request with IMI 'REQ10'! ! ! |
| ! ! ! The report <10> is immediately generated! ! ! |
| ! ! ! and transmitted to the ACARS MU. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !8200!8.2 ! ACARS MU uplink request IMI 'G10': ! ! ! |
| ! ! ! The report <10> is generated at the next! ! ! |
| ! ! ! start of engine 1 and 2 when N2 = N2 ! ! ! |
| ! ! ! trigger after entering PH1.1. ! ! ! |
| !----------------------------------------------------------------------! |
| ! A = Programmable by Airbus ! |
| ! C = Programmable by Customer ! |
| +----------------------------------------------------------------------+ |
(11) Engine Start Report Logic <10> (Engine Type CFMI with Advanced EVMU)
| +----------------------------------------------------------------------+ |
| !Code!Item ! !Progr.!Standard ! |
| ! No.!No. ! Description of Function Item !MCDU !Value or ! |
| ! ! ! !GSE !Table ! |
| !----!------!-----------------------------------------!------!---------! |
| ! !A ! Report Format ! ! ! |
| ! !B ! Parameter Table ! ! ! |
| ! !C ! First three lines of Report ! C ! Blank ! |
| ! !D ! Print-out Rules ! C ! see ! |
| ! ! ! ! ! separate! |
| ! ! ! ! ! link ! |
| ! !E ! Transfer to ACARS MU ! C ! see ! |
| ! ! ! ! ! separate! |
| ! ! ! ! ! link ! |
| ! !F ! Increment of the report counter if the ! C ! 1 ! |
| ! ! ! report was triggered by a code number ! ! ! |
| ! ! ! > 1000; 1=yes, 0=no ! ! ! |
| ! !G ! 'Y10.1' Pre-event print interval in sec.! C ! 5 ! |
| ! ! ! 'Y10.1' shall be programmable in the ! ! ! |
| ! ! ! range from 1 to 7 ! ! ! |
| ! !H ! 'Y10.2'Post-event print interval in sec.! C ! 2 ! |
| ! ! ! 'Y10.2'shall be programmable in the ! ! ! |
| ! ! ! range from 1 to 61 ! ! ! |
| ! !I ! 'Y10.3' time in seconds when Fuel Flow ! A ! 20 ! |
| ! ! ! is measured after SAV = open ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !1000!1 ! Manual selection via MCDU ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !2000!2 ! Flight phase dependent manual ! ! ! |
| ! ! ! selection via remote print button ! ! ! |
| ! ! ! if programmed. ! ! ! |
| ! !2.1 ! Remote Print Button assignment. ! C ! 1.1 ! |
| !----!------!-----------------------------------------!------!---------! |
| !3000!3 ! Programmable Start Logic ! ! ! |
| ! !3.1 ! Trigger condition ! C ! not ! |
| ! ! ! ! ! progr. ! |
| !----!------!-----------------------------------------!------!---------! |
| ! !4 ! Aborted engine 1 or 2 start detected ! ! ! |
| ! ! ! by FADEC: ! ! ! |
| ! ! ! Start Abort Active ! ! ! |
| ! ! ! Engine 1 7C.1.270.01.26 = 1 ! ! ! |
| ! ! ! Engine 2 7C.2.270.10.26 = 1 ! ! ! |
| ! ! ! ! ! ! |
| ! !4.1 ! Logic algorithm ! ! ! |
| ! ! ! The report is generated if the a.m. ! ! ! |
| ! ! ! Start Abort Active bit and one of the ! ! ! |
| ! ! ! following bits (item 4.1.1 to 4.1.8) of ! ! ! |
| ! ! ! the same engine are set to '1'. ! ! ! |
| ! ! ! ! ! ! |
| !4410!4.1.1 ! Start Abort -> SAV Demand/Position ! ! ! |
| ! ! ! Disagree ! ! ! |
| ! ! ! Engine 1 7C.1.270.01.15 = 1 ! ! ! |
| ! ! ! Engine 2 7C.2.270.10.15 = 1 ! ! ! |
| !4420!4.1.2 ! Start Abort -> HPSOV Demand/Position ! ! ! |
| ! ! ! Disagree ! ! ! |
| ! ! ! Engine 1 7C.1.270.01.16 = 1 ! ! ! |
| ! ! ! Engine 2 7C.2.270.10.16 = 1 ! ! ! |
| !4430!4.1.3 ! Start Abort -> EGT Overtemperature ! ! ! |
| ! ! ! Detected ! ! ! |
| ! ! ! Engine 1 7C.1.270.01.17 = 1 ! ! ! |
| ! ! ! Engine 2 7C.2.270.10.17 = 1 ! ! ! |
| !4440!4.1.4 ! Start Abort -> Stall Detected ! ! ! |
| ! ! ! Engine 1 7C.1.270.01.18 = 1 ! ! ! |
| ! ! ! Engine 2 7C.2.270.10.18 = 1 ! ! ! |
| !4450!4.1.5 ! Start Abort -> No Engine Lightoff ! ! ! |
| ! ! ! Detected ! ! ! |
| ! ! ! Engine 1 7C.1.270.01.20 = 1 ! ! ! |
| ! ! ! Engine 2 7C.2.270.10.20 = 1 ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !4460!4.1.6 ! Hung Start ! ! ! |
| ! ! ! Engine 1 7C.1.270.01.21 = 1 ! ! ! |
| ! ! ! Engine 2 7C.2.270.10.21 = 1 ! ! ! |
| ! ! ! or ! ! ! |
| ! ! ! Engine 1 7C.1.270.01.15 = 1 ! ! ! |
| ! ! ! Engine 2 7C.2.270.10.15 = 1 ! ! ! |
| !4470!4.1.7 ! Start Abort -> Illegal Start Sequence ! ! ! |
| ! ! ! Engine 1 7C.1.270.01.24 = 1 ! ! ! |
| ! ! ! Engine 2 7C.2.270.10.24 = 1 ! ! ! |
| !4480!4.1.8 ! Slow Start Detected ! ! ! |
| ! ! ! Engine 1 7C.1.270.01.25 = 1 ! ! ! |
| ! ! ! Engine 2 7C.2.270.10.25 = 1 ! ! ! |
| ! ! ! ! ! ! |
| ! !4.2 ! It is possible to suppress each logic ! ! ! |
| ! ! ! item individually via the MCDU. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !5000!5 ! In case of exceedance of EGTL during ! ! ! |
| ! ! ! appropriate engine start. ! ! ! |
| ! !5.1 ! EGTL limit in C ! C ! limit- ! |
| ! ! ! ! ! table ! |
| !----!------!-----------------------------------------!------!---------! |
| !6000!6 ! Every 'F10.1'th cycle at the moment when! ! ! |
| ! ! ! N2 is equal or greater than N2trigger ! ! ! |
| ! ! ! during engine start. ! ! ! |
| ! ! ! N2 Engine 1 7C.1.344.01 ! ! ! |
| ! ! ! Engine 2 7C.2.344.10 ! ! ! |
| ! !6.1 ! 'F10.1' cycle ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !6.2 ! N2 trigger value in %rpm ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !6.3 ! In this case 7 post-event data sets are ! ! ! |
| ! ! ! printed out. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !7001!7 ! A programmable number 'X10' of ! ! ! |
| !. ! ! consecutive legs. ! ! ! |
| !7002! ! ! ! ! |
| !7003! ! This means: During the next 'X10' legs ! ! ! |
| !7004! ! the engine start report is automatically! ! ! |
| !7005! ! generated when N2 >= N2trigger during ! ! ! |
| !. ! ! appropriate engine start. ! ! ! |
| !. ! ! ! ! ! |
| !700X!7.1 ! Number 'X10' for consecutive legs ! C ! limit- ! |
| ! ! ! programmable up to 9. ! ! table ! |
| !----!------!-----------------------------------------!------!---------! |
| !8100!8.1 ! ACARS MU uplink request with IMI 'REQ10'! ! ! |
| ! ! ! The report <10> is immediately generated! ! ! |
| ! ! ! and transmitted to the ACARS MU. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !8200!8.2 ! ACARS MU uplink request IMI 'G10': ! ! ! |
| ! ! ! The report <01> is generated at the next! ! ! |
| ! ! ! start of engine 1 and 2 (2 reports) when! ! ! |
| ! ! ! N2 = N2trigger after entering flight ! ! ! |
| ! ! ! phase 1.1 (based on code 6000). ! ! ! |
| !----------------------------------------------------------------------! |
| ! A = Programmable by Airbus ! |
| ! C = Programmable by Customer ! |
| +----------------------------------------------------------------------+ |
(12) Engine Start Report Logic <10> (Engine Type CFMI with Advanced EVMU)
| +----------------------------------------------------------------------+ |
| !Code!Item ! !Progr.!Standard ! |
| ! No.!No. ! Description of Function Item !MCDU !Value or ! |
| ! ! ! !GSE !Table ! |
| !----!------!-----------------------------------------!------!---------! |
| ! !A ! Report Format ! ! ! |
| ! !B ! Parameter Table ! ! ! |
| ! !C ! First three lines of Report ! C ! Blank ! |
| ! !D ! Print-out Rules ! C ! see ! |
| ! ! ! ! ! separate! |
| ! ! ! ! ! link ! |
| ! !E ! Transfer to ACARS MU ! C ! see ! |
| ! ! ! ! ! separate! |
| ! ! ! ! ! link ! |
| ! !F ! Increment of the report counter if the ! C ! 1 ! |
| ! ! ! report was triggered by a code number ! ! ! |
| ! ! ! > 1000; 1=yes, 0=no ! ! ! |
| ! !G ! 'Y10.1' Pre-event print interval in sec.! C ! 5 ! |
| ! ! ! 'Y10.1' shall be programmable in the ! ! ! |
| ! ! ! range from 1 to 7 ! ! ! |
| ! !H ! 'Y10.2'Post-event print interval in sec.! C ! 2 ! |
| ! ! ! 'Y10.2'shall be programmable in the ! ! ! |
| ! ! ! range from 1 to 61 ! ! ! |
| ! !I ! 'Y10.3' time in seconds when Fuel Flow ! A ! 20 ! |
| ! ! ! is measured after SAV = open ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !1000!1 ! Manual selection via MCDU ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !2000!2 ! Flight phase dependent manual ! ! ! |
| ! ! ! selection via remote print button ! ! ! |
| ! ! ! if programmed. ! ! ! |
| ! !2.1 ! Remote Print Button assignment. ! C ! 1.1 ! |
| !----!------!-----------------------------------------!------!---------! |
| !3000!3 ! Programmable Start Logic ! ! ! |
| ! !3.1 ! Trigger condition ! C ! not ! |
| ! ! ! ! ! progr. ! |
| !----!------!-----------------------------------------!------!---------! |
| ! !4 ! Aborted engine 1 or 2 start detected ! ! ! |
| ! ! ! by FADEC: ! ! ! |
| ! ! ! Start Abort Active ! ! ! |
| ! ! ! Engine 1 7C.1.270.01.26 = 1 ! ! ! |
| ! ! ! Engine 2 7C.2.270.10.26 = 1 ! ! ! |
| ! ! ! ! ! ! |
| ! !4.1 ! Logic algorithm ! ! ! |
| ! ! ! The report is generated if the a.m. ! ! ! |
| ! ! ! Start Abort Active bit and one of the ! ! ! |
| ! ! ! following bits (item 4.1.1 to 4.1.8) of ! ! ! |
| ! ! ! the same engine are set to '1'. ! ! ! |
| ! ! ! ! ! ! |
| !4410!4.1.1 ! Start Abort -> SAV Demand/Position ! ! ! |
| ! ! ! Disagree ! ! ! |
| ! ! ! Engine 1 7C.1.270.01.15 = 1 ! ! ! |
| ! ! ! Engine 2 7C.2.270.10.15 = 1 ! ! ! |
| !4420!4.1.2 ! Start Abort -> HPSOV Demand/Position ! ! ! |
| ! ! ! Disagree ! ! ! |
| ! ! ! Engine 1 7C.1.270.01.16 = 1 ! ! ! |
| ! ! ! Engine 2 7C.2.270.10.16 = 1 ! ! ! |
| !4430!4.1.3 ! Start Abort -> EGT Overtemperature ! ! ! |
| ! ! ! Detected ! ! ! |
| ! ! ! Engine 1 7C.1.270.01.17 = 1 ! ! ! |
| ! ! ! Engine 2 7C.2.270.10.17 = 1 ! ! ! |
| !4440!4.1.4 ! Start Abort -> Stall Detected ! ! ! |
| ! ! ! Engine 1 7C.1.270.01.18 = 1 ! ! ! |
| ! ! ! Engine 2 7C.2.270.10.18 = 1 ! ! ! |
| !4450!4.1.5 ! Start Abort -> No Engine Lightoff ! ! ! |
| ! ! ! Detected ! ! ! |
| ! ! ! Engine 1 7C.1.270.01.20 = 1 ! ! ! |
| ! ! ! Engine 2 7C.2.270.10.20 = 1 ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !4460!4.1.6 ! Hung Start ! ! ! |
| ! ! ! Engine 1 7C.1.270.01.21 = 1 ! ! ! |
| ! ! ! Engine 2 7C.2.270.10.21 = 1 ! ! ! |
| ! ! ! or ! ! ! |
| ! ! ! Engine 1 7C.1.270.01.22 = 1 ! ! ! |
| ! ! ! Engine 2 7C.2.270.10.22 = 1 ! ! ! |
| !4470!4.1.7 ! Start Abort -> Illegal Start Sequence ! ! ! |
| ! ! ! Engine 1 7C.1.270.01.24 = 1 ! ! ! |
| ! ! ! Engine 2 7C.2.270.10.24 = 1 ! ! ! |
| !4480!4.1.8 ! Slow Start Detected ! ! ! |
| ! ! ! Engine 1 7C.1.270.01.25 = 1 ! ! ! |
| ! ! ! Engine 2 7C.2.270.10.25 = 1 ! ! ! |
| ! ! ! ! ! ! |
| ! !4.2 ! It is possible to suppress each logic ! ! ! |
| ! ! ! item individually via the MCDU. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !5000!5 ! In case of exceedance of EGTL during ! ! ! |
| ! ! ! appropriate engine start. ! ! ! |
| ! !5.1 ! EGTL limit in deg. C ! C ! limit- ! |
| ! ! ! ! ! table ! |
| !----!------!-----------------------------------------!------!---------! |
| !6000!6 ! Every 'F10.1'th cycle at the moment when! ! ! |
| ! ! ! N2 is equal or greater than N2trigger ! ! ! |
| ! ! ! during engine start. ! ! ! |
| ! ! ! N2 Engine 1 7C.1.344.01 ! ! ! |
| ! ! ! Engine 2 7C.2.344.10 ! ! ! |
| ! !6.1 ! 'F10.1' cycle ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !6.2 ! N2 trigger value in %rpm ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !6.3 ! In this case 7 post-event data sets are ! ! ! |
| ! ! ! printed out. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !7001!7 ! A programmable number 'X10' of ! ! ! |
| !. ! ! consecutive legs. ! ! ! |
| !7002! ! ! ! ! |
| !7003! ! This means: During the next 'X10' legs ! ! ! |
| !7004! ! the engine start report is automatically! ! ! |
| !7005! ! generated when N2 >= N2trigger during ! ! ! |
| !. ! ! appropriate engine start. ! ! ! |
| !. ! ! ! ! ! |
| !. ! ! ! ! ! |
| !700X! ! ! ! ! |
| ! !7.1 ! Number 'X10' for consecutive legs ! C ! limit- ! |
| ! ! ! programmable up to 9. ! ! table ! |
| !----!------!-----------------------------------------!------!---------! |
| !8100!8.1 ! ACARS MU uplink request with IMI 'REQ10'! ! ! |
| ! ! ! The report <10> is immediately generated! ! ! |
| ! ! ! and transmitted to the ACARS MU. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !8200!8.2 ! ACARS MU uplink request IMI 'G10': ! ! ! |
| ! ! ! The report <01> is generated at the next! ! ! |
| ! ! ! start of engine 1 and 2 (2 reports) when! ! ! |
| ! ! ! N2 >= N2trigger after entering flight ! ! ! |
| ! ! ! phase 1.1 (based on code 6000). ! ! ! |
| !----------------------------------------------------------------------! |
| ! A = Programmable by Airbus ! |
| ! C = Programmable by Customer ! |
| +----------------------------------------------------------------------+ |
(13) Engine Start Report Logic <10> (Engine Type CFMI with Advanced EVMU)
| +----------------------------------------------------------------------+ |
| !Code!Item ! !Progr.!Standard ! |
| ! No.!No. ! Description of Function Item !------!Value or ! |
| ! ! ! !MCDU/ !Table ! |
| ! ! ! !GSE ! ! |
| !----!------!-----------------------------------------!------!---------! |
| ! !A ! Report Format ! ! ! |
| ! !A.1 ! "R010RLID" Report Layout Identifier ! ! 01 ! |
| ! ! ! (for ACARS header) ! ! ! |
| ! !A.2 ! "R010RLIS" Report Layout Issue ! ! 01 ! |
| ! ! ! (for ACARS header) ! ! ! |
| ! !B ! Parameter Table ! ! ! |
| ! !C ! First three lines of Report ! C ! Blank ! |
| ! !D ! Print-out Rules ! C ! see ! |
| ! ! ! ! ! separate! |
| ! ! ! ! ! link ! |
| ! !E ! Transfer to ACARS MU ! C ! see ! |
| ! ! ! ! ! separate! |
| ! ! ! ! ! link ! |
| ! !F ! Increment of the report counter if the ! C ! 1 ! |
| ! ! ! report was triggered by a code number ! ! ! |
| ! ! ! > 1000; 1=yes, 0=no ! ! ! |
| ! !G ! "Y10.1" Pre-event print interval in sec.! C ! 5 ! |
| ! ! ! "Y10.1" is programmable in the range ! ! ! |
| ! ! ! from 1 to 7 ! ! ! |
| ! !H ! "Y10.2"Post-event print interval in sec.! C ! 2 ! |
| ! ! ! "Y10.2" is programmable in the range ! ! ! |
| ! ! ! from 1 to 61 ! ! ! |
| ! !I ! "Y10.3" time in seconds when Fuel Flow ! A ! 20 ! |
| ! ! ! is measured after SAV = open ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !1000!1 ! Manual selection through MCDU ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !2000!2 ! Flight phase dependent manual ! ! ! |
| ! ! ! selection through remote print button ! ! ! |
| ! ! ! if programmed. ! ! ! |
| ! !2.1 ! Remote Print Button assignment. ! C ! 1.1 ! |
| !----!------!-----------------------------------------!------!---------! |
| !3000!3 ! Programmable Start Logic ! ! ! |
| ! !3.1 ! Trigger condition ! C ! not ! |
| ! ! ! ! ! progr. ! |
| !----!------!-----------------------------------------!------!---------! |
| ! !4 ! Aborted engine 1 or 2 start detected ! ! ! |
| ! ! ! by FADEC: ! ! ! |
| ! ! ! Start Abort Active ! ! ! |
| ! ! ! Engine 1 7C.1.270.01.26 = 1 ! ! ! |
| ! ! ! Engine 2 7C.2.270.10.26 = 1 ! ! ! |
| ! ! ! ! ! ! |
| ! !4.1 ! Logic algorithm ! ! ! |
| ! ! ! The report is generated if the a.m. ! ! ! |
| ! ! ! Start Abort Active bit and one of the ! ! ! |
| ! ! ! following bits (item 4.1.1 to 4.1.8) of ! ! ! |
| ! ! ! the same engine are set to '1'. ! ! ! |
| ! ! ! ! ! ! |
| !4410!4.1.1 ! Start Abort -> SAV Demand/Position ! ! ! |
| ! ! ! Disagree ! ! ! |
| ! ! ! Engine 1 7C.1.270.01.15 = 1 ! ! ! |
| ! ! ! Engine 2 7C.2.270.10.15 = 1 ! ! ! |
| !4420!4.1.2 ! Start Abort -> HPSOV Demand/Position ! ! ! |
| ! ! ! Disagree ! ! ! |
| ! ! ! Engine 1 7C.1.270.01.16 = 1 ! ! ! |
| ! ! ! Engine 2 7C.2.270.10.16 = 1 ! ! ! |
| !4430!4.1.3 ! Start Abort -> EGT Overtemperature ! ! ! |
| ! ! ! Detected ! ! ! |
| ! ! ! Engine 1 7C.1.270.01.17 = 1 ! ! ! |
| ! ! ! Engine 2 7C.2.270.10.17 = 1 ! ! ! |
| !4440!4.1.4 ! Start Abort -> Stall Detected ! ! ! |
| ! ! ! Engine 1 7C.1.270.01.18 = 1 ! ! ! |
| ! ! ! Engine 2 7C.2.270.10.18 = 1 ! ! ! |
| !4450!4.1.5 ! Start Abort -> No Engine Lightoff ! ! ! |
| ! ! ! Detected ! ! ! |
| ! ! ! Engine 1 7C.1.270.01.20 = 1 ! ! ! |
| ! ! ! Engine 2 7C.2.270.10.20 = 1 ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !4460!4.1.6 ! Hung Start ! ! ! |
| ! ! ! Engine 1 7C.1.270.01.21 = 1 ! ! ! |
| ! ! ! Engine 2 7C.2.270.10.21 = 1 ! ! ! |
| ! ! ! or ! ! ! |
| ! ! ! Engine 1 7C.1.270.01.22 = 1 ! ! ! |
| ! ! ! Engine 2 7C.2.270.10.22 = 1 ! ! ! |
| !4470!4.1.7 ! Start Abort -> Illegal Start Sequence ! ! ! |
| ! ! ! Engine 1 7C.1.270.01.24 = 1 ! ! ! |
| ! ! ! Engine 2 7C.2.270.10.24 = 1 ! ! ! |
| !4480!4.1.8 ! Slow Start Detected ! ! ! |
| ! ! ! Engine 1 7C.1.270.01.25 = 1 ! ! ! |
| ! ! ! Engine 2 7C.2.270.10.25 = 1 ! ! ! |
| ! ! ! ! ! ! |
| ! !4.2 ! It is possible to suppress each logic ! ! ! |
| ! ! ! item individually through the MCDU. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !5000!5 ! In case of exceedance of EGTL during ! ! ! |
| ! ! ! appropriate engine start. ! ! ! |
| ! !5.1 ! EGTL limit in deg. C ! C ! limit- ! |
| ! ! ! ! ! table ! |
| !----!------!-----------------------------------------!------!---------! |
| !6000!6 ! Every "F10.1"th cycle at the moment when! ! ! |
| ! ! ! N2 is equal or greater than N2trigger ! ! ! |
| ! ! ! during engine start. ! ! ! |
| ! ! ! N2 Engine 1 7C.1.344.01 ! ! ! |
| ! ! ! Engine 2 7C.2.344.10 ! ! ! |
| ! !6.1 ! "F10.1" cycle ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !6.2 ! N2 trigger value in %rpm ! C ! limit- ! |
| ! ! ! ! ! table ! |
| ! !6.3 ! In this case 7 post-event data sets are ! ! ! |
| ! ! ! printed out. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !7001!7 ! A programmable number "X10" of ! ! ! |
| !. ! ! consecutive legs. ! ! ! |
| !7002! ! ! ! ! |
| !7003! ! This means: During the next "X10" legs ! ! ! |
| !7004! ! the engine start report is automatically! ! ! |
| !7005! ! generated when N2 >= N2trigger during ! ! ! |
| !. ! ! appropriate engine start. ! ! ! |
| !. ! ! ! ! ! |
| !. ! ! ! ! ! |
| !700X! ! ! ! ! |
| ! !7.1 ! Number "X10" for consecutive legs ! C ! limit- ! |
| ! ! ! programmable up to 9. ! ! table ! |
| !----!------!-----------------------------------------!------!---------! |
| !8100!8.1 ! ACARS MU uplink request with IMI "REQ10"! ! ! |
| ! ! ! The report <10> is immediately generated! ! ! |
| ! ! ! and transmitted to the ACARS MU. ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !8200!8.2 ! ACARS MU uplink request IMI "G10": ! ! ! |
| ! ! ! The report <10> is generated at the next! ! ! |
| ! ! ! start of engine 1 and 2 (2 reports) when! ! ! |
| ! ! ! N2 >= N2 trigger after entering flight ! ! ! |
| ! ! ! phase 1.1 (based on code 6000). ! ! ! |
| !----------------------------------------------------------------------! |
| ! A = Programmable by Airbus ! |
| ! C = Programmable by Customer ! |
| +----------------------------------------------------------------------+ |
P. AIDS Reports Print Rules - Default Values for Report <10>
| +------------------------------------------------+ |
| ! ! ! ! |
| ! Code ! Printer Output ! ACARS-output ! |
| ! ! ! ! |
| !-------!-----------------------!----------------! |
| ! ! ! ! |
| ! 1000 ! Print immediatly ! No ACARS ! |
| ! ! ! ! |
| !-------!-----------------------!----------------! |
| ! ! ! ! |
| ! 2000 ! Print immediatly ! No ACARS ! |
| ! ! ! ! |
| !-------!-----------------------!----------------! |
| ! ! ! ! |
| ! 4410 ! Print at landing ! ACARS VHF ! |
| ! ! ! ! |
| !-------!-----------------------!----------------! |
| ! ! ! ! |
| ! 4420 ! Print at landing ! ACARS VHF ! |
| ! ! ! ! |
| !-------!-----------------------!----------------! |
| ! ! ! ! |
| ! 4430 ! Print at landing ! ACARS VHF ! |
| ! ! ! ! |
| !-------!-----------------------!----------------! |
| ! ! ! ! |
| ! 4440 ! Print at landing ! ACARS VHF ! |
| ! ! ! ! |
| !-------!-----------------------!----------------! |
| ! ! ! ! |
| ! 4450 ! Print at landing ! ACARS VHF ! |
| ! ! ! ! |
| !-------!-----------------------!----------------! |
| ! ! ! ! |
| ! 4460 ! Print at landing ! ACARS VHF ! |
| ! ! ! ! |
| !-------!-----------------------!----------------! |
| ! ! ! ! |
| ! 4470 ! Print at landing ! ACARS VHF ! |
| ! ! ! ! |
| !-------!-----------------------!----------------! |
| ! ! ! ! |
| ! 4480 ! Print at landing ! ACARS VHF ! |
| ! ! ! ! |
| !-------!-----------------------!----------------! |
| ! ! ! ! |
| ! 5000 ! Print at landing ! ACARS VHF ! |
| ! ! ! ! |
| !-------!-----------------------!----------------! |
| ! ! ! ! |
| ! 6000 ! Print at landing ! ACARS VHF ! |
| ! ! ! ! |
| !-------!-----------------------!----------------! |
| ! ! ! ! |
| ! 700x ! Print at landing ! ACARS VHF ! |
| ! ! ! ! |
| !-------!-----------------------!----------------! |
| ! ! ! ! |
| ! 8100 ! No print ! ACARS VHF ! |
| ! ! ! ! |
| !-------!-----------------------!----------------! |
| ! ! ! ! |
| ! 8200 ! Print at landing ! ACARS VHF ! |
| ! ! ! ! |
| +------------------------------------------------+ |
| +-------------------------------------------------------------------------+ |
| !Trigger! to ACARS ! to printer ! store ! |
| ! Code !------------------------------ -!-----------------!--------------! |
| ! No !Ground ! VHF ! SAT- ! HF ! at ! imme- ! internal& ! |
| ! ! ! ! COM ! !landing ! diate ! external ! |
| ! ! ! ! ! ! ! !(build in RAM&! |
| ! ! ! ! ! ! ! ! PCMCIA) ! |
| !-------!-------!--------!-------!-------!--------!--------!--------------! |
| ! ! ! If ! ! ! ! If !PCMCIA only if! |
| ! 1000 ! NO ! 'SEND' ! NO ! NO ! NO !'PRINT' ! 'STORE' ! |
| ! ! !selected! ! ! !selected! selected on ! |
| ! ! !on MCDU ! ! ! !on MCDU ! MCDU ! |
| !-------!-------!--------!-------!-------!--------!--------!--------------! |
| ! 2000 ! NO ! NO ! NO ! NO ! ! YES ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 3000 ! NO ! NO ! NO ! NO ! ! NO ! YES ! |
| !-------!-------!--------!------ !-------! !--------!--------------! |
| ! 4410 ! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 4420 ! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 4430 ! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 4440 ! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 4450 ! NO ! YES ! NO ! NO ! Y ! NO ! YES ! |
| !-------!-------!--------!-------!-------! E !--------!--------------! |
| ! 4460 ! NO ! YES ! NO ! NO ! S ! NO ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 4470 ! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 4480 ! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 5000 ! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 6000 ! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 7001..! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| ! 700X ! ! ! ! ! ! NO ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 8100 ! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 8200 ! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| +-------------------------------------------------------------------------+ |
| +-------------------------------------------------------------------------+ |
| !Trigger! to ACARS ! to printer ! store ! |
| ! Code !------------------------------ -!-----------------!--------------! |
| ! No !Ground ! VHF ! SAT- ! HF ! at ! imme- ! internal& ! |
| ! ! ! ! COM ! !landing ! diate ! external ! |
| ! ! ! ! ! ! ! !(build in RAM&! |
| ! ! ! ! ! ! ! ! PCMCIA) ! |
| !-------!-------!--------!-------!-------!--------!--------!--------------! |
| ! 1000 ! NO ! NO ! NO ! NO ! NO ! YES ! YES ! |
| !-------!-------!--------!-------!-------!--------!--------!--------------! |
| ! 2000 ! NO ! NO ! NO ! NO ! NO ! YES ! YES ! |
| !-------!-------!--------!-------!-------!--------!--------!--------------! |
| ! 3000 ! NO ! NO ! NO ! NO ! NO ! NO ! YES ! |
| !-------!-------!--------!------ !-------!--------!--------!--------------! |
| ! 4410 ! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 4420 ! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 4430 ! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 4440 ! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 4450 ! NO ! YES ! NO ! NO ! Y ! NO ! YES ! |
| !-------!-------!--------!-------!-------! E !--------!--------------! |
| ! 4460 ! NO ! YES ! NO ! NO ! S ! NO ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 4470 ! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 4480 ! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 5000 ! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 6000 ! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 7001..! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| ! 700X ! ! ! ! ! ! NO ! YES ! |
| !-------!-------!--------!-------!-------!--------!--------!--------------! |
| ! 8100 ! NO ! YES ! NO ! NO ! NO ! NO ! YES ! |
| !-------!-------!--------!-------!-------!--------!--------!--------------! |
| ! 8200 ! NO ! YES ! NO ! NO ! NO ! NO ! YES ! |
| +-------------------------------------------------------------------------+ |
Q. Engine Run Up Report <11>
Engine Run Up Report <11> (Engine Type CFMI with Advanced EVMU)
Engine Run Up Report <11> (Engine Type CFMI with Advanced EVMU)
Engine Run Up Report <11> (Engine Type CFMI with Advanced EVMU) ** ON A/C NOT FOR ALL
Engine Run Up Report <11> (Engine Type CFMI with Advanced EVMU) ** ON A/C NOT FOR ALL
Engine Run Up Report <11> (Engine Type CFMI with Advanced EVMU) ** ON A/C NOT FOR ALL
The Engine Run Up Report shall be an averange collection of engine related parameters. The report will be primarily triggered manually via MCDU menu and the Remoto Print Button. The report is generated when one of the logic conditions 1000 to 3000 (for details see the Engine Run Up Report logic) is present.
Engine Run Up Report <11> (Engine Type CFMI with Advanced EVMU) Engine Run Up Report <11> (Engine Type CFMI with Advanced EVMU) Engine Run Up Report <11> (Engine Type CFMI with Advanced EVMU) ** ON A/C NOT FOR ALL Engine Run Up Report <11> (Engine Type CFMI with Advanced EVMU) ** ON A/C NOT FOR ALL Engine Run Up Report <11> (Engine Type CFMI with Advanced EVMU) ** ON A/C NOT FOR ALL NOTE: For the standard header definition of the report refer to (Ref. AMM D/O 31-36-00-00).
(1) Engine Run Up Report Data Field Description <11> (Engine Type CFMI with Advanced EVMU)
NOTE: Reports that are transmitted from the ACARS system do not have report lines without a line identifier.
| +---------------------------------------------------------------------+ |
| ! Value ! Content Description ! |
| !--------------!------------------------------------------------------! |
| ! ESN ! Engine Serial Number ! |
| ! 999999 ! (000000 to 999999) ! |
| ! ! Eng 1 param. 7C.1.046.01 digit 3, 2, 1 ! |
| ! ! 7C.1.047.01 digit 6, 5, 4 ! |
| ! ! Eng 2 param. 7C.2.046.01 digit 3, 2, 1 ! |
| ! ! 7C.2.047.01 digit 6, 5, 4 ! |
| !--------------!------------------------------------------------------! |
| ! EHRS ! Engine Flight Hours ! |
| ! 99999 ! (00000 to 99999 hours) ! |
| ! ! DMU Engine 1 and Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! ERT ! Engine Running Time ! |
| ! 99999 ! (00000 to 65536 hours) ! |
| ! ! Eng 1 param. 7C.1.050.01 ! |
| ! ! Eng 2 param. 7C.2.050.10 ! |
| !--------------!------------------------------------------------------! |
| ! ECYC ! Engine Cycle ! |
| ! 99999 ! (00000 to 99999) ! |
| !--------------!------------------------------------------------------! |
| ! AP ! Auto Pilot Status ! |
| ! 99 ! (00 to G8) ! |
| ! ! FMGC 1 and 2 (FGC part) for Auto Pilot AP1 and AP2 ! |
| ! ! ! |
| ! ! XX Auto Pilot Modes: ! |
| ! ! !! ! |
| ! ! !!__Lateral Modes: 0 = NO MODE ! |
| ! ! ! 1 = HEADING ! |
| ! ! ! 2 = TRACK ! |
| ! ! ! 3 = NAV ! |
| ! ! ! 4 = LOC CAPTURE ! |
| ! ! ! 5 = LOC TRACK ! |
| ! ! ! 6 = LAND TRACK ! |
| ! ! ! 7 = RUNWAY ! |
| ! ! ! 8 = ROLL GO AROUND ! |
| ! ! ! ! |
| ! ! !__Longitudinal Modes: 0 = NO MODE ! |
| ! ! 1 = PITCH G/A ! |
| ! ! 2 = PITCH T/O ! |
| ! ! 3 = G/S TRACK ! |
| ! ! 4 = G/S CAPTURE ! |
| ! ! 5 = V/S ! |
| ! ! 6 = FPA ! |
| ! ! 7 = ALT ! |
| ! ! 8 = ALT ACQ ! |
| ! ! 9 = OPEN CLB ! |
| ! ! A = OPEN DES ! |
| ! ! B = IM CLB ! |
| ! ! C = IM DES ! |
| ! ! D = CLB ! |
| ! ! E = DES ! |
| ! ! F = FINAL DES ! |
| ! ! G = EXPEDITE ! |
| ! ! ! |
| ! ! AP1 ! AP2 ! |
| ! ! Report Line EC: ! Report Line EE: !Difinition: ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! / ! / !No Mode Act. ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.11 = 1 ! 01.2.275.00.11 = 1!RUNWAY Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.12 = 1 ! 01.2.275.00.12 = 1!NAV Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.13 = 1 ! 01.2.275.00.13 = 1!LOC CAPTURE ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.14 = 1 ! 01.2.275.00.14 = 1!LOC TRACK ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.15 = 1 ! 01.2.275.00.15 = 1!Roll GO ! |
| ! ! ! !AROUND Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.16 = 1 ! 01.2.275.00.16 = 1!HEADING Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.17 = 1 ! 01.2.275.00.17 = 1!TRACK Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.15 = 1 ! 01.2.274.00.15 = 1!PITCH TO Mode! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.16 = 1 ! 01.2.274.00.16 = 1!PITCH GA Mode! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.17 = 1 ! 01.2.274.00.17 = 1!V/S Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.18 = 1 ! 01.2.274.00.18 = 1!FPA Mode ! |
| ! ! -------------------!-------------------!-------------! |
| ! ! 01.1.274.00.19 = 1 ! 01.2.274.00.19 = 1!ALT Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.20 = 1 ! 01.2.274.00.20 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.19 = 1 ! 01.2.274.00.19 = 1!ALT ACQ ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.21 = 1 ! 01.2.274.00.21 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.20 = 1 ! 01.2.274.00.20 = 1!G/S TRACK ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.22 = 1 ! 01.2.274.00.22 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.21 = 1 ! 01.2.274.00.21 = 1!G/S CAPTURE ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.22 = 1 ! 01.2.274.00.22 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.23 = 1 ! 01.2.274.00.23 = 1!FINAL DES ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.2.274.00.24 = 1 ! 01.2.274.00.24 = 1!EXPED. Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.146.00.14 = 1 ! 01.2.146.00.14 = 1!LAND TRACK ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!CLB Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.13 = 0 ! 01.2.274.00.13 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.14 = 0 ! 01.2.274.00.14 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.24 = 0 ! 01.2.274.00.24 = 0! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!DES Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.13 = 0 ! 01.2.274.00.13 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.14 = 0 ! 01.2.274.00.14 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.24 = 0 ! 01.2.274.00.24 = 0! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!IM. CLIMB ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.13 = 1 ! 01.2.274.00.13 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!IM. DES Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.13 = 1 ! 01.2.274.00.13 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!OPEN CLB ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.14 = 1 ! 01.2.274.00.14 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!OPEN DES ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.14 = 1 ! 01.2.274.00.14 = 1! ! |
| ! ! ---------------------------------------------------- ! |
| ! ! Auto Pilot Status DMU: ! |
| ! ! AP1 printed in report line EC ! |
| ! ! AP2 printed in report line EE ! |
| !--------------!------------------------------------------------------! |
| ! N1 ! Selected N1 Actual ! |
| ! 9999 ! (0 to 120.0 %rpm) ! |
| ! ! Eng 1 param. 7C.1.346.01 ! |
| ! ! Eng 2 param. 7C.2.346.10 ! |
| !--------------!------------------------------------------------------! |
| ! N1C ! N1 Command ! |
| ! 9999 ! (0 to 120.0 %rpm) ! |
| ! ! Eng 1 param. 7C.1.341.01 ! |
| ! ! Eng 2 param. 7C.2.341.10 ! |
| !--------------!------------------------------------------------------! |
| ! N2 ! Selected N2 Actual ! |
| ! 9999 ! (0 to 120.0 %rpm) ! |
| ! ! Eng 1 param. 7C.1.344.01 ! |
| ! ! Eng 2 param. 7C.2.344.10 ! |
| !--------------!------------------------------------------------------! |
| ! EGT ! Selected T494 (Exhaust Gas Temperature) ! |
| ! X999 ! (-55 to 999.9 C) ! |
| ! ! Eng 1 param. 7C.1.345.01 ! |
| ! ! Eng 2 param. 7C.2.345.10 ! |
| !--------------!------------------------------------------------------! |
| ! FF ! Engine Fuel Flow ! |
| ! 9999 ! ( 0 to 7000 kg/h) ! |
| ! ! Eng 1 param. 7C.1.244.01 ! |
| ! ! Eng 2 param. 7C.2.244.10 ! |
| !--------------!------------------------------------------------------! |
| ! PS13 ! PS13 Static Air Pressure at Position 1.3 ! |
| ! 99999 ! (0.0 to 30.000 psia) ! |
| ! ! Eng 1 param. 7C.1.127.01 ! |
| ! ! Eng 2 param. 7C.2.127.10 ! |
| !--------------!------------------------------------------------------! |
| ! P25 ! Total Air Pressure at Position 2.5 ! |
| ! 99999 ! (0.0 to 50.000 psia) ! |
| ! ! Eng 1 param. 7C.1.262.01 ! |
| ! ! Eng 2 param. 7C.2.262.10 ! |
| !--------------!------------------------------------------------------! |
| ! T25 ! Selected T25 ! |
| ! X999 ! (-55.0 to 120.0 C) ! |
| ! ! Eng 1 param. 7C.1.263.01 ! |
| ! ! Eng 2 param. 7C.2.263.10 ! |
| !--------------!------------------------------------------------------! |
| ! P3 ! Selected PS3 ! |
| ! 9999 ! (0.0 to 450.0 psia) ! |
| ! ! Eng 1 param. 7C.1.264.01 ! |
| ! ! Eng 2 param. 7C.2.264.10 ! |
| !--------------!------------------------------------------------------! |
| ! T3 ! Temperature at Position 3 ! |
| ! X999 ! (-55.0 to 850.0 C) ! |
| ! ! Eng 1 param. 7C.1.265.01 ! |
| ! ! Eng 2 param. 7C.2.265.10 ! |
| !--------------!------------------------------------------------------! |
| ! T5 ! Temperature at Position 5 ! |
| ! X999 ! (-55.0 to 850.0 C) ! |
| ! ! Eng 1 param. 7C.1.260.01 ! |
| ! ! Eng 2 param. 7C.2.260.10 ! |
| !--------------!------------------------------------------------------! |
| ! VSV ! Variable Statore Vane Position ! |
| ! X99 ! (-5.0 to 45.0 deg) ! |
| ! ! Eng 1 param. 7C.1.072.01 ! |
| ! ! Eng 2 param. 7C.2.072.10 ! |
| !--------------!------------------------------------------------------! |
| ! VBV ! Variable Bleed Valve Position ! |
| ! X99 ! (-9.9 to 40.0 deg) ! |
| ! ! Eng 1 param. 7C.1.071.01 ! |
| ! ! Eng 2 param. 7C.2.071.10 ! |
| !--------------!------------------------------------------------------! |
| ! HPT ! High-Pressure Turbine Clearance Position ! |
| ! X99 ! (-10 to 100 %) ! |
| ! ! Eng 1 param. 7C.1.306.01 ! |
| ! ! Eng 2 param. 7C.2.306.10 ! |
| !--------------!------------------------------------------------------! |
| ! LPT ! Low-Pressure Turbine Position ! |
| ! X99 ! (-10 to 100 %) ! |
| ! ! Eng 1 param. 7C.1.307.01 ! |
| ! ! Eng 2 param. 7C.2.307.10 ! |
| !--------------!------------------------------------------------------! |
| ! GLE ! Engine Generator Load ! |
| ! 999 ! (0 to 100 %) ! |
| ! ! Eng 1 param. 29.1.077.01 ! |
| ! ! 29.2.077.01 ! |
| ! ! Eng 2 param. 29.1.077.10 ! |
| ! ! 29.2.077.10 ! |
| !--------------!------------------------------------------------------! |
| ! PD ! Precooler Inlet Pressure ! |
| ! 99 ! (0 to 50 psi) ! |
| ! ! Eng 1 param. 06F.1.143.01 ! |
| ! ! 06F.1.143.10 ! |
| ! ! Eng 2 param. 06F.2.142.10 ! |
| ! ! 06F.2.142.01 ! |
| !--------------!------------------------------------------------------! |
| ! TN ! Nacelle Temperature ! |
| ! X99 ! Eng 1 param. 26.1.322.01 ! |
| ! ! 26.2.322.01 ! |
| ! ! Eng 2 param. 26.1.322.10 ! |
| ! ! 26.2.322.10 ! |
| !--------------!------------------------------------------------------! |
| ! PT2 ! Total Air Pressure at Position 2 ! |
| ! 99999 ! (o.o to 25.000 psia) ! |
| ! ! Eng 1 param. 7C.1.131.01 ! |
| ! ! Eng 2 param. 7C.2.131.10 ! |
| !--------------!------------------------------------------------------! |
| ! VN ! FAN Pick Up N1 Track Vibration ! |
| ! 99 ! (0.0 to 10.0) ! |
| ! ! Eng 1 param. 3D.1.227.01 ! |
| ! ! Eng 2 param. 3D.1.227.10 ! |
| !--------------!------------------------------------------------------! |
| ! VL ! TRF Pick Up N1 Vibration ! |
| ! 99 ! (0.0 to 10.0) ! |
| ! ! Eng 1 param. 3D.1.227.11 ! |
| ! ! Eng 2 param. 3D.1.227.00 ! |
| !--------------!------------------------------------------------------! |
| ! PHA ! FAN Pick Up Phase Angle ! |
| ! 999 ! (0 to 360 deg) ! |
| ! ! Eng 1 param. 3D.1.226.11 ! |
| ! ! Eng 2 param. 3D.1.226.00 ! |
| !--------------!------------------------------------------------------! |
| ! PHT ! TRF Pick Up Phase Angle ! |
| ! 999 ! (0 to 360 deg) ! |
| ! ! Eng 1 param. 3D.1.226.11 ! |
| ! ! Eng 2 param. 3D.1.226.00 ! |
| !--------------!------------------------------------------------------! |
| ! VC ! FAN Pick Up N2 Track Vibration ! |
| ! 99 ! (0.0 to 4.0) ! |
| ! ! Eng 1 param. 3D.1.230.01 ! |
| ! ! Eng 2 param. 3D.1.230.10 ! |
| !--------------!------------------------------------------------------! |
| ! VH ! TRF Pick Up N2 Track Vibration ! |
| ! 99 ! (0.0 to 4.0) ! |
| ! ! Eng 1 param. 3D.1.230.11 ! |
| ! ! Eng 2 param. 3D.1.230.00 ! |
| !--------------!------------------------------------------------------! |
| ! EVM ! Engine Vibration Status Word ! |
| ! XXXXX ! Eng 1 param. 3D.1.035.01 ! |
| ! ! Eng 2 param. 3D.1.035.10 ! |
| ! ! Each 'X' represents 4 Bits in hexadecimal code of ! |
| ! ! a defined ARINC 429 word: ! |
| ! ! XXXXX Bits HEX ! |
| ! ! !!!!!___________ 14, 13, 12, 11 0...F ! |
| ! ! !!!!____________ 18, 17, 16, 15 0...F ! |
| ! ! !!!_____________ 22, 21, 20, 19 0...F ! |
| ! ! !!______________ 26, 25, 24, 23 0...F ! |
| ! ! !_______________ 29, 28, 27 0...7 ! |
| ! ! -------------------------------------------- ! |
| !--------------!------------------------------------------------------! |
| ! OIP ! Engine Oil Pressure ! |
| ! 999 ! (0 to 400 psia) ! |
| ! ! Eng 1 param. 26.1.317.01 ! |
| ! ! 26.2.317.01 ! |
| ! ! Eng 2 param. 26.1.317.10 ! |
| ! ! 26.2.317.10 ! |
| !--------------!------------------------------------------------------! |
| ! OIT ! Engine Oil Temperature ! |
| ! X99 ! (-60 to 250 C) ! |
| ! ! Eng 1 param. 26.1.316.01 ! |
| ! ! 26.2.316.01 ! |
| ! ! Eng 2 param. 26.1.316.10 ! |
| ! ! 26.2.316.10 ! |
| !--------------!------------------------------------------------------! |
| ! ECW1 ! Engine Control Word 1 ! |
| ! XXXXX ! Each 'X' represents 4 Bits in hexadecimal code of ! |
| ! ! a defined ARINC 429 word: ! |
| ! ! XXXXX Bits HEX ! |
| ! ! !!!!!___________ 14, 13, 12, 11 0...F ! |
| ! ! !!!!____________ 18, 17, 16, 15 0...F ! |
| ! ! !!!_____________ 22, 21, 20, 19 0...F ! |
| ! ! !!______________ 26, 25, 24, 23 0...F ! |
| ! ! !_______________ 29, 28, 27 0...7 ! |
| ! ! -------------------------------------------- ! |
| ! ! Bit Label Parameter Description ! |
| ! ! 11 7C.X.272.XX.19 = 1 Auto Thrust Active ! |
| ! ! 12 7C.X.272.XX.20 = 1 VSV Position Fault ! |
| ! ! 13 SPARE ! |
| ! ! 14 SPARE ! |
| ! ! 15 7C.X.351.XX.29 = 1 Fuel Flow Measurement ! |
| ! ! Invalid ! |
| ! ! 16 7C.X.275.XX.15 = 1 N1/N2 Control ACtive ! |
| ! ! 17 7C.X.275.XX.26 = 1 Channel A Active ! |
| ! ! 18 7C.X.275.XX.27 = 1 Channel B Active ! |
| ! ! 19 SPARE ! |
| ! ! 20 SPARE ! |
| ! ! 21 SPARE ! |
| ! ! 22 SPARE ! |
| ! ! 23 SPARE ! |
| ! ! 24 SPARE ! |
| ! ! 25 SPARE ! |
| ! ! 26 SPARE ! |
| ! ! 27 SPARE ! |
| ! ! 28 SPARE ! |
| ! ! 29 SPARE ! |
| !--------------!------------------------------------------------------! |
| ! SSEL ! Engine Control Word 1 ! |
| ! XXXXXXX ! Status of different FADEC sensors ! |
| ! XXXXXXX ! XXXXXXXXXXXXXX Label: Selected: Bit 11 --> 15) ! |
| ! ! IIIIIIIIIIIIII__ 346 N1 actual ! |
| ! ! IIIIIIIIIIIII___ 345 EGT ! |
| ! ! IIIIIIIIIIII____ 344 N2 actual ! |
| ! ! IIIIIIIIIII_____ 263 T25 ! |
| ! ! IIIIIIIIII______ 264 PS3 ! |
| ! ! IIIIIIIII_______ 265 T3 ! |
| ! ! IIIIIIII________ 072 VSV Position ! |
| ! ! IIIIIII_________ 071 VBV Position ! |
| ! ! IIIIII__________ 306 HPTC Position ! |
| ! ! IIIII___________ 307 LPTC Position ! |
| ! ! IIII____________ 347 FMV Position ! |
| ! ! III_____________ 211 TAT ! |
| ! ! II______________ 114 P0 ! |
| ! ! I_______________ 133 TLA Position ! |
| ! ! (All labels Bit 11 --> 15) ! |
| ! ! Source: ECU, different labels ! |
| ! ! The indicated values shall be coded as follows: ! |
| ! ! Bit: 15 14 13 12 11 ! indicated value ! |
| ! ! --------------------!---------------- ! |
| ! ! 0 0 0 0 0 ! 0 ! |
| ! ! 0 0 0 0 1 ! 1 ! |
| ! ! 0 0 0 1 0 ! 2 ! |
| ! ! 0 0 0 1 1 ! 3 ! |
| ! ! 0 0 1 0 0 ! 4 ! |
| ! ! 0 0 1 0 1 ! 5 ! |
| ! ! 0 0 1 1 0 ! 6 ! |
| ! ! 0 0 1 1 1 ! 7 ! |
| ! ! 0 1 0 0 0 ! 8 ! |
| ! ! 0 1 0 0 1 ! 9 ! |
| ! ! 0 1 0 1 0 ! A ! |
| ! ! 0 1 0 1 1 ! B ! |
| ! ! 0 1 1 0 0 ! C ! |
| ! ! 0 1 1 0 1 ! D ! |
| ! ! 0 1 1 1 0 ! E ! |
| ! ! 0 1 1 1 1 ! F ! |
| ! ! 1 0 0 0 0 ! G ! |
| ! ! 1 0 0 0 1 ! H ! |
| ! ! 1 0 0 1 0 ! I ! |
| ! ! 1 0 0 1 1 ! J ! |
| ! ! 1 0 1 0 0 ! K ! |
| ! ! 1 0 1 0 1 ! L ! |
| ! ! 1 0 1 1 0 ! M ! |
| ! ! 1 0 1 1 1 ! N ! |
| ! ! 1 1 0 0 0 ! O ! |
| ! ! 1 1 0 0 1 ! P ! |
| ! ! 1 1 0 1 0 ! Q ! |
| ! ! 1 1 0 1 1 ! R ! |
| ! ! 1 1 1 0 0 ! S ! |
| ! ! 1 1 1 0 1 ! T ! |
| ! ! 1 1 1 1 0 ! U ! |
| ! ! 1 1 1 1 1 ! V ! |
| ! ! ! |
| !--------------!------------------------------------------------------! |
| ! EGTK ! Corrected Exhaust Gas Temperature ! |
| ! X999 ! (-55 to 999.9 C) ! |
| ! ! Eng.1 param. 7C.1.345.01 ! |
| ! ! Eng.2 param. 7C.2.345.10 ! |
| !--------------!------------------------------------------------------! |
| ! N1K ! Corrected N1 ! |
| ! 9999 ! (0 to 120%rpm) ! |
| ! ! Eng.1 param. 7C.1.346.01 ! |
| ! ! Eng.2 param. 7C.2.346.10 ! |
| !--------------!------------------------------------------------------! |
| ! N2K ! Corrected N2 ! |
| ! 9999 ! (0 to 120%rpm) ! |
| ! ! Eng.1 param. 7C.1.344.01 ! |
| ! ! Eng.2 param. 7C.2.344.10 ! |
| !--------------!------------------------------------------------------! |
| ! FFK ! Corrected Engine Fuel Flow ! |
| ! 9999 ! (0 to 70000 kg/h) ! |
| ! ! Eng.1 param. 7C.1.345.01 = FF ! |
| ! ! Eng.2 param. 7C.2.345.10 ! |
| ! ! Eng.1 param. 7C.1.131.01 = PT2 ! |
| ! ! Eng.2 param. 7C.2.131.10 ! |
| +---------------------------------------------------------------------+ |
(2) Engine Run Up Report Data Field Description <11> (Engine Type CFMI with Advanced EVMU)
NOTE: Reports that are transmitted from the ACARS system do not have report lines without a line identifier.
NOTE: Only the parts of the ENGINE RUN UP REPORT <11> which are not included in the ENGINE CRUISE REPORT <01> are given in the subsequent table.
| +---------------------------------------------------------------------+ |
| ! Value ! Content Description ! |
| !--------------!------------------------------------------------------! |
| ! EGTK ! Corrected Exhaust Gas Temperature ! |
| ! X999 ! (-55 to 999.9 C) ! |
| ! ! TAT = 06.1.211.01 ! |
| ! ! 06.2.211.10 ! |
| ! ! EGT = 7C.1.345.01 Engine 1 ! |
| ! ! 7C.2.345.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! N1K ! Corrected N1 ! |
| ! 9999 ! (0 to 120%rpm) ! |
| ! ! TAT = 06.1.211.01 ! |
| ! ! 06.2.211.10 ! |
| ! ! N1 = 7C.1.346.01 Engine 1 ! |
| ! ! 7C.2.346.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! N2K ! Corrected N2 ! |
| ! 9999 ! (0 to 120%rpm) ! |
| ! ! TAT = 06.1.211.01 ! |
| ! ! 06.2.211.10 ! |
| ! ! N2 = 7C.1.344.01 Engine 1 ! |
| ! ! 7C.2.344.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! FFK ! Corrected Engine Fuel Flow ! |
| ! 9999 ! (0 to 70000 kg/h) ! |
| ! ! TAT = 06.1.211.01 ! |
| ! ! 06.2.211.10 ! |
| ! ! FF = 7C.1.345.01 Engine 1 ! |
| ! ! 7C.2.345.10 Engine 2 ! |
| ! ! PT2 = 7C.1.131.01 Engine 1 ! |
| ! ! 7C.2.131.10 Engine 2 ! |
| +---------------------------------------------------------------------+ |
(3) Engine Run Up Report Data Field Description <11> (Engine Type CFMI with Advanced EVMU)
NOTE: Reports that are transmitted from the ACARS system do not have report lines without a line identifier.
NOTE: Only the parts of the ENGINE RUN UP REPORT <11> which are not included in the ENGINE CRUISE REPORT <01> are given in the subsequent table.
| +---------------------------------------------------------------------+ |
| ! Value ! Content Description ! |
| !--------------!------------------------------------------------------! |
| ! EGTK ! Corrected Exhaust Gas Temperature ! |
| ! X999 ! (-55 to 999.9 °C) ! |
| ! ! TAT = 06.1.211.01 ! |
| ! ! 06.2.211.10 ! |
| ! ! EGT = 7C.1.345.01 Engine 1 ! |
| ! ! 7C.2.345.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! N1K ! Corrected N1 ! |
| ! 9999 ! DMU (0 to 120%rpm) ! |
| ! ! TAT = 06.1.211.01 ! |
| ! ! 06.2.211.10 ! |
| ! ! N1 = 7C.1.346.10 Engine 1 ! |
| ! ! 7C.2.346.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! N2K ! Corrected N2 ! |
| ! 9999 ! DMU (0 to 120%rpm) ! |
| ! ! TAT = 06.1.211.01 ! |
| ! ! 06.2.211.10 ! |
| ! ! N2 = 7C.1.344.01 Engine 1 ! |
| ! ! 7C.2.344.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! FFK ! Corrected Engine Fuel Flow ! |
| ! 9999 ! DMU (0 to 70000 kg/h or 0 to 15000 p/h) ! |
| ! ! TAT = 06.1.211.01 ! |
| ! ! 06.2.211.10 ! |
| ! ! FF = 7C.1.244.01 Engine 1 ! |
| ! ! 7C.2.244.10 Engine 2 ! |
| ! ! PT2 = 7C.1.131.01 Engine 1 ! |
| ! ! 7C.2.131.10 Engine 2 ! |
| +---------------------------------------------------------------------+ |
(4) Engine Run Up Report Data Field Description <11> (Engine Type CFMI with Advanced EVMU)
NOTE: Reports that are transmitted from the ACARS system do not have report lines without a line identifier.
| +---------------------------------------------------------------------+ |
| ! Value ! Content Description ! |
| !--------------!------------------------------------------------------! |
| ! ESN ! Engine Serial Number ! |
| ! 999999 ! (000000 to 999999) ! |
| ! ! ECU Engine 1 7C.1.046.01 digit 3, 2, 1 ! |
| ! ! 7C.1.047.01 digit 6, 5, 4 ! |
| ! ! Engine 2 7C.2.046.10 digit 3, 2, 1 ! |
| ! ! 7C.2.047.10 digit 6, 5, 4 ! |
| !--------------!------------------------------------------------------! |
| ! EHRS ! Engine Flight Hours ! |
| ! 99999 ! (00000 to 99999 hours) ! |
| ! ! DMU Engine 1 ! |
| ! ! Engine 2 ! |
| ! ! Remark: Time between "Main (LH and RH) Landing Gear! |
| ! ! Decompressed" and "Main (LH and RH) Landing! |
| ! ! Gear Compressed". The EHRS shall be set to ! |
| ! ! zero if a new ESN is recognized by the DMU.! |
| ! ! It shall be possible to set the EHRS via ! |
| ! ! the MCDU, e.g. if the DMU is changed on the! |
| ! ! a/c. ! |
| !--------------!------------------------------------------------------! |
| ! ERT ! Engine Running Time ! |
| ! 99999 ! (00000 to 65536 hours) ! |
| ! ! ECU 7C.1.050.01 Engine 1 ! |
| ! ! 7C.2.050.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! ECYC ! Engine Cycle ! |
| ! 99999 ! (00000 to 99999) ! |
| ! ! DMU Engine 1 ! |
| ! ! Engine 2 ! |
| ! ! Remark: Each time when flight phase 5 (climb) is ! |
| ! ! reached, the counter shall be incremented ! |
| ! ! by one. The ECYC is set to zero if a new ! |
| ! ! ESN is recognized by the DMU. It shall be ! |
| ! ! possible to set ECYC via the MCDU, if the ! |
| ! ! DMU is changed on the a/c. ! |
| !--------------!------------------------------------------------------! |
| ! AP ! Auto Pilot Status ! |
| ! 99 ! Number of respective status (00 to G8) ! |
| ! ! FMGC 1 and 2 (FGC part) for Auto Pilot AP1 and AP2 ! |
| ! ! ! |
| ! ! Parameter for AP1 ! Parameter for AP2 ! ! |
| ! ! Report Line EC: ! Report Line EE: !Definition: ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! / ! / !No Mode ! |
| ! ! ! !Active ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.11 = 1 ! 01.2.275.00.11 = 1!RUNWAY Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.12 = 1 ! 01.2.275.00.12 = 1!NAV Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.13 = 1 ! 01.2.275.00.13 = 1!LOC CAPTURE ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.14 = 1 ! 01.2.275.00.14 = 1!LOC TRACK ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.15 = 1 ! 01.2.275.00.15 = 1!Roll GO ! |
| ! ! ! !AROUND Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.16 = 1 ! 01.2.275.00.16 = 1!HEADING Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.17 = 1 ! 01.2.275.00.17 = 1!TRACK Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.15 = 1 ! 01.2.274.00.15 = 1!PITCH T/O ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.16 = 1 ! 01.2.274.00.16 = 1!PITCH GA Mode! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.17 = 1 ! 01.2.274.00.17 = 1!V/S Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.18 = 1 ! 01.2.274.00.18 = 1!FPA Mode ! |
| ! ! -------------------!-------------------!-------------! |
| ! ! 01.1.274.00.19 = 1 ! 01.2.274.00.19 = 1!ALT Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.20 = 1 ! 01.2.274.00.20 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.19 = 1 ! 01.2.274.00.19 = 1!ALT ACQ ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.21 = 1 ! 01.2.274.00.21 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.20 = 1 ! 01.2.274.00.20 = 1!G/S TRACK ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.22 = 1 ! 01.2.274.00.22 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.21 = 1 ! 01.2.274.00.21 = 1!G/S CAPTURE ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.22 = 1 ! 01.2.274.00.22 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.23 = 1 ! 01.2.274.00.23 = 1!FINAL DES ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.24 = 1 ! 01.2.274.00.24 = 1!EXPED. Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.146.00.14 = 1 ! 01.2.146.00.14 = 1!LAND TRACK ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!CLB Mode ! |
| ! ! AND ! AND ! ! |
| ! ! ! ! ! ! ! |
| ! ! -------------- ! -------------- ! ! |
| ! ! 01.1.274.00.13 = 0 ! 01.2.274.00.13 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.14 = 0 ! 01.2.274.00.14 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.24 = 0 ! 01.2.274.00.24 = 0! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!DES Mode ! |
| ! ! AND ! AND ! ! |
| ! ! ! ! ! ! ! |
| ! ! -------------- ! -------------- ! ! |
| ! ! 01.1.274.00.13 = 0 ! 01.2.274.00.13 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.14 = 0 ! 01.2.274.00.14 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.24 = 0 ! 01.2.274.00.24 = 0! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!IM. CLIMB ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.13 = 1 ! 01.2.274.00.13 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!IM. DES Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.13 = 1 ! 01.2.274.00.13 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!OPEN CLB ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.14 = 1 ! 01.2.274.00.14 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!OPEN. DES ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.14 = 1 ! 01.2.274.00.14 = 1! ! |
| ! ! ---------------------------------------------------- ! |
| ! ! Auto Pilot Status DMU: ! |
| ! ! Auto Pilot AP1 printed in report line EC ! |
| ! ! Auto Pilot AP2 printed in report line EE ! |
| ! ! Combined Auto Pilot Modes ! |
| ! ! The longitudinal auto pilot mode (1 to G) shall ! |
| ! ! appear on the left position for the AP1 and AP2 print! |
| ! ! format. ! |
| ! ! The lateral auto pilot mode (1 to 8) shall appear on ! |
| ! ! the right position for the AP1 and AP2 print format. ! |
| ! ! In case of a combined auto pilot mode e.g. DES mode ! |
| ! ! and NAV mode are engaged simultaneously, the 'E3' ! |
| ! ! shall appear below AP1 and AP2. ! |
| ! ! XX Auto Pilot Modes: ! |
| ! ! !! ! |
| ! ! !!__Lateral Modes: 0 = NO MODE ! |
| ! ! ! 1 = HEADING ! |
| ! ! ! 2 = TRACK ! |
| ! ! ! 3 = NAV ! |
| ! ! ! 4 = LOC CAPTURE ! |
| ! ! ! 5 = LOCK TRACK ! |
| ! ! ! 6 = LAND TRACK ! |
| ! ! ! 7 = RUNWAY ! |
| ! ! ! 8 = ROLL GO AROUND ! |
| ! ! ! ! |
| ! ! !__Longitudinal Modes: 0 = NO MODE ! |
| ! ! 1 = PITCH G/A ! |
| ! ! 2 = PITCH TO ! |
| ! ! 3 = G/S TRACK ! |
| ! ! 4 = G/S CAPTURE ! |
| ! ! 5 = V/S ! |
| ! ! 6 = FPA ! |
| ! ! 7 = ALT ! |
| ! ! 8 = ALT ACQ ! |
| ! ! 9 = OPEN CLB ! |
| ! ! A = OPEN DES ! |
| ! ! B = IM CLB ! |
| ! ! C = IM DES ! |
| ! ! D = CLB ! |
| ! ! E = DES ! |
| ! ! F = FINAL DES ! |
| ! ! G = EXPEDITE ! |
| !--------------!------------------------------------------------------! |
| ! N1 ! Selected N1 Actual ! |
| ! 9999 ! (0 to 120.0 %rpm) ! |
| ! ! ECU 7C.1.346.01 Engine 1 ! |
| ! ! 7C.2.346.10 Engine 2 ! |
| ! ! Remark: In the report line V3 and V4 the values ! |
| ! ! from the last stable descent shall be ! |
| ! ! printed. ! |
| ! ! In the report line V5 and V6 the values ! |
| ! ! from the last stable climb shall be ! |
| ! ! printed. ! |
| !--------------!------------------------------------------------------! |
| ! N1C ! N1 Command ! |
| ! 9999 ! (0 to 120.0 %rpm) ! |
| ! ! ECU 7C.1.341.01 Engine 1 ! |
| ! ! 7C.2.341.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! N2 ! Selected N2 Actual ! |
| ! 9999 ! (0 to 120.0 %rpm) ! |
| ! ! ECU 7C.1.344.01 Engine 1 ! |
| ! ! 7C.2.344.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! EGT ! Selected T495 (Exhaust Gas Temperature) ! |
| ! X999 ! (-55 to 999.9 [C) ! |
| ! ! Negative values shall be indicated by '-' on the ! |
| ! ! first position. Otherwise the first position shall ! |
| ! ! be used for the value. ! |
| ! ! ECU 7C.1.345.01 Engine 1 ! |
| ! ! 7C.2.345.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! FF ! Engine Fuel Flow ! |
| ! 9999 ! 0 to 7000 kg/h (0 to 15000 p/h) ! |
| ! ! ECU 7C.1.244.01 Engine 1 ! |
| ! ! 7C.2.244.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! PS13 ! PS13 Static Air Pressure at Position 1.3 ! |
| ! 99999 ! (0.0 to 30.000 psia) ! |
| ! ! ECU 7C.1.127.01 Engine 1 ! |
| ! ! 7C.2.127.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! P25 ! P25 Total Air Pressure at Position 2.5 ! |
| ! 99999 ! (0.0 to 50.000 psia) ! |
| ! ! ECU 7C.1.262.01 Engine 1 ! |
| ! ! 7C.2.262.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! P3 ! Selected PS3 (Burner Pressure) ! |
| ! 9999 ! (0.0 to 450.0 psia) ! |
| ! ! ECU 7C.1.264.01 Engine 1 ! |
| ! ! 7C.2.264.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! T3 ! Selected T3 ! |
| ! X999 ! (-55.0 to 850.0 deg C) ! |
| ! ! Negative values shall be indicated by '-' on the ! |
| ! ! first position. Otherwise the first position shall ! |
| ! ! be used for the value. ! |
| ! ! ECU 7C.1.265.01 Engine 1 ! |
| ! ! 7C.2.265.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! T5 ! T5 Temperature at position T5 ! |
| ! X999 ! (-55.0 to 850.0 [C) ! |
| ! ! Negative values shal be indicated by '-' on the ! |
| ! ! first position. Otherwise the firt position shall ! |
| ! ! be used for the value. ! |
| ! ! ECU 7C.1.260.01 Engine 1 ! |
| ! ! 7C.2.260.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! VSV ! Selected Variable Stator Vane Position ! |
| ! X99 ! (-5.0 to 45.0 deg) ! |
| ! ! Negative values shall be indicated by '-' on the ! |
| ! ! first position. Otherwise the first position shall ! |
| ! ! be used for the value. ! |
| ! ! ECU 7C.1.072.01 Engine 1 ! |
| ! ! 7C.2.072.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! VBV ! Variable Bleed Valve Position ! |
| ! X99 ! (-9.9 to 40.0 deg) ! |
| ! ! Negative values shall be indicated by '-' on the ! |
| ! ! first position. Otherwise the first position shall ! |
| ! ! be used for the value. ! |
| ! ! ECU 7C.1.071.01 Engine 1 ! |
| ! ! 7C.2.071.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! HPT ! Selected High-Pressure Turbine Clearance Position ! |
| ! X99 ! (-10 to 100 %) ! |
| ! ! ECU 7C.1.306.01 Engine 1 ! |
| ! ! 7C.2.306.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! LPT ! Selected LPTC Posiiton ! |
| ! X99 ! (-10 to 100 %) ! |
| ! ! ECU 7C.1.307.01 Engine 1 ! |
| ! ! 7C.2.307.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! GLE ! Engine Generator Load ! |
| ! 999 ! (0 to 100%) ! |
| ! ! SDAC 29.1.077.01 Engine 1 ! |
| ! ! 29.2.077.01 ! |
| ! ! 29.1.077.10 Engine 2 ! |
| ! ! 29.2.077.10 ! |
| !--------------!------------------------------------------------------! |
| ! PD ! Precooler Inlet Pressure ! |
| ! 99 ! (0 to 50 psi) ! |
| ! ! BMC 06F.1.143.01 Engine 1 ! |
| ! ! 06F.2.143.10 ! |
| ! ! 06F.1.142.01 Engine 2 ! |
| ! ! 06F.2.142.10 ! |
| !--------------!------------------------------------------------------! |
| ! TN ! Nacelle Temperature ! |
| ! X99 ! (-55 to 300 [C) ! |
| ! ! Negative values shall be indicated by '-' on the ! |
| ! ! first position. Otherwise the first position shall ! |
| ! ! be used for the value. ! |
| ! ! FWC 26.1.322.01 Engine 1 ! |
| ! ! 26.2.322.01 ! |
| ! ! 26.1.322.10 Engine 2 ! |
| ! ! 26.2.322.10 ! |
| !--------------!------------------------------------------------------! |
| ! PT2 ! PT2 Total Air Pressure at Position 2 ! |
| ! 99999 ! (0.0 to 25.000 psia) ! |
| ! ! ECU 7C.1.131.01 Engine 1 ! |
| ! ! 7C.2.131.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! VN ! FAN Pick Up N1 Track Vibration ! |
| ! 99 ! (0.0 to 10.0) ! |
| ! ! If value is 10.0 then 99 shall be printed. ! |
| ! ! EVM 3D.1.227.01 Engine 1 ! |
| ! ! 3D.1.227.10 Engine 2 ! |
| ! ! Remark: In report line V3 and V4 the values from ! |
| ! ! the last stable descent shall be ! |
| ! ! printed. ! |
| ! ! In report line V5 and V6 the values from ! |
| ! ! the last stable climb shall be printed. ! |
| !--------------!------------------------------------------------------! |
| ! VL ! TRF Pick Up N1 Vibration ! |
| ! 99 ! (0.0 to 10.0) ! |
| ! ! If value is 10.0 then 99 shall be printed. ! |
| ! ! EVM 3D.1.227.11 Engine 1 ! |
| ! ! 3D.1.227.00 Engine 2 ! |
| ! ! Remark: In report line V3 and V4 the values frome ! |
| ! ! the last stable descent shall be ! |
| ! ! printed. ! |
| ! ! In report line V5 and V6 the values frome ! |
| ! ! the last stable climb shall be printed. ! |
| !--------------!------------------------------------------------------! |
| ! PHA ! FAN Pick Up Phase Angle ! |
| ! 999 ! (0 to 360 deg) ! |
| ! ! EVM 3D.1.226.01 Engine 1 ! |
| ! ! 3D.1.226.10 Engine 2 ! |
| ! ! Remark: In report line V3 and V4 the values frome ! |
| ! ! the last stable descent shall be ! |
| ! ! printed. ! |
| ! ! In report line V5 and V6 the values frome ! |
| ! ! the last stable climb shall be printed. ! |
| !--------------!------------------------------------------------------! |
| ! PHT ! TRF Pick Up Phase Angle ! |
| ! 999 ! (0 to 360 deg) ! |
| ! ! EVM 3D.1.226.11 Engine 1 ! |
| ! ! 3D.1.226.00 Engine 2 ! |
| ! ! Remark: In report line V3 and V4 the values frome ! |
| ! ! the last stable descent shall be ! |
| ! ! printed. ! |
| ! ! In report line V5 and V6 the values frome ! |
| ! ! the last stable climb shall be printed. ! |
| !--------------!------------------------------------------------------! |
| ! VC ! FAN Pick Up N2 Track Vibration ! |
| ! 99 ! (0.0 to 4.0) ! |
| ! ! EVM 3D.1.230.01 Engine 1 ! |
| ! ! 3D.1.230.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! VH ! TRF Pick Up N2 Track Vibration ! |
| ! 99 ! (0.0 to 4.0) ! |
| ! ! EVM 3D.1.230.11 Engine 1 ! |
| ! ! 3D.1.230.00 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! EVM ! Engine Vibration Status Word ! |
| ! XXXXX ! EVM 3D.1.035.01 Engine 1 ! |
| ! ! 3D.1.035.10 Engine 2 ! |
| ! ! XXXXX Bits HEX ! |
| ! ! !!!!!________14, 13, 12, 11 0..F ! |
| ! ! !!!!_________18, 17, 16, 15 0..F ! |
| ! ! !!!__________22, 21, 20, 19 0..F ! |
| ! ! !!___________26, 25, 24, 23 0..F ! |
| ! ! !____________ 29, 28, 27 0..F ! |
| !--------------!------------------------------------------------------! |
| ! OIP ! Engine Oil Pressure ! |
| ! 999 ! (0 to 400 psia) ! |
| ! ! FWC 26.1.317.01 Engine 1 ! |
| ! ! 26.2.317.01 ! |
| ! ! 26.1.317.10 Engine 2 ! |
| ! ! 26.2.317.10 ! |
| !--------------!------------------------------------------------------! |
| ! OIT ! Engine Oil Temperature ! |
| ! X99 ! (-60 to 250 C) ! |
| ! ! Negative values shal be indicated by '-' on the ! |
| ! ! first position. Otherwise the firt position shall ! |
| ! ! be used for the value. ! |
| ! ! FWC 26.1.316.01 Engine 1 ! |
| ! ! 26.2.316.01 ! |
| ! ! 26.1.316.10 Engine 2 ! |
| ! ! 26.2.316.10 ! |
| !--------------!------------------------------------------------------! |
| ! ECW1 ! Engine Control Word 1 ! |
| ! XXXXX ! XXXXX Bits HEX ! |
| ! ! !!!!!________14, 13, 12, 11 0..F ! |
| ! ! !!!!_________18, 17, 16, 15 0..F ! |
| ! ! !!!__________22, 21, 20, 19 0..F ! |
| ! ! !!___________26, 25, 24, 23 0..F ! |
| ! ! !____________ 29, 28, 27 0..F ! |
| ! ! Bit Label Parameter Description ! |
| ! ! 11 7C.X.272.XX.19 = 1 Auto Thrust Active ! |
| ! ! 12 7C.X.275.XX.20 = 1 VSV Position Fault ! |
| ! ! 13 SPARE ! |
| ! ! 14 SPARE ! |
| ! ! 15 7C.X.351.XX.29 = 1 Fuel Flow Measurement ! |
| ! ! Invalid ! |
| ! ! 16 7C.X.275.XX.15 = 1 N1/N2 Control Active ! |
| ! ! 17 7C.X.275.XX.26 = 1 Channel A Active ! |
| ! ! 18 7C.X.275.XX.27 = 1 Channel B Active ! |
| ! ! 19 SPARE ! |
| ! ! 20 SPARE ! |
| ! ! 21 SPARE ! |
| ! ! 22 SPARE ! |
| ! ! 23 SPARE ! |
| ! ! 24 SPARE ! |
| ! ! 25 SPARE ! |
| ! ! 26 SPARE ! |
| ! ! 27 SPARE ! |
| ! ! 28 SPARE ! |
| ! ! 29 SPARE ! |
| ! ! The 'X' for the System and SDI definition of the ! |
| ! ! engine parameters shall be as follows: ! |
| ! ! System SDI ! |
| ! ! Engine 1 1 01 ! |
| ! ! Engine 2 2 10 ! |
| !--------------!------------------------------------------------------! |
| ! SSEL ! Engine Control Word 1 ! |
| ! XXXXXXX ! Status of different FADEC sensors ! |
| ! XXXXXXX ! XXXXXXXXXXXXXX Label: Selected: ! |
| ! ! !!!!!!!!!!!!!!_ 346 N1 actual (Bit 11 -> 15)! |
| ! ! !!!!!!!!!!!!!__ 345 EGT (Bit 11 -> 15)! |
| ! ! !!!!!!!!!!!!___ 344 N2 actual (Bit 11 -> 15)! |
| ! ! !!!!!!!!!!!____ 263 T25 (Bit 11 -> 15)! |
| ! ! !!!!!!!!!!_____ 264 PS3 (Bit 11 -> 15)! |
| ! ! !!!!!!!!!______ 265 T3 (Bit 11 -> 15)! |
| ! ! !!!!!!!!_______ 072 VSV Position (Bit 11 -> 15)! |
| ! ! !!!!!!!________ 071 VBV Position (Bit 11 -> 15)! |
| ! ! !!!!!!_________ 306 HPTC Position (Bit 11 -> 15)! |
| ! ! !!!!!__________ 307 LPTH Position (Bit 11 -> 15)! |
| ! ! !!!!___________ 347 FMV Position (Bit 11 -> 15)! |
| ! ! !!!____________ 211 TAT (Bit 11 -> 15)! |
| ! ! !!_____________ 114 P0 (Bit 11 -> 15)! |
| ! ! !______________ 133 TLA Position (Bit 11 -> 15)! |
| ! ! Source: ECU, different labels ! |
| ! ! The indicated values shall be coded as follows: ! |
| ! ! Bit: 15 14 13 12 11 ! indicated value ! |
| ! ! --------------------!---------------- ! |
| ! ! 0 0 0 0 0 ! 0 ! |
| ! ! 0 0 0 0 1 ! 1 ! |
| ! ! 0 0 0 1 0 ! 2 ! |
| ! ! 0 0 0 1 1 ! 3 ! |
| ! ! 0 0 1 0 0 ! 4 ! |
| ! ! 0 0 1 0 1 ! 5 ! |
| ! ! 0 0 1 1 0 ! 6 ! |
| ! ! 0 0 1 1 1 ! 7 ! |
| ! ! 0 1 0 0 0 ! 8 ! |
| ! ! 0 1 0 0 1 ! 9 ! |
| ! ! 0 1 0 1 0 ! A ! |
| ! ! 0 1 0 1 1 ! B ! |
| ! ! 0 1 1 0 0 ! C ! |
| ! ! 0 1 1 0 1 ! D ! |
| ! ! 0 1 1 1 0 ! E ! |
| ! ! 0 1 1 1 1 ! F ! |
| ! ! 1 0 0 0 0 ! G ! |
| ! ! 1 0 0 0 1 ! H ! |
| ! ! 1 0 0 1 0 ! I ! |
| ! ! 1 0 0 1 1 ! J ! |
| ! ! 1 0 1 0 0 ! K ! |
| ! ! 1 0 1 0 1 ! L ! |
| ! ! 1 0 1 1 0 ! M ! |
| ! ! 1 0 1 1 1 ! N ! |
| ! ! 1 1 0 0 0 ! O ! |
| ! ! 1 1 0 0 1 ! P ! |
| ! ! 1 1 0 1 0 ! Q ! |
| ! ! 1 1 0 1 1 ! R ! |
| ! ! 1 1 1 0 0 ! S ! |
| ! ! 1 1 1 0 1 ! T ! |
| ! ! 1 1 1 1 0 ! U ! |
| ! ! 1 1 1 1 1 ! V ! |
| !--------------!------------------------------------------------------! |
| ! EGTK ! Corrected Exhaust Gas Temperature ! |
| ! X999 ! (-55 to 999.9 deg C) ! |
| ! ! EGT ! |
| ! ! EGTK=-------------- ! |
| ! ! pow(THETA2,n2) ! |
| ! ! THETA2 = (TAT+273.15)/288.18 ! |
| ! ! n2 = programmable value, standard value 1.05 ! |
| ! ! TAT = 06.1.211.01 ! |
| ! ! 06.2.211.10 ! |
| ! ! EGT = 7C.1.345.01 ! |
| ! ! 7C.2.345.10 ! |
| !--------------!------------------------------------------------------! |
| ! N1K ! Corrected N1 ! |
| ! 9999 ! (0 to 120 %rpm) ! |
| ! ! N1 ! |
| ! ! N1K=-------------- ! |
| ! ! pow(THETA2,n1) ! |
| ! ! THETA2 = (TAT+273.15)/288.18 ! |
| ! ! n1 = programmable value, standard value 0.5 ! |
| ! ! TAT = 06.1.211.01 ! |
| ! ! 06.2.211.10 ! |
| ! ! N1 = 7C.1.346.10 Engine ! |
| ! ! 7C.2.346.10 Engine ! |
| !--------------!------------------------------------------------------! |
| ! N2K ! Corrected N2 ! |
| ! 9999 ! (0 to 120 %rpm) ! |
| ! ! N2 ! |
| ! ! N2K=-------------- ! |
| ! ! pow(THETA2,n3) ! |
| ! ! THETA2 = (TAT+273.15)/288.18 ! |
| ! ! n3 = programmable value, standard value 0.5 ! |
| ! ! TAT = 06.1.211.01 ! |
| ! ! 06.2.211.10 ! |
| ! ! N2 = 7C.1.344.01 Engine 1 ! |
| ! ! 7C.2.344.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! FFK ! Corrected Engine Fuel Low ! |
| ! 9999 ! (0 to 7000Kg/h ( 0 to 15000 p/h)) ! |
| ! ! FF ! |
| ! ! FFK=--------------------- ! |
| ! ! pow(THETA2,n4)*delta2 ! |
| ! ! THETA2 = (TAT+273.15)/288.18 ! |
| ! ! n4 = programmable value, standard value 0.63 ! |
| ! ! delta2 = PT2/14.696 ! |
| ! ! TAT = 06.1.211.01 ! |
| ! ! 06.2.211.10 ! |
| ! ! FF = 7C.1.244.01 Engine 1 ! |
| ! ! 7C.2.244.10 Engine 2 ! |
| ! ! PT2 = 7C.1.131.01 Engine 1 ! |
| ! ! 7C.2.131.10 Engine 2 ! |
| +---------------------------------------------------------------------+ |
(5) Engine Run Up Report Data Field Description <11> (Engine Type CFMI with Advanced EVMU)
NOTE: Reports that are transmitted from the ACARS system do not have report lines without a line identifier.
| +---------------------------------------------------------------------+ |
| ! Value ! Content Description ! |
| !--------------!------------------------------------------------------! |
| ! ESN ! Engine Serial Number ! |
| ! 999999 ! (000000 to 999999) ! |
| ! ! ECU Engine 1 7C.1.046.01 digit 3, 2, 1 ! |
| ! ! 7C.1.047.01 digit 6, 5, 4 ! |
| ! ! Engine 2 7C.2.046.10 digit 3, 2, 1 ! |
| ! ! 7C.2.047.10 digit 6, 5, 4 ! |
| !--------------!------------------------------------------------------! |
| ! EHRS ! Engine Flight Hours ! |
| ! 99999 ! (00000 to 99999 hours) ! |
| ! ! DMU Engine 1 ! |
| ! ! Engine 2 ! |
| ! ! Remark: Time between "Main (LH and RH) Landing Gear! |
| ! ! Decompressed" and "Main (LH and RH) Landing! |
| ! ! Gear Compressed". The EHRS shall be set to ! |
| ! ! zero if a new ESN is recognized by the DMU.! |
| ! ! It shall be possible to set the EHRS via ! |
| ! ! the MCDU, e.g. if the DMU is changed on the! |
| ! ! a/c. ! |
| !--------------!------------------------------------------------------! |
| ! ERT ! Engine Running Time ! |
| ! 99999 ! (00000 to 65536 hours) ! |
| ! ! ECU 7C.1.050.01 Engine 1 ! |
| ! ! 7C.2.050.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! ECYC ! Engine Cycle ! |
| ! 99999 ! (00000 to 99999) ! |
| ! ! DMU Engine 1 ! |
| ! ! Engine 2 ! |
| ! ! Remark: Each time when flight phase 5 (climb) is ! |
| ! ! reached, the counter shall be incremented ! |
| ! ! by one. The ECYC is set to zero if a new ! |
| ! ! ESN is recognized by the DMU. It shall be ! |
| ! ! possible to set ECYC via the MCDU, if the ! |
| ! ! DMU is changed on the a/c. ! |
| !--------------!------------------------------------------------------! |
| ! AP ! Auto Pilot Status ! |
| ! 99 ! Number of respective status (00 to G8) ! |
| ! ! FMGC 1 and 2 (FGC part) for Auto Pilot AP1 and AP2 ! |
| ! ! ! |
| ! ! Parameter for AP1 ! Parameter for AP2 ! ! |
| ! ! Report Line EC: ! Report Line EE: !Definition: ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! / ! / !No Mode ! |
| ! ! ! !Active ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.11 = 1 ! 01.2.275.00.11 = 1!RUNWAY Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.12 = 1 ! 01.2.275.00.12 = 1!NAV Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.13 = 1 ! 01.2.275.00.13 = 1!LOC CAPTURE ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.14 = 1 ! 01.2.275.00.14 = 1!LOC TRACK ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.15 = 1 ! 01.2.275.00.15 = 1!Roll GO ! |
| ! ! ! !AROUND Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.16 = 1 ! 01.2.275.00.16 = 1!HEADING Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.275.00.17 = 1 ! 01.2.275.00.17 = 1!TRACK Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.15 = 1 ! 01.2.274.00.15 = 1!PITCH T/O ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.16 = 1 ! 01.2.274.00.16 = 1!PITCH GA Mode! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.17 = 1 ! 01.2.274.00.17 = 1!V/S Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.18 = 1 ! 01.2.274.00.18 = 1!FPA Mode ! |
| ! ! -------------------!-------------------!-------------! |
| ! ! 01.1.274.00.19 = 1 ! 01.2.274.00.19 = 1!ALT Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.20 = 1 ! 01.2.274.00.20 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.19 = 1 ! 01.2.274.00.19 = 1!ALT ACQ ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.21 = 1 ! 01.2.274.00.21 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.20 = 1 ! 01.2.274.00.20 = 1!G/S TRACK ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.22 = 1 ! 01.2.274.00.22 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.21 = 1 ! 01.2.274.00.21 = 1!G/S CAPTURE ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.22 = 1 ! 01.2.274.00.22 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.23 = 1 ! 01.2.274.00.23 = 1!FINAL DES ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.24 = 1 ! 01.2.274.00.24 = 1!EXPED. Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.146.00.14 = 1 ! 01.2.146.00.14 = 1!LAND TRACK ! |
| ! ! ! !Mode ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!CLB Mode ! |
| ! ! AND ! AND ! ! |
| ! ! ! ! ! ! ! |
| ! ! -------------- ! -------------- ! ! |
| ! ! 01.1.274.00.13 = 0 ! 01.2.274.00.13 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.14 = 0 ! 01.2.274.00.14 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.24 = 0 ! 01.2.274.00.24 = 0! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!DES Mode ! |
| ! ! AND ! AND ! ! |
| ! ! ! ! ! ! ! |
| ! ! -------------- ! -------------- ! ! |
| ! ! 01.1.274.00.13 = 0 ! 01.2.274.00.13 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.14 = 0 ! 01.2.274.00.14 = 0! ! |
| ! ! OR ! OR ! ! |
| ! ! 01.1.274.00.24 = 0 ! 01.2.274.00.24 = 0! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!IM. CLIMB ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.13 = 1 ! 01.2.274.00.13 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!IM. DES Mode ! |
| ! ! AND ! AND ! ! |
| ! ! 01.1.274.00.13 = 1 ! 01.2.274.00.13 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!OPEN CLB ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.14 = 1 ! 01.2.274.00.14 = 1! ! |
| ! ! -------------------!-------------------!------------ ! |
| ! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!OPEN. DES ! |
| ! ! AND ! AND !Mode ! |
| ! ! 01.1.274.00.14 = 1 ! 01.2.274.00.14 = 1! ! |
| ! ! ---------------------------------------------------- ! |
| ! ! Auto Pilot Status DMU: ! |
| ! ! Auto Pilot AP1 printed in report line EC ! |
| ! ! Auto Pilot AP2 printed in report line EE ! |
| ! ! Combined Auto Pilot Modes ! |
| ! ! The longitudinal auto pilot mode (1 to G) shall ! |
| ! ! appear on the left position for the AP1 and AP2 print! |
| ! ! format. ! |
| ! ! The lateral auto pilot mode (1 to 8) shall appear on ! |
| ! ! the right position for the AP1 and AP2 print format. ! |
| ! ! In case of a combined auto pilot mode e.g. DES mode ! |
| ! ! and NAV mode are engaged simultaneously, the 'E3' ! |
| ! ! shall appear below AP1 and AP2. ! |
| ! ! XX Auto Pilot Modes: ! |
| ! ! !! ! |
| ! ! !!__Lateral Modes: 0 = NO MODE ! |
| ! ! ! 1 = HEADING ! |
| ! ! ! 2 = TRACK ! |
| ! ! ! 3 = NAV ! |
| ! ! ! 4 = LOC CAPTURE ! |
| ! ! ! 5 = LOCK TRACK ! |
| ! ! ! 6 = LAND TRACK ! |
| ! ! ! 7 = RUNWAY ! |
| ! ! ! 8 = ROLL GO AROUND ! |
| ! ! ! ! |
| ! ! !__Longitudinal Modes: 0 = NO MODE ! |
| ! ! 1 = PITCH G/A ! |
| ! ! 2 = PITCH TO ! |
| ! ! 3 = G/S TRACK ! |
| ! ! 4 = G/S CAPTURE ! |
| ! ! 5 = V/S ! |
| ! ! 6 = FPA ! |
| ! ! 7 = ALT ! |
| ! ! 8 = ALT ACQ ! |
| ! ! 9 = OPEN CLB ! |
| ! ! A = OPEN DES ! |
| ! ! B = IM CLB ! |
| ! ! C = IM DES ! |
| ! ! D = CLB ! |
| ! ! E = DES ! |
| ! ! F = FINAL DES ! |
| ! ! G = EXPEDITE ! |
| !--------------!------------------------------------------------------! |
| ! N1 ! Selected N1 Actual ! |
| ! 9999 ! (0 to 120.0 %rpm) ! |
| ! ! ECU 7C.1.346.01 Engine 1 ! |
| ! ! 7C.2.346.10 Engine 2 ! |
| ! ! Remark: In the report line V3 and V4 the values ! |
| ! ! from the last stable descent shall be ! |
| ! ! printed. ! |
| ! ! In the report line V5 and V6 the values ! |
| ! ! from the last stable climb shall be ! |
| ! ! printed. ! |
| !--------------!------------------------------------------------------! |
| ! N1C ! N1 Command ! |
| ! 9999 ! (0 to 120.0 %rpm) ! |
| ! ! ECU 7C.1.341.01 Engine 1 ! |
| ! ! 7C.2.341.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! N2 ! Selected N2 Actual ! |
| ! 9999 ! (0 to 120.0 %rpm) ! |
| ! ! ECU 7C.1.344.01 Engine 1 ! |
| ! ! 7C.2.344.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! EGT ! Selected T495 (Exhaust Gas Temperature) ! |
| ! X999 ! (-55 to 999.9 [C) ! |
| ! ! Negative values are indicated by 'N' on the ! |
| ! ! first position. Otherwise the first position is ! |
| ! ! used for the value. ! |
| ! ! ECU 7C.1.345.01 Engine 1 ! |
| ! ! 7C.2.345.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! FF ! Engine Fuel Flow ! |
| ! 9999 ! 0 to 7000 kg/h (0 to 15000 p/h) ! |
| ! ! ECU 7C.1.244.01 Engine 1 ! |
| ! ! 7C.2.244.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! PS13 ! PS13 Static Air Pressure at Position 1.3 ! |
| ! 99999 ! (0.0 to 30.000 psia) ! |
| ! ! ECU 7C.1.127.01 Engine 1 ! |
| ! ! 7C.2.127.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! P25 ! P25 Total Air Pressure at Position 2.5 ! |
| ! 99999 ! (0.0 to 50.000 psia) ! |
| ! ! ECU 7C.1.262.01 Engine 1 ! |
| ! ! 7C.2.262.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! P3 ! Selected PS3 (Burner Pressure) ! |
| ! 9999 ! (0.0 to 450.0 psia) ! |
| ! ! ECU 7C.1.264.01 Engine 1 ! |
| ! ! 7C.2.264.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! T3 ! Selected T3 ! |
| ! X999 ! (-55.0 to 850.0 deg C) ! |
| ! ! Negative values are indicated by 'N' on the ! |
| ! ! first position. Otherwise the first position is ! |
| ! ! used for the value. ! |
| ! ! ECU 7C.1.265.01 Engine 1 ! |
| ! ! 7C.2.265.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! T5 ! T5 Temperature at position T5 ! |
| ! X999 ! (-55.0 to 850.0 [C) ! |
| ! ! Negative values are indicated by 'N' on the ! |
| ! ! first position. Otherwise the firt position is ! |
| ! ! used for the value. ! |
| ! ! ECU 7C.1.260.01 Engine 1 ! |
| ! ! 7C.2.260.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! VSV ! Selected Variable Stator Vane Position ! |
| ! X99 ! (-5.0 to 45.0 deg) ! |
| ! ! Negative values are indicated by 'N' on the ! |
| ! ! first position. Otherwise the first position is ! |
| ! ! used for the value. ! |
| ! ! ECU 7C.1.072.01 Engine 1 ! |
| ! ! 7C.2.072.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! VBV ! Variable Bleed Valve Position ! |
| ! X99 ! (-9.9 to 40.0 deg) ! |
| ! ! Negative values are indicated by 'N' on the ! |
| ! ! first position. Otherwise the first position is ! |
| ! ! used for the value. ! |
| ! ! ECU 7C.1.071.01 Engine 1 ! |
| ! ! 7C.2.071.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! HPT ! Selected High-Pressure Turbine Clearance Position ! |
| ! X99 ! (-10 to 100 %) ! |
| ! ! ECU 7C.1.306.01 Engine 1 ! |
| ! ! 7C.2.306.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! LPT ! Selected LPTC Posiiton ! |
| ! X99 ! (-10 to 100 %) ! |
| ! ! ECU 7C.1.307.01 Engine 1 ! |
| ! ! 7C.2.307.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! GLE ! Engine Generator Load ! |
| ! 999 ! (0 to 100%) ! |
| ! ! SDAC 29.1.077.01 Engine 1 ! |
| ! ! 29.2.077.01 ! |
| ! ! 29.1.077.10 Engine 2 ! |
| ! ! 29.2.077.10 ! |
| !--------------!------------------------------------------------------! |
| ! PD ! Precooler Inlet Pressure ! |
| ! 99 ! (0 to 50 psi) ! |
| ! ! BMC 06F.1.143.01 Engine 1 ! |
| ! ! 06F.2.143.10 ! |
| ! ! 06F.1.142.01 Engine 2 ! |
| ! ! 06F.2.142.10 ! |
| !--------------!------------------------------------------------------! |
| ! TN ! Nacelle Temperature ! |
| ! X99 ! (-55 to 300 [C) ! |
| ! ! Negative values are indicated by 'N' on the ! |
| ! ! first position. Otherwise the first position is ! |
| ! ! used for the value. ! |
| ! ! FWC 26.1.322.01 Engine 1 ! |
| ! ! 26.2.322.01 ! |
| ! ! 26.1.322.10 Engine 2 ! |
| ! ! 26.2.322.10 ! |
| !--------------!------------------------------------------------------! |
| ! PT2 ! PT2 Total Air Pressure at Position 2 ! |
| ! 99999 ! (0.0 to 25.000 psia) ! |
| ! ! ECU 7C.1.131.01 Engine 1 ! |
| ! ! 7C.2.131.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! VN ! FAN Pick Up N1 Track Vibration ! |
| ! 99 ! (0.0 to 10.0) ! |
| ! ! If value is 10.0 then 99 shall be printed. ! |
| ! ! EVM 3D.1.227.01 Engine 1 ! |
| ! ! 3D.1.227.10 Engine 2 ! |
| ! ! Remark: In report line V3 and V4 the values from ! |
| ! ! the last stable descent shall be ! |
| ! ! printed. ! |
| ! ! In report line V5 and V6 the values from ! |
| ! ! the last stable climb shall be printed. ! |
| !--------------!------------------------------------------------------! |
| ! VL ! TRF Pick Up N1 Vibration ! |
| ! 99 ! (0.0 to 10.0) ! |
| ! ! If value is 10.0 then 99 shall be printed. ! |
| ! ! EVM 3D.1.227.11 Engine 1 ! |
| ! ! 3D.1.227.00 Engine 2 ! |
| ! ! Remark: In report line V3 and V4 the values frome ! |
| ! ! the last stable descent shall be ! |
| ! ! printed. ! |
| ! ! In report line V5 and V6 the values frome ! |
| ! ! the last stable climb shall be printed. ! |
| !--------------!------------------------------------------------------! |
| ! PHA ! FAN Pick Up Phase Angle ! |
| ! 999 ! (0 to 360 deg) ! |
| ! ! EVM 3D.1.226.01 Engine 1 ! |
| ! ! 3D.1.226.10 Engine 2 ! |
| ! ! Remark: In report line V3 and V4 the values frome ! |
| ! ! the last stable descent shall be ! |
| ! ! printed. ! |
| ! ! In report line V5 and V6 the values frome ! |
| ! ! the last stable climb shall be printed. ! |
| !--------------!------------------------------------------------------! |
| ! PHT ! TRF Pick Up Phase Angle ! |
| ! 999 ! (0 to 360 deg) ! |
| ! ! EVM 3D.1.226.11 Engine 1 ! |
| ! ! 3D.1.226.00 Engine 2 ! |
| ! ! Remark: In report line V3 and V4 the values frome ! |
| ! ! the last stable descent shall be ! |
| ! ! printed. ! |
| ! ! In report line V5 and V6 the values frome ! |
| ! ! the last stable climb shall be printed. ! |
| !--------------!------------------------------------------------------! |
| ! VC ! FAN Pick Up N2 Track Vibration ! |
| ! 99 ! (0.0 to 4.0) ! |
| ! ! EVM 3D.1.230.01 Engine 1 ! |
| ! ! 3D.1.230.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! VH ! TRF Pick Up N2 Track Vibration ! |
| ! 99 ! (0.0 to 4.0) ! |
| ! ! EVM 3D.1.230.11 Engine 1 ! |
| ! ! 3D.1.230.00 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! EVM ! Engine Vibration Status Word ! |
| ! XXXXX ! EVM 3D.1.035.01 Engine 1 ! |
| ! ! 3D.1.035.10 Engine 2 ! |
| ! ! XXXXX Bits HEX ! |
| ! ! !!!!!________14, 13, 12, 11 0..F ! |
| ! ! !!!!_________18, 17, 16, 15 0..F ! |
| ! ! !!!__________22, 21, 20, 19 0..F ! |
| ! ! !!___________26, 25, 24, 23 0..F ! |
| ! ! !____________ 29, 28, 27 0..F ! |
| !--------------!------------------------------------------------------! |
| ! OIP ! Engine Oil Pressure ! |
| ! 999 ! (0 to 400 psia) ! |
| ! ! FWC 26.1.317.01 Engine 1 ! |
| ! ! 26.2.317.01 ! |
| ! ! 26.1.317.10 Engine 2 ! |
| ! ! 26.2.317.10 ! |
| !--------------!------------------------------------------------------! |
| ! OIT ! Engine Oil Temperature ! |
| ! X99 ! (-60 to 250 C) ! |
| ! ! Negative values are indicated by 'N' on the ! |
| ! ! first position. Otherwise the firt position is ! |
| ! ! used for the value. ! |
| ! ! FWC 26.1.316.01 Engine 1 ! |
| ! ! 26.2.316.01 ! |
| ! ! 26.1.316.10 Engine 2 ! |
| ! ! 26.2.316.10 ! |
| !--------------!------------------------------------------------------! |
| ! ECW1 ! Engine Control Word 1 ! |
| ! XXXXX ! XXXXX Bits HEX ! |
| ! ! !!!!!________14, 13, 12, 11 0..F ! |
| ! ! !!!!_________18, 17, 16, 15 0..F ! |
| ! ! !!!__________22, 21, 20, 19 0..F ! |
| ! ! !!___________26, 25, 24, 23 0..F ! |
| ! ! !____________ 29, 28, 27 0..F ! |
| ! ! Bit Label Parameter Description ! |
| ! ! 11 7C.X.272.XX.19 = 1 Auto Thrust Active ! |
| ! ! 12 7C.X.275.XX.20 = 1 VSV Position Fault ! |
| ! ! 13 SPARE ! |
| ! ! 14 SPARE ! |
| ! ! 15 7C.X.351.XX.29 = 1 Fuel Flow Measurement ! |
| ! ! Invalid ! |
| ! ! 16 7C.X.275.XX.15 = 1 N1/N2 Control Active ! |
| ! ! 17 7C.X.275.XX.26 = 1 Channel A Active ! |
| ! ! 18 7C.X.275.XX.27 = 1 Channel B Active ! |
| ! ! 19 SPARE ! |
| ! ! 20 SPARE ! |
| ! ! 21 SPARE ! |
| ! ! 22 SPARE ! |
| ! ! 23 SPARE ! |
| ! ! 24 SPARE ! |
| ! ! 25 SPARE ! |
| ! ! 26 SPARE ! |
| ! ! 27 SPARE ! |
| ! ! 28 SPARE ! |
| ! ! 29 SPARE ! |
| ! ! The 'X' for the System and SDI definition of the ! |
| ! ! engine parameters shall be as follows: ! |
| ! ! System SDI ! |
| ! ! Engine 1 1 01 ! |
| ! ! Engine 2 2 10 ! |
| !--------------!------------------------------------------------------! |
| ! SSEL ! Engine Control Word 1 ! |
| ! XXXXXXX ! Status of different FADEC sensors ! |
| ! XXXXXXX ! XXXXXXXXXXXXXX Label: Selected: ! |
| ! ! !!!!!!!!!!!!!!_ 346 N1 actual (Bit 11 -> 15)! |
| ! ! !!!!!!!!!!!!!__ 345 EGT (Bit 11 -> 15)! |
| ! ! !!!!!!!!!!!!___ 344 N2 actual (Bit 11 -> 15)! |
| ! ! !!!!!!!!!!!____ 263 T25 (Bit 11 -> 15)! |
| ! ! !!!!!!!!!!_____ 264 PS3 (Bit 11 -> 15)! |
| ! ! !!!!!!!!!______ 265 T3 (Bit 11 -> 15)! |
| ! ! !!!!!!!!_______ 072 VSV Position (Bit 11 -> 15)! |
| ! ! !!!!!!!________ 071 VBV Position (Bit 11 -> 15)! |
| ! ! !!!!!!_________ 306 HPTC Position (Bit 11 -> 15)! |
| ! ! !!!!!__________ 307 LPTH Position (Bit 11 -> 15)! |
| ! ! !!!!___________ 347 FMV Position (Bit 11 -> 15)! |
| ! ! !!!____________ 211 TAT (Bit 11 -> 15)! |
| ! ! !!_____________ 114 P0 (Bit 11 -> 15)! |
| ! ! !______________ 133 TLA Position (Bit 11 -> 15)! |
| ! ! Source: ECU, different labels ! |
| ! ! The indicated values shall be coded as follows: ! |
| ! ! Bit: 15 14 13 12 11 ! indicated value ! |
| ! ! --------------------!---------------- ! |
| ! ! 0 0 0 0 0 ! 0 ! |
| ! ! 0 0 0 0 1 ! 1 ! |
| ! ! 0 0 0 1 0 ! 2 ! |
| ! ! 0 0 0 1 1 ! 3 ! |
| ! ! 0 0 1 0 0 ! 4 ! |
| ! ! 0 0 1 0 1 ! 5 ! |
| ! ! 0 0 1 1 0 ! 6 ! |
| ! ! 0 0 1 1 1 ! 7 ! |
| ! ! 0 1 0 0 0 ! 8 ! |
| ! ! 0 1 0 0 1 ! 9 ! |
| ! ! 0 1 0 1 0 ! A ! |
| ! ! 0 1 0 1 1 ! B ! |
| ! ! 0 1 1 0 0 ! C ! |
| ! ! 0 1 1 0 1 ! D ! |
| ! ! 0 1 1 1 0 ! E ! |
| ! ! 0 1 1 1 1 ! F ! |
| ! ! 1 0 0 0 0 ! G ! |
| ! ! 1 0 0 0 1 ! H ! |
| ! ! 1 0 0 1 0 ! I ! |
| ! ! 1 0 0 1 1 ! J ! |
| ! ! 1 0 1 0 0 ! K ! |
| ! ! 1 0 1 0 1 ! L ! |
| ! ! 1 0 1 1 0 ! M ! |
| ! ! 1 0 1 1 1 ! N ! |
| ! ! 1 1 0 0 0 ! O ! |
| ! ! 1 1 0 0 1 ! P ! |
| ! ! 1 1 0 1 0 ! Q ! |
| ! ! 1 1 0 1 1 ! R ! |
| ! ! 1 1 1 0 0 ! S ! |
| ! ! 1 1 1 0 1 ! T ! |
| ! ! 1 1 1 1 0 ! U ! |
| ! ! 1 1 1 1 1 ! V ! |
| !--------------!------------------------------------------------------! |
| ! EGTK ! Corrected Exhaust Gas Temperature ! |
| ! X999 ! (-55 to 999.9 deg C) ! |
| ! ! EGT ! |
| ! ! EGTK=-------------- ! |
| ! ! pow(THETA2,n2) ! |
| ! ! THETA2 = (TAT+273.15)/288.18 ! |
| ! ! n2 = programmable value, standard value 1.05 ! |
| ! ! TAT = 06.1.211.01 ! |
| ! ! 06.2.211.10 ! |
| ! ! EGT = 7C.1.345.01 Engine 1 ! |
| ! ! 7C.2.345.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! N1K ! Corrected N1 ! |
| ! 9999 ! (0 to 120 %rpm) ! |
| ! ! N1 ! |
| ! ! N1K=-------------- ! |
| ! ! pow(THETA2,n1) ! |
| ! ! THETA2 = (TAT+273.15)/288.18 ! |
| ! ! n1 = programmable value, standard value 0.5 ! |
| ! ! TAT = 06.1.211.01 ! |
| ! ! 06.2.211.10 ! |
| ! ! N1 = 7C.1.346.10 Engine 1 ! |
| ! ! 7C.2.346.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! N2K ! Corrected N2 ! |
| ! 9999 ! (0 to 120 %rpm) ! |
| ! ! N2 ! |
| ! ! N2K=-------------- ! |
| ! ! pow(THETA2,n3) ! |
| ! ! THETA2 = (TAT+273.15)/288.18 ! |
| ! ! n3 = programmable value, standard value 0.5 ! |
| ! ! TAT = 06.1.211.01 ! |
| ! ! 06.2.211.10 ! |
| ! ! N2 = 7C.1.344.01 Engine 1 ! |
| ! ! 7C.2.344.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! FFK ! Corrected Engine Fuel Low ! |
| ! 9999 ! (0 to 7000Kg/h ( 0 to 15000 p/h)) ! |
| ! ! FF ! |
| ! ! FFK=--------------------- ! |
| ! ! pow(THETA2,n4)*delta2 ! |
| ! ! THETA2 = (TAT+273.15)/288.18 ! |
| ! ! n4 = programmable value, standard value 0.63 ! |
| ! ! delta2 = PT2/14.696 ! |
| ! ! TAT = 06.1.211.01 ! |
| ! ! 06.2.211.10 ! |
| ! ! FF = 7C.1.244.01 Engine 1 ! |
| ! ! 7C.2.244.10 Engine 2 ! |
| ! ! PT2 = 7C.1.131.01 Engine 1 ! |
| ! ! 7C.2.131.10 Engine 2 ! |
| +---------------------------------------------------------------------+ |
(6) Engine Run Up Report Data Field Description <11> (Engine Type CFMI with Advanced EVMU)
NOTE: Reports that are transmitted from the ACARS system do not have report lines without a line identifier.
NOTE: Only the parts of the ENGINE RUN UP REPORT <11> which are not included in the ENGINE CRUISE REPORT <01> are given in the subsequent table.
| +---------------------------------------------------------------------+ |
| ! Value ! Content Description ! |
| !--------------!------------------------------------------------------! |
| ! EGTK ! Corrected Exhaust Gas Temperature ! |
| ! X999 ! (-55 to 999.9 deg. C) ! |
| ! ! TAT = 06.1.211.01 ! |
| ! ! 06.2.211.10# ! |
| ! ! EGT = 7C.1.345.01 Engine 1 ! |
| ! ! 7C.2.345.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! N1K ! Corrected N1 ! |
| ! 9999 ! DMU (0 to 120%rpm) ! |
| ! ! TAT = 06.1.211.01 ! |
| ! ! 06.2.211.10# ! |
| ! ! N1 = 7C.1.346.10 Engine 1 ! |
| ! ! 7C.2.346.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! N2K ! Corrected N2 ! |
| ! 9999 ! DMU (0 to 120%rpm) ! |
| ! ! TAT = 06.1.211.01 ! |
| ! ! 06.2.211.10# ! |
| ! ! N2 = 7C.1.344.01 Engine 1 ! |
| ! ! 7C.2.344.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! FFK ! Corrected Engine Fuel Flow ! |
| ! 9999 ! DMU (0 to 70000 kg/h or 0 to 15000 p/h) ! |
| ! ! TAT = 06.1.211.01 ! |
| ! ! 06.2.211.10# ! |
| ! ! FF = 7C.1.244.01 Engine 1 ! |
| ! ! 7C.2.244.10 Engine 2 ! |
| ! ! PT2 = 7C.1.131.01 Engine 1 ! |
| ! ! 7C.2.131.10 Engine 2 ! |
| +---------------------------------------------------------------------+ |
(7) Engine Run Up Report Data Field Description <11> (Engine Type CFMI with Advanced EVMU)
NOTE: Reports that are transmitted from the ACARS system do not have report lines without a line identifier.
NOTE: Only the parts of the ENGINE RUN UP REPORT <11> which are not included in the ENGINE CRUISE REPORT <01> are given in the subsequent table.
| +---------------------------------------------------------------------+ |
| ! Value ! Content Description ! |
| !--------------!------------------------------------------------------! |
| ! EGTK ! Corrected Exhaust Gas Temperature ! |
| ! X999 ! (-55 to 999.9 °C) ! |
| ! ! EGT ! |
| ! ! EGTK=---------------- ! |
| ! ! pow(THETA2,n2) ! |
| ! ! THETA2 = (TAT+273.15)/288.15 ! |
| ! ! n2 = programmable value, standard value 1.05 ! |
| ! ! TAT = 06.1.211.01 ! |
| ! ! 06.2.211.10# ! |
| ! ! EGT = 7C.1.345.01 Engine 1 ! |
| ! ! 7C.2.345.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! N1K ! Corrected N1 ! |
| ! 9999 ! (0 to 120%rpm) ! |
| ! ! N1 ! |
| ! ! N1K=----------------- ! |
| ! ! pow(THETA2,n1) ! |
| ! ! THETA2 = (TAT+273.15)/288.15 ! |
| ! ! n1 = programmable value, standard value 0.5 ! |
| ! ! TAT = 06.1.211.01 ! |
| ! ! 06.2.211.10# ! |
| ! ! N1 = 7C.1.346.01 Engine 1 ! |
| ! ! 7C.2.346.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! N2K ! Corrected N2 ! |
| ! 9999 ! (0 to 120%rpm) ! |
| ! ! N2 ! |
| ! ! N2K=---------------- ! |
| ! ! pow(THETA2,n3) ! |
| ! ! THETA2 = (TAT+273.15)/288.15 ! |
| ! ! n3 = programmable value, standard value 0.5 ! |
| ! ! TAT = 06.1.211.01 ! |
| ! ! 06.2.211.10# ! |
| ! ! N2 = 7C.1.344.01 Engine 1 ! |
| ! ! 7C.1.344.10 Engine 2 ! |
| !--------------!------------------------------------------------------! |
| ! FFK ! Corrected Engine Fuel Flow ! |
| ! 9999 ! (0 to 7000 kg/h or 0 to 15000 p/h) ! |
| ! ! FF ! |
| ! ! FFK=----------------------- ! |
| ! ! pow(THETA2,n4)*delta2 ! |
| ! ! THETA2 = (TAT+273.15)/288.15 ! |
| ! ! n4 = programmable value, standard value 0.63 ! |
| ! ! delta2 = PT2/14.696 ! |
| ! ! TAT = 06.1.211.01 ! |
| ! ! 06.2.211.10# ! |
| ! ! FF = 7C.1.345.01 Engine 1 ! |
| ! ! 7C.1.345.10 Engine 2 ! |
| ! ! PT2 = 7C.1.131.01 Engine 1 ! |
| ! ! 7C.1.131.10 Engine 2 ! |
| +---------------------------------------------------------------------+ |
(8) Parameter Logic
| +---------------------------------------------------------------------+ |
| ! Param. ! Print Value (Standard Progr.) ! |
| !--------------!------------------------------------------------------! |
| ! ESN ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! EHRS ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! ERT ! Value at moment of trigger ! |
| !--------------! -----------------------------------------------------! |
| ! ECYC ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! AP ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! N1 ! Arithmetic average for 20 sec. ! |
| !--------------!------------------------------------------------------! |
| ! N1C ! Arithmetic average for 20 sec. ! |
| !--------------!------------------------------------------------------! |
| ! N2 ! Arithmetic average for 20 sec. ! |
| !--------------!------------------------------------------------------! |
| ! EGT ! Arithmetic average for 20 sec. ! |
| !--------------!------------------------------------------------------! |
| ! FF ! Arithmetic average for 20 sec. ! |
| !--------------!------------------------------------------------------! |
| ! PS13 ! Arithmetic average for 20 sec. ! |
| !--------------!------------------------------------------------------! |
| ! P25 ! Arithmetic average for 20 sec. ! |
| !--------------!------------------------------------------------------! |
| ! P3 ! Arithmetic average for 20 sec. ! |
| !--------------!------------------------------------------------------! |
| ! T3 ! Arithmetic average for 20 sec. ! |
| !--------------!------------------------------------------------------! |
| ! T5 ! Arithmetic average for 20 sec. ! |
| !--------------!------------------------------------------------------! |
| ! VSV ! Arithmetic average for 20 sec. ! |
| !--------------!------------------------------------------------------! |
| ! VBV ! Arithmetic average for 20 sec. ! |
| !--------------!------------------------------------------------------! |
| ! HPT ! Arithmetic average for 20 sec. ! |
| !--------------!------------------------------------------------------! |
| ! LPT ! Arithmetic average for 20 sec. ! |
| !--------------!------------------------------------------------------! |
| ! GLE ! Arithmetic average for 20 sec. ! |
| !--------------!------------------------------------------------------! |
| ! PD ! Arithmetic average for 20 sec. ! |
| !--------------!------------------------------------------------------! |
| ! TN ! Arithmetic average for 20 sec. ! |
| !--------------!------------------------------------------------------! |
| ! PT2 ! Arithmetic average for 20 sec. ! |
| !--------------!------------------------------------------------------! |
| ! VN ! Arithmetic average for 20 sec. ! |
| !--------------!------------------------------------------------------! |
| ! VL ! Arithmetic average for 20 sec. ! |
| !--------------!------------------------------------------------------! |
| ! PHA ! Arithmetic average for 20 sec. ! |
| !--------------!------------------------------------------------------! |
| ! PHT ! Arithmetic average for 20 sec. ! |
| !--------------!------------------------------------------------------! |
| ! VC ! Arithmetic average for 20 sec. ! |
| !--------------!------------------------------------------------------! |
| ! VH ! Arithmetic average for 20 sec. ! |
| !--------------!------------------------------------------------------! |
| ! EVM ! Value at the moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! OIP ! Arithmetic average for 20 sec. ! |
| !--------------!------------------------------------------------------! |
| ! OIT ! Arithmetic average for 20 sec. ! |
| !--------------!------------------------------------------------------! |
| ! ECW1 ! Value at the moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! SSEL ! Value at the moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! EGTK ! Arithmetic average for 20 sec. ! |
| !--------------!------------------------------------------------------! |
| ! N1K ! Arithmetic average for 20 sec. ! |
| !--------------!------------------------------------------------------! |
| ! N2K ! Arithmetic average for 20 sec. ! |
| !--------------!------------------------------------------------------! |
| ! FFK ! Arithmetic average for 20 sec. ! |
| +---------------------------------------------------------------------+ |
(9) Parameter Logic
| +---------------------------------------------------------------------+ |
| ! Param. ! Print Value (Standard Progr.) ! |
| !--------------!------------------------------------------------------! |
| ! ESN ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! EHRS ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! ERT ! Value at moment of trigger ! |
| !--------------! -----------------------------------------------------! |
| ! ECYC ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! AP ! Value at moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! N1 ! Arithmetic average for 20 sec. ! |
| !--------------!------------------------------------------------------! |
| ! N1C ! Arithmetic average for 20 sec. ! |
| !--------------!------------------------------------------------------! |
| ! N2 ! Arithmetic average for 20 sec. ! |
| !--------------!------------------------------------------------------! |
| ! EGT ! Arithmetic average for 20 sec. ! |
| !--------------!------------------------------------------------------! |
| ! FF ! Arithmetic average for 20 sec. ! |
| !--------------!------------------------------------------------------! |
| ! PS13 ! Arithmetic average for 20 sec. ! |
| !--------------!------------------------------------------------------! |
| ! P25 ! Arithmetic average for 20 sec. ! |
| !--------------!------------------------------------------------------! |
| ! P3 ! Arithmetic average for 20 sec. ! |
| !--------------!------------------------------------------------------! |
| ! T3 ! Arithmetic average for 20 sec. ! |
| !--------------!------------------------------------------------------! |
| ! T5 ! Arithmetic average for 20 sec. ! |
| !--------------!------------------------------------------------------! |
| ! VSV ! Arithmetic average for 20 sec. ! |
| !--------------!------------------------------------------------------! |
| ! VBV ! Arithmetic average for 20 sec. ! |
| !--------------!------------------------------------------------------! |
| ! HPT ! Arithmetic average for 20 sec. ! |
| !--------------!------------------------------------------------------! |
| ! LPT ! Arithmetic average for 20 sec. ! |
| !--------------!------------------------------------------------------! |
| ! GLE ! Arithmetic average for 20 sec. ! |
| !--------------!------------------------------------------------------! |
| ! PD ! Arithmetic average for 20 sec. ! |
| !--------------!------------------------------------------------------! |
| ! TN ! Arithmetic average for 20 sec. ! |
| !--------------!------------------------------------------------------! |
| ! PT2 ! Arithmetic average for 20 sec. ! |
| !--------------!------------------------------------------------------! |
| ! VN ! Arithmetic average for 20 sec. ! |
| !--------------!------------------------------------------------------! |
| ! VL ! Arithmetic average for 20 sec. ! |
| !--------------!------------------------------------------------------! |
| ! PHA ! Arithmetic average for 20 sec. ! |
| !--------------!------------------------------------------------------! |
| ! PHT ! Arithmetic average for 20 sec. ! |
| !--------------!------------------------------------------------------! |
| ! VC ! Arithmetic average for 20 sec. ! |
| !--------------!------------------------------------------------------! |
| ! VH ! Arithmetic average for 20 sec. ! |
| !--------------!------------------------------------------------------! |
| ! EVM ! Value at the moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! OIP ! Arithmetic average for 20 sec. ! |
| !--------------!------------------------------------------------------! |
| ! OIT ! Arithmetic average for 20 sec. ! |
| !--------------!------------------------------------------------------! |
| ! ECW1 ! Value at the moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! SSEL ! Value at the moment of trigger ! |
| !--------------!------------------------------------------------------! |
| ! EGTK ! Arithmetic average for 20 sec. ! |
| !--------------!------------------------------------------------------! |
| ! N1K ! Arithmetic average for 20 sec. ! |
| !--------------!------------------------------------------------------! |
| ! N2K ! Arithmetic average for 20 sec. ! |
| !--------------!------------------------------------------------------! |
| ! FFK ! Arithmetic average for 20 sec. ! |
| +---------------------------------------------------------------------+ |
(10) Engine Run Up Report Logic <11> (Engine Type CFMI with Advanced EVMU)
| +----------------------------------------------------------------------+ |
| !Code!Item ! !Progr.!Standard ! |
| ! No.!No. ! Description of Function Item !MCDU !Value or ! |
| ! ! ! !GSE !Table ! |
| !----!------!-----------------------------------------!------!---------! |
| ! !A ! Report Format ! ! ! |
| ! !B ! Parameter Table ! ! ! |
| ! !C ! First three lines of Report ! C ! Blank ! |
| ! !D ! Print-out Rules ! C ! 2 ! |
| ! !E ! Transfer to ACARS MU ! C ! No ! |
| ! !F ! Increment of the report counter if the ! C ! 1 ! |
| ! ! ! report was triggered by a code number ! ! ! |
| ! ! ! > 1000; 1=yes, 0=no ! ! ! |
| ! !G1 ! n1 value (N1) ! A ! 0.5 ! |
| ! !G2 ! n2 value (EGT) ! A ! 1.05 ! |
| ! !G3 ! n3 value (N2) ! A ! 0.5 ! |
| ! !G4 ! n4 value (FF) ! A ! 0.63 ! |
| !----!------!-----------------------------------------!------!---------! |
| !1000!1 ! Manual selection via MCDU ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !2000!2 ! Flight phase dependent manual ! ! ! |
| ! ! ! selection via remote print button ! ! ! |
| ! ! ! if programmed. ! ! ! |
| ! !2.1 ! Remote Print Button assignment. ! C ! 2 and 3 ! |
| !----!------!-----------------------------------------!------!---------! |
| !3000!3 ! Programmable Start Logic ! ! ! |
| ! !3.1 ! Trigger condition ! C ! not ! |
| !----!------!-----------------------------------------!------!---------! |
| !8100!8.1 ! ACARS MU uplink request with IMI 'REQ11'! ! ! |
| ! ! ! The report <11> is immediately generated! ! ! |
| ! ! ! and transmitted to the ACARS MU. ! ! ! |
| !----------------------------------------------------------------------! |
| ! A = Programmable by Airbus ! |
| ! C = Programmable by Customer ! |
| +----------------------------------------------------------------------+ |
(11) Engine Run Up Report Logic <11> (Engine Type CFMI with Advanced EVMU)
| +----------------------------------------------------------------------+ |
| !Code!Item ! !Progr.!Standard ! |
| ! No.!No. ! Description of Function Item !MCDU !Value or ! |
| ! ! ! !/GSE !Table TXY! |
| !----!------!-----------------------------------------!------!---------! |
| ! !A ! Report Format ! ! ! |
| ! !B ! Parameter Table ! ! ! |
| ! !C ! First three lines of Report ! C ! Blank ! |
| ! !D ! Print-out Rules ! C ! See ! |
| ! ! ! ! ! separate! |
| ! ! ! ! ! list ! |
| ! !E ! Transfer to ACARS MU ! C ! see ! |
| ! ! ! ! ! separate! |
| ! ! ! ! ! list ! |
| ! !F ! Increment of the report counter if the ! C ! 1 ! |
| ! ! ! report was triggered by a code number ! ! ! |
| ! ! ! > 1000; 1=yes, 0=no ! ! ! |
| ! ! ! Exponents for correction of N1, N2 EGT ! ! ! |
| ! ! ! and FF. ! ! ! |
| ! !G1 ! n1 value (N1) ! A ! 0.5 ! |
| ! !G2 ! n2 value (EGT) ! A ! 1.05 ! |
| ! !G3 ! n3 value (N2) ! A ! 0.5 ! |
| ! !G4 ! n4 value (FF) ! A ! 0.63 ! |
| !----!------!-----------------------------------------!------!---------! |
| !1000!1 ! Manual selection via MCDU ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !2000!2 ! Flight phase dependent manual ! ! ! |
| ! ! ! selection via remote print button ! ! ! |
| ! ! ! if programmed. ! ! ! |
| ! !2.1 ! Remote Print Button assignment. ! C ! 2 and 3 ! |
| !----!------!-----------------------------------------!------!---------! |
| !3000!3 ! Programmable Start Logic ! ! ! |
| ! !3.1 ! Trigger condition ! C ! not ! |
| ! ! ! ! ! progr. ! |
| !----!------!-----------------------------------------!------!---------! |
| !8100!8.1 ! ACARS MU uplink request with IMI 'REQ1' ! ! ! |
| ! ! ! The report <11> is immediately generated! ! ! |
| ! ! ! and transmitted to the ACARS MU. ! ! ! |
| !----------------------------------------------------------------------! |
| ! A = Programmable by Airbus ! |
| ! C = Programmable by Customer ! |
| +----------------------------------------------------------------------+ |
(12) Engine Run Up Report Logic <11> (Engine Type CFMI with Advanced EVMU)
| +-----------------------------------------------------------------------+ |
| !Code!Item ! !Progr.!Standard ! |
| ! No.!No. ! Description of Function Item !------!Value or ! |
| ! ! ! !MCDU/ !Table TXY! |
| ! ! ! !GSE ! ! |
| !----!------!-----------------------------------------!------!---------! |
| ! !A ! Report Format ! ! ! |
| ! !A.1 ! "R011RLID" Report Layout Identifier ! ! 01 ! |
| ! ! ! (for ACARS header) ! ! ! |
| ! !A.2 ! "R011RLIS" Report Layout Issue ! ! 01 ! |
| ! ! ! (for ACARS header) ! ! ! |
| ! !B ! Parameter Table ! ! ! |
| ! !C ! First three lines of Report ! C ! Blank ! |
| ! !D ! Print-out Rules ! C ! See ! |
| ! ! ! ! ! separate! |
| ! ! ! ! ! list ! |
| ! !E ! Transfer to ACARS MU ! C ! see ! |
| ! ! ! ! ! separate! |
| ! ! ! ! ! list ! |
| ! !F ! Increment of the report counter if the ! C ! 1 ! |
| ! ! ! report was triggered by a code number ! ! ! |
| ! ! ! > 1000; 1=yes, 0=no ! ! ! |
| ! ! ! Exponents for correction of N1, N2 EGT ! ! ! |
| ! ! ! and FF. ! ! ! |
| ! !G1 ! n1 value (N1) ! A ! 0.5 ! |
| ! !G2 ! n2 value (EGT) ! A ! 1.05 ! |
| ! !G3 ! n3 value (N2) ! A ! 0.5 ! |
| ! !G4 ! n4 value (FF) ! A ! 0.63 ! |
| !----!------!-----------------------------------------!------!---------! |
| !1000!1 ! Manual selection through MCDU ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !2000!2 ! Flight phase dependent manual ! ! ! |
| ! ! ! selection through remote print button ! ! ! |
| ! ! ! if programmed. ! ! ! |
| ! !2.1 ! Remote Print Button assignment. ! C ! 2 and 3 ! |
| !----!------!-----------------------------------------!------!---------! |
| !3000!3 ! Programmable Start Logic ! ! ! |
| ! !3.1 ! Trigger condition ! C ! not ! |
| ! ! ! ! ! progr. ! |
| !----!------!-----------------------------------------!------!---------! |
| !8100!8.1 ! ACARS MU uplink request with IMI "REQ1" ! ! ! |
| ! ! ! The report <11> is immediately generated! ! ! |
| ! ! ! and transmitted to the ACARS MU. ! ! ! |
| !----------------------------------------------------------------------! |
| ! A = Programmable by Airbus ! |
| ! C = Programmable by Customer ! |
| +----------------------------------------------------------------------+ |
(13) Engine Run Up Report Logic <11> (Engine Type CFMI with Advanced EVMU)
| +----------------------------------------------------------------------+ |
| !Code!Item ! !Progr.!Standard ! |
| ! No.!No. ! Description of Function Item !MCDU !Value or ! |
| ! ! ! !/GSE !Table TXY! |
| !----!------!-----------------------------------------!------!---------! |
| ! !A ! Report Format ! ! ! |
| ! !B ! Parameter Table ! ! ! |
| ! !C ! First three lines of Report ! C ! Blank ! |
| ! !D ! Print-out Rules ! C ! See ! |
| ! ! ! ! ! separate! |
| ! ! ! ! ! list ! |
| ! !E ! Transfer to ACARS MU ! C ! see ! |
| ! ! ! ! ! separate! |
| ! ! ! ! ! list ! |
| ! !F ! Increment of the report counter if the ! C ! 1 ! |
| ! ! ! report was triggered by a code number ! ! ! |
| ! ! ! > 1000; 1=yes, 0=no ! ! ! |
| ! ! ! Exponents for correction of N1, N2 EGT ! ! ! |
| ! ! ! and FF. ! ! ! |
| ! !G1 ! n1 value (N1) ! A ! 0.5 ! |
| ! !G2 ! n2 value (EGT) ! A ! 1.05 ! |
| ! !G3 ! n3 value (N2) ! A ! 0.5 ! |
| ! !G4 ! n4 value (FF) ! A ! 0.63 ! |
| !----!------!-----------------------------------------!------!---------! |
| !1000!1 ! Manual selection via MCDU ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !2000!2 ! Flight phase dependent manual ! ! ! |
| ! ! ! selection via remote print button ! ! ! |
| ! ! ! if programmed. ! ! ! |
| ! !2.1 ! Remote Print Button assignment. ! C ! 2 and 3 ! |
| !----!------!-----------------------------------------!------!---------! |
| !3000!3 ! Programmable Start Logic ! ! ! |
| ! !3.1 ! Trigger condition ! C ! not ! |
| ! ! ! ! ! progr. ! |
| !----!------!-----------------------------------------!------!---------! |
| !8100!8.1 ! ACARS MU uplink request with IMI 'REQ1' ! ! ! |
| ! ! ! The report <11> is immediately generated! ! ! |
| ! ! ! and transmitted to the ACARS MU. ! ! ! |
| !----------------------------------------------------------------------! |
| ! A = Programmable by Airbus ! |
| ! C = Programmable by Customer ! |
| +----------------------------------------------------------------------+ |
(14) Engine Run Up Report Logic <11> (Engine Type CFMI with Advanced EVMU)
| +----------------------------------------------------------------------+ |
| !Code!Item ! !Progr.!Standard ! |
| ! No.!No. ! Description of Function Item !MCDU !Value or ! |
| ! ! ! !/GSE !Table TXY! |
| !----!------!-----------------------------------------!------!---------! |
| ! !A ! Report Format ! ! ! |
| ! !B ! Parameter Table ! ! ! |
| ! !C ! First three lines of Report ! C ! Blank ! |
| ! !D ! Print-out Rules ! C ! See ! |
| ! ! ! ! ! separate! |
| ! ! ! ! ! list ! |
| ! !E ! Transfer to ACARS MU ! C ! see ! |
| ! ! ! ! ! separate! |
| ! ! ! ! ! list ! |
| ! !F ! Increment of the report counter if the ! C ! 1 ! |
| ! ! ! report was triggered by a code number ! ! ! |
| ! ! ! > 1000; 1=yes, 0=no ! ! ! |
| ! ! ! Exponents for correction of N1, N2 EGT ! ! ! |
| ! ! ! and FF. ! ! ! |
| ! !G1 ! n1 value (N1) ! A ! 0.5 ! |
| ! !G2 ! n2 value (EGT) ! A ! 1.05 ! |
| ! !G3 ! n3 value (N2) ! A ! 0.5 ! |
| ! !G4 ! n4 value (FF) ! A ! 0.63 ! |
| !----!------!-----------------------------------------!------!---------! |
| !1000!1 ! Manual selection via MCDU ! ! ! |
| !----!------!-----------------------------------------!------!---------! |
| !2000!2 ! Flight phase dependent manual ! ! ! |
| ! ! ! selection via remote print button ! ! ! |
| ! ! ! if programmed. ! ! ! |
| ! !2.1 ! Remote Print Button assignment. ! C ! 2 and 3 ! |
| !----!------!-----------------------------------------!------!---------! |
| !3000!3 ! Programmable Start Logic ! ! ! |
| ! !3.1 ! Trigger condition ! C ! not ! |
| ! ! ! ! ! progr. ! |
| !----!------!-----------------------------------------!------!---------! |
| !8100!8.1 ! ACARS MU uplink request with IMI 'REQ11'! ! ! |
| ! ! ! The report <11> is immediately generated! ! ! |
| ! ! ! and transmitted to the ACARS MU. ! ! ! |
| !----------------------------------------------------------------------! |
| ! A = Programmable by Airbus ! |
| ! C = Programmable by Customer ! |
| +----------------------------------------------------------------------+ |
R. AIDS Reports Print Rules - Default Values for Report <11>
| +------------------------------------------------+ |
| ! ! ! ! |
| ! Code ! Printer Output ! ACARS-output ! |
| ! ! ! ! |
| !-------!-----------------------!----------------! |
| ! ! ! ! |
| ! 1000 ! Print immediatly ! No ACARS ! |
| ! ! ! ! |
| !-------!-----------------------!----------------! |
| ! ! ! ! |
| ! 2000 ! Print immediatly ! No ACARS ! |
| ! ! ! ! |
| !-------!-----------------------!----------------! |
| ! ! ! ! |
| ! 8100 ! No print ! ACARS VHF ! |
| ! ! ! ! |
| +------------------------------------------------+ |
| +-------------------------------------------------------------------------+ |
| !Trigger! to ACARS ! to printer ! store ! |
| ! Code !------------------------------ -!-----------------!--------------! |
| ! No !Ground ! VHF ! SAT- ! HF ! at ! imme- ! internal& ! |
| ! ! ! ! COM ! !landing ! diate ! external ! |
| ! ! ! ! ! ! ! !(build in RAM&! |
| ! ! ! ! ! ! ! ! PCMCIA) ! |
| !-------!-------!--------!-------!-------!--------!--------!--------------! |
| ! ! ! If ! ! ! ! If !PCMCIA only if! |
| ! 1000 ! NO ! 'SEND' ! NO ! NO ! !'PRINT' ! 'STORE' ! |
| ! ! !selected! ! ! !selected! selected on ! |
| ! ! !on MCDU ! ! ! !on MCDU ! MCDU ! |
| !-------!-------!--------!-------!-------! !--------!--------------! |
| ! 2000 ! NO ! NO ! NO ! NO ! N ! YES ! YES ! |
| !-------!-------!--------!-------!-------! O !--------!--------------! |
| ! 3000 ! NO ! NO ! NO ! NO ! ! NO ! YES ! |
| !-------!-------!--------!------ !-------! !--------!--------------! |
| ! 8100 ! NO ! YES ! NO ! NO ! ! NO ! YES ! |
| +-------------------------------------------------------------------------+ |
| +-------------------------------------------------------------------------+ |
| !Trigger! to ACARS ! to printer ! store ! |
| ! Code !------------------------------ -!-----------------!--------------! |
| ! No !Ground ! VHF ! SAT- ! HF ! at ! imme- ! internal& ! |
| ! ! ! ! COM ! !landing ! diate ! external ! |
| ! ! ! ! ! ! ! !(build in RAM&! |
| ! ! ! ! ! ! ! ! PCMCIA) ! |
| !-------!-------!--------!-------!-------!--------!--------!--------------! |
| ! 1000 ! NO ! NO ! NO ! NO ! NO ! YES ! YES ! |
| !-------!-------!--------!-------!-------!--------!--------!--------------! |
| ! 2000 ! NO ! NO ! NO ! NO ! NO ! YES ! YES ! |
| !-------!-------!--------!-------!-------!--------!--------!--------------! |
| ! 3000 ! NO ! NO ! NO ! NO ! NO ! NO ! YES ! |
| !-------!-------!--------!------ !-------!--------!--------!--------------! |
| ! 8100 ! NO ! YES ! NO ! NO ! NO ! NO ! YES ! |
| +-------------------------------------------------------------------------+ |
S. Report Limits for Engine Cruise Report <01>
(1) A320: CFMI Engines 56-5-A1, 56-5-A3, 56-5-B4
| +-----------------------------------------------------------------------------+ |
| !Report! Limit ! Description of Report Item !56-5-A1!56-5-A3!56-5-B4! Unit ! |
| !Item ! No. ! ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.1 ! 4 ! Y01.1: flight hours counter ! 0 ! 0 ! 0 ! hours! |
| ! ! ! (0=inhibit logic) ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.2 ! 5 ! Y01.2: time delay after ! 10 ! 10 ! 10 ! min ! |
| ! ! ! entry in cruise ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.3 ! 6 ! Y01.3: flight leg counter ! 1 ! 1 ! 1 ! legs ! |
| ! ! ! (0=inhibit logic) ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.1 ! 3 ! P01: stable periods ! 5 ! 5 ! 5 ! ! |
| ! ! ! (1 period = 20 sec) ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.2.1! 8 ! HPTL1 valve position lower ! 0 ! 0 ! 70 ! % ! |
| ! ! ! limit ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.2.2! 9 ! HPTL2 valve position upper ! 20 ! 20 ! 100 ! % ! |
| ! ! ! limit ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.3 ! 10 ! IALT stable frame variation ! 150 ! 150 ! 150 ! feet ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.3.1! 24 ! Weighting Factor Wa of IALT ! 1 ! 1 ! 1 ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.4 ! 11 ! GS stable frame variation ! 6 ! 6 ! 6 ! kts ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.4.1! 25 ! Weighting Factor Wa of GS ! 1 ! 1 ! 1 ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.5 ! 12 ! ROLL stable frame variation ! 4 ! 4 ! 4 ! deg ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.5.1! 26 ! Weighting Factor Wa of ROLL ! 1 ! 1 ! 1 ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.6 ! 13 ! TAT stable frame variation ! 2 ! 2 ! 2 ! deg C! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.6.1! 27 ! Weighting Factor Wa of TAT ! 1 ! 1 ! 1 ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.7 ! 14 ! N2 stable frame variation ! .9 ! .9 ! .9 ! % ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.7.1! 28 ! Weighting Factor Wa of N2 ! 1 ! 1 ! 1 ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.8 ! 15 ! EGT stable frame variation ! 18 ! 18 ! 18 ! deg C! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.8.1! 29 ! Weighting Factor Wa of EGT ! 1 ! 1 ! 1 ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.9 ! 16 ! VACC stable frame variation ! .1 ! .1 ! .1 ! g ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.9.1! 30 ! Weighting Factor Wa of VACC ! 1 ! 1 ! 1 ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.10 ! 17 ! MACH stable frame variation ! .01 ! .01 ! .01 ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| !5.10.1! 31 ! Weighting Factor Wa of MACH ! 1 ! 1 ! 1 ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.11 ! 18 ! N1 stable frame variation ! 1.6 ! 1.6 ! 1.6 ! % ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| !5.11.1! 32 ! Weighting Factor Wa of N1 ! 1 ! 1 ! 1 ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.12 ! 19 ! PT2 stable frame variation ! .1 ! .1 ! .1 ! psia ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| !5.12.1! 33 ! Weighting Factor Wa of PT2 ! 1 ! 1 ! 1 ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.13 ! 20 ! FF stable frame variation ! 100 ! 100 ! 100 ! kg/h ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| !5.13.1! 34 ! Weighting Factor Wa of FF ! 1 ! 1 ! 1 ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.14 ! 21 ! HPT stable frame variation ! 8 ! 8 ! 10 ! % ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| !5.14.1! 35 ! Weighting Factor Wa of HPT ! 1 ! 1 ! 1 ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.15 ! 22 ! LPT stable frame variation ! 10 ! 10 ! 10 ! % ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| !5.15.1! 36 ! Weighting Factor Wa of LPT ! 1 ! 1 ! 1 ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 6.1 ! 7 ! Number 'X01' for consecutive ! 5 ! 5 ! 5 ! ! |
| ! ! ! reports. ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 9.1 ! 38 ! 'NIT.1' stable N1 value for ! 62 ! 62 ! 62 ! %rpm ! |
| ! * ! ! descent ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 9.2 ! 39 ! 'X1.1' tolerance band for !+/-1.5 !+/-1.5 !+/-1.5 ! % ! |
| ! * ! ! descent ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 9.3 ! 40 ! 'T1.1' stable observing time ! 20 ! 20 ! 20 !second! |
| ! * ! ! for descent (max. 20 seconds) ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| !10.1 ! 41 ! 'NIT.1' stable N1 value for ! 93 ! 93 ! 93 ! %rpm ! |
| ! * ! ! take off ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| !10.2 ! ! 'X1.2' tolerance band for !+/-1.5 !+/-1.5 !+/-1.5 ! % ! |
| ! * ! ! take off ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| !10.3 ! ! 'T1.2' stable observing time ! 20 ! 20 ! 20 !second! |
| ! * ! ! for take off ! ! ! ! ! |
| ! ! ! (max. 20 seconds) ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! * Remark: Only for Advanced EVMU available ! |
| +-----------------------------------------------------------------------------+ |
(2) A321: CFMI Engines 56-5-B1, 56-5-B2, 56-5-B3
| +-----------------------------------------------------------------------------+ |
| !Report! Limit ! Description of Report Item !56-5-B1!56-5-B2!56-5-B3! Unit ! |
| !Item ! No. ! ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.1 ! 4 ! Y01.1: flight hours ! 0 ! 0 ! 0 ! hours! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.2 ! 5 ! Y01.2: minutes after cruise ! 10 ! 10 ! 10 ! min ! |
| ! ! ! entry ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.3 ! 6 ! Y01.3: flight legs ! 1 ! 1 ! 1 ! legs ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.1 ! 3 ! P01: stable periods ! 5 ! 5 ! 5 ! ! |
| ! ! ! (1 period = 20 seconds) ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.2.1! 8 ! HPTL1 valve position lower ! 70 ! 70 ! 70 ! % ! |
| ! ! ! limits ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.2.2! 9 ! HPTL2 valve position upper ! 100 ! 100 ! 100 ! % ! |
| ! ! ! limits ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.3 ! 10 ! IALT stable frame variation ! 150 ! 150 ! 150 ! feet ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.3.1! 24 ! Weighting Factor Wa of IALT ! 1 ! 1 ! 1 ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.4 ! 11 ! GS stable frame variation ! 6 ! 6 ! 6 ! kts ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.4.1! 25 ! Weighting Factor Wa of GS ! 1 ! 1 ! 1 ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.5 ! 12 ! ROLL stable frame variation ! 4 ! 4 ! 4 ! deg ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.5.1! 26 ! Weighting Factor Wa of ROLL ! 1 ! 1 ! 1 ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.6 ! 13 ! TAT stable frame variation ! 2 ! 2 ! 2 ! deg C! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.6.1! 27 ! Weighting Factor Wa of TAT ! 1 ! 1 ! 1 ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.7 ! 14 ! N2 stable frame variation ! .9 ! .9 ! .9 ! % ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.7.1! 28 ! Weighting Factor Wa of N2 ! 1 ! 1 ! 1 ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.8 ! 15 ! EGT stable frame variation ! 18 ! 18 ! 18 ! deg C! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.8.1! 29 ! Weighting Factor Wa of EGT ! 1 ! 1 ! 1 ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.9 ! 16 ! VACC stable frame variation ! .1 ! .1 ! .1 ! g ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.9.1! 30 ! Weighting Factor Wa of VACC ! 1 ! 1 ! 1 ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.10 ! 17 ! MACH stable frame variation ! .01 ! .01 ! .01 ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| !5.10.1! 31 ! Weighting Factor Wa of MACH ! 1 ! 1 ! 1 ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.11 ! 18 ! N1 stable frame variation ! 1.6 ! 1.6 ! 1.6 ! % ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| !5.11.1! 32 ! Weighting Factor Wa of N1 ! 1 ! 1 ! 1 ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.12 ! 19 ! PT2 stable frame variation ! .1 ! .1 ! .1 ! psia ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| !5.12.1! 33 ! Weighting Factor Wa of PT2 ! 1 ! 1 ! 1 ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.13 ! 20 ! FF stable frame variation ! 100 ! 100 ! 100 ! kg/h ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| !5.13.1! 34 ! Weighting Factor Wa of FF ! 1 ! 1 ! 1 ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.14 ! 21 ! HPT stable frame variation ! 10 ! 10 ! 10 ! % ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| !5.14.1! 35 ! Weighting Factor Wa of HPT ! 1 ! 1 ! 1 ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.16 ! 22 ! LPT stable frame variation ! 10 ! 10 ! 10 ! % ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| !5.16.1! 36 ! Weighting Factor Wa of LPT ! 1 ! 1 ! 1 ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 6.1 ! 7 ! Number 'X01' for consecutive ! 5 ! 5 ! 5 ! ! |
| ! ! ! reports ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 9.1 ! 38 ! 'NIT.1' stable N1 value for ! 62 ! 62 ! 62 ! %rpm ! |
| ! * ! ! descent ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 9.2 ! 39 ! 'X1.1' tolerance band for !+/-1.5 !+/-1.5 !+/-1.5 ! % ! |
| ! * ! ! descent ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 9.3 ! 40 ! 'T1.1' stable observing time ! 20 ! 20 ! 20 !second! |
| ! * ! ! for descent (max. 20 seconds) ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| !10.1 ! 41 ! 'NIT.1' stable N1 value for ! 93 ! 93 ! 93 ! %rpm ! |
| ! * ! ! take off ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| !10.2 ! ! 'X1.2' tolerance band for !+/-1.5 !+/-1.5 !+/-1.5 ! % ! |
| ! * ! ! take off ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| !10.3 ! ! 'T1.2' stable observing time ! 20 ! 20 ! 20 !second! |
| ! * ! ! for take off ! ! ! ! ! |
| ! ! ! (max. 20 seconds) ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! * Remark: Only for Advanced EVMU available ! |
| +-----------------------------------------------------------------------------+ |
(3) A319: CFMI Engines 56-5-A5, 56-5-B6, 56-5-B5, 56-5-A4
| +-----------------------------------------------------------------------------+ |
| !Report! Description of Report Item ! CFM ! CFM ! CFM ! CFM ! Unit ! |
| !Item ! !56-5-A5!56-5-B6!56-5-B5!56-5-A4! ! |
| ! ! !-------!-------!-------!-------!------! |
| ! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! ! |
| ! ! ! C7xxxx! C8xxxx! C4xxxx! C6xxxx! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.1 !'Y01.1' flight hours ! 0 ! 0 ! 0 ! 0 ! hour ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.2 !'Y01.2' minutes after cruise ! 10 ! 10 ! 10 ! 10 ! min ! |
| ! ! entry ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.3 !'Y01.3' flight legs ! 1 ! 1 ! 1 ! 1 ! min ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.1 ! P01: stable periods ! 5 ! 5 ! 5 ! 5 ! ! |
| ! ! (1 period = 20 seconds) ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.2.1! HPTL1 valve position lower ! 0 ! 70 ! 70 ! 0 ! % ! |
| ! ! limit ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.2.2! HPTL2 valve position upper ! 20 ! 105 ! 105 ! 20 ! % ! |
| ! ! limit ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.3 ! IALT stable frame variation ! 150 ! 150 ! 150 ! 150 ! ft ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.3.1! Weighting Factor Wa of IALT ! 1 ! 1 ! 1 ! 1 ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.4 ! GS stable frame variation ! 6 ! 6 ! 6 ! 6 ! kts ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.4.1! Weighting Factor Wa of GS ! 1 ! 1 ! 1 ! 1 ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.5 ! ROLL ANGLE stable frame ! 4.0 ! 4.0 ! 4.0 ! 4.0 ! deg ! |
| ! ! variation ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.5.1! Weighting Factor Wa of ROLL ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! ANGLE ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.6 ! TAT stable frame variation ! 2.0 ! 2.0 ! 2.0 ! 2.0 ! deg C! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.6.1! Weighting Factor Wa of TAT ! 1 ! 1 ! 1 ! 1 ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.7 ! N2 stable frame variation ! 0.9 ! 0.9 ! 0.9 ! 0.9 ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.7.1! Weighting Factor Wa of N2 ! 1 ! 1 ! 1 ! 1 ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.8 ! EGT stable frame variation ! 18.0 ! 18.0 ! 18.0 ! 18.0 ! deg C! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.8.1! Weighting Factor Wa of EGT ! 1 ! 1 ! 1 ! 1 ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.9 ! VACC stable frame variation ! 0.10 ! 0.10 ! 0.10 ! 0.10 ! g ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.9.1! Weighting Factor Wa of VACC ! 1 ! 1 ! 1 ! 1 ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.10 ! MN stable frame variation ! 0.010 ! 0.010 ! 0.010 ! 0.010 !Mach ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !5.10.1! Weighting Factor Wa of MACH ! 1 ! 1 ! 1 ! 1 ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.11 ! N1 stable frame variation ! 1.6 ! 1.6 ! 1.6 ! 1.6 ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !5.11.1! Weighting Factor Wa of N1 ! 1 ! 1 ! 1 ! 1 ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.12 ! PT2 stable frame variation ! 0.10 ! 0.10 ! 0.10 ! 0.10 ! psia ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !5.12.1! Weighting Factor Wa of PT2 ! 1 ! 1 ! 1 ! 1 ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.13 ! FF stable frame variation ! 100 ! 100 ! 100 ! 100 ! kg/h ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !5.13.1! Weighting Factor Wa of FF ! 1 ! 1 ! 1 ! 1 ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.14 ! HPT stable frame variation ! 10 ! 10 ! 10 ! 10 ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !5.14.1! Weighting Factor Wa of HPT ! 1 ! 1 ! 1 ! 1 ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.15 ! LPT stable frame variation ! 10.0 ! 10.0 ! 10.0 ! 10.0 ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !5.15.1! Weighting Factor Wa of LPT ! 1 ! 1 ! 1 ! 1 ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 6.2 ! Number 'X01' for consecutive ! 5 ! 5 ! 5 ! 5 ! ! |
| ! ! reports ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 9.1 ! 'N1T.1' stable N1 value for ! 62 ! 62 ! 62 ! 62 ! %rpm ! |
| ! * ! descent ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 9.2 ! 'X1.1' tolerance band for !+/-1.5 !+/-1.5 !+/-1.5 !+/-1.5 ! % ! |
| ! * ! descent ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 9.3 ! 'T1.1' stable observing time ! 20 ! 20 ! 20 ! 20 !second! |
| ! * ! for descent (max. 20 seconds) ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 10.1 ! 'N1T.1' stable N1 value for ! 93 ! 93 ! 93 ! 93 ! %rpm ! |
| ! * ! take off ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 10.2 ! 'X1.2' tolerance band for !+/-1.5 !+/-1.5 !+/-1.5 !+/-1.5 ! % ! |
| ! * ! take off ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 10.3 ! 'T1.2' stable observing time ! 20 ! 20 ! 20 ! 20 !second! |
| ! * ! for take off (max. 20 seconds)! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! * Remark: Only for Advanced EVMU available ! |
| +-----------------------------------------------------------------------------+ |
(4) A319: CFMI Engine 56-5-B7
| +-----------------------------------------------------------------------------+ |
| !Report! Description of Report Item ! CFM ! SPARE ! SPARE ! SPARE ! Unit ! |
| !Item ! !56-5-B7! ! ! ! ! |
| ! ! !-------!-------!-------!-------!------! |
| ! ! !DMU/ID ! ! ! ! ! |
| ! ! ! C5xxxx! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.1 !'Y01.1' flight hours ! 0 ! ! ! ! hour ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.2 !'Y01.2' minutes after cruise ! 10 ! ! ! ! min ! |
| ! ! entry ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.3 !'Y01.1' flight legs ! 1 ! ! ! ! hour ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.1 !'P01': stable periods ! 5 ! ! ! ! ! |
| ! ! (1 period = 20 seconds) ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.2.1! HPTL1 valve position lower ! 70 ! ! ! ! % ! |
| ! ! limit ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.2.2! HPTL2 valve position upper ! 105 ! ! ! ! % ! |
| ! ! limit ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.3 ! IALT stable frame variation ! 150 ! ! ! ! ft ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.3.1! Weighting Factor Wa of IALT ! 1 ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.4 ! GS stable frame variation ! 6 ! ! ! ! kts ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.4.1! Weighting Factor Wa of GS ! 1 ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.5 ! ROLL ANGLE stable frame ! 4.0 ! ! ! ! deg ! |
| ! ! variation ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.5.1! Weighting Factor Wa of ROLL ! 1 ! ! ! ! ! |
| ! ! ANGLE ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.6 ! TAT stable frame variation ! 2.0 ! ! ! ! deg C! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.6.1! Weighting Factor Wa of TAT ! 1 ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.7 ! N2 stable frame variation ! 0.9 ! ! ! ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.7.1! Weighting Factor Wa of N2 ! 1 ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.8 ! EGT stable frame variation ! 18.0 ! ! ! ! deg C! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.8.1! Weighting Factor Wa of EGT ! 1 ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.9 ! VACC stable frame variation ! 0.10 ! ! ! ! g ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.9.1! Weighting Factor Wa of VACC ! 1 ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.10 ! MN stable frame variation ! 0.010 ! ! ! !Mach ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !5.10.1! Weighting Factor Wa of MACH ! 1 ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.11 ! N1 stable frame variation ! 1.6 ! ! ! ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !5.11.1! Weighting Factor Wa of N1 ! 1 ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.12 ! PT2 stable frame variation ! 0.10 ! ! ! ! psia ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !5.12.1! Weighting Factor Wa of PT2 ! 1 ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.13 ! FF stable frame variation ! 100 ! ! ! ! kg/h ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !5.13.1! Weighting Factor Wa of FF ! 1 ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.14 ! HPT stable frame variation ! 10 ! ! ! ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !5.14.1! Weighting Factor Wa of HPT ! 1 ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.15 ! LPT stable frame variation ! 10.0 ! ! ! ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !5.15.1! Weighting Factor Wa of LPT ! 1 ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 6.2 ! Number 'X01' for consecutive ! 5 ! ! ! ! ! |
| ! ! reports ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 9.1 ! 'N1T.1' stable N1 value for ! 62 ! ! ! ! %rpm ! |
| ! * ! descent ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 9.2 ! 'X1.1' tolerance band for !+/-1.5 ! ! ! ! % ! |
| ! * ! descent ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 9.3 ! 'T1.1' stable observing time ! 20 ! ! ! !second! |
| ! * ! for descent (max. 20 seconds) ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 10.1 ! 'N1T.1' stable N1 value for ! 93 ! ! ! ! %rpm ! |
| ! * ! take off ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 10.2 ! 'X1.2' tolerance band for !+/-1.5 ! ! ! ! % ! |
| ! * ! take off ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 10.3 ! 'T1.2' stable observing time ! 20 ! ! ! !second! |
| ! * ! for take off (max. 20 seconds)! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! * Remark: Only for Advanced EVMU available ! |
| +-----------------------------------------------------------------------------+ |
(5) A320: CFMI Engines 56-5-A1, 56-5-A3, 56-5-B4, 56-5-B5, 56-5-B6
| +----------------------------------------------------------------------------+ |
| !Report! Description of ! CFM ! CFM ! CFM ! CFM ! CFM ! Unit ! |
| !Item ! Report Item !56-5-A1!56-5-A3!56-5-B4!56-5-B5!56-5-B6! ! |
| ! ! !-------!-------!-------!-------!-------!------! |
| ! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! ! |
| ! ! ! CFM #1! CFM #2! CFM #3! CFM #4! CFM #8! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.1 !'Y01.1' flight hours ! 0 ! 0 ! 0 ! 0 ! 0 ! hours! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.2 !'Y01.2' minutes after ! 10 ! 10 ! 10 ! 10 ! 10 ! min ! |
| ! ! cruise entry ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.3 !'Y01.3' flight legs ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.1 !'P01' stable periods ! 5 ! 5 ! 5 ! 5 ! 5 ! ! |
| ! ! ( 1 period = 20 sec) ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.2.1! HPTL1 valve position ! 0 ! 0 ! 70 ! 70 ! 70 ! % ! |
| ! ! lower limit ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.2.2! HPTL2 valve position ! 20 ! 20 ! 105 ! 105 ! 105 ! % ! |
| ! ! upper limit ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.3 ! IALT stable frame ! 150 ! 150 ! 150 ! 150 ! 150 ! ft ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.3.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of IALT ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.4 ! GS stable frame ! 6 ! 6 ! 6 ! 6 ! 6 ! kts ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.4.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of GS ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.5 ! ROLL ANGLE stable ! 4.0 ! 4.0 ! 4.0 ! 4.0 ! 4.0 ! deg ! |
| ! ! frame variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.5.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of ROLL ANGLE ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.6 ! TAT stable frame ! 2.0 ! 2.0 ! 2.0 ! 2.0 ! 2.0 ! deg C! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.6.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of TAT ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.7 ! N2 stable frame ! 0.9 ! 0.9 ! 0.9 ! 0.9 ! 0.9 ! % ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.7.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of N2 ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.8 ! EGT stable frame ! 18.0 ! 18.0 ! 18.0 ! 18.0 ! 18.0 ! deg C! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.8.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of EGT ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.9 ! VACC stable frame ! 0.10 ! 0.10 ! 0.10 ! 0.10 ! 0.10 ! g ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.9.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of VACC ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.10 ! MN stable frame ! 0.01 ! 0.01 ! 0.01 ! 0.01 ! 0.01 ! Mach ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| !5.10.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of MACH ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.11 ! N1 stable frame ! 1.6 ! 1.6 ! 1.6 ! 1.6 ! 1.6 ! % ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| !5.11.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of N1 ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.12 ! PT2 stable frame ! 0.10 ! 0.10 ! 0.10 ! 0.10 ! 0.10 ! psia ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| !5.12.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of PT2 ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.13 ! FF stable frame ! 100 ! 100 ! 100 ! 100 ! 100 ! kg/h ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| !5.13.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of FF ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.14 ! HPT stable frame ! 10.0 ! 10.0 ! 10.0 ! 10.0 ! 10.0 ! % ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| !5.14.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of HPT ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.15 ! LPT stable frame ! 10.0 ! 10.0 ! 10.0 ! 10.0 ! 10.0 ! % ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| !5.15.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of LPT ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 6.2 ! Number 'X01' for ! 5 ! 5 ! 5 ! 5 ! 5 ! ! |
| ! ! consecutive reports ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 9.1 ! 'NIT.1' stable N1 ! 62 ! 62 ! 62 ! 62 ! 62 ! %rpm ! |
| ! * ! value for descent ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 9.2 ! 'X1.1' tolerance !+/-1.5 !+/-1.5 !+/-1.5 !+/-1.5 !+/-1.5 ! % ! |
| ! * ! band for descent ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 9.3 !'T1.1' stable observing! 20 ! 20 ! 20 ! 20 ! 20 !second! |
| ! * ! time for descent ! ! ! ! ! ! ! |
| ! ! (max. 20 seconds) ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| !10.1 ! 'N1T.1' stable N1 ! 93 ! 93 ! 93 ! 93 ! 93 ! %rpm ! |
| ! * ! value for take off ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| !10.2 ! 'X1.2' tolerance !+/-1.5 !+/-1.5 !+/-1.5 !+/-1.5 !+/-1.5 ! % ! |
| ! * ! band for take off ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| !10.3 !'T1.2' stable observing! 20 ! 20 ! 20 ! 20 ! 20 !second! |
| ! * ! time for take off ! ! ! ! ! ! ! |
| ! ! (max. 20 seconds) ! ! ! ! ! ! ! |
| !-----------------------------------------------------------------------------! |
| ! * Remark: Only for Advanced EVMU available ! |
| +-----------------------------------------------------------------------------+ |
(6) A321: CFMI Engines 56-5-B1, 56-5-B2, 56-5-B3, 56-5-B4
| +-----------------------------------------------------------------------------+ |
| !Report! Description of Report Item ! CFM ! CFM ! CFM ! CFM ! Unit ! |
| !Item ! !56-5-B1!56-5-B2!56-5-B3!56-5-B4! ! |
| ! ! !-------!-------!-------!-------!------! |
| ! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! ! |
| ! ! ! CFM #5! CFM #6! CFM #7! CFM #3! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.1 !'Y01.1' flight hours ! 0 ! 0 ! 0 ! 0 ! hours! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.2 !'Y01.2' minutes after cruise ! 10 ! 10 ! 10 ! 10 ! min ! |
| ! ! entry ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.3 !'Y01.3' flight legs ! 1 ! 1 ! 1 ! 1 ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.1 !'P01' stable periods ! 5 ! 5 ! 5 ! 5 ! ! |
| ! ! (1 period = 20 seconds) ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.2.1! HPTL1 valve position lower ! 70 ! 70 ! 70 ! 70 ! % ! |
| ! ! limit ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.2.2! HPTL2 valve position upper ! 105 ! 105 ! 105 ! 105 ! % ! |
| ! ! limit ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.3 ! IALT stable frame variation ! 150 ! 150 ! 150 ! 150 ! ft ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.3.1! Weighting Factor Wa of IALT ! 1 ! 1 ! 1 ! 1 ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.4 ! GS stable frame variation ! 6 ! 6 ! 6 ! 6 ! kts ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.4.1! Weighting Factor Wa of GS ! 1 ! 1 ! 1 ! 1 ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.5 ! ROLL ANGLE stable frame ! 4.0 ! 4.0 ! 4.0 ! 4.0 ! deg ! |
| ! ! variation ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.5.1! Weighting Factor Wa of ROLL ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! ANGLE ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.6 ! TAT stable frame variation ! 2.0 ! 2.0 ! 2.0 ! 2.0 ! deg C! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.6.1! Weighting Factor Wa of TAT ! 1 ! 1 ! 1 ! 1 ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.7 ! N2 stable frame variation ! 0.9 ! 0.9 ! 0.9 ! 0.9 ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.7.1! Weighting Factor Wa of N2 ! 1 ! 1 ! 1 ! 1 ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.8 ! EGT stable frame variation ! 18.0 ! 18.0 ! 18.0 ! 18.0 ! deg C! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.8.1! Weighting Factor Wa of EGT ! 1 ! 1 ! 1 ! 1 ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.9 ! VACC stable frame variation ! 0.10 ! 0.10 ! 0.10 ! 0.10 ! g ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.9.1! Weighting Factor Wa of VACC ! 1 ! 1 ! 1 ! 1 ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.10 ! MN stable frame variation ! 0.010 ! 0.010 ! 0.010 ! 0.010 ! Mach ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !5.10.1! Weighting Factor Wa of MACH ! 1 ! 1 ! 1 ! 1 ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.11 ! N1 stable frame variation ! 1.6 ! 1.6 ! 1.6 ! 1.6 ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !5.11.1! Weighting Factor Wa of N1 ! 1 ! 1 ! 1 ! 1 ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.12 ! PT2 stable frame variation ! 0.10 ! 0.10 ! 0.10 ! 0.10 ! psia ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !5.12.1! Weighting Factor Wa of PT2 ! 1 ! 1 ! 1 ! 1 ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.13 ! FF stable frame variation ! 100 ! 100 ! 100 ! 100 ! kg/h ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !5.13.1! Weighting Factor Wa of FF ! 1 ! 1 ! 1 ! 1 ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.14 ! HPT stable frame variation ! 10.0 ! 10.0 ! 10.0 ! 10.0 ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !5.14.1! Weighting Factor Wa of HPT ! 1 ! 1 ! 1 ! 1 ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.15 ! LPT stable frame variation ! 10.0 ! 10.0 ! 10.0 ! 10.0 ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !5.15.1! Weighting Factor Wa of LPT ! 1 ! 1 ! 1 ! 1 ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 6.1 ! Number 'X01' for consecutive ! 5 ! 5 ! 5 ! 5 ! ! |
| ! ! reports ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 9.1 ! 'NIT.1' stable N1 value for ! 62 ! 62 ! 62 ! 62 ! %rpm ! |
| ! * ! descent ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 9.2 ! 'X1.1' tolerance band for !+/-1.5 !+/-1.5 !+/-1.5 !+/-1.5 ! % ! |
| ! * ! descent ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 9.3 ! 'T1.1' stable observing time ! 20 ! 20 ! 20 ! 20 !second! |
| ! * ! for descent (max. 20 seconds) ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !10.1 ! 'N1T.1' stable N1 value for ! 93 ! 93 ! 93 ! 93 ! %rpm ! |
| ! * ! take off ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !10.2 ! 'X1.2' tolerance band for !+/-1.5 !+/-1.5 !+/-1.5 !+/-1.5 ! % ! |
| ! * ! take off ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !10.3 ! 'T1.2' stable observing time ! 20 ! 20 ! 20 ! 20 !second! |
| ! * ! for take off (max. 20 seconds)! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! * Remark: Only for Advanced EVMU available ! |
| +-----------------------------------------------------------------------------+ |
(7) A319: CFMI Engines 56-5-A5, 56-5-B6, 56-5-B5, 56-5-A4, 56-5-B7
| +----------------------------------------------------------------------------+ |
| !Report! Description of ! CFM ! CFM ! CFM ! CFM ! CFM ! Unit ! |
| !Item ! Report Item !56-5-A5!56-5-B6!56-5-B5!56-5-A4!56-5-B7! ! |
| ! ! !-------!-------!-------!-------!-------!------! |
| ! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! ! |
| ! ! ! C7xxx ! C8xxxx! C4xxxx! C6xxxx! C5xxxx! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.1 !'Y01.1' flight hours ! 0 ! 0 ! 0 ! 0 ! 0 ! hours! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.2 !'Y01.2' minutes after ! 10 ! 10 ! 10 ! 10 ! 10 ! min ! |
| ! ! cruise entry ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.3 !'Y01.3' flight legs ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.1 !'P01' stable periods ! 5 ! 5 ! 5 ! 5 ! 5 ! ! |
| ! ! ( 1 period = 20 sec) ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.2.1! HPTL1 valve position ! 0 ! 70 ! 70 ! 0 ! 70 ! % ! |
| ! ! lower limit ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.2.2! HPTL2 valve position ! 20 ! 105 ! 105 ! 20 ! 105 ! % ! |
| ! ! upper limit ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.3 ! IALT stable frame ! 150 ! 150 ! 150 ! 150 ! 150 ! ft ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.3.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of IALT ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.4 ! GS stable frame ! 6 ! 6 ! 6 ! 6 ! 6 ! kts ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.4.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of GS ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.5 ! ROLL ANGLE stable ! 4.0 ! 4.0 ! 4.0 ! 4.0 ! 4.0 ! deg ! |
| ! ! frame variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.5.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of ROLL ANGLE ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.6 ! TAT stable frame ! 2.0 ! 2.0 ! 2.0 ! 2.0 ! 2.0 ! deg C! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.6.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of TAT ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.7 ! N2 stable frame ! 0.9 ! 0.9 ! 0.9 ! 0.9 ! 0.9 ! % ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.7.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of N2 ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.8 ! EGT stable frame ! 18.0 ! 18.0 ! 18.0 ! 18.0 ! 18.0 ! deg C! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.8.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of EGT ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.9 ! VACC stable frame ! 0.10 ! 0.10 ! 0.10 ! 0.10 ! 0.10 ! g ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.9.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of VACC ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.10 ! MN stable frame ! 0.01 ! 0.01 ! 0.01 ! 0.01 ! 0.01 ! Mach ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| !5.10.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of MACH ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.11 ! N1 stable frame ! 1.6 ! 1.6 ! 1.6 ! 1.6 ! 1.6 ! % ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| !5.11.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of N1 ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.12 ! PT2 stable frame ! 0.10 ! 0.10 ! 0.10 ! 0.10 ! 0.10 ! psia ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| !5.12.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of PT2 ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.13 ! FF stable frame ! 100 ! 100 ! 100 ! 100 ! 100 ! kg/h ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| !5.13.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of FF ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.14 ! HPT stable frame ! 10.0 ! 10.0 ! 10.0 ! 10.0 ! 10.0 ! % ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| !5.14.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of HPT ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.15 ! LPT stable frame ! 10.0 ! 10.0 ! 10.0 ! 10.0 ! 10.0 ! % ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| !5.15.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of LPT ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 6.2 ! Number 'X01' for ! 5 ! 5 ! 5 ! 5 ! 5 ! ! |
| ! ! consecutive reports ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 9.1 ! 'NIT.1' stable N1 ! 62 ! 62 ! 62 ! 62 ! 62 ! %rpm ! |
| ! * ! value for descent ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 9.2 ! 'X1.1' tolerance !+/-1.5 !+/-1.5 !+/-1.5 !+/-1.5 !+/-1.5 ! % ! |
| ! * ! band for descent ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 9.3 !'T1.1' stable observing! 20 ! 20 ! 20 ! 20 ! 20 !second! |
| ! * ! time for descent ! ! ! ! ! ! ! |
| ! ! (max. 20 seconds) ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| !10.1 ! 'N1T.1' stable N1 ! 93 ! 93 ! 93 ! 93 ! 93 ! %rpm ! |
| ! * ! value for take off ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| !10.2 ! 'X1.2' tolerance !+/-1.5 !+/-1.5 !+/-1.5 !+/-1.5 !+/-1.5 ! % ! |
| ! * ! band for take off ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| !10.3 !'T1.2' stable observing! 20 ! 20 ! 20 ! 20 ! 20 !second! |
| ! * ! time for take off ! ! ! ! ! ! ! |
| ! ! (max. 20 seconds) ! ! ! ! ! ! ! |
| !-----------------------------------------------------------------------------! |
| ! * Remark: Only for Advanced EVMU available ! |
| +-----------------------------------------------------------------------------+ |
(8) A318: CFMI Engine 56-5-B8, 56-5-B9
| +-----------------------------------------------------------------------------+ |
| !Report! Description of Report Item ! CFM ! CFM ! SPARE ! SPARE ! Unit ! |
| !Item ! !56-5-B8!56-5-B9! ! ! ! |
| ! ! !-------!-------!-------!-------!------! |
| ! ! !DMU/ID !DMU/ID ! ! ! ! |
| ! ! ! C1xxxx! C2xxxx! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.1 !'Y01.1' flight hours ! 0 ! 0 ! ! ! hour ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.2 !'Y01.2' minutes after cruise ! 10 ! 10 ! ! ! min ! |
| ! ! entry ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.3 !'Y01.1' flight legs ! 1 ! 1 ! ! ! hour ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.1 !'P01': stable periods ! 5 ! 5 ! ! ! ! |
| ! ! (1 period = 20 seconds) ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.2.1! HPTL1 valve position lower ! 70 ! 70 ! ! ! % ! |
| ! ! limit ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.2.2! HPTL2 valve position upper ! 105 ! 105 ! ! ! % ! |
| ! ! limit ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.3 ! IALT stable frame variation ! 150 ! 150 ! ! ! ft ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.3.1! Weighting Factor Wa of IALT ! 1 ! 1 ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.4 ! GS stable frame variation ! 6 ! 6 ! ! ! kts ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.4.1! Weighting Factor Wa of GS ! 1 ! 1 ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.5 ! ROLL ANGLE stable frame ! 4.0 ! 4.0 ! ! ! deg ! |
| ! ! variation ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.5.1! Weighting Factor Wa of ROLL ! 1 ! 1 ! ! ! ! |
| ! ! ANGLE ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.6 ! TAT stable frame variation ! 2.0 ! 2.0 ! ! ! deg C! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.6.1! Weighting Factor Wa of TAT ! 1 ! 1 ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.7 ! N2 stable frame variation ! 0.9 ! 0.9 ! ! ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.7.1! Weighting Factor Wa of N2 ! 1 ! 1 ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.8 ! EGT stable frame variation ! 18.0 ! 18.0 ! ! ! deg C! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.8.1! Weighting Factor Wa of EGT ! 1 ! 1 ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.9 ! VACC stable frame variation ! 0.10 ! 0.10 ! ! ! g ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.9.1! Weighting Factor Wa of VACC ! 1 ! 1 ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.10 ! MN stable frame variation ! 0.010 ! 0.010 ! ! !Mach ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !5.10.1! Weighting Factor Wa of MACH ! 1 ! 1 ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.11 ! N1 stable frame variation ! 1.6 ! 1.6 ! ! ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !5.11.1! Weighting Factor Wa of N1 ! 1 ! 1 ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.12 ! PT2 stable frame variation ! 0.10 ! 0.10 ! ! ! psia ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !5.12.1! Weighting Factor Wa of PT2 ! 1 ! 1 ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.13 ! FF stable frame variation ! 100 ! 100 ! ! ! kg/h ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !5.13.1! Weighting Factor Wa of FF ! 1 ! 1 ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.14 ! HPT stable frame variation ! 10.0 ! 10.0 ! ! ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !5.14.1! Weighting Factor Wa of HPT ! 1 ! 1 ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.15 ! LPT stable frame variation ! 10.0 ! 10.0 ! ! ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !5.15.1! Weighting Factor Wa of LPT ! 1 ! 1 ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 6.1 ! Number 'X01' for consecutive ! 5 ! 5 ! ! ! ! |
| ! ! reports ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 9.1 ! 'N1T.1' stable N1 value for ! 62 ! 62 ! ! ! %rpm ! |
| ! * ! descent ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 9.2 ! 'X1.1' tolerance band for !+/-1.5 !+/-1.5 ! ! ! % ! |
| ! * ! descent ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 9.3 ! 'T1.1' stable observing time ! 20 ! 20 ! ! !second! |
| ! * ! for descent (max. 20 seconds) ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 10.1 ! 'N1T.1' stable N1 value for ! 93 ! 93 ! ! ! %rpm ! |
| ! * ! take off ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 10.2 ! 'X1.2' tolerance band for !+/-1.5 !+/-1.5 ! ! ! % ! |
| ! * ! take off ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 10.3 ! 'T1.2' stable observing time ! 20 ! 20 ! ! !second! |
| ! * ! for take off (max. 20 seconds)! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! * Remark: Only for Advanced EVMU available ! |
| +-----------------------------------------------------------------------------+ |
(9) A320: CFMI Engines 56-5-A1, 56-5-A3, 56-5-B4, 56-5-B5, 56-5-B6
| +----------------------------------------------------------------------------+ |
| !Report! Description of ! CFM ! CFM ! CFM ! CFM ! CFM ! Unit ! |
| !Item ! Report Item !56-5-A1!56-5-A3!56-5-B4!56-5-B5!56-5-B6! ! |
| ! ! !-------!-------!-------!-------!-------!------! |
| ! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! ! |
| ! ! ! CFM #1! CFM #2! CFM #3! CFM #4! CFM #8! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.1 !'Y01.1' flight hours ! 0 ! 0 ! 0 ! 0 ! 0 ! hours! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.2 !'Y01.2' minutes after ! 10 ! 10 ! 10 ! 10 ! 10 ! min ! |
| ! ! cruise entry ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.3 !'Y01.3' flight legs ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.1 !'P01' stable periods ! 5 ! 5 ! 5 ! 5 ! 5 ! ! |
| ! ! ( 1 period = 20 sec) ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.2.1! HPTL1 valve position ! 0 ! 0 ! 70 ! 70 ! 70 ! % ! |
| ! ! lower limit ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.2.2! HPTL2 valve position ! 20 ! 20 ! 105 ! 105 ! 105 ! % ! |
| ! ! upper limit ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.3 ! IALT stable frame ! 150 ! 150 ! 150 ! 150 ! 150 ! ft ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.3.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of IALT ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.4 ! GS stable frame ! 6 ! 6 ! 6 ! 6 ! 6 ! kts ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.4.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of GS ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.5 ! ROLL ANGLE stable ! 4.0 ! 4.0 ! 4.0 ! 4.0 ! 4.0 ! deg ! |
| ! ! frame variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.5.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of ROLL ANGLE ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.6 ! TAT stable frame ! 2.0 ! 2.0 ! 2.0 ! 2.0 ! 2.0 ! deg C! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.6.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of TAT ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.7 ! N2 stable frame ! 0.9 ! 0.9 ! 0.9 ! 0.9 ! 0.9 ! % ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.7.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of N2 ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.8 ! EGT stable frame ! 18.0 ! 18.0 ! 18.0 ! 18.0 ! 18.0 ! deg C! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.8.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of EGT ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.9 ! VACC stable frame ! 0.10 ! 0.10 ! 0.10 ! 0.10 ! 0.10 ! g ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.9.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of VACC ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.10 ! MN stable frame ! 0.010! 0.010! 0.010! 0.010! 0.010! Mach ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| !5.10.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of MACH ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.11 ! N1 stable frame ! 1.6 ! 1.6 ! 1.6 ! 1.6 ! 1.6 ! % ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| !5.11.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of N1 ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.12 ! PT2 stable frame ! 0.10 ! 0.10 ! 0.10 ! 0.10 ! 0.10 ! psia ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| !5.12.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of PT2 ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.13 ! FF stable frame ! 100 ! 100 ! 100 ! 100 ! 100 ! kg/h ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| !5.13.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of FF ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.14 ! HPT stable frame ! 10.0 ! 10.0 ! 10.0 ! 10.0 ! 10.0 ! % ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| !5.14.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of HPT ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.15 ! LPT stable frame ! 10.0 ! 10.0 ! 10.0 ! 10.0 ! 10.0 ! % ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| !5.15.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of LPT ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 6.2 ! Number 'X01' for ! 5 ! 5 ! 5 ! 5 ! 5 ! ! |
| ! ! consecutive reports ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 9.1 ! 'NIT.1' stable N1 ! 62 ! 62 ! 62 ! 62 ! 62 ! %rpm ! |
| ! * ! value for descent ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 9.2 ! 'X1.1' tolerance !+/-1.5 !+/-1.5 !+/-1.5 !+/-1.5 !+/-1.5 ! % ! |
| ! * ! band for descent ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 9.3 !'T1.1' stable observing! 20 ! 20 ! 20 ! 20 ! 20 !second! |
| ! * ! time for descent ! ! ! ! ! ! ! |
| ! ! (max. 20 seconds) ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| !10.1 ! 'N1T.1' stable N1 ! 93 ! 93 ! 93 ! 93 ! 93 ! %rpm ! |
| ! * ! value for take off ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| !10.2 ! 'X1.2' tolerance !+/-1.5 !+/-1.5 !+/-1.5 !+/-1.5 !+/-1.5 ! % ! |
| ! * ! band for take off ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| !10.3 !'T1.2' stable observing! 20 ! 20 ! 20 ! 20 ! 20 !second! |
| ! * ! time for take off ! ! ! ! ! ! ! |
| ! ! (max. 20 seconds) ! ! ! ! ! ! ! |
| !-----------------------------------------------------------------------------! |
| ! * Remark: Only for Advanced EVMU available ! |
| +-----------------------------------------------------------------------------+ |
(10) A321: CFMI Engines 56-5-B1, 56-5-B2, 56-5-B3, 56-5-B4
| +-----------------------------------------------------------------------------+ |
| !Report! Description of Report Item ! CFM ! CFM ! CFM ! CFM ! Unit ! |
| !Item ! !56-5-B1!56-5-B2!56-5-B3!56-5-B4! ! |
| ! ! !-------!-------!-------!-------!------! |
| ! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! ! |
| ! ! ! CFM #5! CFM #6! CFM #7! CFM #3! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.1 !'Y01.1' flight hours ! 0 ! 0 ! 0 ! 0 ! hours! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.2 !'Y01.2' minutes after cruise ! 10 ! 10 ! 10 ! 10 ! min ! |
| ! ! entry ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.3 !'Y01.3' flight legs ! 1 ! 1 ! 1 ! 1 ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.1 !'P01' stable periods ! 5 ! 5 ! 5 ! 5 ! ! |
| ! ! (1 period = 20 seconds) ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.2.1! HPTL1 valve position lower ! 70 ! 70 ! 70 ! 70 ! % ! |
| ! ! limit ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.2.2! HPTL2 valve position upper ! 105 ! 105 ! 105 ! 105 ! % ! |
| ! ! limit ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.3 ! IALT stable frame variation ! 150 ! 150 ! 150 ! 150 ! ft ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.3.1! Weighting Factor Wa of IALT ! 1 ! 1 ! 1 ! 1 ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.4 ! GS stable frame variation ! 6 ! 6 ! 6 ! 6 ! kts ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.4.1! Weighting Factor Wa of GS ! 1 ! 1 ! 1 ! 1 ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.5 ! ROLL ANGLE stable frame ! 4.0 ! 4.0 ! 4.0 ! 4.0 ! deg ! |
| ! ! variation ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.5.1! Weighting Factor Wa of ROLL ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! ANGLE ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.6 ! TAT stable frame variation ! 2.0 ! 2.0 ! 2.0 ! 2.0 ! deg C! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.6.1! Weighting Factor Wa of TAT ! 1 ! 1 ! 1 ! 1 ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.7 ! N2 stable frame variation ! 0.9 ! 0.9 ! 0.9 ! 0.9 ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.7.1! Weighting Factor Wa of N2 ! 1 ! 1 ! 1 ! 1 ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.8 ! EGT stable frame variation ! 18.0 ! 18.0 ! 18.0 ! 18.0 ! deg C! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.8.1! Weighting Factor Wa of EGT ! 1 ! 1 ! 1 ! 1 ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.9 ! VACC stable frame variation ! 0.10 ! 0.10 ! 0.10 ! 0.10 ! g ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.9.1! Weighting Factor Wa of VACC ! 1 ! 1 ! 1 ! 1 ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.10 ! MN stable frame variation ! 0.010 ! 0.010 ! 0.010 ! 0.010 ! Mach ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !5.10.1! Weighting Factor Wa of MACH ! 1 ! 1 ! 1 ! 1 ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.11 ! N1 stable frame variation ! 1.6 ! 1.6 ! 1.6 ! 1.6 ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !5.11.1! Weighting Factor Wa of N1 ! 1 ! 1 ! 1 ! 1 ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.12 ! PT2 stable frame variation ! 0.10 ! 0.10 ! 0.10 ! 0.10 ! psia ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !5.12.1! Weighting Factor Wa of PT2 ! 1 ! 1 ! 1 ! 1 ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.13 ! FF stable frame variation ! 100 ! 100 ! 100 ! 100 ! kg/h ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !5.13.1! Weighting Factor Wa of FF ! 1 ! 1 ! 1 ! 1 ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.14 ! HPT stable frame variation ! 10.0 ! 10.0 ! 10.0 ! 10.0 ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !5.14.1! Weighting Factor Wa of HPT ! 1 ! 1 ! 1 ! 1 ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.15 ! LPT stable frame variation ! 10.0 ! 10.0 ! 10.0 ! 10.0 ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !5.15.1! Weighting Factor Wa of LPT ! 1 ! 1 ! 1 ! 1 ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 6.1 ! Number 'X01' for consecutive ! 5 ! 5 ! 5 ! 5 ! ! |
| ! ! reports ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 9.1 ! 'NIT.1' stable N1 value for ! 62 ! 62 ! 62 ! 62 ! %rpm ! |
| ! * ! descent ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 9.2 ! 'X1.1' tolerance band for !+/-1.5 !+/-1.5 !+/-1.5 !+/-1.5 ! % ! |
| ! * ! descent ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 9.3 ! 'T1.1' stable observing time ! 20 ! 20 ! 20 ! 20 !second! |
| ! * ! for descent (max. 20 seconds) ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !10.1 ! 'N1T.1' stable N1 value for ! 93 ! 93 ! 93 ! 93 ! %rpm ! |
| ! * ! take off ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !10.2 ! 'X1.2' tolerance band for !+/-1.5 !+/-1.5 !+/-1.5 !+/-1.5 ! % ! |
| ! * ! take off ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !10.3 ! 'T1.2' stable observing time ! 20 ! 20 ! 20 ! 20 !second! |
| ! * ! for take off (max. 20 seconds)! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! * Remark: Only for Advanced EVMU available ! |
| +-----------------------------------------------------------------------------+ |
(11) A319: CFMI Engines 56-5-A5, 56-5-B6, 56-5-B5, 56-5-A4, 56-5-B7
| +----------------------------------------------------------------------------+ |
| !Report! Description of ! CFM ! CFM ! CFM ! CFM ! CFM ! Unit ! |
| !Item ! Report Item !56-5-A5!56-5-B6!56-5-B5!56-5-A4!56-5-B7! ! |
| ! ! !-------!-------!-------!-------!-------!------! |
| ! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! ! |
| ! ! ! C7xxx ! C8xxxx! C4xxxx! C6xxxx! C5xxxx! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.1 !'Y01.1' flight hours ! 0 ! 0 ! 0 ! 0 ! 0 ! hours! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.2 !'Y01.2' minutes after ! 10 ! 10 ! 10 ! 10 ! 10 ! min ! |
| ! ! cruise entry ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.3 !'Y01.3' flight legs ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.1 !'P01' stable periods ! 5 ! 5 ! 5 ! 5 ! 5 ! ! |
| ! ! ( 1 period = 20 sec) ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.2.1! HPTL1 valve position ! 0 ! 70 ! 70 ! 0 ! 70 ! % ! |
| ! ! lower limit ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.2.2! HPTL2 valve position ! 20 ! 105 ! 105 ! 20 ! 105 ! % ! |
| ! ! upper limit ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.3 ! IALT stable frame ! 150 ! 150 ! 150 ! 150 ! 150 ! ft ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.3.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of IALT ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.4 ! GS stable frame ! 6 ! 6 ! 6 ! 6 ! 6 ! kts ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.4.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of GS ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.5 ! ROLL ANGLE stable ! 4.0 ! 4.0 ! 4.0 ! 4.0 ! 4.0 ! deg ! |
| ! ! frame variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.5.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of ROLL ANGLE ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.6 ! TAT stable frame ! 2.0 ! 2.0 ! 2.0 ! 2.0 ! 2.0 ! deg C! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.6.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of TAT ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.7 ! N2 stable frame ! 0.9 ! 0.9 ! 0.9 ! 0.9 ! 0.9 ! % ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.7.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of N2 ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.8 ! EGT stable frame ! 18.0 ! 18.0 ! 18.0 ! 18.0 ! 18.0 ! deg C! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.8.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of EGT ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.9 ! VACC stable frame ! 0.10 ! 0.10 ! 0.10 ! 0.10 ! 0.10 ! g ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.9.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of VACC ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.10 ! MN stable frame ! 0.010! 0.010! 0.010! 0.010! 0.010! Mach ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| !5.10.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of MACH ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.11 ! N1 stable frame ! 1.6 ! 1.6 ! 1.6 ! 1.6 ! 1.6 ! % ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| !5.11.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of N1 ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.12 ! PT2 stable frame ! 0.10 ! 0.10 ! 0.10 ! 0.10 ! 0.10 ! psia ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| !5.12.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of PT2 ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.13 ! FF stable frame ! 100 ! 100 ! 100 ! 100 ! 100 ! kg/h ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| !5.13.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of FF ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.14 ! HPT stable frame ! 10.0 ! 10.0 ! 10.0 ! 10.0 ! 10.0 ! % ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| !5.14.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of HPT ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.15 ! LPT stable frame ! 10.0 ! 10.0 ! 10.0 ! 10.0 ! 10.0 ! % ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| !5.15.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of LPT ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 6.2 ! Number 'X01' for ! 5 ! 5 ! 5 ! 5 ! 5 ! ! |
| ! ! consecutive reports ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 9.1 ! 'NIT.1' stable N1 ! 62 ! 62 ! 62 ! 62 ! 62 ! %rpm ! |
| ! * ! value for descent ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 9.2 ! 'X1.1' tolerance !+/-1.5 !+/-1.5 !+/-1.5 !+/-1.5 !+/-1.5 ! % ! |
| ! * ! band for descent ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 9.3 !'T1.1' stable observing! 20 ! 20 ! 20 ! 20 ! 20 !second! |
| ! * ! time for descent ! ! ! ! ! ! ! |
| ! ! (max. 20 seconds) ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| !10.1 ! 'N1T.1' stable N1 ! 93 ! 93 ! 93 ! 93 ! 93 ! %rpm ! |
| ! * ! value for take off ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| !10.2 ! 'X1.2' tolerance !+/-1.5 !+/-1.5 !+/-1.5 !+/-1.5 !+/-1.5 ! % ! |
| ! * ! band for take off ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| !10.3 !'T1.2' stable observing! 20 ! 20 ! 20 ! 20 ! 20 !second! |
| ! * ! time for take off ! ! ! ! ! ! ! |
| ! ! (max. 20 seconds) ! ! ! ! ! ! ! |
| !-----------------------------------------------------------------------------! |
| ! * Remark: Only for Advanced EVMU available ! |
| +-----------------------------------------------------------------------------+ |
(12) A318: CFMI Engine 56-5-B8, 56-5-B9
| +-----------------------------------------------------------------------------+ |
| !Report! Description of Report Item ! CFM ! CFM ! SPARE ! SPARE ! Unit ! |
| !Item ! !56-5-B8!56-5-B9! ! ! ! |
| ! ! !-------!-------!-------!-------!------! |
| ! ! !DMU/ID !DMU/ID ! ! ! ! |
| ! ! ! C1xxxx! C2xxxx! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.1 !'Y01.1' flight hours ! 0 ! 0 ! ! ! hour ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.2 !'Y01.2' minutes after cruise ! 10 ! 10 ! ! ! min ! |
| ! ! entry ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.3 !'Y01.1' flight legs ! 1 ! 1 ! ! ! hour ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.1 !'P01': stable periods ! 5 ! 5 ! ! ! ! |
| ! ! (1 period = 20 seconds) ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.2.1! HPTL1 valve position lower ! 70 ! 70 ! ! ! % ! |
| ! ! limit ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.2.2! HPTL2 valve position upper ! 105 ! 105 ! ! ! % ! |
| ! ! limit ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.3 ! IALT stable frame variation ! 150 ! 150 ! ! ! ft ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.3.1! Weighting Factor Wa of IALT ! 1 ! 1 ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.4 ! GS stable frame variation ! 6 ! 6 ! ! ! kts ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.4.1! Weighting Factor Wa of GS ! 1 ! 1 ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.5 ! ROLL ANGLE stable frame ! 4.0 ! 4.0 ! ! ! deg ! |
| ! ! variation ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.5.1! Weighting Factor Wa of ROLL ! 1 ! 1 ! ! ! ! |
| ! ! ANGLE ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.6 ! TAT stable frame variation ! 2.0 ! 2.0 ! ! ! deg C! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.6.1! Weighting Factor Wa of TAT ! 1 ! 1 ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.7 ! N2 stable frame variation ! 0.9 ! 0.9 ! ! ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.7.1! Weighting Factor Wa of N2 ! 1 ! 1 ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.8 ! EGT stable frame variation ! 18.0 ! 18.0 ! ! ! deg C! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.8.1! Weighting Factor Wa of EGT ! 1 ! 1 ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.9 ! VACC stable frame variation ! 0.10 ! 0.10 ! ! ! g ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.9.1! Weighting Factor Wa of VACC ! 1 ! 1 ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.10 ! MN stable frame variation ! 0.010 ! 0.010 ! ! !Mach ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !5.10.1! Weighting Factor Wa of MACH ! 1 ! 1 ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.11 ! N1 stable frame variation ! 1.6 ! 1.6 ! ! ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !5.11.1! Weighting Factor Wa of N1 ! 1 ! 1 ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.12 ! PT2 stable frame variation ! 0.10 ! 0.10 ! ! ! psia ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !5.12.1! Weighting Factor Wa of PT2 ! 1 ! 1 ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.13 ! FF stable frame variation ! 100 ! 100 ! ! ! kg/h ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !5.13.1! Weighting Factor Wa of FF ! 1 ! 1 ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.14 ! HPT stable frame variation ! 10.0 ! 10.0 ! ! ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !5.14.1! Weighting Factor Wa of HPT ! 1 ! 1 ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.15 ! LPT stable frame variation ! 10.0 ! 10.0 ! ! ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !5.15.1! Weighting Factor Wa of LPT ! 1 ! 1 ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 6.1 ! Number 'X01' for consecutive ! 5 ! 5 ! ! ! ! |
| ! ! reports ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 9.1 ! 'N1T.1' stable N1 value for ! 62 ! 62 ! ! ! %rpm ! |
| ! * ! descent ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 9.2 ! 'X1.1' tolerance band for !+/-1.5 !+/-1.5 ! ! ! % ! |
| ! * ! descent ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 9.3 ! 'T1.1' stable observing time ! 20 ! 20 ! ! !second! |
| ! * ! for descent (max. 20 seconds) ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 10.1 ! 'N1T.1' stable N1 value for ! 93 ! 93 ! ! ! %rpm ! |
| ! * ! take off ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 10.2 ! 'X1.2' tolerance band for !+/-1.5 !+/-1.5 ! ! ! % ! |
| ! * ! take off ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 10.3 ! 'T1.2' stable observing time ! 20 ! 20 ! ! !second! |
| ! * ! for take off (max. 20 seconds)! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! * Remark: Only for Advanced EVMU available ! |
| +-----------------------------------------------------------------------------+ |
(13) A320: CFMI Engines 56-5-A1, 56-5-A3, 56-5-B4, 56-5-B5, 56-5-B6
| +-----------------------------------------------------------------------------+ |
| !Report!Limit!Description of ! CFM ! CFM ! CFM ! CFM ! CFM ! Unit ! |
| !Item !No. !Report Item !56-5-A1!56-5-A3!56-5-B4!56-5-B5!56-5-B6! ! |
| ! ! ! !-------!-------!-------!-------!-------!------! |
| ! ! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! ! |
| ! ! ! ! CFM #1! CFM #2! CFM #3! CFM #4! CFM #8! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.1 ! 4 !"Y01.1" flight ! 0 ! 0 ! 0 ! 0 ! 0 ! hours! |
| ! ! !hours ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.2 ! 5 !"Y01.2" minutes ! 10 ! 10 ! 10 ! 10 ! 10 ! min ! |
| ! ! !after cruise ! ! ! ! ! ! ! |
| ! ! !entry ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.3 ! 6 !"Y01.3" flight ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! !legs ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.1 ! 3 !"P01" stable ! 5 ! 5 ! 5 ! 5 ! 5 ! ! |
| ! ! !periods ! ! ! ! ! ! ! |
| ! ! !(1period = 20sec)! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.2.1! 8 !HPTL1 valve ! 0 ! 0 ! 70 ! 70 ! 70 ! % ! |
| ! ! !position lower ! ! ! ! ! ! ! |
| ! ! !limit ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.2.2! 9 !HPTL2 valve ! 20 ! 20 ! 105 ! 105 ! 105 ! % ! |
| ! ! !position upper ! ! ! ! ! ! ! |
| ! ! !limit ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.3 ! 10 !IALT stable frame! 150 ! 150 ! 150 ! 150 ! 150 ! ft ! |
| ! ! !variation ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.3.1! 24 !Weighting Factor ! 100 ! 100 ! 100 ! 100 ! 100 ! ! |
| ! ! !Wa of IALT ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.4 ! 11 !GS stable frame ! 6 ! 6 ! 6 ! 6 ! 6 ! kts ! |
| ! ! !variation ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.4.1! 25 !Weighting Factor ! 100 ! 100 ! 100 ! 100 ! 100 ! ! |
| ! ! !Wa of GS ! ! ! ! ! ! ! |
| !------!-----!- ---------------!-------!-------!-------!-------!-------!------! |
| ! 5.5 ! 12 !ROLL ANGLE stable! 4.0 ! 4.0 ! 4.0 ! 4.0 ! 4.0 ! deg ! |
| ! ! !frame variation ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.5.1! 26 !Weighting Factor ! 100 ! 100 ! 100 ! 100 ! 100 ! ! |
| ! ! !Wa of ROLL ANGLE ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.6 ! 13 !TAT stable frame ! 2.0 ! 2.0 ! 2.0 ! 2.0 ! 2.0 ! deg C! |
| ! ! !variation ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.6.1! 27 !Weighting Factor ! 100 ! 100 ! 100 ! 100 ! 100 ! ! |
| ! ! !Wa of TAT ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.7 ! 14 !N2 stable frame ! 0.9 ! 0.9 ! 0.9 ! 0.9 ! 0.9 ! % ! |
| ! ! !variation ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.7.1! 28 ! Weighting Factor! 100 ! 100 ! 100 ! 100 ! 100 ! ! |
| ! ! ! Wa of N2 ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.8 ! 15 !EGT stable frame ! 18.0 ! 18.0 ! 18.0 ! 18.0 ! 18.0 ! deg C! |
| ! ! !variation ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.8.1! 29 !Weighting Factor ! 100 ! 100 ! 100 ! 100 ! 100 ! ! |
| ! ! !Wa of EGT ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.9 ! 16 !VACC stable frame! 0.10 ! 0.10 ! 0.10 ! 0.10 ! 0.10 ! g ! |
| ! ! !variation ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.9.1! 30 !Weighting Factor ! 100 ! 100 ! 100 ! 100 ! 100 ! ! |
| ! ! !Wa of VACC ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.10 ! 17 !MACH stable frame! 0.01 ! 0.01 ! 0.01 ! 0.01 ! 0.01 ! Mach ! |
| ! ! !variation ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| !5.10.1! 31 !Weighting Factor ! 100 ! 100 ! 100 ! 100 ! 100 ! ! |
| ! ! !Wa of MACH ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.11 ! 18 !N1 stable frame ! 1.6 ! 1.6 ! 1.6 ! 1.6 ! 1.6 ! % ! |
| ! ! !variation ! ! ! ! ! ! ! |
| !------!-----!---------------- !-------!-------!-------!-------!-------!------! |
| !5.11.1! 32 !Weighting Factor ! 100 ! 100 ! 100 ! 100 ! 100 ! ! |
| ! ! !Wa of N1 ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.12 ! 19 !PT2 stable frame ! 0.10 ! 0.10 ! 0.10 ! 0.10 ! 0.10 ! psia ! |
| ! ! !variation ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| !5.12.1! 33 !Weighting Factor ! 100 ! 100 ! 100 ! 100 ! 100 ! ! |
| ! ! !Wa of PT2 ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.13 ! 20 !FF stable frame ! 100 ! 100 ! 100 ! 100 ! 100 ! kg/h ! |
| ! ! !variation ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| !5.13.1! 34 !Weighting Factor ! 100 ! 100 ! 100 ! 100 ! 100 ! ! |
| ! ! !Wa of FF ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.14 ! 21 !HPT stable frame ! 10.0 ! 10.0 ! 10.0 ! 10.0 ! 10.0 ! % ! |
| ! ! !variation ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| !5.14.1! 35 !Weighting Factor ! 100 ! 100 ! 100 ! 100 ! 100 ! ! |
| ! ! !Wa of HPT ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.15 ! 22 !LPT stable frame ! 10.0 ! 10.0 ! 10.0 ! 10.0 ! 10.0 ! % ! |
| ! ! !variation ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| !5.15.1! 36 !Weighting Factor ! 100 ! 100 ! 100 ! 100 ! 100 ! ! |
| ! ! !Wa of LPT ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 6.2 ! 7 !Number "X01" for ! 5 ! 5 ! 5 ! 5 ! 5 ! ! |
| ! ! !consecutive ! ! ! ! ! ! ! |
| ! ! !reports ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 9.1 ! 38 !"NIT.1" stable N1! 62 ! 62 ! 62 ! 62 ! 62 ! %rpm ! |
| ! * ! !value for descent! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 9.2 ! 39 !"X1.1"tolerance !+/-1.5 !+/-1.5 !+/-1.5 !+/-1.5 !+/-1.5 ! % ! |
| ! * ! !band for descent ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 9.3 ! 40 ! "T1.1" stable ! 20 ! 20 ! 20 ! 20 ! 20 !second! |
| ! * ! !observing time ! ! ! ! ! ! ! |
| ! ! !for descent ! ! ! ! ! ! ! |
| ! ! !(max. 20 seconds)! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| !10.1 ! 41 !"N1T.1" stable N1! 93 ! 93 ! 93 ! 93 ! 93 ! %rpm ! |
| ! * ! !value for take ! ! ! ! ! ! ! |
| ! ! !off ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| !10.2 ! 42 !"X1.1" tolerance !+/-1.5 !+/-1.5 !+/-1.5 !+/-1.5 !+/-1.5 ! % ! |
| ! * ! !band for climb ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| !10.3 ! 43 !"T1.1" stable ! 20 ! 20 ! 20 ! 20 ! 20 !second! |
| ! * ! !observing time ! ! ! ! ! ! ! |
| ! ! !for climb ! ! ! ! ! ! ! |
| ! ! !(max. 20 seconds)! ! ! ! ! ! ! |
| !-----------------------------------------------------------------------------! |
| ! * Remark: Only for Advanced EVMU available ! |
| +-----------------------------------------------------------------------------+ |
(14) A321: CFMI Engines 56-5-B1, 56-5-B2, 56-5-B3, 56-5-B4
| +-----------------------------------------------------------------------------+ |
| !Report!Limit! Description of ! CFM ! CFM ! CFM ! CFM ! Unit ! |
| !Item !No. ! Report Item !56-5-B1!56-5-B2!56-5-B3!56-5-B4! ! |
| ! ! ! !-------!-------!-------!-------!------! |
| ! ! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! ! |
| ! ! ! ! CFM #5! CFM #6! CFM #7! CFM #3! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.1 ! 4 !"Y01.1" flight hours ! 0 ! 0 ! 0 ! 0 ! hours! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.2 ! 5 !"Y01.2" minutes after ! 10 ! 10 ! 10 ! 10 ! min ! |
| ! ! !cruise entry ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.3 ! 6 !"Y01.3" flight legs ! 1 ! 1 ! 1 ! 1 ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.1 ! 3 !"P01" stable periods ! 5 ! 5 ! 5 ! 5 ! ! |
| ! ! !(1 period = 20 seconds) ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.2.1! 8 !HPTL1 valve position ! 70 ! 70 ! 70 ! 70 ! % ! |
| ! ! !lower limit ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.2.2! 9 !HPTL2 valve position ! 105 ! 105 ! 105 ! 105 ! % ! |
| ! ! !upper limit ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.3 ! 10 !IALT stable frame ! 150 ! 150 ! 150 ! 150 ! ft ! |
| ! ! !variation ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.3.1! 24 !Weighting Factor Wa of ! 100 ! 100 ! 100 ! 100 ! ! |
| ! ! !IALT ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.4 ! 11 !GS stable frame variation! 6 ! 6 ! 6 ! 6 ! kts ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.4.1! 25 !Weighting Factor Wa of GS! 100 ! 100 ! 100 ! 100 ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.5 ! 12 !ROLL ANGLE stable frame ! 4.0 ! 4.0 ! 4.0 ! 4.0 ! deg ! |
| ! ! !variation ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.5.1! 26 !Weighting Factor Wa of ! 100 ! 100 ! 100 ! 100 ! ! |
| ! ! !ROLL ANGLE ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.6 ! 13 !TAT stable frame ! 2.0 ! 2.0 ! 2.0 ! 2.0 ! deg C! |
| ! ! !variation ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.6.1! 27 !Weighting Factor Wa ! 100 ! 100 ! 100 ! 100 ! ! |
| ! ! !of TAT ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.7 ! 14 !N2 stable frame variation! 0.9 ! 0.9 ! 0.9 ! 0.9 ! % ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.7.1! 28 !Weighting Factor Wa of N2! 100 ! 100 ! 100 ! 100 ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.8 ! 15 !EGT stable frame ! 18.0 ! 18.0 ! 18.0 ! 18.0 ! deg C! |
| ! ! !variation ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.8.1! 29 !Weighting Factor Wa of ! 100 ! 100 ! 100 ! 100 ! ! |
| ! ! !EGT ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.9 ! 16 !VACC stable frame ! 0.10 ! 0.10 ! 0.10 ! 0.10 ! g ! |
| ! ! !variation ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.9.1! 30 !Weighting Factor Wa of ! 100 ! 100 ! 100 ! 100 ! ! |
| ! ! !VACC ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.10 ! 17 !MACH stable frame ! 0.010 ! 0.010 ! 0.010 ! 0.010 ! Mach ! |
| ! ! !variation ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| !5.10.1! 31 !Weighting Factor Wa of ! 100 ! 100 ! 100 ! 100 ! ! |
| ! ! !MACH ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.11 ! 18 !N1 stable frame variation! 1.6 ! 1.6 ! 1.6 ! 1.6 ! % ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| !5.11.1! 32 !Weighting Factor Wa of N1! 100 ! 100 ! 100 ! 100 ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.12 ! 19 !PT2 stable frame ! 0.10 ! 0.10 ! 0.10 ! 0.10 ! psia ! |
| ! ! !variation ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| !5.12.1! 33 !Weighting Factor Wa ! 100 ! 100 ! 100 ! 100 ! ! |
| ! ! !of PT2 ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.13 ! 20 !FF stable frame ! 100 ! 100 ! 100 ! 100 ! kg/h ! |
| ! ! !variation ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| !5.13.1! 34 !Weighting Factor Wa of FF! 100 ! 100 ! 100 ! 100 ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.14 ! 21 !HPT stable frame ! 10.0 ! 10.0 ! 10.0 ! 10.0 ! % ! |
| ! ! !variation ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| !5.14.1! 35 !Weighting Factor Wa ! 100 ! 100 ! 100 ! 100 ! ! |
| ! ! !of HPT ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.15 ! 22 !LPT stable frame ! 10.0 ! 10.0 ! 10.0 ! 10.0 ! % ! |
| ! ! !variation ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| !5.15.1! 36 !Weighting Factor Wa of ! 100 ! 100 ! 100 ! 100 ! ! |
| ! ! !LPT ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 6.2 ! 7 !Number "X01" for ! 5 ! 5 ! 5 ! 5 ! ! |
| ! ! !consecutive reports ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 9.1 ! 38 !"NIT.1" stable N1 value ! 62 ! 62 ! 62 ! 62 ! %rpm ! |
| ! * ! ! for descent ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 9.2 ! 39 !"X1.1" tolerance band for!+/-1.5 !+/-1.5 !+/-1.5 !+/-1.5 ! % ! |
| ! * ! !descent ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 9.3 ! 40 !"T1.1" stable observing ! 20 ! 20 ! 20 ! 20 !second! |
| ! * ! !time for descent ! ! ! ! ! ! |
| ! ! !(max. 20 seconds) ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| !10.1 ! 41 !"N1T.1" stable N1 value ! 93 ! 93 ! 93 ! 93 ! %rpm ! |
| ! * ! !for climb ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| !10.2 ! 42 !"X1.1" tolerance band !+/-1.5 !+/-1.5 !+/-1.5 !+/-1.5 ! % ! |
| ! * ! !for climb ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| !10.3 ! 43 !"T1.1" stable observing ! 20 ! 20 ! 20 ! 20 !second! |
| ! * ! !time for climb ! ! ! ! ! ! |
| ! ! !(max. 20 seconds) ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! * Remark: Only for Advanced EVMU available ! |
| +-----------------------------------------------------------------------------+ |
(15) A319: CFMI Engines 56-5-A5, 56-5-B6, 56-5-B5, 56-5-A4, 56-5-B7
| +----------------------------------------------------------------------------+ |
| !Report!Limit! Description of ! CFM ! CFM ! CFM ! CFM ! CFM ! Unit ! |
| !Item !No. ! Report Item !56-5-A5!56-5-B6!56-5-B5!56-5-A4!56-5-B7! ! |
| ! ! ! !-------!-------!-------!-------!-------!------! |
| ! ! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! ! |
| ! ! ! ! C7xxx ! C8xxxx! C4xxxx! C6xxxx! C5xxxx! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.1 ! 4 !"Y01.1" flight ! 0 ! 0 ! 0 ! 0 ! 0 ! hours! |
| ! ! !hours ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.2 ! 5 !"Y01.2" minutes ! 10 ! 10 ! 10 ! 10 ! 10 ! min ! |
| ! ! !after cruise ! ! ! ! ! ! ! |
| ! ! !entry ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.3 ! 6 !"Y01.3" flight ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! !legs ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.1 ! 3 !"P01" stable ! 5 ! 5 ! 5 ! 5 ! 5 ! ! |
| ! ! !periods ! ! ! ! ! ! ! |
| ! ! !(1period = 20sec)! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.2.1! 8 !HPTL1 valve ! 0 ! 70 ! 70 ! 0 ! 70 ! % ! |
| ! ! !position lower ! ! ! ! ! ! ! |
| ! ! !limit ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.2.2! 9 !HPTL2 valve ! 20 ! 105 ! 105 ! 20 ! 105 ! % ! |
| ! ! !position upper ! ! ! ! ! ! ! |
| ! ! !limit ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.3 ! 10 !IALT stable frame! 150 ! 150 ! 150 ! 150 ! 150 ! ft ! |
| ! ! !variation ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.3.1! 24 !Weighting Factor ! 100 ! 100 ! 100 ! 100 ! 100 ! ! |
| ! ! !Wa of IALT ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.4 ! 11 !GS stable frame ! 6 ! 6 ! 6 ! 6 ! 6 ! kts ! |
| ! ! !variation ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.4.1! 25 !Weighting Factor ! 100 ! 100 ! 100 ! 100 ! 100 ! ! |
| ! ! !Wa of GS ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.5 ! 12 !ROLL ANGLE stable! 4.0 ! 4.0 ! 4.0 ! 4.0 ! 4.0 ! deg ! |
| ! ! !frame variation ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.5.1! 26 !Weighting Factor ! 100 ! 100 ! 100 ! 100 ! 100 ! ! |
| ! ! !Wa of ROLL ANGLE ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.6 ! 13 !TAT stable frame ! 2.0 ! 2.0 ! 2.0 ! 2.0 ! 2.0 ! deg C! |
| ! ! !variation ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.6.1! 27 !Weighting Factor ! 100 ! 100 ! 100 ! 100 ! 100 ! ! |
| ! ! !Wa of TAT ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.7 ! 14 !N2 stable frame ! 0.9 ! 0.9 ! 0.9 ! 0.9 ! 0.9 ! % ! |
| ! ! !variation ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.7.1! 28 !Weighting Factor ! 100 ! 100 ! 100 ! 100 ! 100 ! ! |
| ! ! !Wa of N2 ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.8 ! 15 !EGT stable frame ! 18.0 ! 18.0 ! 18.0 ! 18.0 ! 18.0 ! deg C! |
| ! ! !variation ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.8.1! 29 !Weighting Factor ! 100 ! 100 ! 100 ! 100 ! 100 ! ! |
| ! ! !Wa of EGT ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.9 ! 16 !VACC stable frame! 0.10 ! 0.10 ! 0.10 ! 0.10 ! 0.10 ! g ! |
| ! ! !variation ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.9.1! 30 !Weighting Factor !100 ! 100 ! 100 ! 100 ! 100 ! ! |
| ! ! !Wa of VACC ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.10 ! 17 !MACH stable frame! 0.01 ! 0.01 ! 0.01 ! 0.01 ! 0.01 ! Mach ! |
| ! ! !variation ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| !5.10.1! 31 !Weighting Factor ! 100 ! 100 ! 100 ! 100 ! 100 ! ! |
| ! ! !Wa of MACH ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.11 ! 18 !N1 stable frame ! 1.6 ! 1.6 ! 1.6 ! 1.6 ! 1.6 ! % ! |
| ! ! !variation ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| !5.11.1! 32 !Weighting Factor ! 100 ! 100 ! 100 ! 100 ! 100 ! ! |
| ! ! !Wa of N1 ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.12 ! 19 !PT2 stable frame ! 0.10 ! 0.10 ! 0.10 ! 0.10 ! 0.10 ! psia ! |
| ! ! !variation ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| !5.12.1! 33 !Weighting Factor ! 100 ! 100 ! 100 ! 100 ! 100 ! ! |
| ! ! !Wa of PT2 ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.13 ! 20 !FF stable frame ! 100 ! 100 ! 100 ! 100 ! 100 ! kg/h ! |
| ! ! !variation ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| !5.13.1! 34 !Weighting Factor ! 100 ! 100 ! 100 ! 100 ! 100 ! ! |
| ! ! !Wa of FF ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.14 ! 21 !HPT stable frame ! 10.0 ! 10.0 ! 10.0 ! 10.0 ! 10.0 ! % ! |
| ! ! !variation ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| !5.14.1! 35 !Weighting Factor ! 100 ! 100 ! 100 ! 100 ! 100 ! ! |
| ! ! !Wa of HPT ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.15 ! 22 !LPT stable frame ! 10.0 ! 10.0 ! 10.0 ! 10.0 ! 10.0 ! % ! |
| ! ! !variation ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| !5.15.1! 36 !Weighting Factor ! 100 ! 100 ! 100 ! 100 ! 100 ! ! |
| ! ! !Wa of LPT ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 6.2 ! 7 !Number 'X01' for ! 5 ! 5 ! 5 ! 5 ! 5 ! ! |
| ! ! !consecutive ! ! ! ! ! ! ! |
| ! ! !reports ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 9.1 ! 38 !"NIT.1" stable N1! 62 ! 62 ! 62 ! 62 ! 62 ! %rpm ! |
| ! * ! !value for descent! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 9.2 ! 39 !"X1.1" tolerance !+/-1.5 !+/-1.5 !+/-1.5 !+/-1.5 !+/-1.5 ! % ! |
| ! * ! !band for descent ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 9.3 ! 40 !"T1.1" stable ! 20 ! 20 ! 20 ! 20 ! 20 !second! |
| ! * ! !time observing ! ! ! ! ! ! ! |
| ! ! !for descent ! ! ! ! ! ! ! |
| ! ! !(max. 20 seconds)! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| !10.1 ! 41 !"N1T.1" stable N1! 93 ! 93 ! 93 ! 93 ! 93 ! %rpm ! |
| ! * ! !value for climb ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| !10.2 ! 42 !"X1.1" tolerance !+/-1.5 !+/-1.5 !+/-1.5 !+/-1.5 !+/-1.5 ! % ! |
| ! * ! !band for climb ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| !10.3 ! 43 !"T1.1" stable ! 20 ! 20 ! 20 ! 20 ! 20 !second! |
| ! ! !observing time ! ! ! ! ! ! ! |
| ! * ! !for climb ! ! ! ! ! ! ! |
| ! ! !(max. 20 seconds)! ! ! ! ! ! ! |
| !-----------------------------------------------------------------------------! |
| ! * Remark: Only for Advanced EVMU available ! |
| +-----------------------------------------------------------------------------+ |
(16) A318: CFMI Engine 56-5-B8, 56-5-B9
| +-----------------------------------------------------------------------------+ |
| !Report!Limit! Description of ! CFM ! CFM ! SPARE ! SPARE ! Unit ! |
| !Item !No. ! Report Item !56-5-B8!56-5-B9! ! ! ! |
| ! ! ! !-------!-------!-------!-------!------! |
| ! ! ! !DMU/ID !DMU/ID ! ! ! ! |
| ! ! ! ! C1xxxx! C2xxxx! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.1 ! 4 !"Y01.1" flight hours ! 0 ! 0 ! ! ! hour ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.2 ! 5 !"Y01.2" minutes after ! 10 ! 10 ! ! ! min ! |
| ! ! !cruise entry ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.3 ! 6 !"Y01.1" flight legs ! 1 ! 1 ! ! ! hour ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.1 ! 3 !"P01": stable periods ! 5 ! 5 ! ! ! ! |
| ! ! !(1 period = 20 seconds) ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.2.1! 8 !HPTL1 valve position ! 70 ! 70 ! ! ! % ! |
| ! ! !lower limit ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.2.2! 9 !HPTL2 valve position ! 105 ! 105 ! ! ! % ! |
| ! ! !upper limit ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.3 ! 10 !IALT stable frame ! 150 ! 150 ! ! ! ft ! |
| ! ! !variation ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.3.1! 24 !Weighting Factor Wa of ! 100 ! 100 ! ! ! ! |
| ! ! !IALT ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.4 ! 11 !GS stable frame variation! 6 ! 6 ! ! ! kts ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.4.1! 25 !Weighting Factor Wa of GS! 100 ! 100 ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.5 ! 12 !ROLL ANGLE stable frame ! 4.0 ! 4.0 ! ! ! deg ! |
| ! ! !variation ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.5.1! 26 !Weighting Factor Wa of ! 100 ! 100 ! ! ! ! |
| ! ! !ROLL ANGLE ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.6 ! 13 !TAT stable frame ! 2.0 ! 2.0 ! ! ! deg C! |
| ! ! !variation ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.6.1! 27 !Weighting Factor Wa of ! 100 ! 100 ! ! ! ! |
| ! ! !TAT ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.7 ! 14 !N2 stable frame variation! 0.9 ! 0.9 ! ! ! % ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.7.1! 28 !Weighting Factor Wa of N2! 100 ! 100 ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.8 ! 15 !EGT stable frame ! 18.0 ! 18.0 ! ! ! deg C! |
| ! ! !variation ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.8.1! 29 !Weighting Factor Wa of ! 100 ! 100 ! ! ! ! |
| ! ! !EGT ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.9 ! 16 !VACC stable frame ! 0.10 ! 0.10 ! ! ! g ! |
| ! ! !variation ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.9.1! 30 !Weighting Factor Wa of ! 100 ! 100 ! ! ! ! |
| ! ! !VACC ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.10 ! 17 !MACH stable frame ! 0.010 ! 0.010 ! ! !Mach ! |
| ! ! !variation ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| !5.10.1! 31 !Weighting Factor Wa of ! 100 ! 100 ! ! ! ! |
| ! ! !MACH ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.11 ! 18 !N1 stable frame variation! 1.6 ! 1.6 ! ! ! % ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| !5.11.1! 32 !Weighting Factor Wa of N1! 100 ! 100 ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.12 ! 19 !PT2 stable frame ! 0.10 ! 0.10 ! ! ! psia ! |
| ! ! !variation ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| !5.12.1! 33 !Weighting Factor Wa of ! 100 ! 100 ! ! ! ! |
| ! ! !PT2 ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.13 ! 20 !FF stable frame variation! 100 ! 100 ! ! ! kg/h ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| !5.13.1! 34 !Weighting Factor Wa of FF! 100 ! 100 ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.14 ! 21 !HPT stable frame ! 10.0 ! 10.0 ! ! ! % ! |
| ! ! !variation ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| !5.14.1! 35 !Weighting Factor Wa of ! 100 ! 100 ! ! ! ! |
| ! ! !HPT ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.15 ! 22 !LPT stable frame ! 10.0 ! 10.0 ! ! ! % ! |
| ! ! !variation ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| !5.15.1! 36 !Weighting Factor Wa of ! 100 ! 100 ! ! ! ! |
| ! ! !LPT ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 6.2 ! 7 !Number "X01" for ! 5 ! 5 ! ! ! ! |
| ! ! !consecutive reports ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 9.1 ! 38 !"N1T.1" stable N1 value ! 62 ! 62 ! ! ! %rpm ! |
| ! * ! !for descent ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 9.2 ! 39 !"X1.1" tolerance band for!+/-1.5 !+/-1.5 ! ! ! % ! |
| ! * ! !descent ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 9.3 ! 40 !"T1.1" stable observing ! 20 ! 20 ! ! !second! |
| ! * ! !time for descent ! ! ! ! ! ! |
| ! ! !(max. 20 seconds) ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 10.1 ! 41 !"N1T.1" stable N1 value ! 93 ! 93 ! ! ! %rpm ! |
| ! * ! !for climb ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 10.2 ! 42 !"X1.1" tolerance band for!+/-1.5 !+/-1.5 ! ! ! % ! |
| ! * ! !climb ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 10.3 ! 43 !"T1.1" stable observing ! 20 ! 20 ! ! !second! |
| ! * ! !time for climb ! ! ! ! ! ! |
| ! ! !(max. 20 seconds) ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! * Remark: Only for Advanced EVMU available ! |
| +-----------------------------------------------------------------------------+ |
T. Report Limits for Cruise Performance Report <02>
(1) A320: CFMI Engines 56-5-A1, 56-5-A3, 56-5-B4
| +-----------------------------------------------------------------------------+ |
| !Report! Limit ! Description of Report Item !56-5-A1!56-5-A3!56-5-B4! Unit ! |
| !Item N! No. ! ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.1 ! 54 ! Y02.1: flight hours ! 1 ! 1 ! 1 ! hours! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.2 ! 55 ! Y02.2: flight legs ! 1 ! 1 ! 1 ! legs ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.3 ! 53 ! 'P02' stable periods ! 5 ! 5 ! 5 ! ! |
| ! ! ! (1 period = 20 seconds) ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.4.1! 56 ! HPTL1 valve position lower ! 0 ! 0 ! 70 ! % ! |
| ! ! ! limit ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.4.2! 57 ! HPTL2 valve position upper ! 20 ! 20 ! 100 ! % ! |
| ! ! ! limit ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.5 ! 58 ! IALT stable frame variation ! 150 ! 150 ! 150 ! feet ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.5.1! 72 ! Weighting Factor Wa of IALT ! 1 ! 1 ! 1 ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.6 ! 59 ! GS stable frame variation ! 6 ! 6 ! 6 ! kts ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.6.1! 73 ! Weighting Factor Wa of GS ! 1 ! 1 ! 1 ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.7 ! 60 ! ROLL stable frame variation ! .8 ! .8 ! .8 ! deg ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.7.1! 74 ! Weighting Factor Wa of ROLL ! 1 ! 1 ! 1 ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.8 ! 61 ! TAT stable frame variation ! 1.1 ! 1.1 ! 1.1 ! deg C! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.8.1! 75 ! Weighting Factor Wa of TAT ! 1 ! 1 ! 1 ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.9 ! 62 ! N2 stable frame variation ! .9 ! .9 ! .9 ! % ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.9.1! 76 ! Weighting Factor Wa of N2 ! 1 ! 1 ! 1 ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.10 ! 63 ! EGT stable frame variation ! 18 ! 18 ! 18 ! deg C! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| !5.10.1! 77 ! Weighting Factor Wa of EGT ! 1 ! 1 ! 1 ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.11 ! 64 ! VACC stable frame variation ! .03 ! .03 ! .03 ! g ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| !5.11.1! 78 ! Weighting Factor Wa of VACC ! 1 ! 1 ! 1 ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.12 ! 65 ! MACH stable frame variation ! .008! .008! .008! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| !5.12.1! 79 ! Weighting Factor Wa of MACH ! 1 ! 1 ! 1 ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.13 ! 66 ! N1 stable frame variation ! 1.6 ! 1.6 ! 1.6 ! % ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| !5.13.1! 80 ! Weighting Factor Wa of N1 ! 1 ! 1 ! 1 ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.14 ! 67 ! PT2 stable frame variation ! .05 ! .05 ! .05 ! psia ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| !5.14.1! 81 ! Weighting Factor Wa of PT2 ! 1 ! 1 ! 1 ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.15 ! 68 ! FF stable frame variation ! 100 ! 100 ! 100 ! kg/h ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| !5.15.1! 82 ! Weighting Factor Wa of FF ! 1 ! 1 ! 1 ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.16 ! 69 ! HPT stable frame variation ! 8 ! 8 ! 10 ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| !5.16.1! 83 ! Weighting Factor Wa of HPT ! 1 ! 1 ! 1 ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.17 ! 70 ! LPT stable frame variation ! 10 ! 10 ! 10 ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| !5.17.1! 84 ! Weighting Factor Wa of LPT ! 1 ! 1 ! 1 ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 6.1 ! 86 ! 'NIT.1' stable N1 value for ! 62 ! 62 ! 62 ! %rpm ! |
| ! * ! ! descent ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 6.2 ! 87 ! 'X1.1' tolerance band for !+/-1.5 !+/-1.5 !+/-1.5 ! % ! |
| ! * ! ! descent ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 6.3 ! 88 ! 'T1.1' stable observing time ! 20 ! 20 ! 20 !second! |
| ! * ! ! for descent (max. 20 seconds) ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 7.1 ! 89 ! 'NIT.2' stable N1 value for ! 93 ! 93 ! 93 ! %rpm ! |
| ! * ! ! take off ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 7.2 ! ! 'X1.2' tolerance band for !+/-1.5 !+/-1.5 !+/-1.5 ! % ! |
| ! * ! ! take off ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 7.3 ! ! 'T1.2' stable observing time ! 20 ! 20 ! 20 !second! |
| ! * ! ! for take off (max. 20 seconds)! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! * Remark: Only for Advanced EVMU available ! |
| +-----------------------------------------------------------------------------+ |
(2) A321: CFMI Engines 56-5-B1, 56-5-B2, 56-5-B3
| +-----------------------------------------------------------------------------+ |
| !Report! Limit ! Description of Report Item !56-5-B1!56-5-B2!56-5-B3! Unit ! |
| !Item N! ! ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.1 ! 54 ! Y02.1: flight hours ! 1 ! 1 ! 1 ! hours! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.2 ! 55 ! Y02.2: flight legs ! 1 ! 1 ! 1 ! legs ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.3 ! 53 ! 'P02' stable periods ! 5 ! 5 ! 5 ! ! |
| ! ! ! (1 period = 20 seconds) ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.4.1! 56 ! HPTL1 valve position lower ! 70 ! 70 ! 70 ! % ! |
| ! ! ! limit ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.4.2! 57 ! HPTL2 valve position upper ! 100 ! 100 ! 100 ! % ! |
| ! ! ! limit ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.5 ! 58 ! IALT stable frame variation ! 150 ! 150 ! 150 ! feet ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.5.1! 72 ! Weighting Factor Wa of IALT ! 1 ! 1 ! 1 ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.6 ! 59 ! GS stable frame variation ! 6 ! 6 ! 6 ! kts ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.6.1! 73 ! Weighting Factor Wa of GS ! 1 ! 1 ! 1 ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.7 ! 60 ! ROLL stable frame variation ! .8 ! .8 ! .8 ! deg ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.7.1! 74 ! Weighting Factor Wa of ROLL ! 1 ! 1 ! 1 ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.8 ! 61 ! TAT stable frame variation ! 1.1 ! 1.1 ! 1.1 ! deg C! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.8.1! 75 ! Weighting Factor Wa of TAT ! 1 ! 1 ! 1 ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.9 ! 62 ! N2 stable frame variation ! .9 ! .9 ! .9 ! % ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.9.1! 76 ! Weighting Factor Wa of N2 ! 1 ! 1 ! 1 ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.10 ! 63 ! EGT stable frame variation ! 18 ! 18 ! 18 ! deg C! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| !5.10.1! 77 ! Weighting Factor Wa of EGT ! 1 ! 1 ! 1 ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.11 ! 64 ! VACC stable frame variation ! .03 ! .03 ! .03 ! g ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| !5.11.1! 78 ! Weighting Factor Wa of VACC ! 1 ! 1 ! 1 ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.12 ! 65 ! MACH stable frame variation ! .008! .008! .008! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| !5.12.1! 79 ! Weighting Factor Wa of MACH ! 1 ! 1 ! 1 ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.13 ! 66 ! N1 stable frame variation ! 1.6 ! 1.6 ! 1.6 ! % ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| !5.13.1! 80 ! Weighting Factor Wa of N1 ! 1 ! 1 ! 1 ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.14 ! 67 ! PT2 stable frame variation ! .05 ! .05 ! .05 ! psia ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| !5.14.1! 81 ! Weighting Factor Wa of PT2 ! 1 ! 1 ! 1 ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.15 ! 68 ! FF stable frame variation ! 100 ! 100 ! 100 ! kg/h ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| !5.15.1! 82 ! Weighting Factor Wa of FF ! 1 ! 1 ! 1 ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.16 ! 69 ! HPT stable frame variation ! 10 ! 10 ! 10 ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| !5.16.1! 83 ! Weighting Factor Wa of HPT ! 1 ! 1 ! 1 ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.17 ! 70 ! LPT stable frame variation ! 10 ! 10 ! 10 ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| !5.17.1! 84 ! Weighting Factor Wa of LPT ! 1 ! 1 ! 1 ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 6.1 ! 86 ! 'NIT.1' stable N1 value for ! 62 ! 62 ! 62 ! %rpm ! |
| ! * ! ! descent ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 6.2 ! 87 ! 'X1.1' tolerance band for !+/-1.5 !+/-1.5 !+/-1.5 ! % ! |
| ! * ! ! descent ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 6.3 ! 88 ! 'T1.1' stable observing time ! 20 ! 20 ! 20 !second! |
| ! * ! ! for descent (max. 20 seconds) ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 7.1 ! ! 'NIT.2' stable N1 value for ! 93 ! 93 ! 93 ! %rpm ! |
| ! * ! ! take off ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 7.2 ! ! 'X1.2' tolerance band for !+/-1.5 !+/-1.5 !+/-1.5 ! % ! |
| ! * ! ! take off ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 7.3 ! ! 'T1.2' stable observing time ! 20 ! 20 ! 20 !second! |
| ! * ! ! for take off (max. 20 seconds)! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! * Remark: Only for Advanced EVMU available ! |
| +-----------------------------------------------------------------------------+ |
(3) A319: CFMI Engines 56-5-A5, 56-5-B6, 56-5-B5, 56-5A4
| +-----------------------------------------------------------------------------+ |
| !Report! Limit ! Description of !56-5-A5!56-5-B6!56-5-B5!56-5A4! Unit ! |
| !Item N! No. ! Report Item ! ! ! ! ! ! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! 4.3 ! 55 ! Y02.1: flight legs ! 1 ! 1 ! 1 ! 1 ! legs ! |
| ! ! ! (0=inhibit logic) ! ! ! ! ! ! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! 4.6.1! 56 ! HPTL1 valve position ! 0 ! 70 ! 70 ! 0 ! % ! |
| ! ! ! lower limit ! ! ! ! ! ! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! 4.6.2! 57 ! HPTL2 valve position ! 20 ! 100 ! 100 ! 20 ! % ! |
| ! ! ! upper limit ! ! ! ! ! ! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! 4.7 ! 53 ! 'P02' stable frame ! 5 ! 5 ! 5 ! 5 ! ! |
| ! ! ! variation (1 period = ! ! ! ! ! ! |
| ! ! ! 20 seconds) ! ! ! ! ! ! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! 4.8 ! 58 ! IALT stable frame ! 150 ! 150 ! 150 ! 150 ! feet ! |
| ! ! ! variation ! ! ! ! ! ! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! W.1 ! 72 ! Weighting Factor Wa ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! ! of IALT ! ! ! ! ! ! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! 4.9 ! 59 ! GS stable frame ! 6 ! 6 ! 6 ! 6 ! kts ! |
| ! ! ! variation ! ! ! ! ! ! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! W.2 ! 73 ! Weighting Factor Wa ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! ! of GS ! ! ! ! ! ! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! 4.10 ! 60 ! ROLL stable frame ! .8 ! .8 ! .8 ! .8 ! deg ! |
| ! ! ! variation ! ! ! ! ! ! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! W.3 ! 74 ! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! ! of ROLL ! ! ! ! ! ! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! 4.11 ! 61 ! TAT stable frame ! 1.1 ! 1.1 ! 1.1 ! 1.1 ! deg C! |
| ! ! ! variation ! ! ! ! ! ! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! W.4 ! 75 ! Weighting Factor Wa ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! ! of TAT ! ! ! ! ! ! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! 4.12 ! 62 ! N2 stable frame ! .9 ! .9 ! .9 ! .9 ! % ! |
| ! ! ! variation ! ! ! ! ! ! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! W.5 ! 76 ! Weighting Factor Wa ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! ! of N2 ! ! ! ! ! ! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! 4.13 ! 63 ! EGT stable frame ! 18 ! 18 ! 18 ! 18 ! deg C! |
| ! ! ! variation ! ! ! ! ! ! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! W.6 ! 77 ! Weighting Factor Wa ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! ! of EGT ! ! ! ! ! ! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! 4.14 ! 64 ! VACC stable frame ! .03 ! .03 ! .03 ! .03 ! g ! |
| ! ! ! variation ! ! ! ! ! ! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! W.7 ! 78 ! Weighting Factor Wa ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! ! of VACC ! ! ! ! ! ! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! 4.15 ! 65 ! MACH stable frame ! ! ! ! ! ! |
| ! ! ! variation ! ! ! ! ! ! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! W.8 ! 79 ! Weighting Factor Wa ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! ! of MACH ! ! ! ! ! ! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! 4.16 ! 66 ! N1 stable frame ! 1.6 ! 1.6 ! 1.6 ! 1.6 ! % ! |
| ! ! ! variation ! ! ! ! ! ! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! W.9 ! 80 ! Weighting Factor Wa ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! ! of N1 ! ! ! ! ! ! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! 4.17 ! 67 ! PT2 stable frame ! .05 ! .05 ! .05 ! .05 ! psia ! |
| ! ! ! variation ! ! ! ! ! ! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! W.10 ! 81 ! Weighting Factor Wa ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! ! of PT2 ! ! ! ! ! ! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! 4.18 ! 68 ! FF stable frame ! 100 ! 100 ! 100 ! 100 ! kg/h ! |
| ! ! ! variation ! ! ! ! ! ! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! W.11 ! 82 ! Weighting Factor Wa ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! ! of FF ! ! ! ! ! ! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! 4.19 ! 69 ! HPT stable frame ! 10 ! 10 ! 10 ! 10 ! ! |
| ! ! ! variation ! ! ! ! ! ! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! W.12 ! 83 ! Weighting Factor Wa ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! ! of HPT ! ! ! ! ! ! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! 4.20 ! 70 ! LPT stable frame ! 10 ! 10 ! 10 ! 10 ! ! |
| ! ! ! variation ! ! ! ! ! ! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! W.13 ! 84 ! Weighting Factor Wa ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! ! of LPT ! ! ! ! ! ! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! 5.1 ! 86 ! 'NIT.1' stable N1 ! 62 ! 62 ! 62 ! 62 ! %rpm ! |
| ! * ! ! value for descent ! ! ! ! ! ! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! 5.2 ! 87 ! 'X1.1' tolerance !+/-1.5 !+/-1.5 !+/-1.5 !+/-1.5! % ! |
| ! * ! ! band for descent ! ! ! ! ! ! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! 5.3 ! 88 ! 'T1.1' stable obser- ! 20 ! 20 ! 20 ! 20 !second! |
| ! * ! ! ving time for descent ! ! ! ! ! ! |
| ! ! ! (max. 20 seconds) ! ! ! ! ! ! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! 6.1 ! ! 'NIT.2' stable N1 ! 93 ! 93 ! 93 ! 93 ! %rpm ! |
| ! * ! ! value for take off ! ! ! ! ! ! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! 6.2 ! ! 'X1.2' tolerance band !+/-1.5 !+/-1.5 !+/-1.5 !+/-1.5! % ! |
| ! * ! ! for take off ! ! ! ! ! ! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! 6.3 ! ! 'T1.2' stable obser- ! 20 ! 20 ! 20 ! 20 !second! |
| ! * ! ! ving time for take off ! ! ! ! ! ! |
| ! ! ! (max. 20 seconds) ! ! ! ! ! ! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! * Remark: Only for Advanced EVMU available ! |
| +-----------------------------------------------------------------------------+ |
(4) A319: CFMI Engines 56-5-B7
| +-----------------------------------------------------------------------------+ |
| !Report! Limit ! Desccription of Report Item !56-5-B7! SPARE ! SPARE ! Unit ! |
| !Item N! No. ! ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.3 ! 54 ! Y02.1: flight legs ! 1 ! ! ! legs ! |
| ! ! ! (0=inhibit logic) ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.6.1! 56 ! HPTL1 valve position lower ! 70 ! ! ! % ! |
| ! ! ! limit ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.6.2! 57 ! HPTL2 valve position upper ! 100 ! ! ! % ! |
| ! ! ! limit ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.7 ! 53 ! 'P02' stable frame variation ! 5 ! ! ! ! |
| ! ! ! (1 periods = 20 seconds) ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.8 ! 58 ! IALT stable frame variation ! 150 ! ! ! feet ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! W.1 ! 72 ! Weighting Factor Wa of IALT ! 1 ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.9 ! 59 ! GS stable frame variation ! 6 ! ! ! kts ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! W.2 ! 73 ! Weighting Factor Wa of GS ! 1 ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.10 ! 60 ! ROLL stable frame variation ! .8 ! ! ! deg ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! W.3 ! 74 ! Weighting Factor Wa of ROLL ! 1 ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.11 ! 61 ! TAT stable frame variation ! 1.1 ! ! ! deg C! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! W.4 ! 75 ! Weighting Factor Wa of TAT ! 1 ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.12 ! 62 ! N2 stable frame variation ! .9 ! ! ! % ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! W.5 ! 76 ! Weighting Factor Wa of N2 ! 1 ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.13 ! 63 ! EGT stable frame variation ! 18 ! ! ! deg C! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! W.6 ! 77 ! Weighting Factor Wa of EGT ! 1 ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.14 ! 64 ! VACC stable frame variation ! .03 ! ! ! g ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! W.7 ! 78 ! Weighting Factor Wa of VACC ! 1 ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.15 ! 65 ! MACH stable frame variation ! .008! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! W.8 ! 79 ! Weighting Factor Wa of MACH ! 1 ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.16 ! 66 ! N1 stable frame variation ! 1.6 ! ! ! % ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! W.9 ! 80 ! Weighting Factor Wa of N1 ! 1 ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.17 ! 67 ! PT2 stable frame variation ! .05 ! ! ! psia ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! W.10 ! 81 ! Weighting Factor Wa of PT2 ! 1 ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.18 ! 68 ! FF stable frame variation ! 100 ! ! ! kg/h ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! W.11 ! 82 ! Weighting Factor Wa of FF ! 1 ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.19 ! 69 ! HPT stable frame variation ! 10 ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! W.12 ! 83 ! Weighting Factor Wa of HPT ! 1 ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.20 ! 70 ! LPT stable frame variation ! 10 ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! W.13 ! 84 ! Weighting Factor Wa of LPT ! 1 ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.1 ! 86 ! 'NIT.1' stable N1 value for ! 62 ! ! ! %rpm ! |
| ! * ! ! descent ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.2 ! 87 ! 'X1.1' tolerance band for !+/-1.5 ! ! ! % ! |
| ! * ! ! descent ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.3 ! 88 ! 'T1.1' stable observing time ! 20 ! ! !second! |
| ! * ! ! for descent (max. 20 seconds) ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 6.1 ! ! 'NIT.2' stable N1 value for ! 93 ! ! ! %rpm ! |
| ! * ! ! take off ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 6.2 ! ! 'X1.2' tolerance band for !+/-1.5 ! ! ! % ! |
| ! * ! ! take off ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 6.3 ! ! 'T1.2' stable observing time ! 20 ! ! !second! |
| ! * ! ! for take off (max. 20 seconds)! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! * Remark: Only for Advanced EVMU available ! |
| +-----------------------------------------------------------------------------+ |
(5) A320: CFMI Engines 56-5-A1, 56-5-A3, 56-5-B4, 56-5-B5, 56-5-B6
| +----------------------------------------------------------------------------+ |
| !Report! Description of ! CFM ! CFM ! CFM ! CFM ! CFM ! Unit ! |
| !Item ! Report Item !56-5-A1!56-5-A3!56-5-B4!56-5-B5!56-5-B6! ! |
| ! ! !-------!-------!-------!-------!-------!------! |
| ! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! ! |
| ! ! ! CFM #1! CFM #2! CFM #3! CFM #4! CFM #8! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.1 !'Y01.1' flight hours ! 1 ! 1 ! 1 ! 1 ! 1 ! hours! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.2 !'Y01.3' flight legs ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.3 !'P01' stable periods ! 5 ! 5 ! 5 ! 5 ! 5 ! ! |
| ! ! ( 1 period = 20 sec) ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.4.1! HPTL1 valve position ! 0 ! 0 ! 70 ! 70 ! 70 ! % ! |
| ! ! lower limit ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.4.2! HPTL2 valve position ! 20 ! 20 ! 105 ! 105 ! 105 ! % ! |
| ! ! upper limit ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.5 ! IALT stable frame ! 150 ! 150 ! 150 ! 150 ! 150 ! ft ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.5.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of IALT ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.6 ! GS stable frame ! 6 ! 6 ! 6 ! 6 ! 6 ! kts ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.6.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of GS ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.7 ! ROLL ANGLE stable ! 0.8 ! 0.8 ! 0.8 ! 0.8 ! 0.8 ! deg ! |
| ! ! frame variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.7.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of ROLL ANGLE ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.8 ! TAT stable frame ! 1.1 ! 1.1 ! 1.1 ! 1.1 ! 1.1 ! deg C! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.8.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of TAT ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.9 ! N2 stable frame ! 0.9 ! 0.9 ! 0.9 ! 0.9 ! 0.9 ! % ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.9.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of N2 ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.10 ! EGT stable frame ! 18.0 ! 18.0 ! 18.0 ! 18.0 ! 18.0 ! deg C! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| !5.10.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of EGT ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.11 ! VACC stable frame ! 0.03 ! 0.03 ! 0.03 ! 0.03 ! 0.03 ! g ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| !5.11.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of VACC ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.12 ! MN stable frame ! 0.008 ! 0.008 ! 0.008 ! 0.008 ! 0.008 ! Mach ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| !5.12.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of MN ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.13 ! N1 stable frame ! 1.6 ! 1.6 ! 1.6 ! 1.6 ! 1.6 ! % ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| !5.13.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of N1 ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.14 ! PT2 stable frame ! 0.05 ! 0.05 ! 0.05 ! 0.05 ! 0.05 ! psia ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| !5.14.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of PT2 ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.15 ! FF stable frame ! 100 ! 100 ! 100 ! 100 ! 100 ! kg/h ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| !5.15.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of FF ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.16 ! HPT stable frame ! 10.0 ! 10.0 ! 10.0 ! 10.0 ! 10.0 ! % ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| !5.16.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of HPT ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.17 ! LPT stable frame ! 10.0 ! 10.0 ! 10.0 ! 10.0 ! 10.0 ! % ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| !5.17.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of LPT ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 6.1 ! 'NIT.1' stable N1 ! 62 ! 62 ! 62 ! 62 ! 62 ! % ! |
| ! * ! value for descent ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 6.2 ! 'X1.1' tolerance !+/-1.5 !+/-1.5 !+/-1.5 !+/-1.5 !+/-1.5 ! % ! |
| ! * ! band for descent ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 6.3 !'T1.1' stable observing! 20 ! 20 ! 20 ! 20 ! 20 !second! |
| ! * ! time for descent ! ! ! ! ! ! ! |
| ! ! (max. 20 seconds) ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 7.1 ! 'N1T.2' stable N1 ! 93 ! 93 ! 93 ! 93 ! 93 ! % ! |
| ! * ! value for take off ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 7.2 ! 'X1.2' rpm tolerance !+/-1.5 !+/-1.5 !+/-1.5 !+/-1.5 !+/-1.5 ! % ! |
| ! * ! band for take off ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| !10.3 !'T1.2' stable observing! 20 ! 20 ! 20 ! 20 ! 20 !second! |
| ! * ! time for take off ! ! ! ! ! ! ! |
| ! ! (max. 20 seconds) ! ! ! ! ! ! ! |
| !-----------------------------------------------------------------------------! |
| ! * Remark: Only for Advanced EVMU available ! |
| +-----------------------------------------------------------------------------+ |
(6) A321: CFMI Engines 56-5-B1, 56-5-B2, 56-5-B3, 56-5-B4
| +-----------------------------------------------------------------------------+ |
| !Report! Description of Report Item ! CFM ! CFM ! CFM ! CFM ! Unit ! |
| !Item ! !56-5-B1!56-5-B2!56-5-B3!56-5-B4! ! |
| ! ! !-------!-------!-------!-------!------! |
| ! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! ! |
| ! ! ! CFM #5! CFM #6! CFM #7! CFM #3! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.1 !'Y02.1' flight hours ! 1 ! 1 ! 1 ! 1 ! hours! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.2 !'Y02.2' flight legs ! 1 ! 1 ! 1 ! 1 ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.3 !'P02' stable periods ! 5 ! 5 ! 5 ! 5 ! ! |
| ! ! (1 period = 20 seconds) ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.4.1! HPTL1 valve position lower ! 70 ! 70 ! 70 ! 70 ! % ! |
| ! ! limit ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.4.2! HPTL2 valve position upper ! 105 ! 105 ! 105 ! 105 ! % ! |
| ! ! limit ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.5 ! IALT stable frame variation ! 150 ! 150 ! 150 ! 150 ! ft ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.5.1! Weighting Factor Wa of IALT ! 1 ! 1 ! 1 ! 1 ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.6 ! GS stable frame variation ! 6 ! 6 ! 6 ! 6 ! kts ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.6.1! Weighting Factor Wa of GS ! 1 ! 1 ! 1 ! 1 ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.7 ! ROLL ANGLE stable frame ! 0.8 ! 0.8 ! 0.8 ! 0.8 ! deg ! |
| ! ! variation ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.7.1! Weighting Factor Wa of ROLL ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! ANGLE ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.8 ! TAT stable frame variation ! 1.1 ! 1.1 ! 1.1 ! 1.1 ! deg C! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.8.1! Weighting Factor Wa of TAT ! 1 ! 1 ! 1 ! 1 ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.9 ! N2 stable frame variation ! 0.9 ! 0.9 ! 0.9 ! 0.9 ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.9.1! Weighting Factor Wa of N2 ! 1 ! 1 ! 1 ! 1 ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.10 ! EGT stable frame variation ! 18.0 ! 18.0 ! 18.0 ! 18.0 ! deg C! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !5.10.1! Weighting Factor Wa of EGT ! 1 ! 1 ! 1 ! 1 ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.11 ! VACC stable frame variation ! 0.03 ! 0.03 ! 0.03 ! 0.03 ! g ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !5.11.1! Weighting Factor Wa of VACC ! 1 ! 1 ! 1 ! 1 ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.12 ! MN stable frame variation ! 0.008 ! 0.008 ! 0.008 ! 0.008 !Mach ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !5.12.1! Weighting Factor Wa of MN ! 1 ! 1 ! 1 ! 1 ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.13 ! N1 stable frame variation ! 1.6 ! 1.6 ! 1.6 ! 1.6 ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !5.13.1! Weighting Factor Wa of N1 ! 1 ! 1 ! 1 ! 1 ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.14 ! PT2 stable frame variation ! 0.05 ! 0.05 ! 0.05 ! 0.05 ! psia ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !5.14.1! Weighting Factor Wa of PT2 ! 1 ! 1 ! 1 ! 1 ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.15 ! FF stable frame variation ! 100 ! 100 ! 100 ! 100 ! kg/h ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !5.15.1! Weighting Factor Wa of FF ! 1 ! 1 ! 1 ! 1 ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.16 ! HPT stable frame variation ! 10.0 ! 10.0 ! 10.0 ! 10.0 ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !5.16.1! Weighting Factor Wa of HPT ! 1 ! 1 ! 1 ! 1 ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.17 ! LPT stable frame variation ! 10.0 ! 10.0 ! 10.0 ! 10.0 ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !5.17.1! Weighting Factor Wa of LPT ! 1 ! 1 ! 1 ! 1 ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 6.1 ! 'NIT.1' stable N1 value for ! 62 ! 62 ! 62 ! 62 ! % ! |
| ! * ! descent ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 6.2 ! 'X1.1' tolerance band for !+/-1.5 !+/-1.5 !+/-1.5 !+/-1.5 ! % ! |
| ! * ! descent ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 6.3 ! 'T1.1' stable observing time ! 20 ! 20 ! 20 ! 20 !second! |
| ! * ! for descent (max. 20 seconds) ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 7.1 ! 'N1T.2' stable N1 value for ! 93 ! 93 ! 93 ! 93 ! %rpm ! |
| ! * ! take off ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 7.2 ! 'X1.2' rpm tolerance band for !+/-1.5 !+/-1.5 !+/-1.5 !+/-1.5 ! % ! |
| ! * ! take off ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 7.3 ! 'T1.2' stable observing time ! 20 ! 20 ! 20 ! 20 !second! |
| ! * ! for take off (max. 20 seconds)! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! * Remark: Only for Advanced EVMU available ! |
| +-----------------------------------------------------------------------------+ |
(7) A319: CFMI Engines 56-5-A5, 56-5-B6, 56-5-B5, 56-5-A4, 56-5-B7
| +----------------------------------------------------------------------------+ |
| !Report! Description of ! CFM ! CFM ! CFM ! CFM ! CFM ! Unit ! |
| !Item ! Report Item !56-5-A5!56-5-B6!56-5-B5!56-5-A4!56-5-B7! ! |
| ! ! !-------!-------!-------!-------!-------!------! |
| ! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! ! |
| ! ! ! C7xxx ! C8xxxx! C4xxxx! C6xxxx! C5xxxx! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.1 !'Y02.1' flight hours ! 1 ! 1 ! 1 ! 1 ! 1 ! hours! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.2 !'Y02.2' flight legs ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.3 !'P02' stable periods ! 5 ! 5 ! 5 ! 5 ! 5 ! ! |
| ! ! ( 1 period = 20 sec) ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.4.1! HPTL1 valve position ! 0 ! 70 ! 70 ! 0 ! 70 ! % ! |
| ! ! lower limit ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.4.2! HPTL2 valve position ! 20 ! 105 ! 105 ! 20 ! 105 ! % ! |
| ! ! upper limit ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.5 ! IALT stable frame ! 150 ! 150 ! 150 ! 150 ! 150 ! ft ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.5.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of IALT ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.6 ! GS stable frame ! 6 ! 6 ! 6 ! 6 ! 6 ! kts ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.6.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of GS ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.7 ! ROLL ANGLE stable ! 0.8 ! 0.8 ! 0.8 ! 0.8 ! 0.8 ! deg ! |
| ! ! frame variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.7.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of ROLL ANGLE ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.8 ! TAT stable frame ! 1.1 ! 1.1 ! 1.1 ! 1.1 ! 1.1 ! deg C! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.8.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of TAT ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.9 ! N2 stable frame ! 0.9 ! 0.9 ! 0.9 ! 0.9 ! 0.9 ! % ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.9.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of N2 ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.10 ! EGT stable frame ! 18.0 ! 18.0 ! 18.0 ! 18.0 ! 18.0 ! deg C! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| !5.10.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of EGT ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.11 ! VACC stable frame ! 0.03 ! 0.03 ! 0.03 ! 0.03 ! 0.03 ! g ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| !5.11.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of VACC ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.12 ! MN stable frame ! 0.008 ! 0.008 ! 0.008 ! 0.008 ! 0.008 ! Mach ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| !5.12.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of MN ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.13 ! N1 stable frame ! 1.6 ! 1.6 ! 1.6 ! 1.6 ! 1.6 ! % ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| !5.13.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of N1 ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.14 ! PT2 stable frame ! 0.05 ! 0.05 ! 0.05 ! 0.05 ! 0.05 ! psia ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| !5.14.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of PT2 ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.15 ! FF stable frame ! 100 ! 100 ! 100 ! 100 ! 100 ! kg/h ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| !5.15.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of FF ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.16 ! HPT stable frame ! 10.0 ! 10.0 ! 10.0 ! 10.0 ! 10.0 ! % ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| !5.16.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of HPT ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.17 ! LPT stable frame ! 10.0 ! 10.0 ! 10.0 ! 10.0 ! 10.0 ! % ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| !5.17.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of LPT ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 6.1 ! 'NIT.1' stable N1 ! 62 ! 62 ! 62 ! 62 ! 62 ! % ! |
| ! * ! value for descent ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 6.2 ! 'X1.1' tolerance !+/-1.5 !+/-1.5 !+/-1.5 !+/-1.5 !+/-1.5 ! % ! |
| ! * ! band for descent ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 6.3 !'T1.1' stable observing! 20 ! 20 ! 20 ! 20 ! 20 !second! |
| ! * ! time for descent ! ! ! ! ! ! ! |
| ! ! (max. 20 seconds) ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 7.1 ! 'N1T.1' stable N1 ! 93 ! 93 ! 93 ! 93 ! 93 ! %rpm ! |
| ! * ! value for take off ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 7.2 ! 'X1.2' rpm tolerance !+/-1.5 !+/-1.5 !+/-1.5 !+/-1.5 !+/-1.5 ! % ! |
| ! * ! band for take off ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 7.3 !'T1.2' stable observing! 20 ! 20 ! 20 ! 20 ! 20 !second! |
| ! * ! time for take off ! ! ! ! ! ! ! |
| ! ! (max. 20 seconds) ! ! ! ! ! ! ! |
| !-----------------------------------------------------------------------------! |
| ! * Remark: Only for Advanced EVMU available ! |
| +-----------------------------------------------------------------------------+ |
(8) A318: CFMI Engine 56-5-B8, 56-5-B9
| +-----------------------------------------------------------------------------+ |
| !Report! Description of Report Item ! CFM ! CFM ! SPARE ! SPARE ! Unit ! |
| !Item ! !56-5-B8!56-5-B9! ! ! ! |
| ! ! !-------!-------!-------!-------!------! |
| ! ! !DMU/ID !DMU/ID ! ! ! ! |
| ! ! !C1xxxxx! C2xxxx! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.1 !'Y02.1' flight hours ! 1 ! 1 ! ! ! hour ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.2 !'Y02.2' flight legs ! 1 ! 1 ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.3 !'P02': stable periods ! 5 ! 5 ! ! ! ! |
| ! ! (1 period = 20 seconds) ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.4.1! HPTL1 valve position lower ! 70 ! 70 ! ! ! % ! |
| ! ! limit ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.4.2! HPTL2 valve position upper ! 105 ! 105 ! ! ! % ! |
| ! ! limit ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.5 ! IALT stable frame variation ! 150 ! 150 ! ! ! ft ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.5.1! Weighting Factor Wa of IALT ! 1 ! 1 ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.6 ! GS stable frame variation ! 6 ! 6 ! ! ! kts ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.6.1! Weighting Factor Wa of GS ! 1 ! 1 ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.7 ! ROLL ANGLE stable frame ! 0.8 ! 0.8 ! ! ! deg ! |
| ! ! variation ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.7.1! Weighting Factor Wa of ROLL ! 1 ! 1 ! ! ! ! |
| ! ! ANGLE ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.8 ! TAT stable frame variation ! 1.1 ! 1.1 ! ! ! deg C! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.8.1! Weighting Factor Wa of TAT ! 1 ! 1 ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.9 ! N2 stable frame variation ! 0.9 ! 0.9 ! ! ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.9.1! Weighting Factor Wa of N2 ! 1 ! 1 ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.10 ! EGT stable frame variation ! 18.0 ! 18.0 ! ! ! deg C! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !5.10.1! Weighting Factor Wa of EGT ! 1 ! 1 ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.11 ! VACC stable frame variation ! 0.03 ! 0.03 ! ! ! g ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !5.11.1! Weighting Factor Wa of VACC ! 1 ! 1 ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.12 ! MN stable frame variation ! 0.008 ! 0.008 ! ! ! Mach ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !5.12.1! Weighting Factor Wa of MN ! 1 ! 1 ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.13 ! N1 stable frame variation ! 1.6 ! 1.6 ! ! ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !5.13.1! Weighting Factor Wa of N1 ! 1 ! 1 ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.14 ! PT2 stable frame variation ! 0.05 ! 0.05 ! ! ! psia ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !5.14.1! Weighting Factor Wa of PT2 ! 1 ! 1 ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.15 ! FF stable frame variation ! 100 ! 100 ! ! ! kg/h ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !5.15.1! Weighting Factor Wa of FF ! 1 ! 1 ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.16 ! HPT stable frame variation ! 10.0 ! 10.0 ! ! ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !5.16.1! Weighting Factor Wa of HPT ! 1 ! 1 ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.17 ! LPT stable frame variation ! 10.0 ! 10.0 ! ! ! 5 ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !5.17.1! Weighting Factor Wa of LPT ! 1 ! 1 ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 6.1 ! 'N1T.1' stable N1 value for ! 62 ! 62 ! ! ! %rpm ! |
| ! * ! descent ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 6.2 ! 'X1.1' tolerance band for !+/-1.5 !+/-1.5 ! ! ! % ! |
| ! * ! descent ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 6.3 ! 'T1.1' stable observing time ! 20 ! 20 ! ! !second! |
| ! * ! for descent (max. 20 seconds) ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 7.1 ! 'N1T.2' stable N1 value for ! 93 ! 93 ! ! ! %rpm ! |
| ! * ! take off ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 7.2 ! 'X1.2' rpm tolerance band for !+/-1.5 !+/-1.5 ! ! ! % ! |
| ! * ! take off ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 7.3 ! 'T1.2' stable observing time ! 20 ! 20 ! ! !second! |
| ! * ! for take off (max. 20 seconds)! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! * Remark: Only for Advanced EVMU available ! |
| +-----------------------------------------------------------------------------+ |
(9) A320: CFMI Engines 56-5-A1, 56-5-A3, 56-5-B4, 56-5-B5, 56-5-B6
| +----------------------------------------------------------------------------+ |
| !Report! Description of ! CFM ! CFM ! CFM ! CFM ! CFM ! Unit ! |
| !Item ! Report Item !56-5-A1!56-5-A3!56-5-B4!56-5-B5!56-5-B6! ! |
| ! ! !-------!-------!-------!-------!-------!------! |
| ! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! ! |
| ! ! ! CFM #1! CFM #2! CFM #3! CFM #4! CFM #8! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.1 !'Y02.1' flight hours ! 1 ! 1 ! 1 ! 1 ! 1 ! hours! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.2 !'Y02.2' flight legs ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.3 !'P02' stable periods ! 5 ! 5 ! 5 ! 5 ! 5 ! ! |
| ! ! ( 1 period = 20 sec) ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.4.1! HPTL1 valve position ! 0 ! 0 ! 70 ! 70 ! 70 ! % ! |
| ! ! lower limit ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.4.2! HPTL2 valve position ! 20 ! 20 ! 105 ! 105 ! 105 ! % ! |
| ! ! upper limit ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.5 ! IALT stable frame ! 150 ! 150 ! 150 ! 150 ! 150 ! ft ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.5.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of IALT ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.6 ! GS stable frame ! 6 ! 6 ! 6 ! 6 ! 6 ! kts ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.6.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of GS ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.7 ! ROLL ANGLE stable ! 0.8 ! 0.8 ! 0.8 ! 0.8 ! 0.8 ! deg ! |
| ! ! frame variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.7.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of ROLL ANGLE ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.8 ! TAT stable frame ! 1.1 ! 1.1 ! 1.1 ! 1.1 ! 1.1 ! deg C! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.8.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of TAT ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.9 ! N2 stable frame ! 0.9 ! 0.9 ! 0.9 ! 0.9 ! 0.9 ! % ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.9.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of N2 ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.10 ! EGT stable frame ! 18.0 ! 18.0 ! 18.0 ! 18.0 ! 18.0 ! deg C! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| !5.10.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of EGT ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.11 ! VACC stable frame ! 0.03 ! 0.03 ! 0.03 ! 0.03 ! 0.03 ! g ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| !5.11.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of VACC ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.12 ! MN stable frame ! 0.008 ! 0.008 ! 0.008 ! 0.008 ! 0.008 ! Mach ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| !5.12.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of MN ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.13 ! N1 stable frame ! 1.6 ! 1.6 ! 1.6 ! 1.6 ! 1.6 ! % ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| !5.13.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of N1 ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.14 ! PT2 stable frame ! 0.05 ! 0.05 ! 0.05 ! 0.05 ! 0.05 ! psia ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| !5.14.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of PT2 ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.15 ! FF stable frame ! 100 ! 100 ! 100 ! 100 ! 100 ! kg/h ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| !5.15.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of FF ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.16 ! HPT stable frame ! 10.0 ! 10.0 ! 10.0 ! 10.0 ! 10.0 ! % ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| !5.16.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of HPT ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.17 ! LPT stable frame ! 10.0 ! 10.0 ! 10.0 ! 10.0 ! 10.0 ! % ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| !5.17.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of LPT ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 6.1 ! 'NIT.1' stable N1 ! 62 ! 62 ! 62 ! 62 ! 62 ! % ! |
| ! * ! value for descent ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 6.2 ! 'X1.1' tolerance !+/-1.5 !+/-1.5 !+/-1.5 !+/-1.5 !+/-1.5 ! % ! |
| ! * ! band for descent ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 6.3 !'T1.1' stable observing! 20 ! 20 ! 20 ! 20 ! 20 !second! |
| ! * ! time for descent ! ! ! ! ! ! ! |
| ! ! (max. 20 seconds) ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 7.1 ! 'N1T.2' stable N1 ! 93 ! 93 ! 93 ! 93 ! 93 ! % ! |
| ! * ! value for take off ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 7.2 ! 'X1.2' rpm tolerance !+/-1.5 !+/-1.5 !+/-1.5 !+/-1.5 !+/-1.5 ! % ! |
| ! * ! band for take off ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| !10.3 !'T1.2' stable observing! 20 ! 20 ! 20 ! 20 ! 20 !second! |
| ! * ! time for take off ! ! ! ! ! ! ! |
| ! ! (max. 20 seconds) ! ! ! ! ! ! ! |
| !-----------------------------------------------------------------------------! |
| ! * Remark: Only for Advanced EVMU available ! |
| +-----------------------------------------------------------------------------+ |
(10) A321: CFMI Engines 56-5-B1, 56-5-B2, 56-5-B3, 56-5-B4
| +-----------------------------------------------------------------------------+ |
| !Report! Description of Report Item ! CFM ! CFM ! CFM ! CFM ! Unit ! |
| !Item ! !56-5-B1!56-5-B2!56-5-B3!56-5-B4! ! |
| ! ! !-------!-------!-------!-------!------! |
| ! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! ! |
| ! ! ! CFM #5! CFM #6! CFM #7! CFM #3! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.1 !'Y02.1' flight hours ! 1 ! 1 ! 1 ! 1 ! hours! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.2 !'Y02.2' flight legs ! 1 ! 1 ! 1 ! 1 ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.3 !'P02' stable periods ! 5 ! 5 ! 5 ! 5 ! ! |
| ! ! (1 period = 20 seconds) ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.4.1! HPTL1 valve position lower ! 70 ! 70 ! 70 ! 70 ! % ! |
| ! ! limit ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.4.2! HPTL2 valve position upper ! 105 ! 105 ! 105 ! 105 ! % ! |
| ! ! limit ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.5 ! IALT stable frame variation ! 150 ! 150 ! 150 ! 150 ! ft ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.5.1! Weighting Factor Wa of IALT ! 1 ! 1 ! 1 ! 1 ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.6 ! GS stable frame variation ! 6 ! 6 ! 6 ! 6 ! kts ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.6.1! Weighting Factor Wa of GS ! 1 ! 1 ! 1 ! 1 ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.7 ! ROLL ANGLE stable frame ! 0.8 ! 0.8 ! 0.8 ! 0.8 ! deg ! |
| ! ! variation ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.7.1! Weighting Factor Wa of ROLL ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! ANGLE ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.8 ! TAT stable frame variation ! 1.1 ! 1.1 ! 1.1 ! 1.1 ! deg C! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.8.1! Weighting Factor Wa of TAT ! 1 ! 1 ! 1 ! 1 ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.9 ! N2 stable frame variation ! 0.9 ! 0.9 ! 0.9 ! 0.9 ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.9.1! Weighting Factor Wa of N2 ! 1 ! 1 ! 1 ! 1 ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.10 ! EGT stable frame variation ! 18.0 ! 18.0 ! 18.0 ! 18.0 ! deg C! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !5.10.1! Weighting Factor Wa of EGT ! 1 ! 1 ! 1 ! 1 ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.11 ! VACC stable frame variation ! 0.03 ! 0.03 ! 0.03 ! 0.03 ! g ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !5.11.1! Weighting Factor Wa of VACC ! 1 ! 1 ! 1 ! 1 ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.12 ! MN stable frame variation ! 0.008 ! 0.008 ! 0.008 ! 0.008 !Mach ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !5.12.1! Weighting Factor Wa of MN ! 1 ! 1 ! 1 ! 1 ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.13 ! N1 stable frame variation ! 1.6 ! 1.6 ! 1.6 ! 1.6 ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !5.13.1! Weighting Factor Wa of N1 ! 1 ! 1 ! 1 ! 1 ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.14 ! PT2 stable frame variation ! 0.05 ! 0.05 ! 0.05 ! 0.05 ! psia ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !5.14.1! Weighting Factor Wa of PT2 ! 1 ! 1 ! 1 ! 1 ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.15 ! FF stable frame variation ! 100 ! 100 ! 100 ! 100 ! kg/h ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !5.15.1! Weighting Factor Wa of FF ! 1 ! 1 ! 1 ! 1 ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.16 ! HPT stable frame variation ! 10.0 ! 10.0 ! 10.0 ! 10.0 ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !5.16.1! Weighting Factor Wa of HPT ! 1 ! 1 ! 1 ! 1 ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.17 ! LPT stable frame variation ! 10.0 ! 10.0 ! 10.0 ! 10.0 ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !5.17.1! Weighting Factor Wa of LPT ! 1 ! 1 ! 1 ! 1 ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 6.1 ! 'NIT.1' stable N1 value for ! 62 ! 62 ! 62 ! 62 ! % ! |
| ! * ! descent ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 6.2 ! 'X1.1' tolerance band for !+/-1.5 !+/-1.5 !+/-1.5 !+/-1.5 ! % ! |
| ! * ! descent ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 6.3 ! 'T1.1' stable observing time ! 20 ! 20 ! 20 ! 20 !second! |
| ! * ! for descent (max. 20 seconds) ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 7.1 ! 'N1T.2' stable N1 value for ! 93 ! 93 ! 93 ! 93 ! %rpm ! |
| ! * ! take off ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 7.2 ! 'X1.2' rpm tolerance band for !+/-1.5 !+/-1.5 !+/-1.5 !+/-1.5 ! % ! |
| ! * ! take off ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 7.3 ! 'T1.2' stable observing time ! 20 ! 20 ! 20 ! 20 !second! |
| ! * ! for take off (max. 20 seconds)! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! * Remark: Only for Advanced EVMU available ! |
| +-----------------------------------------------------------------------------+ |
(11) A319: CFMI Engines 56-5-A5, 56-5-B6, 56-5-B5, 56-5-A4, 56-5-B7
| +----------------------------------------------------------------------------+ |
| !Report! Description of ! CFM ! CFM ! CFM ! CFM ! CFM ! Unit ! |
| !Item ! Report Item !56-5-A5!56-5-B6!56-5-B5!56-5-A4!56-5-B7! ! |
| ! ! !-------!-------!-------!-------!-------!------! |
| ! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! ! |
| ! ! ! C7xxx ! C8xxxx! C4xxxx! C6xxxx! C5xxxx! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.1 !'Y02.1' flight hours ! 1 ! 1 ! 1 ! 1 ! 1 ! hours! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.2 !'Y02.2' flight legs ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.3 !'P02' stable periods ! 5 ! 5 ! 5 ! 5 ! 5 ! ! |
| ! ! ( 1 period = 20 sec) ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.4.1! HPTL1 valve position ! 0 ! 70 ! 70 ! 0 ! 70 ! % ! |
| ! ! lower limit ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.4.2! HPTL2 valve position ! 20 ! 105 ! 105 ! 20 ! 105 ! % ! |
| ! ! upper limit ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.5 ! IALT stable frame ! 150 ! 150 ! 150 ! 150 ! 150 ! ft ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.5.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of IALT ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.6 ! GS stable frame ! 6 ! 6 ! 6 ! 6 ! 6 ! kts ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.6.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of GS ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.7 ! ROLL ANGLE stable ! 0.8 ! 0.8 ! 0.8 ! 0.8 ! 0.8 ! deg ! |
| ! ! frame variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.7.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of ROLL ANGLE ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.8 ! TAT stable frame ! 1.1 ! 1.1 ! 1.1 ! 1.1 ! 1.1 ! deg C! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.8.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of TAT ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.9 ! N2 stable frame ! 0.9 ! 0.9 ! 0.9 ! 0.9 ! 0.9 ! % ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.9.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of N2 ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.10 ! EGT stable frame ! 18.0 ! 18.0 ! 18.0 ! 18.0 ! 18.0 ! deg C! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| !5.10.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of EGT ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.11 ! VACC stable frame ! 0.03 ! 0.03 ! 0.03 ! 0.03 ! 0.03 ! g ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| !5.11.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of VACC ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.12 ! MN stable frame ! 0.008 ! 0.008 ! 0.008 ! 0.008 ! 0.008 ! Mach ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| !5.12.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of MN ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.13 ! N1 stable frame ! 1.6 ! 1.6 ! 1.6 ! 1.6 ! 1.6 ! % ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| !5.13.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of N1 ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.14 ! PT2 stable frame ! 0.05 ! 0.05 ! 0.05 ! 0.05 ! 0.05 ! psia ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| !5.14.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of PT2 ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.15 ! FF stable frame ! 100 ! 100 ! 100 ! 100 ! 100 ! kg/h ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| !5.15.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of FF ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.16 ! HPT stable frame ! 10.0 ! 10.0 ! 10.0 ! 10.0 ! 10.0 ! % ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| !5.16.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of HPT ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.17 ! LPT stable frame ! 10.0 ! 10.0 ! 10.0 ! 10.0 ! 10.0 ! % ! |
| ! ! variation ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| !5.17.1! Weighting Factor ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! Wa of LPT ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 6.1 ! 'NIT.1' stable N1 ! 62 ! 62 ! 62 ! 62 ! 62 ! % ! |
| ! * ! value for descent ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 6.2 ! 'X1.1' tolerance !+/-1.5 !+/-1.5 !+/-1.5 !+/-1.5 !+/-1.5 ! % ! |
| ! * ! band for descent ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 6.3 !'T1.1' stable observing! 20 ! 20 ! 20 ! 20 ! 20 !second! |
| ! * ! time for descent ! ! ! ! ! ! ! |
| ! ! (max. 20 seconds) ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 7.1 ! 'N1T.1' stable N1 ! 93 ! 93 ! 93 ! 93 ! 93 ! %rpm ! |
| ! * ! value for take off ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 7.2 ! 'X1.2' rpm tolerance !+/-1.5 !+/-1.5 !+/-1.5 !+/-1.5 !+/-1.5 ! % ! |
| ! * ! band for take off ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 7.3 !'T1.2' stable observing! 20 ! 20 ! 20 ! 20 ! 20 !second! |
| ! * ! time for take off ! ! ! ! ! ! ! |
| ! ! (max. 20 seconds) ! ! ! ! ! ! ! |
| !-----------------------------------------------------------------------------! |
| ! * Remark: Only for Advanced EVMU available ! |
| +-----------------------------------------------------------------------------+ |
(12) A318: CFMI Engine 56-5-B8, 56-5-B9
| +-----------------------------------------------------------------------------+ |
| !Report! Description of Report Item ! CFM ! CFM ! SPARE ! SPARE ! Unit ! |
| !Item ! !56-5-B8!56-5-B9! ! ! ! |
| ! ! !-------!-------!-------!-------!------! |
| ! ! !DMU/ID !DMU/ID ! ! ! ! |
| ! ! !C1xxxxx! C2xxxx! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.1 !'Y02.1' flight hours ! 1 ! 1 ! ! ! hour ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.2 !'Y02.2' flight legs ! 1 ! 1 ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.3 !'P02': stable periods ! 5 ! 5 ! ! ! ! |
| ! ! (1 period = 20 seconds) ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.4.1! HPTL1 valve position lower ! 70 ! 70 ! ! ! % ! |
| ! ! limit ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.4.2! HPTL2 valve position upper ! 105 ! 105 ! ! ! % ! |
| ! ! limit ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.5 ! IALT stable frame variation ! 150 ! 150 ! ! ! ft ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.5.1! Weighting Factor Wa of IALT ! 1 ! 1 ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.6 ! GS stable frame variation ! 6 ! 6 ! ! ! kts ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.6.1! Weighting Factor Wa of GS ! 1 ! 1 ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.7 ! ROLL ANGLE stable frame ! 0.8 ! 0.8 ! ! ! deg ! |
| ! ! variation ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.7.1! Weighting Factor Wa of ROLL ! 1 ! 1 ! ! ! ! |
| ! ! ANGLE ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.8 ! TAT stable frame variation ! 1.1 ! 1.1 ! ! ! deg C! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.8.1! Weighting Factor Wa of TAT ! 1 ! 1 ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.9 ! N2 stable frame variation ! 0.9 ! 0.9 ! ! ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.9.1! Weighting Factor Wa of N2 ! 1 ! 1 ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.10 ! EGT stable frame variation ! 18.0 ! 18.0 ! ! ! deg C! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !5.10.1! Weighting Factor Wa of EGT ! 1 ! 1 ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.11 ! VACC stable frame variation ! 0.03 ! 0.03 ! ! ! g ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !5.11.1! Weighting Factor Wa of VACC ! 1 ! 1 ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.12 ! MN stable frame variation ! 0.008 ! 0.008 ! ! ! Mach ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !5.12.1! Weighting Factor Wa of MN ! 1 ! 1 ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.13 ! N1 stable frame variation ! 1.6 ! 1.6 ! ! ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !5.13.1! Weighting Factor Wa of N1 ! 1 ! 1 ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.14 ! PT2 stable frame variation ! 0.05 ! 0.05 ! ! ! psia ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !5.14.1! Weighting Factor Wa of PT2 ! 1 ! 1 ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.15 ! FF stable frame variation ! 100 ! 100 ! ! ! kg/h ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !5.15.1! Weighting Factor Wa of FF ! 1 ! 1 ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.16 ! HPT stable frame variation ! 10.0 ! 10.0 ! ! ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !5.16.1! Weighting Factor Wa of HPT ! 1 ! 1 ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.17 ! LPT stable frame variation ! 10.0 ! 10.0 ! ! ! 5 ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !5.17.1! Weighting Factor Wa of LPT ! 1 ! 1 ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 6.1 ! 'N1T.1' stable N1 value for ! 62 ! 62 ! ! ! %rpm ! |
| ! * ! descent ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 6.2 ! 'X1.1' tolerance band for !+/-1.5 !+/-1.5 ! ! ! % ! |
| ! * ! descent ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 6.3 ! 'T1.1' stable observing time ! 20 ! 20 ! ! !second! |
| ! * ! for descent (max. 20 seconds) ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 7.1 ! 'N1T.2' stable N1 value for ! 93 ! 93 ! ! ! %rpm ! |
| ! * ! take off ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 7.2 ! 'X1.2' rpm tolerance band for !+/-1.5 !+/-1.5 ! ! ! % ! |
| ! * ! take off ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 7.3 ! 'T1.2' stable observing time ! 20 ! 20 ! ! !second! |
| ! * ! for take off (max. 20 seconds)! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! * Remark: Only for Advanced EVMU available ! |
| +-----------------------------------------------------------------------------+ |
(13) A320: CFMI Engines 56-5-A1, 56-5-A3, 56-5-B4, 56-5-B5, 56-5-B6
| +-----------------------------------------------------------------------------+ |
| !Report!Limit! Description of ! CFM ! CFM ! CFM ! CFM ! CFM ! Unit ! |
| !Item !No. ! Report Item !56-5-A1!56-5-A3!56-5-B4!56-5-B5!56-5-B6! ! |
| ! ! ! !-------!-------!-------!-------!-------!------! |
| ! ! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! ! |
| ! ! ! ! CFM #5! CFM #6! CFM #7! CFM #4! CFM #8! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.1 ! 54 !"Y02.1" flight ! 1 ! 1 ! 1 ! 1 ! 1 ! hours! |
| ! ! !hours counter ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.2 ! 55 !"Y02.2" flight ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! !legs ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.3 ! 53 !"P02" stable ! 5 ! 5 ! 5 ! 5 ! 5 ! ! |
| ! ! !periods ! ! ! ! ! ! ! |
| ! ! !(1period = 20sec)! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.4.1! 56 !HPTL1 valve ! 0 ! 0 ! 70 ! 70 ! 70 ! % ! |
| ! ! !position lower ! ! ! ! ! ! ! |
| ! ! !limit ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.4.2! 57 !HPTL2 valve ! 20 ! 20 ! 105 ! 105 ! 105 ! % ! |
| ! ! !position upper ! ! ! ! ! ! ! |
| ! ! !limit ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.5 ! 58 !IALT stable frame! 150 ! 150 ! 150 ! 150 ! 150 ! ft ! |
| ! ! !variation ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.5.1! 72 !Weighting Factor ! 100 ! 100 ! 100 ! 100 ! 100 ! ! |
| ! ! !Wa of IALT ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.6 ! 59 !GS stable frame ! 6 ! 6 ! 6 ! 6 ! 6 ! kts ! |
| ! ! !variation ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.6.1! 73 !Weighting Factor ! 100 ! 100 ! 100 ! 100 ! 100 ! ! |
| ! ! !Wa of GS ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.7 ! 60 !ROLL ANGLE stable! 0.8 ! 0.8 ! 0.8 ! 0.8 ! 0.8 ! deg ! |
| ! ! !frame variation ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.7.1! 74 !Weighting Factor ! 100 ! 100 ! 100 ! 100 ! 100 ! ! |
| ! ! !Wa of ROLL ANGLE ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.8 ! 61 !TAT stable frame ! 1.1 ! 1.1 ! 1.1 ! 1.1 ! 1.1 ! deg C! |
| ! ! !variation ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.8.1! 75 !Weighting Factor ! 100 ! 100 ! 100 ! 100 ! 100 ! ! |
| ! ! !Wa of TAT ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.9 ! 62 !N2 stable frame ! 0.9 ! 0.9 ! 0.9 ! 0.9 ! 0.9 ! % ! |
| ! ! !variation ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.9.1! 76 !Weighting Factor ! 100 ! 100 ! 100 ! 100 ! 100 ! ! |
| ! ! !Wa of N2 ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.10 ! 63 !EGT stable frame ! 18.0 ! 18.0 ! 18.0 ! 18.0 ! 18.0 ! deg C! |
| ! ! !variation ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| !5.10.1! 77 !Weighting Factor ! 100 ! 100 ! 100 ! 100 ! 100 ! ! |
| ! ! !Wa of EGT ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.11 ! 64 !VACC stable frame! 0.03 ! 0.03 ! 0.03 ! 0.03 ! 0.03 ! g ! |
| ! ! !variation ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| !5.11.1! 78 !Weighting Factor ! 100 ! 100 ! 100 ! 100 ! 100 ! ! |
| ! ! !Wa of VACC ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.12 ! 65 !MACH stable frame! 0.008 ! 0.008 ! 0.008 ! 0.008 ! 0.008 ! Mach ! |
| ! ! !variation ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| !5.12.1! 79 !Weighting Factor ! 100 ! 100 ! 100 ! 100 ! 100 ! ! |
| ! ! !Wa of MACH ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.13 ! 66 !N1 stable frame ! 1.6 ! 1.6 ! 1.6 ! 1.6 ! 1.6 ! % ! |
| ! ! !variation ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| !5.13.1! 80 !Weighting Factor ! 100 ! 100 ! 100 ! 100 ! 100 ! ! |
| ! ! !Wa of N1 ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.14 ! 67 !PT2 stable frame ! 0.05 ! 0.05 ! 0.05 ! 0.05 ! 0.05 ! psia ! |
| ! ! !variation ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| !5.14.1! 81 !Weighting Factor ! 100 ! 100 ! 100 ! 100 ! 100 ! ! |
| ! ! !Wa of PT2 ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.15 ! 68 !FF stable frame ! 100 ! 100 ! 100 ! 100 ! 100 ! kg/h ! |
| ! ! !variation ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| !5.15.1! 82 !Weighting Factor ! 100 ! 100 ! 100 ! 100 ! 100 ! ! |
| ! ! !Wa of FF ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.16 ! 69 !HPT stable frame ! 10.0 ! 10.0 ! 10.0 ! 10.0 ! 10.0 ! % ! |
| ! ! !variation ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| !5.16.1! 83 !Weighting Factor ! 100 ! 100 ! 100 ! 100 ! 100 ! ! |
| ! ! !Wa of HPT ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.17 ! 70 !LPT stable frame ! 10.0 ! 10.0 ! 10.0 ! 10.0 ! 10.0 ! % ! |
| ! ! !variation ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| !5.17.1! 84 !Weighting Factor ! 100 ! 100 ! 100 ! 100 ! 100 ! ! |
| ! ! !Wa of LPT ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 6.1 ! 86 !"NIT.1" stable N1! 62 ! 62 ! 62 ! 62 ! 62 ! % ! |
| ! * ! !value for descent! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 6.2 ! 87 !"X1.1" tolerance !+/-1.5 !+/-1.5 !+/-1.5 !+/-1.5 !+/-1.5 ! % ! |
| ! * ! !band for descent ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 6.3 ! 88 !"T1.1" stable ! 20 ! 20 ! 20 ! 20 ! 20 !second! |
| ! * ! !observing ! ! ! ! ! ! ! |
| ! ! ! time for descent! ! ! ! ! ! ! |
| ! ! ! (max.20 seconds)! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 7.1 ! 89 !"N1T.1" stable N1! 93 ! 93 ! 93 ! 93 ! 93 ! % ! |
| ! * ! !value for climb ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 7.2 ! 90 !"X1.1" rpm !+/-1.5 !+/-1.5 !+/-1.5 !+/-1.5 !+/-1.5 ! % ! |
| ! * ! !tolerance band ! ! ! ! ! ! ! |
| ! ! !for climb ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 7.3 ! 91 !"T1.1" stable ! 20 ! 20 ! 20 ! 20 ! 20 !second! |
| ! * ! !observing ! ! ! ! ! ! ! |
| ! ! !time for climb ! ! ! ! ! ! ! |
| ! ! !(max. 20 seconds)! ! ! ! ! ! ! |
| !-----------------------------------------------------------------------------! |
| ! * Remark: Only for Advanced EVMU available ! |
| +-----------------------------------------------------------------------------+ |
(14) A321: CFMI Engines 56-5-B1, 56-5-B2, 56-5-B3, 56-5-B4
| +------------------------------------------------------------------------------+ |
| !Report!Limit! Description of Report ! CFM ! CFM ! CFM ! CFM ! Unit ! |
| !Item !No. ! Item !56-5-B1!56-5-B2!56-5-B3!56-5-B4! ! |
| ! ! ! !-------!-------!-------!-------!------! |
| ! ! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! ! |
| ! ! ! ! CFM #5! CFM #6! CFM #7! CFM #3! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.1 ! 54 !"Y02.1" flight hours ! 1 ! 1 ! 1 ! 1 ! hours! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.2 ! 55 !"Y02.2" flight legs ! 1 ! 1 ! 1 ! 1 ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.3 ! 53 !"P02" stable periods ! 5 ! 5 ! 5 ! 5 ! ! |
| ! ! !(1 period = 20 seconds) ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.4.1! 56 !HPTL1 valve position ! 70 ! 70 ! 70 ! 70 ! % ! |
| ! ! !lower limit ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.4.2! 57 !HPTL2 valve position ! 105 ! 105 ! 105 ! 105 ! % ! |
| ! ! !upper limit ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.5 ! 58 !IALT stable frame ! 150 ! 150 ! 150 ! 150 ! ft ! |
| ! ! !variation ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.5.1! 72 !Weighting Factor Wa of ! 100 ! 100 ! 100 ! 100 ! ! |
| ! ! !IALT ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.6 ! 59 !GS stable frame ! 6 ! 6 ! 6 ! 6 ! kts ! |
| ! ! !variation ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.6.1! 73 !Weighting Factor Wa of GS! 100 ! 100 ! 100 ! 100 ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.7 ! 60 !ROLL ANGLE stable frame ! 0.8 ! 0.8 ! 0.8 ! 0.8 ! deg ! |
| ! ! !variation ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.7.1! 74 !Weighting Factor Wa of ! 100 ! 100 ! 100 ! 100 ! ! |
| ! ! !ROLL ANGLE ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.8 ! 61 !TAT stable frame ! 1.1 ! 1.1 ! 1.1 ! 1.1 ! deg C! |
| ! ! !variation ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.8.1! 75 !Weighting Factor Wa of ! 100 ! 100 ! 100 ! 100 ! ! |
| ! ! !TAT ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.9 ! 62 !N2 stable frame variation! 0.9 ! 0.9 ! 0.9 ! 0.9 ! % ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.9.1! 76 !Weighting Factor Wa of N2! 100 ! 100 ! 100 ! 100 ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.10 ! 63 !EGT stable frame ! 18.0 ! 18.0 ! 18.0 ! 18.0 ! deg C! |
| ! ! !variation ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| !5.10.1! 77 !Weighting Factor Wa of ! 100 ! 100 ! 100 ! 100 ! ! |
| ! ! !EGT ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.11 ! 64 !VACC stable frame ! 0.03 ! 0.03 ! 0.03 ! 0.03 ! g ! |
| ! ! !variation ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| !5.11.1! 78 !Weighting Factor Wa of ! 100 ! 100 ! 100 ! 100 ! ! |
| ! ! !VACC ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.12 ! 65 !MACH stable frame ! 0.008 ! 0.008 ! 0.008 ! 0.008 !Mach ! |
| ! ! !variation ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| !5.12.1! 79 !Weighting Factor Wa of ! 100 ! 100 ! 100 ! 100 ! ! |
| ! ! !MACH ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.13 ! 66 !N1 stable frame variation! 1.6 ! 1.6 ! 1.6 ! 1.6 ! % ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| !5.13.1! 80 !Weighting Factor Wa of N1! 100 ! 100 ! 100 ! 100 ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.14 ! 67 !PT2 stable frame ! 0.05 ! 0.05 ! 0.05 ! 0.05 ! psia ! |
| ! ! !variation ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| !5.14.1! 81 !Weighting Factor Wa of ! 100 ! 100 ! 100 ! 100 ! ! |
| ! ! !PT2 ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.15 ! 68 !FF stable frame variation! 100 ! 100 ! 100 ! 100 ! kg/h ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| !5.15.1! 81 !Weighting Factor Wa of FF! 100 ! 100 ! 100 ! 100 ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.16 ! 82 !HPT stable frame ! 10.0 ! 10.0 ! 10.0 ! 10.0 ! % ! |
| ! ! !variation ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| !5.16.1! 83 !Weighting Factor Wa of ! 100 ! 100 ! 100 ! 100 ! ! |
| ! ! !HPT ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.17 ! 70 !LPT stable frame ! 10.0 ! 10.0 ! 10.0 ! 10.0 ! % ! |
| ! ! !variation ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| !5.17.1! 84 !Weighting Factor Wa of ! 100 ! 100 ! 100 ! 100 ! ! |
| ! ! !LPT ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 6.1 ! 86 !"NIT.1" stable N1 value ! 62 ! 62 ! 62 ! 62 ! % ! |
| ! * ! !for descent ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 6.2 ! 87 !"X1.1" tolerance band for!+/-1.5 !+/-1.5 !+/-1.5 !+/-1.5 ! % ! |
| ! * ! !descent ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 6.3 ! 88 !"T1.1" stable observing ! 20 ! 20 ! 20 ! 20 !second! |
| ! * ! !time for descent ! ! ! ! ! ! |
| ! ! !(max. 20 seconds) ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 7.1 ! 89 !"N1T.1" stable N1 value ! 93 ! 93 ! 93 ! 93 ! %rpm ! |
| ! * ! !for climb ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 7.2 ! 90 !"X1.1" rpm tolerance band!+/-1.5 !+/-1.5 !+/-1.5 !+/-1.5 ! % ! |
| ! * ! !for climb ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 7.3 ! 91 !"T1.1" stable observing ! 20 ! 20 ! 20 ! 20 !second! |
| ! * ! !time for climb ! ! ! ! ! ! |
| ! ! !(max. 20 seconds) ! ! ! ! ! ! |
| !-----------------------------------------------------------------------------! |
| ! * Remark: Only for Advanced EVMU available ! |
| +-----------------------------------------------------------------------------+ |
(15) A319: CFMI Engines 56-5-A5, 56-5-B6, 56-5-B5, 56-5-A4, 56-5-B7
| +-----------------------------------------------------------------------------+ |
| !Report!Limit! Description of ! CFM ! CFM ! CFM ! CFM ! CFM ! Unit ! |
| !Item !No. ! Report Item !56-5-A5!56-5-B6!56-5-B5!56-5-A4!56-5-B7! ! |
| ! ! ! !-------!-------!-------!-------!-------!------! |
| ! ! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! ! |
| ! ! ! ! C7xxxx! C8xxxx! C4xxxx! C6xxxx! C5xxxx! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.1 ! 54 !"Y02.1" flight ! 1 ! 1 ! 1 ! 1 ! 1 ! hours! |
| ! ! !hours ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.2 ! 55 !"Y02.2" flight ! 1 ! 1 ! 1 ! 1 ! 1 ! ! |
| ! ! !legs ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.3 ! 53 !"P02" stable ! 5 ! 5 ! 5 ! 5 ! 5 ! ! |
| ! ! !periods ! ! ! ! ! ! ! |
| ! ! !(1period = 20sec)! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.4.1! 56 !HPTL1 valve ! 0 ! 70 ! 70 ! 0 ! 70 ! % ! |
| ! ! !position lower ! ! ! ! ! ! ! |
| ! ! !limit ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.4.2! 57 !HPTL2 valve ! 20 ! 105 ! 105 ! 20 ! 105 ! % ! |
| ! ! !position upper ! ! ! ! ! ! ! |
| ! ! !limit ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.5 ! 58 !IALT stable frame! 150 ! 150 ! 150 ! 150 ! 150 ! ft ! |
| ! ! !variation ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.5.1! 72 !Weighting Factor ! 100 ! 100 ! 100 ! 100 ! 100 ! ! |
| ! ! !Wa of IALT ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.6 ! 59 !GS stable frame ! 6 ! 6 ! 6 ! 6 ! 6 ! kts ! |
| ! ! !variation ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.6.1! 73 !Weighting Factor ! 100 ! 100 ! 100 ! 100 ! 100 ! ! |
| ! ! !Wa of GS ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.7 ! 60 !ROLL ANGLE stable! 0.8 ! 0.8 ! 0.8 ! 0.8 ! 0.8 ! deg ! |
| ! ! !frame variation ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.7.1! 74 !Weighting Factor ! 100 ! 100 ! 100 ! 100 ! 100 ! ! |
| ! ! !Wa of ROLL ANGLE ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.8 ! 61 !TAT stable frame ! 1.1 ! 1.1 ! 1.1 ! 1.1 ! 1.1 ! deg C! |
| ! ! !variation ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.8.1! 75 !Weighting Factor ! 100 ! 100 ! 100 ! 100 ! 100 ! ! |
| ! ! !Wa of TAT ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.9 ! 62 !N2 stable frame ! 0.9 ! 0.9 ! 0.9 ! 0.9 ! 0.9 ! % ! |
| ! ! !variation ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.9.1! 76 !Weighting Factor ! 100 ! 100 ! 100 ! 100 ! 100 ! ! |
| ! ! !Wa of N2 ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.10 ! 63 !EGT stable frame ! 18.0 ! 18.0 ! 18.0 ! 18.0 ! 18.0 ! deg C! |
| ! ! !variation ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| !5.10.1! 77 !Weighting Factor ! 100 ! 100 ! 100 ! 100 ! 100 ! ! |
| ! ! !Wa of EGT ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.11 ! 64 !VACC stable frame! 0.03 ! 0.03 ! 0.03 ! 0.03 ! 0.03 ! g ! |
| ! ! !variation ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| !5.11.1! 78 !Weighting Factor ! 100 ! 100 ! 100 ! 100 ! 100 ! ! |
| ! ! !Wa of VACC ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.12 ! 65 !MACH stable frame! 0.008 ! 0.008 ! 0.008 ! 0.008 ! 0.008 ! Mach ! |
| ! ! !variation ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| !5.12.1! 79 !Weighting Factor ! 100 ! 100 ! 100 ! 100 ! 100 ! ! |
| ! ! !Wa of MACH ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.13 ! 66 !N1 stable frame ! 1.6 ! 1.6 ! 1.6 ! 1.6 ! 1.6 ! % ! |
| ! ! !variation ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| !5.13.1! 80 !Weighting Factor ! 100 ! 100 ! 100 ! 100 ! 100 ! ! |
| ! ! !Wa of N1 ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.14 ! 67 !PT2 stable frame ! 0.05 ! 0.05 ! 0.05 ! 0.05 ! 0.05 ! psia ! |
| ! ! !variation ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| !5.14.1! 81 !Weighting Factor ! 100 ! 100 ! 100 ! 100 ! 100 ! ! |
| ! ! !Wa of PT2 ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.15 ! 68 !FF stable frame ! 100 ! 100 ! 100 ! 100 ! 100 ! kg/h ! |
| ! ! !variation ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| !5.15.1! 82 !Weighting Factor ! 100 ! 100 ! 100 ! 100 ! 100 ! ! |
| ! ! !Wa of FF ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.16 ! 69 !HPT stable frame ! 10.0 ! 10.0 ! 10.0 ! 10.0 ! 10.0 ! % ! |
| ! ! !variation ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| !5.16.1! 83 !Weighting Factor !100 ! 100 ! 100 ! 100 ! 100 ! ! |
| ! ! !Wa of HPT ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.17 ! 70 !LPT stable frame ! 10.0 ! 10.0 ! 10.0 ! 10.0 ! 10.0 ! % ! |
| ! ! !variation ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| !5.17.1! 84 !Weighting Factor ! 100 ! 100 ! 100 ! 100 ! 100 ! ! |
| ! ! !Wa of LPT ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 6.1 ! 86 !"NIT.1" stable N1! 62 ! 62 ! 62 ! 62 ! 62 ! % ! |
| ! * ! !value for descent! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 6.2 ! 87 !"X1.1" tolerance !+/-1.5 !+/-1.5 !+/-1.5 !+/-1.5 !+/-1.5 ! % ! |
| ! * ! !band for descent ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 6.3 ! 88 !"T1.1" stable ! 20 ! 20 ! 20 ! 20 ! 20 !second! |
| ! * ! !observing time ! ! ! ! ! ! ! |
| ! ! !for descent ! ! ! ! ! ! ! |
| ! ! !(max. 20 seconds)! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 7.1 ! 89 !"N1T.1" stable N1! 93 ! 93 ! 93 ! 93 ! 93 ! %rpm ! |
| ! * ! !value climb ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 7.2 ! 90 !"X1.1" rpm !+/-1.5 !+/-1.5 !+/-1.5 !+/-1.5 !+/-1.5 ! % ! |
| ! * ! !tolerance band ! ! ! ! ! ! ! |
| ! ! !for climb ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 7.3 ! 91 !"T1.1" stable ! 20 ! 20 ! 20 ! 20 ! 20 !second! |
| ! * ! !observing time ! ! ! ! ! ! ! |
| ! ! !for climb ! ! ! ! ! ! ! |
| ! ! !(max. 20 seconds)! ! ! ! ! ! ! |
| !-----------------------------------------------------------------------------! |
| ! * Remark: Only for Advanced EVMU available ! |
| +-----------------------------------------------------------------------------+ |
(16) A318: CFMI Engine 56-5-B8, 56-5-B9
| +-----------------------------------------------------------------------------+ |
| !Report!Limit! Description of ! CFM ! CFM ! SPARE ! SPARE ! Unit ! |
| !Item !No. ! Report Item !56-5-B8!56-5-B9! ! ! ! |
| ! ! ! !-------!-------!-------!-------!------! |
| ! ! ! !DMU/ID !DMU/ID ! ! ! ! |
| ! ! ! !C1xxxxx! C2xxxx! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.1 ! 54 !"Y02.1" flight hours ! 1 ! 1 ! ! ! hour ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.2 ! 55 !"Y02.2" flight legs ! 1 ! 1 ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.3 ! 53 !"P02": stable periods ! 5 ! 5 ! ! ! ! |
| ! ! !(1 period = 20 seconds) ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.4.1! 56 !HPTL1 valve position ! 70 ! 70 ! ! ! % ! |
| ! ! !lower limit ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.4.2! 57 !HPTL2 valve position ! 105 ! 105 ! ! ! % ! |
| ! ! !upper limit ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.5 ! 58 !IALT stable frame ! 150 ! 150 ! ! ! ft ! |
| ! ! !variation ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.5.1! 72 !Weighting Factor Wa of ! 100 ! 100 ! ! ! ! |
| ! ! !IALT ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.6 ! 59 !GS stable frame variation! 6 ! 6 ! ! ! kts ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.6.1! 73 !Weighting Factor Wa of GS! 100 ! 100 ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.7 ! 60 !ROLL ANGLE stable frame ! 0.8 ! 0.8 ! ! ! deg ! |
| ! ! !variation ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.7.1! 74 !Weighting Factor Wa of ! 100 ! 100 ! ! ! ! |
| ! ! !ROLL ANGLE ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.8 ! 61 !TAT stable frame ! 1.1 ! 1.1 ! ! ! deg C! |
| ! ! !variation ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.8.1! 75 !Weighting Factor Wa of ! 100 ! 100 ! ! ! ! |
| ! ! !TAT ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.9 ! 62 !N2 stable frame variation! 0.9 ! 0.9 ! ! ! % ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.9.1! 76 !Weighting Factor Wa of N2! 100 ! 100 ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.10 ! 63 !EGT stable frame ! 18.0 ! 18.0 ! ! ! deg C! |
| ! ! !variation ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| !5.10.1! 77 !Weighting Factor Wa of ! 100 ! 100 ! ! ! ! |
| ! ! !EGT ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.11 ! 64 !VACC stable frame ! 0.03 ! 0.03 ! ! ! g ! |
| ! ! !variation ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| !5.11.1! 78 !Weighting Factor Wa of ! 100 ! 100 ! ! ! ! |
| ! ! !VACC ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.12 ! 65 !MACH stable frame ! 0.008 ! 0.008 ! ! ! Mach ! |
| ! ! !variation ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| !5.12.1! 79 !Weighting Factor Wa of ! 100 ! 100 ! ! ! ! |
| ! ! !MACH ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.13 ! 66 !N1 stable frame variation! 1.6 ! 1.6 ! ! ! % ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| !5.13.1! 80 !Weighting Factor Wa of N1! 100 ! 100 ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.14 ! 67 !PT2 stable frame ! 0.05 ! 0.05 ! ! ! psia ! |
| ! ! !variation ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| !5.14.1! 81 !Weighting Factor Wa of ! 100 ! 100 ! ! ! ! |
| ! ! !PT2 ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.15 ! 68 !FF stable frame variation! 100 ! 100 ! ! ! kg/h ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| !5.15.1! 82 !Weighting Factor Wa of FF! 100 ! 100 ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.16 ! 69 !HPT stable frame ! 10.0 ! 10.0 ! ! ! % ! |
| ! ! !variation ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| !5.16.1! 83 !Weighting Factor Wa of ! 100 ! 100 ! ! ! ! |
| ! ! !HPT ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.17 ! 70 !LPT stable frame ! 10.0 ! 10.0 ! ! ! 5 ! |
| ! ! !variation ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| !5.17.1! 84 !Weighting Factor Wa of ! 100 ! 100 ! ! ! ! |
| ! ! !LPT ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 6.1 ! 86 !"N1T.1" stable N1 value ! 62 ! 62 ! ! ! %rpm ! |
| ! * ! !for descent ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 6.2 ! 87 !"X1.1" tolerance band !+/-1.5 !+/-1.5 ! ! ! % ! |
| ! * ! !for descent ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 6.3 ! 88 !"T1.1" stable ! 20 ! 20 ! ! !second! |
| ! * ! !observing time for ! ! ! ! ! ! |
| ! ! !descent (max. 20 seconds)! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 7.1 ! 89 !"N1T.1" stable N1 value ! 93 ! 93 ! ! ! %rpm ! |
| ! * ! !for climb ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 7.2 ! 90 !"X1.1" rpm tolerance !+/-1.5 !+/-1.5 ! ! ! % ! |
| ! * ! !band for climb ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 7.3 ! 91 !"T1.1" stable ! 20 ! 20 ! ! !second! |
| ! * ! !observing time for climb ! ! ! ! ! ! |
| ! ! ! (max. 20 seconds) ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! * Remark: Only for Advanced EVMU available ! |
| +-----------------------------------------------------------------------------+ |
U. Report Limits for Engine T/O Report <04>
(1) A320: CFMI Engines 56-5-A1, 56-5-A3, 56-5-B4
| +-----------------------------------------------------------------------------+ |
| !Report! Limit ! Description of Report Item !56-5-A1!56-5-A3!56-5-B4! Unit ! |
| !Item N! No. ! ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.3 ! 104 ! EGTL temperature limit cold ! 100 ! 100 ! 100 ! deg C! |
| ! ! ! engine start detection ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.4 ! 105 ! F04th Take Off ! 5 ! 5 ! 5 ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.5 ! 106 ! Y04.1 seconds after PH 4 ! 40 ! 40 ! 40 ! sec ! |
| ! ! ! entry ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.7.1! ! Delta N1 ! >10 ! >10 ! >10 ! % ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.7.2! 110 ! Delta N1 ! 8..10 ! 8..10 ! 8..10 ! % ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.7.3! 111 ! Delta N1 ! 6..8 ! 6..8 ! 6..8 ! % ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.7.4! 112 ! Delta N1 ! 4..6 ! 4..6 ! 4..6 ! % ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.7.5! 113 ! Delta N1 ! 2..4 ! 2..4 ! 2..4 ! % ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.7.6! 114 ! Delta N1 ! 0.2..2! 0.2..2! 0.2..2! % ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.7.7! 115 ! Delta N1 ! </=0.2! </=0.2! </=0.2! % ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.8.1! 108 ! Y04.3 seconds after PH 4 ! 5 ! 5 ! 5 ! sec ! |
| ! ! ! entry calculation of N1 ! ! ! ! ! |
| ! ! ! Summary Limit ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.1 ! 109 ! Number 'X04' consecutive legs ! 5 ! 5 ! 5 ! ! |
| +-----------------------------------------------------------------------------+ |
(2) A321: CFMI Engines 56-5-B1, 56-5-B2, 56-5-B3
| +-----------------------------------------------------------------------------+ |
| !Report! Limit ! Description of Report Item !56-5-B1!56-5-B2!56-5-B3! Unit ! |
| !Item N! No. ! ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.3 ! 104 ! EGTL temperature limit cold ! 100 ! 100 ! 100 ! deg C! |
| ! ! ! engine start detection ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.4 ! 105 ! F04th Take Off ! 5 ! 5 ! 5 ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.5 ! 106 ! Y04.1 seconds after PH 4 ! 40 ! 40 ! 40 ! sec ! |
| ! ! ! entry ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.7.1! ! Delta N1 ! >10 ! >10 ! >10 ! % ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.7.2! 110 ! Delta N1 ! 8..10 ! 8..10 ! 8..10 ! % ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.7.3! 111 ! Delta N1 ! 6..8 ! 6..8 ! 6..8 ! % ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.7.4! 112 ! Delta N1 ! 4..6 ! 4..6 ! 4..6 ! % ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.7.5! 113 ! Delta N1 ! 2..4 ! 2..4 ! 2..4 ! % ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.7.6! 114 ! Delta N1 ! 0.2..2! 0.2..2! 0.2..2! % ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.7.7! 115 ! Delta N1 ! </=0.2! </=0.2! </=0.2! % ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.8.1! 108 ! Y04.3 seconds after PH 4 ! 5 ! 5 ! 5 ! sec ! |
| ! ! ! calculation of N1 ! ! ! ! ! |
| ! ! ! Summary Limit ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.1 ! 109 ! Number 'X04' consecutive legs ! 5 ! 5 ! 5 ! ! |
| +-----------------------------------------------------------------------------+ |
(3) A319: CFMI Engines 56-5-A5, 56-5-B6, 56-5-B5, 56-5A4
| +-----------------------------------------------------------------------------+ |
| !Report! Limit ! Description of Report !56-5-A5!56-5-B6!56-5-B5!56-5A4! Unit ! |
| !Item N! No. ! Item ! ! ! ! ! ! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! 4.1.4! 104 ! EGTL temperature limit ! 100 ! 100 ! 100 ! 100 ! deg C! |
| ! ! ! cold engine ! ! ! ! ! ! |
| ! ! ! start detection ! ! ! ! ! ! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! 4.2 ! 105 ! 'F04'th Take Off ! 5 ! 5 ! 5 ! 5 ! ! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! 4.3 ! 106 ! Y04.1 seconds after ! 40 ! 40 ! 40 ! 40 ! sec ! |
| ! ! ! PH 4 entry ! ! ! ! ! ! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! 4.4.1! ! Delta N1 ! >10 ! >10 ! >10 ! >10 ! % ! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! 4.4.2! 110 ! Delta N1 ! 8..10 ! 8..10 ! 8..10 ! 8..10! % ! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! 4.4.3! 111 ! Delta N1 ! 6..8 ! 6..8 ! 6..8 ! 6..8 ! % ! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! 4.4.4! 112 ! Delta N1 ! 4..6 ! 4..6 ! 4..6 ! 4..6 ! % ! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! 4.4.5! 113 ! Delta N1 ! 2..4 ! 2..4 ! 2..4 !2..4 ! % ! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! 4.4.6! 114 ! Delta N1 ! 0.2..2! 0.2..2! 0.2..2!0.2..2! % ! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! 4.4.7! 115 ! Delta N1 ! </=0.2! </=0.2! </=0.2!</=0.2! % ! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! 4.5.1! 108 ! Y04.3 seconds after ! 5 ! 5 ! 5 ! 5 ! sec ! |
| ! ! ! PH4 entry calculation ! ! ! ! ! ! |
| ! ! ! of N1 Summary Limit ! ! ! ! ! ! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! 5.2 ! 109 ! Number 'X04' ! 5 ! 5 ! 5 ! 5 ! ! |
| ! ! ! consecutive legs ! ! ! ! ! ! |
| +-----------------------------------------------------------------------------+ |
(4) A319: CFMI Engines 56-5-B7
| +-----------------------------------------------------------------------------+ |
| !Report! Limit ! Description of Report Item !56-5-B7! SPARE ! SPARE ! Unit ! |
| !Item N! No. ! ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.1.4! 104 ! EGTL temperature limit cold ! 100 ! ! ! deg C! |
| ! ! ! engine start detection ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.2 ! 105 ! 'F04'th Take Off ! 5 ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.3 ! 106 ! Y04.1 seconds after PH 4 ! 40 ! ! ! sec ! |
| ! ! ! entry ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.4.1! ! Delta N1 ! >10 ! ! ! % ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.4.2! 110 ! Delta N1 ! 8..10 ! ! ! % ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.4.3! 111 ! Delta N1 ! 6..8 ! ! ! % ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.4.4! 112 ! Delta N1 ! 4..6 ! ! ! % ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.4.5! 113 ! Delta N1 ! 2..4 ! ! ! % ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.4.6! 114 ! Delta N1 ! 0.2..2! ! ! % ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.4.7! 115 ! Delta N1 ! </=0.2! ! ! % ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.5.1! 108 ! Y04.3 seconds after ! 5 ! ! ! sec ! |
| ! ! ! PH4 entry calculation of N1 ! ! ! ! ! |
| ! ! ! Summary Limit ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.2 ! 109 ! Number 'X04' consecutive legs ! 5 ! ! ! ! |
| +-----------------------------------------------------------------------------+ |
(5) A320: CFMI Engines 56-5-A1, 56-5-A3, 56-5-B4, 56-5-B5, 56-5-B6
| +-----------------------------------------------------------------------------+ |
| !Report! Description of ! CFM ! CFM ! CFM ! CFM ! CFM ! Unit ! |
| !Item ! Report Item !56-5-A1!56-5-A3!56-5-B4!56-5-B5!56-5-B6! ! |
| ! ! !-------!-------!-------!-------!-------!------! |
| ! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! ! |
| ! ! ! CFM #1! CFM #2! CFM #3! CFM #4! CFM #8! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.3 ! EGTL temperature ! 100 ! 100 ! 100 ! 100 ! 100 ! deg C! |
| ! ! limit cold engine ! ! ! ! ! ! ! |
| ! ! start detection ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.4 ! 'F04'th Take OFF ! 5 ! 5 ! 5 ! 5 ! 5 ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.5 ! 'Y04.1' seconds after ! 40 ! 40 ! 40 ! 40 ! 40 ! sec ! |
| ! ! PH 4 entry ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.7.1! Delta N1 ! >10 ! >10 ! >10 ! >10 ! >10 ! % ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.7.2! Delta N1 ! 8..10 ! 8..10 ! 8..10 ! 8..10 ! 8..10 ! % ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.7.3! Delta N1 ! 6..8 ! 6..8 ! 6..8 ! 6..8 ! 6..8 ! % ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.7.4! Delta N1 ! 4..6 ! 4..6 ! 4..6 ! 4..6 ! 4..6 ! % ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.7.5! Delta N1 ! 2..4 ! 2..4 ! 2..4 ! 2..4 ! 2..4 ! % ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.7.6! Delta N1 ! 0.2..2! 0.2..2! 0.2..2! 0.2..2! 0.2..2! % ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.7.7! Delta N1 ! <= 0.2! <= 0.2! <= 0.2! <= 0.2! <= 0.2! % ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.8.1!'Y04.3' seconds after ! 5 ! 5 ! 5 ! 5 ! 5 ! sec ! |
| ! ! PH 4 entry calculation! ! ! ! ! ! ! |
| ! ! of N1 Summary Limit ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.1 ! Number 'X04' ! 5 ! 5 ! 5 ! 5 ! 5 ! ! |
| ! ! consecutive legs ! ! ! ! ! ! ! |
| +-----------------------------------------------------------------------------+ |
(6) A321: CFMI Engines 56-5-B1, 56-5-B2, 56-5-B3, 56-5-B4
| +-----------------------------------------------------------------------------+ |
| !Report! Description of Report Item ! CFM ! CFM ! CFM ! CFM ! Unit ! |
| !Item ! !56-5-B1!56-5-B2!56-5-B3!56-5-B4! ! |
| ! ! !-------!-------!-------!-------!------! |
| ! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! ! |
| ! ! ! CFM #5! CFM #6! CFM #7! CFM #3! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.3 ! EGTL temperature limit cold ! 100 ! 100 ! 100 ! 100 ! deg C! |
| ! ! engine start detection ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.4 ! 'F04'th Take OFF ! 5 ! 5 ! 5 ! 5 ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.5 ! 'Y04.1' seconds after ! 40 ! 40 ! 40 ! 40 ! sec ! |
| ! ! PH 4 entry ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.7.1! Delta N1 ! >10 ! >10 ! >10 ! >10 ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.7.2! Delta N1 ! 8..10 ! 8..10 ! 8..10 ! 8..10 ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.7.3! Delta N1 ! 6..8 ! 6..8 ! 6..8 ! 6..8 ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.7.4! Delta N1 ! 4..6 ! 4..6 ! 4..6 ! 4..6 ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.7.5! Delta N1 ! 2..4 ! 2..4 ! 2..4 ! 2..4 ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.7.6! Delta N1 ! 0.2..2! 0.2..2! 0.2..2! 0.2..2! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.7.7! Delta N1 ! <= 0.2! <= 0.2! <= 0.2! <= 0.2! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.8.1! 'Y04.3' seconds after ! 5 ! 5 ! 5 ! 5 ! sec ! |
| ! ! PH 4 entry calculation ! ! ! ! ! ! |
| ! ! of N1 Summary Limit ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.1 ! Number 'X04' consecutive legs ! 5 ! 5 ! 5 ! ! ! |
| +-----------------------------------------------------------------------------+ |
(7) A319: CFMI Engines 56-5-A5, 56-5-B6, 56-5-B5, 56-5-A4, 56-5-B7
| +-----------------------------------------------------------------------------+ |
| !Report! Description of ! CFM ! CFM ! CFM ! CFM ! CFM ! Unit ! |
| !Item ! Report Item !56-5-A5!56-5-B6!56-5-B5!56-5-A4!56-5-B7! ! |
| ! ! !-------!-------!-------!-------!-------!------! |
| ! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! ! |
| ! ! ! C7xxxx! C8xxxx! C4xxxx! C6xxxx! C5xxxx! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.3 ! EGTL temperature ! 100 ! 100 ! 100 ! 100 ! 100 ! deg C! |
| ! ! limit cold engine ! ! ! ! ! ! ! |
| ! ! start detection ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.4 ! 'F04'th Take OFF ! 5 ! 5 ! 5 ! 5 ! 5 ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.5 ! 'Y04.1' seconds after ! 40 ! 40 ! 40 ! 40 ! 40 ! sec ! |
| ! ! PH 4 entry ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.7.1! Delta N1 ! >10 ! >10 ! >10 ! >10 ! >10 ! % ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.7.2! Delta N1 ! 8..10 ! 8..10 ! 8..10 ! 8..10 ! 8..10 ! % ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.7.3! Delta N1 ! 6..8 ! 6..8 ! 6..8 ! 6..8 ! 6..8 ! % ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.7.4! Delta N1 ! 4..6 ! 4..6 ! 4..6 ! 4..6 ! 4..6 ! % ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.7.5! Delta N1 ! 2..4 ! 2..4 ! 2..4 ! 2..4 ! 2..4 ! % ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.7.6! Delta N1 ! 0.2..2! 0.2..2! 0.2..2! 0.2..2! 0.2..2! % ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.7.7! Delta N1 ! <= 0.2! <= 0.2! <= 0.2! <= 0.2! <= 0.2! % ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.8.1!'Y04.3' seconds after ! 5 ! 5 ! 5 ! 5 ! 5 ! sec ! |
| ! ! PH 4 entry calculation! ! ! ! ! ! ! |
| ! ! of N1 Summary Limit ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.1 ! Number 'X04' ! 5 ! 5 ! 5 ! 5 ! 5 ! ! |
| ! ! consecutive legs ! ! ! ! ! ! ! |
| +-----------------------------------------------------------------------------+ |
(8) A318: CFMI Engines 56-5-B8, 56-5-B9
| +-----------------------------------------------------------------------------+ |
| !Report! Description of Report Item ! CFM ! CFM ! SPARE ! SPARE ! Unit ! |
| !Item ! !56-5-B8!56-5-B9! ! ! ! |
| ! ! !-------!-------!-------!-------!------! |
| ! ! !DMU/ID !DMU/ID ! ! ! ! |
| ! ! !C1xxxxx! C2xxxx! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.3 ! EGTL temperature limit cold ! 100 ! 100 ! ! ! deg C! |
| ! ! engine start detection ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.4 ! 'F04'th Take OFF ! 5 ! 5 ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.5 ! 'Y04.1' seconds after ! 40 ! 40 ! ! ! sec ! |
| ! ! PH 4 entry ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.7.1! Delta N1 ! >10 ! >10 ! ! ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.7.2! Delta N1 ! 8..10 ! 8..10 ! ! ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.7.3! Delta N1 ! 6..8 ! 6..8 ! ! ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.7.4! Delta N1 ! 4..6 ! 4..6 ! ! ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.7.5! Delta N1 ! 2..4 ! 2..4 ! ! ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.7.6! Delta N1 ! 0.2..2! 0.2..2! ! ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.7.7! Delta N1 ! <= 0.2! <= 0.2! ! ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.8.1! 'Y04.3' seconds after ! ! ! ! ! sec ! |
| ! ! PH 4 entry calculation of ! 5 ! 5 ! ! ! ! |
| ! ! N1 Summary Limit ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.1 ! Number 'X04' consecutive legs ! 5 ! 5 ! ! ! ! |
| +-----------------------------------------------------------------------------+ |
(9) A320: CFMI Engines 56-5-A1, 56-5-A3, 56-5-B4, 56-5-B5, 56-5-B6
| +-----------------------------------------------------------------------------+ |
| !Report! Description of ! CFM ! CFM ! CFM ! CFM ! CFM ! Unit ! |
| !Item ! Report Item !56-5-A1!56-5-A3!56-5-B4!56-5-B5!56-5-B6! ! |
| ! ! !-------!-------!-------!-------!-------!------! |
| ! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! ! |
| ! ! ! CFM #1! CFM #2! CFM #3! CFM #4! CFM #8! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.3 ! EGTL temperature ! 100 ! 100 ! 100 ! 100 ! 100 ! deg C! |
| ! ! limit cold engine ! ! ! ! ! ! ! |
| ! ! start detection ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.4 ! 'F04'th Take OFF ! 5 ! 5 ! 5 ! 5 ! 5 ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.5 ! 'Y04.1' seconds after ! 40 ! 40 ! 40 ! 40 ! 40 ! sec ! |
| ! ! PH 4 entry ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.7.1! Delta N1 ! >10 ! >10 ! >10 ! >10 ! >10 ! % ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.7.2! Delta N1 ! 8..10 ! 8..10 ! 8..10 ! 8..10 ! 8..10 ! % ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.7.3! Delta N1 ! 6..8 ! 6..8 ! 6..8 ! 6..8 ! 6..8 ! % ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.7.4! Delta N1 ! 4..6 ! 4..6 ! 4..6 ! 4..6 ! 4..6 ! % ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.7.5! Delta N1 ! 2..4 ! 2..4 ! 2..4 ! 2..4 ! 2..4 ! % ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.7.6! Delta N1 ! 0.2..2! 0.2..2! 0.2..2! 0.2..2! 0.2..2! % ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.7.7! Delta N1 ! <= 0.2! <= 0.2! <= 0.2! <= 0.2! <= 0.2! % ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.8.1!'Y04.3' seconds after ! 5 ! 5 ! 5 ! 5 ! 5 ! sec ! |
| ! ! PH 4 entry calculation! ! ! ! ! ! ! |
| ! ! of N1 Summary Limit ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.1 ! Number 'X04' ! 5 ! 5 ! 5 ! 5 ! 5 ! ! |
| ! ! consecutive legs ! ! ! ! ! ! ! |
| +-----------------------------------------------------------------------------+ |
(10) A321: CFMI Engines 56-5-B1, 56-5-B2, 56-5-B3, 56-5-B4
| +-----------------------------------------------------------------------------+ |
| !Report! Description of Report Item ! CFM ! CFM ! CFM ! CFM ! Unit ! |
| !Item ! !56-5-B1!56-5-B2!56-5-B3!56-5-B4! ! |
| ! ! !-------!-------!-------!-------!------! |
| ! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! ! |
| ! ! ! CFM #5! CFM #6! CFM #7! CFM #3! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.3 ! EGTL temperature limit cold ! 100 ! 100 ! 100 ! 100 ! deg C! |
| ! ! engine start detection ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.4 ! 'F04'th Take OFF ! 5 ! 5 ! 5 ! 5 ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.5 ! 'Y04.1' seconds after ! 40 ! 40 ! 40 ! 40 ! sec ! |
| ! ! PH 4 entry ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.7.1! Delta N1 ! >10 ! >10 ! >10 ! >10 ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.7.2! Delta N1 ! 8..10 ! 8..10 ! 8..10 ! 8..10 ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.7.3! Delta N1 ! 6..8 ! 6..8 ! 6..8 ! 6..8 ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.7.4! Delta N1 ! 4..6 ! 4..6 ! 4..6 ! 4..6 ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.7.5! Delta N1 ! 2..4 ! 2..4 ! 2..4 ! 2..4 ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.7.6! Delta N1 ! 0.2..2! 0.2..2! 0.2..2! 0.2..2! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.7.7! Delta N1 ! <= 0.2! <= 0.2! <= 0.2! <= 0.2! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.8.1! 'Y04.3' seconds after ! 5 ! 5 ! 5 ! 5 ! sec ! |
| ! ! PH 4 entry calculation ! ! ! ! ! ! |
| ! ! of N1 Summary Limit ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.1 ! Number 'X04' consecutive legs ! 5 ! 5 ! 5 ! ! ! |
| +-----------------------------------------------------------------------------+ |
(11) A319: CFMI Engines 56-5-A5, 56-5-B6, 56-5-B5, 56-5-A4, 56-5-B7
| +-----------------------------------------------------------------------------+ |
| !Report! Description of ! CFM ! CFM ! CFM ! CFM ! CFM ! Unit ! |
| !Item ! Report Item !56-5-A5!56-5-B6!56-5-B5!56-5-A4!56-5-B7! ! |
| ! ! !-------!-------!-------!-------!-------!------! |
| ! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! ! |
| ! ! ! C7xxxx! C8xxxx! C4xxxx! C6xxxx! C5xxxx! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.3 ! EGTL temperature ! 100 ! 100 ! 100 ! 100 ! 100 ! deg C! |
| ! ! limit cold engine ! ! ! ! ! ! ! |
| ! ! start detection ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.4 ! 'F04'th Take OFF ! 5 ! 5 ! 5 ! 5 ! 5 ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.5 ! 'Y04.1' seconds after ! 40 ! 40 ! 40 ! 40 ! 40 ! sec ! |
| ! ! PH 4 entry ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.7.1! Delta N1 ! >10 ! >10 ! >10 ! >10 ! >10 ! % ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.7.2! Delta N1 ! 8..10 ! 8..10 ! 8..10 ! 8..10 ! 8..10 ! % ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.7.3! Delta N1 ! 6..8 ! 6..8 ! 6..8 ! 6..8 ! 6..8 ! % ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.7.4! Delta N1 ! 4..6 ! 4..6 ! 4..6 ! 4..6 ! 4..6 ! % ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.7.5! Delta N1 ! 2..4 ! 2..4 ! 2..4 ! 2..4 ! 2..4 ! % ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.7.6! Delta N1 ! 0.2..2! 0.2..2! 0.2..2! 0.2..2! 0.2..2! % ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.7.7! Delta N1 ! <= 0.2! <= 0.2! <= 0.2! <= 0.2! <= 0.2! % ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.8.1!'Y04.3' seconds after ! 5 ! 5 ! 5 ! 5 ! 5 ! sec ! |
| ! ! PH 4 entry calculation! ! ! ! ! ! ! |
| ! ! of N1 Summary Limit ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.1 ! Number 'X04' ! 5 ! 5 ! 5 ! 5 ! 5 ! ! |
| ! ! consecutive legs ! ! ! ! ! ! ! |
| +-----------------------------------------------------------------------------+ |
(12) A318: CFMI Engines 56-5-B8, 56-5-B9
| +-----------------------------------------------------------------------------+ |
| !Report! Description of Report Item ! CFM ! CFM ! SPARE ! SPARE ! Unit ! |
| !Item ! !56-5-B8!56-5-B9! ! ! ! |
| ! ! !-------!-------!-------!-------!------! |
| ! ! !DMU/ID !DMU/ID ! ! ! ! |
| ! ! !C1xxxxx! C2xxxx! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.3 ! EGTL temperature limit cold ! 100 ! 100 ! ! ! deg C! |
| ! ! engine start detection ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.4 ! 'F04'th Take OFF ! 5 ! 5 ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.5 ! 'Y04.1' seconds after ! 40 ! 40 ! ! ! sec ! |
| ! ! PH 4 entry ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.7.1! Delta N1 ! >10 ! >10 ! ! ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.7.2! Delta N1 ! 8..10 ! 8..10 ! ! ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.7.3! Delta N1 ! 6..8 ! 6..8 ! ! ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.7.4! Delta N1 ! 4..6 ! 4..6 ! ! ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.7.5! Delta N1 ! 2..4 ! 2..4 ! ! ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.7.6! Delta N1 ! 0.2..2! 0.2..2! ! ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.7.7! Delta N1 ! <= 0.2! <= 0.2! ! ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.8.1! 'Y04.3' seconds after ! ! ! ! ! sec ! |
| ! ! PH 4 entry calculation of ! 5 ! 5 ! ! ! ! |
| ! ! N1 Summary Limit ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.1 ! Number 'X04' consecutive legs ! 5 ! 5 ! ! ! ! |
| +-----------------------------------------------------------------------------+ |
(13) A320: CFMI Engines 56-5-A1, 56-5-A3, 56-5-B4, 56-5-B5, 56-5-B6
| +-----------------------------------------------------------------------------+ |
| !Report!Limit! Description of ! CFM ! CFM ! CFM ! CFM ! CFM ! Unit ! |
| !Item !No. ! Report Item !56-5-A1!56-5-A3!56-5-B4!56-5-B5!56-5-B6! ! |
| ! ! ! !-------!-------!-------!-------!-------!------! |
| ! ! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! ! |
| ! ! ! ! CFM #1! CFM #2! CFM #3! CFM #4! CFM #8! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.3 ! 104 !EGT limit at ! 100 ! 100 ! 100 ! 100 ! 100 ! deg C! |
| ! ! !engine start ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.4 ! 105 !"F04"frequency ! 5 ! 5 ! 5 ! 5 ! 5 ! ! |
| ! ! ! of report ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.5 ! 106 !"Y04.1" seconds ! 40 ! 40 ! 40 ! 40 ! 40 ! sec ! |
| ! ! !after PH 4 entry ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.7.1! !Delta N1 ! >10 ! >10 ! >10 ! >10 ! >10 ! % ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.7.2! 110 !Delta N1 limit 1 ! 8..10 ! 8..10 ! 8..10 ! 8..10 ! 8..10 ! % ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.7.3! 111 !Delta N1 limit 2 ! 6..8 ! 6..8 ! 6..8 ! 6..8 ! 6..8 ! % ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.7.4! 112 !Delta N1 limit 3 ! 4..6 ! 4..6 ! 4..6 ! 4..6 ! 4..6 ! % ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.7.5! 113 !Delta N1 limit 4 ! 2..4 ! 2..4 ! 2..4 ! 2..4 ! 2..4 ! % ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.7.6! 114 !Delta N1 limit 5 ! 0.2..2! 0.2..2! 0.2..2! 0.2..2! 0.2..2! % ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.7.7! 115 !Delta N1 limit 6 ! <= 0.2! <= 0.2! <= 0.2! <= 0.2! <= 0.2! % ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.8.1! 108 !"Y04.3" seconds ! 5 ! 5 ! 5 ! 5 ! 5 ! sec ! |
| ! ! !after PH 4 entry ! ! ! ! ! ! ! |
| ! ! !calculation of ! ! ! ! ! ! ! |
| ! ! !Delta N1 Summary ! ! ! ! ! ! ! |
| ! ! !Limit ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.1 ! 109 !Number "X04" ! 5 ! 5 ! 5 ! 5 ! 5 ! ! |
| ! ! !consecutive legs ! ! ! ! ! ! ! |
| +------------------------------------------------------------------------------+ |
(14) A321: CFMI Engines 56-5-B1, 56-5-B2, 56-5-B3, 56-5-B4
| +-----------------------------------------------------------------------------+ |
| !Report!Limit! Description of ! CFM ! CFM ! CFM ! CFM ! Unit ! |
| !Item !No. ! Report Item !56-5-B1!56-5-B2!56-5-B3!56-5-B4! ! |
| ! ! ! !-------!-------!-------!-------!------! |
| ! ! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! ! |
| ! ! ! ! CFM #5! CFM #6! CFM #7! CFM #3! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.3 ! 104 !EGT limit at engine ! 100 ! 100 ! 100 ! 100 ! deg C! |
| ! ! !start ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.4 ! 105 !"F04"frequency of report ! 5 ! 5 ! 5 ! 5 ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.5 ! 106 !"Y04.1" seconds after ! 40 ! 40 ! 40 ! 40 ! sec ! |
| ! ! !PH 4 entry ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.7.1! !Delta N1 ! >10 ! >10 ! >10 ! >10 ! % ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.7.2! 110 !Delta N1 limit 1 ! 8..10 ! 8..10 ! 8..10 ! 8..10 ! % ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.7.3! 111 !Delta N1 limit 2 ! 6..8 ! 6..8 ! 6..8 ! 6..8 ! % ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.7.4! 112 !Delta N1 limit 3 ! 4..6 ! 4..6 ! 4..6 ! 4..6 ! % ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.7.5! 113 !Delta N1 limit 4 ! 2..4 ! 2..4 ! 2..4 ! 2..4 ! % ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.7.6! 114 !Delta N1 limit 5 ! 0.2..2! 0.2..2! 0.2..2! 0.2..2! % ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.7.7! 115 !Delta N1 limit 6 ! <= 0.2! <= 0.2! <= 0.2! <= 0.2! % ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.8.1! 108 !"Y04.3" seconds after ! 5 ! 5 ! 5 ! 5 ! sec ! |
| ! ! !PH 4 entry calculation ! ! ! ! ! ! |
| ! ! !of Delta N1 Summary Limit! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.1 ! 109 !Number "X04" consecutive ! 5 ! 5 ! 5 ! ! ! |
| ! ! !legs ! ! ! ! ! ! |
| +-----------------------------------------------------------------------------+ |
(15) A319: CFMI Engines 56-5-A5, 56-5-B6, 56-5-B5, 56-5-A4, 56-5-B7
| +-----------------------------------------------------------------------------+ |
| !Report!Limit! Description of ! CFM ! CFM ! CFM ! CFM ! CFM ! Unit ! |
| !Item !No. ! Report Item !56-5-A5!56-5-B6!56-5-B5!56-5-A4!56-5-B7! ! |
| ! ! ! !-------!-------!-------!-------!-------!------! |
| ! ! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! ! |
| ! ! ! ! C7xxxx! C8xxxx! C4xxxx! C6xxxx! C5xxxx! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.1.4! 104 !EGT limit at ! 100 ! 100 ! 100 ! 100 ! 100 ! deg C! |
| ! ! !engine start ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.2 ! 105 !"F04"frequency of! 5 ! 5 ! 5 ! 5 ! 5 ! ! |
| ! ! !report ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.3 ! 106 !"Y04.1" seconds ! 40 ! 40 ! 40 ! 40 ! 40 ! sec ! |
| ! ! !after PH 4 entry ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.4.1! !Delta N1 ! >10 ! >10 ! >10 ! >10 ! >10 ! % ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.4.2! 110 !Delta N1 limit 1 ! 8..10 ! 8..10 ! 8..10 ! 8..10 ! 8..10 ! % ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.4.3! 111 !Delta N1 limit 2 ! 6..8 ! 6..8 ! 6..8 ! 6..8 ! 6..8 ! % ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.4.4! 112 !Delta N1 limit 3 ! 4..6 ! 4..6 ! 4..6 ! 4..6 ! 4..6 ! % ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.4.5! 113 !Delta N1 limit 4 ! 2..4 ! 2..4 ! 2..4 ! 2..4 ! 2..4 ! % ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.4.6! 114 !Delta N1 limit 5 ! 0.2..2! 0.2..2! 0.2..2! 0.2..2! 0.2..2! % ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.4.7! 115 !Delta N1 limit 6 ! <= 0.2! <= 0.2! <= 0.2! <= 0.2! <= 0.2! % ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.5.1! 108 !"Y04.3" seconds ! 5 ! 5 ! 5 ! 5 ! 5 ! sec ! |
| ! ! !after PH 4 entry ! ! ! ! ! ! ! |
| ! ! !calculation of ! ! ! ! ! ! ! |
| ! ! !Delta N1 Summary ! ! ! ! ! ! ! |
| ! ! !Limit ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.2 ! 109 !Number "X04" ! 5 ! 5 ! 5 ! 5 ! 5 ! ! |
| ! ! !consecutive legs ! ! ! ! ! ! ! |
| +-----------------------------------------------------------------------------+ |
(16) A318: CFMI Engines 56-5-B8, 56-5-B9
| +-----------------------------------------------------------------------------+ |
| !Report!Limit! Description of ! CFM ! CFM ! SPARE ! SPARE ! Unit ! |
| !Item !No. ! Report Item !56-5-B8!56-5-B9! ! ! ! |
| ! ! ! !-------!-------!-------!-------!------! |
| ! ! ! !DMU/ID !DMU/ID ! ! ! ! |
| ! ! ! !C1xxxxx! C2xxxx! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.3 ! 104 !EGT limit at engine start! 100 ! 100 ! ! ! deg C! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.4 ! 105 !"F04"frequency of report ! 5 ! 5 ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.5 ! 106 !"Y04.1" seconds after ! 40 ! 40 ! ! ! sec ! |
| ! ! !PH 4 entry ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.7.1! !Delta N1 ! >10 ! >10 ! ! ! % ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.7.2! 110 !Delta N1 limit 1 ! 8..10 ! 8..10 ! ! ! % ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.7.3! 111 !Delta N1 limit 2 ! 6..8 ! 6..8 ! ! ! % ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.7.4! 112 !Delta N1 limit 3 ! 4..6 ! 4..6 ! ! ! % ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.7.5! 113 !Delta N1 limit 4 ! 2..4 ! 2..4 ! ! ! % ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.7.6! 114 !Delta N1 limit 5 ! 0.2..2! 0.2..2! ! ! % ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.7.7! 115 !Delta N1 limit 6 ! <= 0.2! <= 0.2! ! ! % ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.8.1! 108 !"Y04.3" seconds after ! ! ! ! ! sec ! |
| ! ! !PH 4 entry calculation of! 5 ! 5 ! ! ! ! |
| ! ! !Delta N1 Summary Limit ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.1 ! 109 !Number "X04" consecutive ! 5 ! 5 ! ! ! ! |
| ! ! !legs ! ! ! ! ! ! |
| +-----------------------------------------------------------------------------+ |
V. Report Limits for Engine Report On Request <05>
(1) A320: CFMI Engines 56-5-A1, 56-5-A3, 56-5-B4
| +-----------------------------------------------------------------------------+ |
| !Report! Limit ! Description of Report Item !56-5-A1!56-5-A3!56-5-B4! Unit ! |
| !Item N! No. ! ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! ! |
| ! N O T A P P L I C A B L E ! |
| ! ! |
| +-----------------------------------------------------------------------------+ |
(2) A321: CFMI Engines 56-5-B1, 56-5-B2, 56-5-B3
| +-----------------------------------------------------------------------------+ |
| !Report! Limit ! Description of Report Item !56-5-B1!56-5-B2!56-5-B3! Unit ! |
| !Item N! No. ! ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! ! |
| ! N O T A P P L I C A B L E ! |
| ! ! |
| +-----------------------------------------------------------------------------+ |
(3) A319: CFMI Engines 56-5-A5, 56-5-B6, 56-5-B5, 56-5A4
| +-----------------------------------------------------------------------------+ |
| !Report! Limit ! Description of Report !56-5-A5!56-5-B6!56-5-B5!56-5A4! Unit ! |
| !Item N! No. ! Item ! ! ! ! ! ! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! ! |
| ! N O T A P P L I C A B L E ! |
| ! ! |
| +-----------------------------------------------------------------------------+ |
(4) A319: CFMI Engines 56-5-B7
| +-----------------------------------------------------------------------------+ |
| !Report! Limit ! Description of Report Item !56-5-B7! SPARE ! SPARE ! Unit ! |
| !Item N! No. ! ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! ! |
| ! N O T A P P L I C A B L E ! |
| ! ! |
| +-----------------------------------------------------------------------------+ |
(5) A320: CFMI Engines 56-5-A1, 56-5-A3, 56-5-B4, 56-5-B5, 56-5-B6
| +-----------------------------------------------------------------------------+ |
| !Report! Description of ! CFM ! CFM ! CFM ! CFM ! CFM ! Unit ! |
| !Item ! Report Item !56-5-A1!56-5-A3!56-5-B4!56-5-B5!56-5-B6! ! |
| ! ! !-------!-------!-------!-------!-------!------! |
| ! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! ! |
| ! ! ! CFM #1! CFM #2! CFM #3! CFM #4! CFM #8! ! |
| !------!-----------------------!-------!-------!-------!-------!-- ----!------! |
| ! ! |
| ! N O T A P P L I C A B L E ! |
| ! ! |
| +-----------------------------------------------------------------------------+ |
(6) A321: CFMI Engines 56-5-B1, 56-5-B2, 56-5-B3, 56-5-B4
| +-----------------------------------------------------------------------------+ |
| !Report! Description of Report Item ! CFM ! CFM ! CFM ! CFM ! Unit ! |
| !Item ! !56-5-B1!56-5-B2!56-5-B3!56-5-B4! ! |
| ! ! !-------!-------!-------!-------!------! |
| ! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! ! |
| ! ! ! CFM #5! CFM #6! CFM #7! CFM #3! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! ! |
| ! N O T A P P L I C A B L E ! |
| ! ! |
| +-----------------------------------------------------------------------------+ |
(7) A319: CFMI Engines 56-5-A5, 56-5-B6, 56-5-B5, 56-5A4, 56-5-B7
| +-----------------------------------------------------------------------------+ |
| !Report! Description of ! CFM ! CFM ! CFM ! CFM ! CFM ! Unit ! |
| !Item ! Report Item !56-5-A5!56-5-B6!56-5-B5!56-5-A4!56-5-B7! ! |
| ! ! !-------!-------!-------!-------!-------!------! |
| ! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! ! |
| ! ! ! C7xxxx! C8xxxx! C4xxxx! C6xxxx! C5xxxx! ! |
| !------!-----------------------!-------!-------!-------!-------!-- ----!------! |
| ! ! |
| ! N O T A P P L I C A B L E ! |
| ! ! |
| +-----------------------------------------------------------------------------+ |
(8) A318: CFMI Engines 56-5-B8, 56-5-B9
| +-----------------------------------------------------------------------------+ |
| !Report! Description of Report Item ! CFM ! CFM ! SPARE ! SPARE ! Unit ! |
| !Item ! !56-5-B8!56-5-B9! ! ! ! |
| ! ! !-------!-------!-------!-------!------! |
| ! ! !DMU/ID !DMU/ID ! ! ! ! |
| ! ! !C1xxxxx! C2xxxx! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! ! |
| ! N O T A P P L I C A B L E ! |
| ! ! |
| +-----------------------------------------------------------------------------+ |
(9) A320: CFMI Engines 56-5-A1, 56-5-A3, 56-5-B4, 56-5-B5, 56-5-B6
| +-----------------------------------------------------------------------------+ |
| !Report! Description of ! CFM ! CFM ! CFM ! CFM ! CFM ! Unit ! |
| !Item ! Report Item !56-5-A1!56-5-A3!56-5-B4!56-5-B5!56-5-B6! ! |
| ! ! !-------!-------!-------!-------!-------!------! |
| ! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! ! |
| ! ! ! CFM #1! CFM #2! CFM #3! CFM #4! CFM #8! ! |
| !------!-----------------------!-------!-------!-------!-------!-- ----!------! |
| ! ! |
| ! N O T A P P L I C A B L E ! |
| ! ! |
| +-----------------------------------------------------------------------------+ |
(10) A321: CFMI Engines 56-5-B1, 56-5-B2, 56-5-B3, 56-5-B4
| +-----------------------------------------------------------------------------+ |
| !Report! Description of Report Item ! CFM ! CFM ! CFM ! CFM ! Unit ! |
| !Item ! !56-5-B1!56-5-B2!56-5-B3!56-5-B4! ! |
| ! ! !-------!-------!-------!-------!------! |
| ! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! ! |
| ! ! ! CFM #5! CFM #6! CFM #7! CFM #3! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! ! |
| ! N O T A P P L I C A B L E ! |
| ! ! |
| +-----------------------------------------------------------------------------+ |
(11) A319: CFMI Engines 56-5-A5, 56-5-B6, 56-5-B5, 56-5A4, 56-5-B7
| +-----------------------------------------------------------------------------+ |
| !Report! Description of ! CFM ! CFM ! CFM ! CFM ! CFM ! Unit ! |
| !Item ! Report Item !56-5-A5!56-5-B6!56-5-B5!56-5-A4!56-5-B7! ! |
| ! ! !-------!-------!-------!-------!-------!------! |
| ! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! ! |
| ! ! ! C7xxxx! C8xxxx! C4xxxx! C6xxxx! C5xxxx! ! |
| !------!-----------------------!-------!-------!-------!-------!-- ----!------! |
| ! ! |
| ! N O T A P P L I C A B L E ! |
| ! ! |
| +-----------------------------------------------------------------------------+ |
(12) A318: CFMI Engines 56-5-B8, 56-5-B9
| +-----------------------------------------------------------------------------+ |
| !Report! Description of Report Item ! CFM ! CFM ! SPARE ! SPARE ! Unit ! |
| !Item ! !56-5-B8!56-5-B9! ! ! ! |
| ! ! !-------!-------!-------!-------!------! |
| ! ! !DMU/ID !DMU/ID ! ! ! ! |
| ! ! !C1xxxxx! C2xxxx! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! ! |
| ! N O T A P P L I C A B L E ! |
| ! ! |
| +-----------------------------------------------------------------------------+ |
W. Report Limits for Engine Gas Path Advisory Report <06>
(1) A320: CFMI Engines 56-5-A1, 56-5-A3, 56-5-B4
| +-----------------------------------------------------------------------------+ |
| !Report! Limit ! Description of Report Item !56-5-A1!56-5-A3!56-5-B4! Unit ! |
| !Item N! No. ! ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.1 ! 125 ! EGTL1 limit ! 895 ! 895 ! 950 ! deg C! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.2 ! 126 ! EGTL2 (yellow limit) ! 855 ! 855 ! 915 ! deg C! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.3 ! 127 ! EGTL3 (red limit) ! 890 ! 890 ! 890 ! deg C! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.4 ! 128 ! N1L1.1 (yellow limit) ! 112 ! 112 ! 112 ! % ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.5 ! 129 ! N1L1.2 (red limit) ! 102 ! 102 ! 102 ! % ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.6 ! 130 ! N2L1.1 (yellow limit) ! 112 ! 112 ! 112 ! % ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.7 ! 131 ! N2L1.2 (red limit) ! 105 ! 105 ! 105 ! % ! |
| +-----------------------------------------------------------------------------+ |
(2) A321: CFMI Engines 56-5-B1, 56-5-B2, 56-5-B3
| +-----------------------------------------------------------------------------+ |
| !Report! Limit ! Description of Report Item !56-5-B1!56-5-B2!56-5-B3! Unit ! |
| !Item N! No. ! ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.1 ! 125 ! EGTL1 limit ! 950 ! 950 ! 950 ! deg C! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.2 ! 126 ! EGTL2 (yellow limit) ! 915 ! 915 ! 915 ! deg C! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.3 ! 127 ! EGTL3 (red limit) ! 950 ! 950 ! 950 ! deg C! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.4 ! 128 ! N1L1.1 (yellow limit) ! 112 ! 112 ! 112 ! % ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.5 ! 129 ! N1L1.2 (red limit) ! 104 ! 104 ! 104 ! % ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.6 ! 130 ! N2L1.1 (yellow limit) ! 112 ! 112 ! 112 ! % ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.7 ! 131 ! N2L1.2 (red limit) ! 105 ! 105 ! 105 ! % ! |
| +-----------------------------------------------------------------------------+ |
(3) A319: CFMI Engines 56-5-A5, 56-5-B6, 56-5-B5, 56-5A4
| +-----------------------------------------------------------------------------+ |
| !Report! Limit ! Description of Report !56-5-A5!56-5-B6!56-5-B5!56-5A4! Unit ! |
| !Item N! No. ! Item ! ! ! ! ! ! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! 5.1 ! 125 ! EGTL1 limit ! 890 ! 950 ! 950 ! 890 ! deg C! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! 5.2 ! 126 ! EGTL2 (yellow limit) ! 855 ! 915 ! 915 ! 855 ! deg C! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! 5.3 ! 127 ! EGTL3 (red limit) ! 890 ! 950 ! 950 ! 890 ! deg C! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! 5.4 ! 128 ! N1L1.1 (yellow limit) ! 112 ! 112 ! 112 ! 112 ! % ! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! 5.5 ! 129 ! N1L1.2 (red limit) ! 102 ! 104 ! 104 ! 102 ! % ! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! 5.6 ! 130 ! N2L1.1 (yellow limit) ! 112 ! 112 ! 112 ! 112 ! % ! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! 5.7 ! 131 ! N2L1.2 (red limit) ! 105 ! 105 ! 105 ! 105 ! % ! |
| +-----------------------------------------------------------------------------+ |
(4) A319: CFMI Engines 56-5-B7
| +-----------------------------------------------------------------------------+ |
| !Report! Limit ! Description of Report Item !56-5-B7! SPARE ! SPARE ! Unit ! |
| !Item N! No. ! ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.1 ! 125 ! EGTL1 limit ! 950 ! ! ! deg C! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.2 ! 126 ! EGTL2 (yellow limit) ! 915 ! ! ! deg C! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.3 ! 127 ! EGTL3 (red limit) ! 950 ! ! ! deg C! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.4 ! 128 ! N1L1.1 (yellow limit) ! 112 ! ! ! % ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.5 ! 129 ! N1L1.2 (red limit) ! 104 ! ! ! % ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.6 ! 130 ! N2L1.1 (yellow limit) ! 112 ! ! ! % ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.7 ! 131 ! N2L1.2 (red limit) ! 105 ! ! ! % ! |
| +-----------------------------------------------------------------------------+ |
(5) A318: CFMI Engines 56-5-B8, 56-5-B9
| +----------------------------------------------------------------------------+ |
| !Report!Limit ! Description of Report Item !56-5-B8!56-5-B9! SPARE ! Unit ! |
| !Item N!No. ! ! ! ! ! ! |
| !------!------!-------------------------------!-------!-------!-------!------! |
| ! 5.1 ! 125 ! EGTL1 limit ! 950 ! 950 ! ! deg C! |
| !------!------!-------------------------------!-------!-------!-------!------! |
| ! 5.2 ! 126 ! EGTL2 (yellow limit) ! 915 ! 915 ! ! deg C! |
| !------!------!-------------------------------!-------!-------!-------!------! |
| ! 5.3 ! 127 ! EGTL3 (red limit) ! 950 ! 950 ! ! deg C! |
| !------!------!-------------------------------!-------!-------!-------!------! |
| ! 5.4 ! 128 ! N1L1.1 (yellow limit) ! 112 ! 112 ! ! % ! |
| !------!------!-------------------------------!-------!-------!-------!------! |
| ! 5.5 ! 129 ! N1L1.2 (red limit) ! 104 ! 104 ! ! % ! |
| !------!------!-------------------------------!-------!-------!-------!------! |
| ! 5.6 ! 130 ! N2L1.1 (yellow limit) ! 112 ! 112 ! ! % ! |
| !------!------!-------------------------------!-------!-------!-------!------! |
| ! 5.7 ! 131 ! N2L1.2 (red limit) ! 105 ! 105 ! ! % ! |
| +----------------------------------------------------------------------------+ |
(6) A320: CFMI Engines 56-5-A1, 56-5-A3, 56-5-B4, 56-5-B5, 56-5-B6
| +-----------------------------------------------------------------------------+ |
| !Report! Description of ! CFM ! CFM ! CFM ! CFM ! CFM ! Unit ! |
| !Item ! Report Item !56-5-A1!56-5-A3!56-5-B4!56-5-B5!56-5-B6! ! |
| ! ! !-------!-------!-------!-------!-------!------! |
| ! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! ! |
| ! ! ! CFM #1! CFM #2! CFM #3! CFM #4! CFM #8! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.1 ! EGTL1 limit ! 890 ! 890 ! 950 ! 950 ! 950 ! deg C! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.2 ! EGTL2 limit ! 855 ! 855 ! 855 ! 915 ! 915 ! deg C! |
| ! ! (yellow limit) ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.3 ! EGTL3 limit ! 890 ! 890 ! 890 ! 950 ! 950 ! deg C! |
| ! ! (red limit) ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.4 ! N1L1.1 limit ! 112 ! 112 ! 112 ! 112 ! 112 ! % ! |
| ! ! (yellow limit) ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.5 ! N1L1.2 limit ! 102 ! 102 ! 104 ! 104 ! 104 ! % ! |
| ! ! (red limit) ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.6 ! N2L1.1 limit ! 112 ! 112 ! 112 ! 112 ! 112 ! % ! |
| ! ! (yellow limit) ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.7 ! N2L1.2 limit ! 105 ! 105 ! 105 ! 105 ! 105 ! % ! |
| ! ! (red limit) ! ! ! ! ! ! ! |
| +-----------------------------------------------------------------------------+ |
(7) A321: CFMI Engines 56-5-B1, 56-5-B2, 56-5-B3, 56-5-B4
| +-----------------------------------------------------------------------------+ |
| !Report! Description of Report Item ! CFM ! CFM ! CFM ! CFM ! Unit ! |
| !Item ! !56-5-B1!56-5-B2!56-5-B3!56-5-B4! ! |
| ! ! !-------!-------!-------!-------!------! |
| ! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! ! |
| ! ! ! CFM #5! CFM #6! CFM #7! CFM #3! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.1 ! EGTL1 limit ! 950 ! 950 ! 950 ! 950 ! deg C! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.2 ! EGTL2 limit (yellow limit) ! 915 ! 915 ! 915 ! 855 ! deg C! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.3 ! EGTL3 limit (red limit) ! 950 ! 950 ! 950 ! 890 ! deg C! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.4 ! N1L1.1 limit (yellow limit) ! 112 ! 112 ! 112 ! 112 ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.5 ! N1L1.2 limit (red limit) ! 104 ! 104 ! 104 ! 104 ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.6 ! N2L1.1 limit (yellow limit) ! 112 ! 112 ! 112 ! 112 ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.7 ! N2L1.2 limit (red limit) ! 105 ! 105 ! 105 ! 105 ! % ! |
| +-----------------------------------------------------------------------------+ |
(8) A319: CFMI Engines 56-5-A5, 56-5-B6, 56-5-B5, 56-5-A4, 56-5-B7
| +-----------------------------------------------------------------------------+ |
| !Report! Description of ! CFM ! CFM ! CFM ! CFM ! CFM ! Unit ! |
| !Item ! Report Item !56-5-A5!56-5-B6!56-5-B5!56-5-A4!56-5-B7! ! |
| ! ! !-------!-------!-------!-------!-------!------! |
| ! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! ! |
| ! ! ! C7xxxx! C8xxxx! C4xxxx! C6xxxx! C5xxxx! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.1 ! EGTL1 limit ! 890 ! 950 ! 950 ! 890 ! 950 ! deg C! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.2 ! EGTL2 limit ! 855 ! 915 ! 915 ! 855 ! 915 ! deg C! |
| ! ! (yellow limit) ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.3 ! EGTL3 limit ! 890 ! 950 ! 950 ! 890 ! 950 ! deg C! |
| ! ! (red limit) ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.4 ! N1L1.1 limit ! 112 ! 112 ! 112 ! 112 ! 112 ! % ! |
| ! ! (yellow limit) ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.5 ! N1L1.2 limit ! 102 ! 104 ! 104 ! 102 ! 104 ! % ! |
| ! ! (red limit) ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.6 ! N2L1.1 limit ! 112 ! 112 ! 112 ! 112 ! 112 ! % ! |
| ! ! (yellow limit) ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.7 ! N2L1.2 limit ! 105 ! 105 ! 105 ! 105 ! 105 ! % ! |
| ! ! (red limit) ! ! ! ! ! ! ! |
| +-----------------------------------------------------------------------------+ |
(9) A318: CFMI Engines 56-5-B8, 56-5-B9
| +-----------------------------------------------------------------------------+ |
| !Report! Description of Report Item ! CFM ! CFM ! SPARE ! SPARE ! Unit ! |
| !Item ! !56-5-B8!56-5-B9! ! ! ! |
| ! ! !-------!-------!-------!-------!------! |
| ! ! !DMU/ID !DMU/ID ! ! ! ! |
| ! ! !C1xxxxx! C2xxxx! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.1 ! EGTL1 limit ! 950 ! 950 ! ! ! deg C! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.2 ! EGTL2 limit (yellow limit) ! 915 ! 915 ! ! ! deg C! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.3 ! EGTL3 limit (red limit) ! 950 ! 950 ! ! ! deg C! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.4 ! N1L1.1 limit (yellow limit) ! 112 ! 112 ! ! ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.5 ! N1L1.2 limit (red limit) ! 104 ! 104 ! ! ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.6 ! N2L1.1 limit (yellow limit) ! 112 ! 112 ! ! ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.7 ! N2L1.2 limit (red limit) ! 105 ! 105 ! ! ! % ! |
| +-----------------------------------------------------------------------------+ |
(10) A320: CFMI Engines 56-5-A1, 56-5-A3, 56-5-B4, 56-5-B5, 56-5-B6
| +-----------------------------------------------------------------------------+ |
| !Report! Description of ! CFM ! CFM ! CFM ! CFM ! CFM ! Unit ! |
| !Item ! Report Item !56-5-A1!56-5-A3!56-5-B4!56-5-B5!56-5-B6! ! |
| ! ! !-------!-------!-------!-------!-------!------! |
| ! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! ! |
| ! ! ! CFM #1! CFM #2! CFM #3! CFM #4! CFM #8! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.1 ! EGTL1 limit ! 890 ! 890 ! 950 ! 950 ! 950 ! deg C! |
| ! ! (red limit) ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.2 ! EGTL2 limit ! 855 ! 855 ! 915 ! 915 ! 915 ! deg C! |
| ! ! (yellow limit) ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.3 ! Not applicable ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.4 ! N1L1.1 limit ! 112 ! 112 ! 112 ! 112 ! 112 ! % ! |
| ! ! (yellow limit) ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.5 ! N1L1.2 limit ! 102 ! 102 ! 104 ! 104 ! 104 ! % ! |
| ! ! (red limit) ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.6 ! N2L1.1 limit ! 112 ! 112 ! 112 ! 112 ! 112 ! % ! |
| ! ! (yellow limit) ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.7 ! N2L1.2 limit ! 105 ! 105 ! 105 ! 105 ! 105 ! % ! |
| ! ! (red limit) ! ! ! ! ! ! ! |
| +-----------------------------------------------------------------------------+ |
(11) A321: CFMI Engines 56-5-B1, 56-5-B2, 56-5-B3, 56-5-B4
| +-----------------------------------------------------------------------------+ |
| !Report! Description of Report Item ! CFM ! CFM ! CFM ! CFM ! Unit ! |
| !Item ! !56-5-B1!56-5-B2!56-5-B3!56-5-B4! ! |
| ! ! !-------!-------!-------!-------!------! |
| ! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! ! |
| ! ! ! CFM #5! CFM #6! CFM #7! CFM #3! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.1 ! EGTL1 limit (red limit) ! 950 ! 950 ! 950 ! 950 ! deg C! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.2 ! EGTL2 limit (yellow limit) ! 915 ! 915 ! 915 ! 915 ! deg C! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.3 ! Not applicable ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.4 ! N1L1.1 limit (yellow limit) ! 112 ! 112 ! 112 ! 112 ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.5 ! N1L1.2 limit (red limit) ! 104 ! 104 ! 104 ! 104 ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.6 ! N2L1.1 limit (yellow limit) ! 112 ! 112 ! 112 ! 112 ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.7 ! N2L1.2 limit (red limit) ! 105 ! 105 ! 105 ! 105 ! % ! |
| +-----------------------------------------------------------------------------+ |
(12) A319: CFMI Engines 56-5-A5, 56-5-B6, 56-5-B5, 56-5-A4, 56-5-B7
| +-----------------------------------------------------------------------------+ |
| !Report! Description of ! CFM ! CFM ! CFM ! CFM ! CFM ! Unit ! |
| !Item ! Report Item !56-5-A5!56-5-B6!56-5-B5!56-5-A4!56-5-B7! ! |
| ! ! !-------!-------!-------!-------!-------!------! |
| ! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! ! |
| ! ! ! C7xxxx! C8xxxx! C4xxxx! C6xxxx! C5xxxx! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.1 ! EGTL1 limit ! 890 ! 950 ! 950 ! 890 ! 950 ! deg C! |
| ! ! (red limit) ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.2 ! EGTL2 limit ! 855 ! 915 ! 915 ! 855 ! 915 ! deg C! |
| ! ! (yellow limit) ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.3 ! Not applicable ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.4 ! N1L1.1 limit ! 112 ! 112 ! 112 ! 112 ! 112 ! % ! |
| ! ! (yellow limit) ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.5 ! N1L1.2 limit ! 102 ! 104 ! 104 ! 102 ! 104 ! % ! |
| ! ! (red limit) ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.6 ! N2L1.1 limit ! 112 ! 112 ! 112 ! 112 ! 112 ! % ! |
| ! ! (yellow limit) ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.7 ! N2L1.2 limit ! 105 ! 105 ! 105 ! 105 ! 105 ! % ! |
| ! ! (red limit) ! ! ! ! ! ! ! |
| +-----------------------------------------------------------------------------+ |
(13) A318: CFMI Engines 56-5-B8, 56-5-B9
| +-----------------------------------------------------------------------------+ |
| !Report! Description of Report Item ! CFM ! CFM ! SPARE ! SPARE ! Unit ! |
| !Item ! !56-5-B8!56-5-B9! ! ! ! |
| ! ! !-------!-------!-------!-------!------! |
| ! ! !DMU/ID !DMU/ID ! ! ! ! |
| ! ! !C1xxxxx! C2xxxx! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.1 ! EGTL1 limit (red limit) ! 950 ! 950 ! ! ! deg C! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.2 ! EGTL2 limit (yellow limit) ! 915 ! 915 ! ! ! deg C! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.3 ! Not applicable ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.4 ! N1L1.1 limit (yellow limit) ! 112 ! 112 ! ! ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.5 ! N1L1.2 limit (red limit) ! 104 ! 104 ! ! ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.6 ! N2L1.1 limit (yellow limit) ! 112 ! 112 ! ! ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.7 ! N2L1.2 limit (red limit) ! 105 ! 105 ! ! ! % ! |
| +-----------------------------------------------------------------------------+ |
(14) A320: CFMI Engines 56-5-A1, 56-5-A3, 56-5-B4, 56-5-B5, 56-5-B6
| +-----------------------------------------------------------------------------+ |
| !Report!Limit! Description of ! CFM ! CFM ! CFM ! CFM ! CFM ! Unit ! |
| !Item !No. ! Report Item !56-5-A1!56-5-A3!56-5-B4!56-5-B5!56-5-B6! ! |
| ! ! ! !-------!-------!-------!-------!-------!------! |
| ! ! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! ! |
| ! ! ! ! CFM #1! CFM #2! CFM #3! CFM #4! CFM #8! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.1 ! 125 !EGTL1 ! 890 ! 890 ! 950 ! 950 ! 950 ! deg C! |
| ! ! !(yellow limit) ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.2 ! 126 !EGTL2 ! 855 ! 855 ! 855 ! 915 ! 915 ! deg C! |
| ! ! !(yellow limit) ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.3 ! 127 !EGTL3 ! 890 ! 890 ! 890 ! 950 ! 950 ! deg C! |
| ! ! !(red limit) ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.4 ! 128 !N1L1.1 ! 112 ! 112 ! 112 ! 112 ! 112 ! % ! |
| ! ! !(yellow limit) ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.5 ! 129 !N1L1.2 ! 102 ! 102 ! 104 ! 104 ! 104 ! % ! |
| ! ! !(red limit) ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.6 ! 130 !N2L1.1 ! 112 ! 112 ! 112 ! 112 ! 112 ! % ! |
| ! ! !(yellow limit) ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.7 ! 131 !N2L1.2 ! 105 ! 105 ! 105 ! 105 ! 105 ! % ! |
| ! ! !(red limit) ! ! ! ! ! ! ! |
| +-----------------------------------------------------------------------------+ |
(15) A321: CFMI Engines 56-5-B1, 56-5-B2, 56-5-B3, 56-5-B4
| +-----------------------------------------------------------------------------+ |
| !Report!Limit! Description of ! CFM ! CFM ! CFM ! CFM ! Unit ! |
| !Item !No. ! Report Item !56-5-B1!56-5-B2!56-5-B3!56-5-B4! ! |
| ! ! ! !-------!-------!-------!-------!------! |
| ! ! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! ! |
| ! ! ! ! CFM #5! CFM #6! CFM #7! CFM #3! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.1 ! 125 !EGTL1 ! 950 ! 950 ! 950 ! 950 ! deg C! |
| ! ! !(yellow limit) ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.2 ! 126 !EGTL2 ! 915 ! 915 ! 915 ! !! |
| ! ! !(yellow limit) ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.3 ! 127 !EGTL3 (red limit) ! 950 ! 950 ! 950 ! 890 ! deg C! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.4 ! 128 !N1L1.1 ! 112 ! 112 ! 112 ! 112 ! % ! |
| ! ! !(yellow limit) ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.5 ! 129 !N1L1.2 (red limit) ! 104 ! 104 ! 104 ! 104 ! % ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.6 ! 130 !N2L1.1 ! 112 ! 112 ! 112 ! 112 ! % ! |
| ! ! !(yellow limit) ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.7 ! 131 !N2L1.2 red limit) ! 105 ! 105 ! 105 ! 105 ! % ! |
| +-----------------------------------------------------------------------------+ |
(16) A319: CFMI Engines 56-5-A5, 56-5-B6, 56-5-B5, 56-5-A4, 56-5-B7
| +-----------------------------------------------------------------------------+ |
| !Report!Limit! Description of ! CFM ! CFM ! CFM ! CFM ! CFM ! Unit ! |
| !Item !No. ! Report Item !56-5-A5!56-5-B6!56-5-B5!56-5-A4!56-5-B7! ! |
| ! ! ! !-------!-------!-------!-------!-------!------! |
| ! ! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! ! |
| ! ! ! ! C7xxxx! C8xxxx! C4xxxx! C6xxxx! C5xxxx! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.1 ! 125 !EGTL1 ! 890 ! 950 ! 950 ! 890 ! 950 ! deg C! |
| ! ! !(yellow limit) ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.2 ! 126 !EGTL2 ! 855 ! 915 ! 915 ! 855 ! 915 ! deg C! |
| ! ! !(yellow limit) ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.3 ! 127 !EGTL3 ! 890 ! 950 ! 950 ! 890 ! 950 ! deg C! |
| ! ! !(red limit) ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.4 ! 128 !N1L1.1 ! 112 ! 112 ! 112 ! 112 ! 112 ! % ! |
| ! ! !(yellow limit) ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.5 ! 129 !N1L1.2 ! 102 ! 104 ! 104 ! 102 ! 104 ! % ! |
| ! ! !(red limit) ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.6 ! 130 !N2L1.1 ! 112 ! 112 ! 112 ! 112 ! 112 ! % ! |
| ! ! !(yellow limit) ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.7 ! 131 !N2L1.2 ! 105 ! 105 ! 105 ! 105 ! 105 ! % ! |
| ! ! !(red limit) ! ! ! ! ! ! ! |
| +-----------------------------------------------------------------------------+ |
(17) A318: CFMI Engines 56-5-B8, 56-5-B9
| +-----------------------------------------------------------------------------+ |
| !Report!Limit! Description of ! CFM ! CFM ! SPARE ! SPARE ! Unit ! |
| !Item !No. ! Report Item !56-5-B8!56-5-B9! ! ! ! |
| ! ! ! !-------!-------!-------!-------!------! |
| ! ! ! !DMU/ID !DMU/ID ! ! ! ! |
| ! ! ! !C1xxxxx! C2xxxx! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.1 ! 125 !EGTL1 ! 950 ! 950 ! ! ! deg C! |
| ! ! !(yellow limit) ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.2 ! 126 !EGTL2 ! 915 ! 915 ! ! ! deg C! |
| ! ! !(yellow limit) ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.3 ! 127 !EGTL3 (red limit) ! 950 ! 950 ! ! ! deg C! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.4 ! 128 !N1L1.1 ! 112 ! 112 ! ! ! % ! |
| ! ! !(yellow limit) ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.5 ! 129 !N1L1.2 (red limit) ! 104 ! 104 ! ! ! % ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.6 ! 130 !N2L1.1 ! 112 ! 112 ! ! ! % ! |
| ! ! !(yellow limit) ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.7 ! 131 !N2L1.2 (red limit) ! 105 ! 105 ! ! ! % ! |
| +-----------------------------------------------------------------------------+ |
(18) A320: CFMI Engines 56-5-A1, 56-5-A3, 56-5-B4, 56-5-B5, 56-5-B6
| +-----------------------------------------------------------------------------+ |
| !Report! Description of ! CFM ! CFM ! CFM ! CFM ! CFM ! Unit ! |
| !Item ! Report Item !56-5-A1!56-5-A3!56-5-B4!56-5-B5!56-5-B6! ! |
| ! ! !-------!-------!-------!-------!-------!------! |
| ! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! ! |
| ! ! ! CFM #1! CFM #2! CFM #3! CFM #4! CFM #8! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.1 ! EGTL1 limit ! 890 ! 890 ! 950 ! 950 ! 950 ! deg C! |
| ! ! (red limit) ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.2 ! EGTL2 limit ! 855 ! 855 ! 915 ! 915 ! 915 ! deg C! |
| ! ! (yellow limit) ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.3 ! Not applicable ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.4 ! N1L1.1 limit ! 112 ! 112 ! 112 ! 112 ! 112 ! % ! |
| ! ! (yellow limit) ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.5 ! N1L1.2 limit ! 102 ! 102 ! 104 ! 104 ! 104 ! % ! |
| ! ! (red limit) ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.6 ! N2L1.1 limit ! 112 ! 112 ! 112 ! 112 ! 112 ! % ! |
| ! ! (yellow limit) ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.7 ! N2L1.2 limit ! 105 ! 105 ! 105 ! 105 ! 105 ! % ! |
| ! ! (red limit) ! ! ! ! ! ! ! |
| +-----------------------------------------------------------------------------+ |
(19) A321: CFMI Engines 56-5-B1, 56-5-B2, 56-5-B3, 56-5-B4
| +-----------------------------------------------------------------------------+ |
| !Report! Description of Report Item ! CFM ! CFM ! CFM ! CFM ! Unit ! |
| !Item ! !56-5-B1!56-5-B2!56-5-B3!56-5-B4! ! |
| ! ! !-------!-------!-------!-------!------! |
| ! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! ! |
| ! ! ! CFM #5! CFM #6! CFM #7! CFM #3! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.1 ! EGTL1 limit (red limit) ! 950 ! 950 ! 950 ! 950 ! deg C! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.2 ! EGTL2 limit (yellow limit) ! 915 ! 915 ! 915 ! 915 ! deg C! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.3 ! Not applicable ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.4 ! N1L1.1 limit (yellow limit) ! 112 ! 112 ! 112 ! 112 ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.5 ! N1L1.2 limit (red limit) ! 104 ! 104 ! 104 ! 104 ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.6 ! N2L1.1 limit (yellow limit) ! 112 ! 112 ! 112 ! 112 ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.7 ! N2L1.2 limit (red limit) ! 105 ! 105 ! 105 ! 105 ! % ! |
| +-----------------------------------------------------------------------------+ |
(20) A319: CFMI Engines 56-5-A5, 56-5-B6, 56-5-B5, 56-5-A4, 56-5-B7
| +-----------------------------------------------------------------------------+ |
| !Report! Description of ! CFM ! CFM ! CFM ! CFM ! CFM ! Unit ! |
| !Item ! Report Item !56-5-A5!56-5-B6!56-5-B5!56-5-A4!56-5-B7! ! |
| ! ! !-------!-------!-------!-------!-------!------! |
| ! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! ! |
| ! ! ! C7xxxx! C8xxxx! C4xxxx! C6xxxx! C5xxxx! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.1 ! EGTL1 limit ! 890 ! 950 ! 950 ! 890 ! 950 ! deg C! |
| ! ! (red limit) ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.2 ! EGTL2 limit ! 855 ! 915 ! 915 ! 855 ! 915 ! deg C! |
| ! ! (yellow limit) ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.3 ! Not applicable ! ! ! ! ! 950 ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.4 ! N1L1.1 limit ! 112 ! 112 ! 112 ! 112 ! 112 ! % ! |
| ! ! (yellow limit) ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.5 ! N1L1.2 limit ! 102 ! 104 ! 104 ! 102 ! 104 ! % ! |
| ! ! (red limit) ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.6 ! N2L1.1 limit ! 112 ! 112 ! 112 ! 112 ! 112 ! % ! |
| ! ! (yellow limit) ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.7 ! N2L1.2 limit ! 105 ! 105 ! 105 ! 105 ! 105 ! % ! |
| ! ! (red limit) ! ! ! ! ! ! ! |
| +-----------------------------------------------------------------------------+ |
(21) A318: CFMI Engines 56-5-B8, 56-5-B9
| +-----------------------------------------------------------------------------+ |
| !Report! Description of Report Item ! CFM ! CFM ! SPARE ! SPARE ! Unit ! |
| !Item ! !56-5-B8!56-5-B9! ! ! ! |
| ! ! !-------!-------!-------!-------!------! |
| ! ! !DMU/ID !DMU/ID ! ! ! ! |
| ! ! !C1xxxxx! C2xxxx! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.1 ! EGTL1 limit (red limit) ! 950 ! 950 ! ! ! deg C! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.2 ! EGTL2 limit (yellow limit) ! 915 ! 915 ! ! ! deg C! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.3 ! ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.4 ! N1L1.1 limit (yellow limit) ! 112 ! 112 ! ! ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.5 ! N1L1.2 limit (red limit) ! 104 ! 104 ! ! ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.6 ! N2L1.1 limit (yellow limit) ! 112 ! 112 ! ! ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.7 ! N2L1.2 limit (red limit) ! 105 ! 105 ! ! ! % ! |
| +-----------------------------------------------------------------------------+ |
X. Report Limits for Engine Mechanical Advisory Report <07>
(1) A320: CFMI Engines 56-5-A1, 56-5-A3, 56-5-B4
| +-----------------------------------------------------------------------------+ |
| !Report! Limit ! Description of Report Item !56-5-A1!56-5-A3!56-5-B4! Unit ! |
| !Item N! No. ! ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.1.1! 155 ! OITL1 ! 175 ! 175 ! 175 ! deg C! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.1.2! 156 ! OITL2 (amber limit) ! 155 ! 155 ! 155 ! deg C! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.1.3! 157 ! OITL3 limit ! 140 ! 140 ! 140 ! deg C! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.1.4! 158 ! Y07.3 time limit ! 15 ! 15 ! 15 ! min ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.2.1! ! OIPL1.1 limits ! ! ! ! ! |
| ! ! ! N2L2.1 : 0 ! 0 ! 0 ! 0 ! ! |
| ! ! ! 54 ! 0 ! 0 ! 0 ! ! |
| ! ! ! 55 ! 13 ! 13 ! 13 ! ! |
| ! ! ! 65 ! 13 ! 13 ! 13 ! ! |
| ! ! ! 105 ! 38 ! 38 ! 38 ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.2.2! ! OIPL1.2 limits ! ! ! ! ! |
| ! ! ! N2L2.2 : 0 ! 0 ! 0 ! 0 ! ! |
| ! ! ! 54 ! 0 ! 0 ! 0 ! ! |
| ! ! ! 55 ! 13 ! 13 ! 13 ! ! |
| ! ! ! 65 ! 13 ! 13 ! 13 ! ! |
| ! ! ! 105 ! 38 ! 38 ! 38 ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.2.3! 193 ! OIPL2 limit ! 350 ! 350 ! 350 ! psi ! |
| +-----------------------------------------------------------------------------+ |
(2) A321: CFMI Engines 56-5-B1, 56-5-B2, 56-5-B3
| +-----------------------------------------------------------------------------+ |
| !Report! Limit ! Description of Report Item !56-5-B1!56-5-B2!56-5-B3! Unit ! |
| !Item N! ! ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.1.1! 155 ! OITL1 ! 175 ! 175 ! 175 ! deg C! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.1.2! 156 ! OITL2 (amber limit) ! 155 ! 155 ! 155 ! deg C! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.1.3! 157 ! OITL3 limit ! 140 ! 140 ! 140 ! deg C! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.1.4! 158 ! Y07.3 time limit ! 15 ! 15 ! 15 ! min ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.2.1! ! OIPL1.1 limits ! ! ! ! psi ! |
| ! ! ! N2L2.1 : 0 ! 0 ! 0 ! 0 ! %rpm ! |
| ! ! ! 54 ! 0 ! 0 ! 0 ! ! |
| ! ! ! 55 ! 13 ! 13 ! 13 ! ! |
| ! ! ! 65 ! 13 ! 13 ! 13 ! ! |
| ! ! ! 105 ! 38 ! 38 ! 38 ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.2.2! ! OIPL1.2 limits ! ! ! ! psi ! |
| ! ! ! N2L2.2 : 0 ! 0 ! 0 ! 0 ! %rpm ! |
| ! ! ! 54 ! 0 ! 0 ! 0 ! ! |
| ! ! ! 55 ! 13 ! 13 ! 13 ! ! |
| ! ! ! 65 ! 13 ! 13 ! 13 ! ! |
| ! ! ! 105 ! 38 ! 38 ! 38 ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.2.3! 193 ! OIPL2 limit ! 350 ! 350 ! 350 ! psi ! |
| +-----------------------------------------------------------------------------+ |
(3) A319: CFMI Engines 56-5-A5, 56-5-B6, 56-5-B5, 56-5A4
| +-----------------------------------------------------------------------------+ |
| !Report! Limit ! Description of Report !56-5-A5!56-5-B6!56-5-B5!56-5A4! Unit ! |
| !Item N! No. ! Item ! ! ! ! ! ! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! 4.1.1! 155 ! OITL1 ! 175 ! 175 ! 175 ! 175 ! deg C! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! 4.1.2! 156 ! OITL2 (amber limit) ! 155 ! 155 ! 155 ! 155 ! deg C! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! 4.1.3! 157 ! OITL3 limit ! 140 ! 140 ! 140 ! 140 ! deg C! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! 4.1.4! 158 ! Y07.3 time limit ! 15 ! 15 ! 15 ! 15 ! min ! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! 4.2.1! ! OIPL1.1 limits ! ! ! ! ! psi ! |
| ! ! ! N2L2.1 : 0 ! 0 ! 0 ! 0 ! 0 ! %rpm ! |
| ! ! ! 54 ! 0 ! 0 ! 0 ! 0 ! ! |
| ! ! ! 55 ! 13 ! 13 ! 13 ! 13 ! ! |
| ! ! ! 65 ! 13 ! 13 ! 13 ! 13 ! ! |
| ! ! ! 105 ! 38 ! 38 ! 38 ! 38 ! ! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! 4.2.2! ! OIPL1.2 limits ! ! ! ! ! psi ! |
| ! ! ! N2L2.2 : 0 ! 0 ! 0 ! 0 ! 0 ! %rpm ! |
| ! ! ! 54 ! 0 ! 0 ! 0 ! 0 ! ! |
| ! ! ! 55 ! 13 ! 13 ! 13 ! 13 ! ! |
| ! ! ! 65 ! 13 ! 13 ! 13 ! 13 ! ! |
| ! ! ! 105 ! 38 ! 38 ! 38 ! 38 ! ! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! 4.2.3! 193 ! OIPL2 limit ! 350 ! 350 ! 350 ! 350 ! psi ! |
| +-----------------------------------------------------------------------------+ |
(4) A319: CFMI Engines 56-5-B7
| +-----------------------------------------------------------------------------+ |
| !Report! Limit ! Description of Report Item !56-5-B7! SPARE ! SPARE ! Unit ! |
| !Item N! No. ! ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.1.1! 155 ! OITL1 ! 175 ! ! ! deg C! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.1.2! 156 ! OITL2 (amber limit) ! 155 ! ! ! deg C! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.1.3! 157 ! OITL3 limit ! 140 ! ! ! deg C! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.1.4! 158 ! Y07.3 time limit ! 15 ! ! ! min ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.2.1! ! OIPL1.1 limits ! ! ! ! psi ! |
| ! ! ! N2L2.1 : 0 ! 0 ! ! ! %rpm ! |
| ! ! ! 54 ! 0 ! ! ! ! |
| ! ! ! 55 ! 13 ! ! ! ! |
| ! ! ! 65 ! 13 ! ! ! ! |
| ! ! ! 105 ! 38 ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.2.2! ! OIPL1.2 limits ! ! ! ! psi ! |
| ! ! ! N2L2.2 : 0 ! 0 ! ! ! %rpm ! |
| ! ! ! 54 ! 0 ! ! ! ! |
| ! ! ! 55 ! 13 ! ! ! ! |
| ! ! ! 65 ! 13 ! ! ! ! |
| ! ! ! 105 ! 38 ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.2.3! 193 ! OIPL2 limit ! 350 ! ! ! psi ! |
| +-----------------------------------------------------------------------------+ |
(5) A320: CFMI Engines 56-5-A1, 56-5-A3, 56-5-B4, 56-5-B5, 56-5-B6
| +-----------------------------------------------------------------------------+ |
| !Report!Limit! Description of ! CFM ! CFM ! CFM ! CFM ! CFM ! Unit ! |
| !Item !No. ! Report Item !56-5-A1!56-5-A3!56-5-B4!56-5-B5!56-5-B6! ! |
| ! ! ! !-------!-------!-------!-------!-------!------! |
| ! ! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! ! |
| ! ! ! ! CFM #1! CFM #2! CFM #3! CFM #4! CFM #8! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.1.1! 155 !OITL1 ! 175 ! 175 ! 175 ! 175 ! 175 ! deg C! |
| ! ! !(yellow limit) ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.1.2! 156 !OITL2 ! 155 ! 155 ! 155 ! 155 ! 155 ! deg C! |
| ! ! !(red limit) ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.1.3! 157 !OITL3 ! 140 ! 140 ! 140 ! 140 ! 140 ! deg C! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.1.4! 158 !'Y07.3'duration ! 15 ! 15 ! 15 ! 15 ! 15 ! min ! |
| ! ! !of OITL3 ! ! ! ! ! ! ! |
| ! ! !exceedance ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.2.1! !OIPL1.1 limits ! ! ! ! ! ! psia ! |
| ! ! ! N2L2.1 : 0 ! 0 ! 0 ! 0 ! 0 ! 0 ! %rpm ! |
| ! ! ! 54 ! 0 ! 0 ! 0 ! 0 ! 0 ! %rpm ! |
| ! ! ! 55 ! 13 ! 13 ! 13 ! 13 ! 13 ! %rpm ! |
| ! ! ! 65 ! 13 ! 13 ! 13 ! 13 ! 13 ! %rpm ! |
| ! ! ! 105 ! 38 ! 38 ! 38 ! 38 ! 38 ! %rpm ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.2.2! !OIPL1.2 limits ! ! ! ! ! ! psia ! |
| ! ! ! N2L2.2 : 0 ! 0 ! 0 ! 0 ! 0 ! 0 ! %rpm ! |
| ! ! ! 54 ! 0 ! 0 ! 0 ! 0 ! 0 ! %rpm ! |
| ! ! ! 55 ! 13 ! 13 ! 13 ! 13 ! 13 ! %rpm ! |
| ! ! ! 65 ! 13 ! 13 ! 13 ! 13 ! 13 ! %rpm ! |
| ! ! ! 105 ! 38 ! 38 ! 38 ! 38 ! 38 ! %rpm ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.2.3! 193 !OIPL2 ! 350 ! 350 ! 350 ! 350 ! 350 ! psi ! |
| +-----------------------------------------------------------------------------+ |
(6) A321: CFMI Engines 56-5-B1, 56-5-B2, 56-5-B3, 56-5-B4
| +-----------------------------------------------------------------------------+ |
| !Report!Limit! Description of ! CFM ! CFM ! CFM ! CFM ! Unit ! |
| !Item !No. ! Report Item !56-5-B1!56-5-B2!56-5-B3!56-5-B4! ! |
| ! ! ! !-------!-------!-------!-------!------! |
| ! ! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! ! |
| ! ! ! ! CFM #5! CFM #6! CFM #7! CFM #3! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.1.1! 155 !OITL1 ! 175 ! 175 ! 175 ! 175 ! deg C! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.1.2! 156 !OITL2 (red limit) ! 155 ! 155 ! 155 ! 155 ! deg C! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.1.3! 157 !OITL3 ! 140 ! 140 ! 140 ! 140 ! deg C! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.1.4! 158 !'Y07.3' duration of OITL3! 15 ! 15 ! 15 ! 15 ! min ! |
| ! ! !exceedance ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.2.1! !OIPL1.1 limits ! ! ! ! ! psia ! |
| ! ! ! N2L2.1 : 0 ! 0 ! 0 ! 0 ! 0 ! %rpm ! |
| ! ! ! 54 ! 0 ! 0 ! 0 ! 0 ! %rpm ! |
| ! ! ! 55 ! 13 ! 13 ! 13 ! 13 ! %rpm ! |
| ! ! ! 65 ! 13 ! 13 ! 13 ! 13 ! %rpm ! |
| ! ! ! 105 ! 38 ! 38 ! 38 ! 38 ! %rpm ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.2.2! !OIPL1.2 limits ! ! ! ! ! psia ! |
| ! ! ! N2L2.2 : 0 ! 0 ! 0 ! 0 ! 0 ! %rpm ! |
| ! ! ! 54 ! 0 ! 0 ! 0 ! 0 ! %rpm ! |
| ! ! ! 55 ! 13 ! 13 ! 13 ! 13 ! %rpm ! |
| ! ! ! 65 ! 13 ! 13 ! 13 ! 13 ! %rpm ! |
| ! ! ! 105 ! 38 ! 38 ! 38 ! 38 ! %rpm ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.2.3! 193 !OIPL2 ! 350 ! 350 ! 350 ! 350 ! psi ! |
| +-----------------------------------------------------------------------------+ |
(7) A319: CFMI Engines 56-5-A5, 56-5-B6, 56-5-B5, 56-5-A4, 56-5-B7
| +-----------------------------------------------------------------------------+ |
| !Report!Limit! Description of ! CFM ! CFM ! CFM ! CFM ! CFM ! Unit ! |
| !Item !No. ! Report Item !56-5-A5!56-5-B6!56-5-B5!56-5-A4!56-5-B7! ! |
| ! ! ! !-------!-------!-------!-------!-------!------! |
| ! ! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! ! |
| ! ! ! ! C7xxxx! C8xxxx! C4xxxx! C6xxxx! C5xxxx! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.1.1! 155 !OITL1 ! 175 ! 175 ! 175 ! 175 ! 175 ! deg C! |
| ! ! !(yellow limit) ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.1.2! 156 !OITL2 limit ! 155 ! 155 ! 155 ! 155 ! 155 ! deg C! |
| ! ! !(red limit) ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.1.3! 157 !OITL3 ! 140 ! 140 ! 140 ! 140 ! 140 ! deg C! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.1.4! 158 !'Y07.3'duration ! 15 ! 15 ! 15 ! 15 ! 15 ! min ! |
| ! ! !of OITL3 ! ! ! ! ! ! ! |
| ! ! !exceedance ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.2.1! ! OIPL1.1 limits ! ! ! ! ! ! psia ! |
| ! ! ! N2L2.1 : 0 ! 0 ! 0 ! 0 ! 0 ! 0 ! %rpm ! |
| ! ! ! 54 ! 0 ! 0 ! 0 ! 0 ! 0 ! %rpm ! |
| ! ! ! 55 ! 13 ! 13 ! 13 ! 13 ! 13 ! %rpm ! |
| ! ! ! 65 ! 13 ! 13 ! 13 ! 13 ! 13 ! %rpm ! |
| ! ! ! 105 ! 38 ! 38 ! 38 ! 38 ! 38 ! %rpm ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.2.2! !OIPL1.2 limits ! ! ! ! ! ! psia ! |
| ! ! ! N2L2.2 : 0 ! 0 ! 0 ! 0 ! 0 ! 0 ! %rpm ! |
| ! ! ! 54 ! 0 ! 0 ! 0 ! 0 ! 0 ! %rpm ! |
| ! ! ! 55 ! 13 ! 13 ! 13 ! 13 ! 13 ! %rpm ! |
| ! ! ! 65 ! 13 ! 13 ! 13 ! 13 ! 13 ! %rpm ! |
| ! ! ! 105 ! 38 ! 38 ! 38 ! 38 ! 38 ! %rpm ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.2.3! 193 !OIPL2 ! 350 ! 350 ! 350 ! 350 ! 350 ! psi ! |
| +-----------------------------------------------------------------------------+ |
(8) A318: CFMI Engines 56-5-B8, 56-5-B9
| +-----------------------------------------------------------------------------+ |
| !Report!Limit! Description of ! CFM ! CFM ! SPARE ! SPARE ! Unit ! |
| !Item !No. ! Report Item !56-5-B8!56-5-B9! ! ! ! |
| ! ! ! !-------!-------!-------!-------!------! |
| ! ! ! !DMU/ID !DMU/ID ! ! ! ! |
| ! ! ! !C1xxxxx! C2xxxx! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.1.1! 155 !OITL1 ! 175 ! 175 ! ! ! deg C! |
| ! ! !(yellow limit) ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.1.2! 156 !OITL2 (red limit) ! 155 ! 155 ! ! ! deg C! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.1.3! 157 !OITL3 ! 140 ! 140 ! ! ! deg C! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.1.4! 158 !'Y07.3' duration of OITL3! 15 ! 15 ! ! ! min ! |
| ! ! !exceedance ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.2.1! !OIPL1.1 limits ! ! ! ! ! psia ! |
| ! ! ! N2L2.1 : 0 ! 0 ! 0 ! ! ! %rpm ! |
| ! ! ! 54 ! 0 ! 0 ! ! ! %rpm ! |
| ! ! ! 55 ! 13 ! 13 ! ! ! %rpm ! |
| ! ! ! 65 ! 13 ! 13 ! ! ! %rpm ! |
| ! ! ! 105 ! 38 ! 38 ! ! ! %rpm ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.2.2! !OIPL1.2 limits ! ! ! ! ! psia ! |
| ! ! ! N2L2.2 : 0 ! 0 ! 0 ! ! ! %rpm ! |
| ! ! ! 54 ! 0 ! 0 ! ! ! %rpm ! |
| ! ! ! 55 ! 13 ! 13 ! ! ! %rpm ! |
| ! ! ! 65 ! 13 ! 13 ! ! ! %rpm ! |
| ! ! ! 105 ! 38 ! 38 ! ! ! %rpm ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.2.3! 193 !OIPL2 ! 350 ! 350 ! ! ! psi ! |
| +-----------------------------------------------------------------------------+ |
(9) A320: CFMI Engines 56-5-A1, 56-5-A3, 56-5-B4, 56-5-B5, 56-5-B6
| +-----------------------------------------------------------------------------+ |
| !Report! Description of ! CFM ! CFM ! CFM ! CFM ! CFM ! Unit ! |
| !Item ! Report Item !56-5-A1!56-5-A3!56-5-B4!56-5-B5!56-5-B6! ! |
| ! ! !-------!-------!-------!-------!-------!------! |
| ! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! ! |
| ! ! ! CFM #1! CFM #2! CFM #3! CFM #4! CFM #8! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.1.1! OITL1 limit ! 175 ! 175 ! 175 ! 175 ! 175 ! deg C! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.1.2! OITL2 limit ! 155 ! 155 ! 155 ! 155 ! 155 ! deg C! |
| ! ! (amber limit) ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.1.3! OITL3 limit ! 140 ! 140 ! 140 ! 140 ! 140 ! deg C! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.1.4! "Y07.3" time limit ! 15 ! 15 ! 15 ! 15 ! 15 ! min ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.2.1! OIPL1.1 limits ! ! ! ! ! ! psia ! |
| ! ! N2L2.1 : 0 ! 0 ! 0 ! 0 ! 0 ! 0 ! %rpm ! |
| ! ! 54 ! 0 ! 0 ! 0 ! 0 ! 0 ! %rpm ! |
| ! ! 55 ! 13 ! 13 ! 13 ! 13 ! 13 ! %rpm ! |
| ! ! 65 ! 13 ! 13 ! 13 ! 13 ! 13 ! %rpm ! |
| ! ! 105 ! 38 ! 38 ! 38 ! 38 ! 38 ! %rpm ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.2.2! OIPL1.2 limits ! ! ! ! ! ! psia ! |
| ! ! N2L2.2 : 0 ! 0 ! 0 ! 0 ! 0 ! 0 ! %rpm ! |
| ! ! 54 ! 0 ! 0 ! 0 ! 0 ! 0 ! %rpm ! |
| ! ! 55 ! 13 ! 13 ! 13 ! 13 ! 13 ! %rpm ! |
| ! ! 65 ! 13 ! 13 ! 13 ! 13 ! 13 ! %rpm ! |
| ! ! 105 ! 38 ! 38 ! 38 ! 38 ! 38 ! %rpm ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.2.3! OIPL2 limit ! 350 ! 350 ! 350 ! 350 ! 350 ! psi ! |
| +-----------------------------------------------------------------------------+ |
(10) A321: CFMI Engines 56-5-B1, 56-5-B2, 56-5-B3, 56-5-B4
| +-----------------------------------------------------------------------------+ |
| !Report! Description of Report Item ! CFM ! CFM ! CFM ! CFM ! Unit ! |
| !Item ! !56-5-B1!56-5-B2!56-5-B3!56-5-B4! ! |
| ! ! !-------!-------!-------!-------!------! |
| ! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! ! |
| ! ! ! CFM #5! CFM #6! CFM #6! CFM #3! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.1.1! OITL1 limit ! 175 ! 175 ! 175 ! 175 ! deg C! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.1.2! OITL2 limit (amber limit) ! 155 ! 155 ! 155 ! 155 ! deg C! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.1.3! OITL3 limit ! 140 ! 140 ! 140 ! 140 ! deg C! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.1.4! "Y07.3" time limit ! 15 ! 15 ! 15 ! 15 ! min ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.2.1! OIPL1.1 limits ! ! ! ! ! psia ! |
| ! ! N2L2.1 : 0 ! 0 ! 0 ! 0 ! 0 ! %rpm ! |
| ! ! 54 ! 0 ! 0 ! 0 ! 0 ! %rpm ! |
| ! ! 55 ! 13 ! 13 ! 13 ! 13 ! %rpm ! |
| ! ! 65 ! 13 ! 13 ! 13 ! 13 ! %rpm ! |
| ! ! 105 ! 38 ! 38 ! 38 ! 38 ! %rpm ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.2.2! OIPL1.2 limits ! ! ! ! ! psia ! |
| ! ! N2L2.2 : 0 ! 0 ! 0 ! 0 ! 0 ! %rpm ! |
| ! ! 54 ! 0 ! 0 ! 0 ! 0 ! %rpm ! |
| ! ! 55 ! 13 ! 13 ! 13 ! 13 ! %rpm ! |
| ! ! 65 ! 13 ! 13 ! 13 ! 13 ! %rpm ! |
| ! ! 105 ! 38 ! 38 ! 38 ! 38 ! %rpm ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.2.3! OIPL2 limit ! 350 ! 350 ! 350 ! 350 ! psi ! |
| +-----------------------------------------------------------------------------+ |
(11) A319: CFMI Engines 56-5-A5, 56-5-B6, 56-5-B5, 56-5-A4, 56-5-B7
| +-----------------------------------------------------------------------------+ |
| !Report! Description of ! CFM ! CFM ! CFM ! CFM ! CFM ! Unit ! |
| !Item ! Report Item !56-5-A5!56-5-B6!56-5-B5!56-5-A4!56-5-B7! ! |
| ! ! !-------!-------!-------!-------!-------!------! |
| ! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! ! |
| ! ! ! C7xxxx! C8xxxx! C4xxxx! C6xxxx! C5xxxx! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.1.1! OITL1 limit ! 175 ! 175 ! 175 ! 175 ! 175 ! deg C! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.1.2! OITL2 limit ! 155 ! 155 ! 155 ! 155 ! 155 ! deg C! |
| ! ! (amber limit) ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.1.3! OITL3 limit ! 140 ! 140 ! 140 ! 140 ! 140 ! deg C! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.1.4! "Y07.3" time limit ! 15 ! 15 ! 15 ! 15 ! 15 ! min ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.2.1! OIPL1.1 limits ! ! ! ! ! ! psia ! |
| ! ! N2L2.1 : 0 ! 0 ! 0 ! 0 ! 0 ! 0 ! %rpm ! |
| ! ! 54 ! 0 ! 0 ! 0 ! 0 ! 0 ! %rpm ! |
| ! ! 55 ! 13 ! 13 ! 13 ! 13 ! 13 ! %rpm ! |
| ! ! 65 ! 13 ! 13 ! 13 ! 13 ! 13 ! %rpm ! |
| ! ! 105 ! 38 ! 38 ! 38 ! 38 ! 38 ! %rpm ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.2.2! OIPL1.2 limits ! ! ! ! ! ! psia ! |
| ! ! N2L2.2 : 0 ! 0 ! 0 ! 0 ! 0 ! 0 ! %rpm ! |
| ! ! 54 ! 0 ! 0 ! 0 ! 0 ! 0 ! %rpm ! |
| ! ! 55 ! 13 ! 13 ! 13 ! 13 ! 13 ! %rpm ! |
| ! ! 65 ! 13 ! 13 ! 13 ! 13 ! 13 ! %rpm ! |
| ! ! 105 ! 38 ! 38 ! 38 ! 38 ! 38 ! %rpm ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.2.3! OIPL2 limit ! 350 ! 350 ! 350 ! 350 ! 350 ! psi ! |
| +-----------------------------------------------------------------------------+ |
(12) A318: CFMI Engines 56-5-B8, 56-5-B9
| +-----------------------------------------------------------------------------+ |
| !Report! Description of Report Item ! CFM ! CFM ! SPARE ! SPARE ! Unit ! |
| !Item ! !56-5-B8!56-5-B9! ! ! ! |
| ! ! !-------!-------!-------!-------!------! |
| ! ! !DMU/ID !DMU/ID ! ! ! ! |
| ! ! !C1xxxxx! C2xxxx! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.1.1! OITL1 limit (yellow limit) ! 175 ! 175 ! ! ! deg C! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.1.2! OITL2 limit (red limit) ! 155 ! 155 ! ! ! deg C! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.1.3! OITL3 limit ! 140 ! 140 ! ! ! deg C! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.1.4! "Y07.3" time limit ! 15 ! 15 ! ! ! min ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.2.1! OIPL1.1 limits ! ! ! ! ! psia ! |
| ! ! N2L2.1 : 0 ! 0 ! 0 ! ! ! %rpm ! |
| ! ! 54 ! 0 ! 0 ! ! ! %rpm ! |
| ! ! 55 ! 13 ! 13 ! ! ! %rpm ! |
| ! ! 65 ! 13 ! 13 ! ! ! %rpm ! |
| ! ! 105 ! 38 ! 38 ! ! ! %rpm ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.2.2! OIPL1.2 limits ! ! ! ! ! psia ! |
| ! ! N2L2.2 : 0 ! 0 ! 0 ! ! ! %rpm ! |
| ! ! 54 ! 0 ! 0 ! ! ! %rpm ! |
| ! ! 55 ! 13 ! 13 ! ! ! %rpm ! |
| ! ! 65 ! 13 ! 13 ! ! ! %rpm ! |
| ! ! 105 ! 38 ! 38 ! ! ! %rpm ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.2.3! OIPL2 limit ! 350 ! 350 ! ! ! psi ! |
| +-----------------------------------------------------------------------------+ |
Y. Report Limits for Engine Divergence Report <09>
(1) A320: CFMI Engines 56-5-A1, 56-5-A3, 56-5-B4
| +-----------------------------------------------------------------------------+ |
| !Report! Limit ! Description of Report Item !56-5-A1!56-5-A3!56-5-B4! Unit ! |
| !Item N! No. ! ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.1.1! 212 ! EGTdivT1 limit ! 25 ! 25 ! 25 ! deg C! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.1.2! 213 ! EGTdivT2 limit ! 30 ! 30 ! 30 ! deg C! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.1.3! 214 ! EGTdivT3 limit ! 35 ! 35 ! 35 ! deg C! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.1.4! 215 ! EGTdivT4 limit ! 40 ! 40 ! 40 ! deg C! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.1.5! 216 ! TNdivT1 limit ! 40 ! 40 ! 40 ! deg C! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.1.6! 217 ! TNdivT2 limit ! 50 ! 50 ! 50 ! deg C! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.1.7! 218 ! TNdivT3 limit ! 60 ! 60 ! 60 ! deg C! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.1.8! 219 ! TNdivT4 limit ! 70 ! 70 ! 70 ! deg C! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.2.1! 220 ! N1L1 limit ! 90 ! 90 ! 90 ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.2.2! 221 ! N1L2 limit ! 115 ! 115 ! 115 ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.2.3! 222 ! N1L3 limit ! 3 ! 3 ! 3 ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.2.5! 224 ! IVVL limit valid during PH 4 ! 150 ! 150 ! 150 !feet/m! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.2.6! 223 ! ALTL limit valid during PH 5.1! 5000 ! 5000 ! 5000 ! feet ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.2.7! 225 ! TATL limit ! 5 ! 5 ! 5 ! deg C! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.2.8! 226 ! N1RL limit ! 2 ! 2 ! 2 ! %rpm/! |
| ! ! ! ! ! ! ! sec ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.2.9! 228 ! Y09: time interval ! 10 ! 10 ! 10 ! sec ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| !4.2.10! 227 ! PFLdelta limit ! .1 ! .1 ! .1 ! kg/s ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.3.6! 229 ! KL limit ! 14 ! 14 ! 14 ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.3.7! 230 ! C09.1 limit for climb (ph 5.1)! 7.7 ! 7.7 ! 7.7 ! deg C! |
| ! ! ! ! ! ! ! /%N1 ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.3.8! 231 ! C09.2 limit for climb (ph 6) ! 7 ! 7 ! 7 ! deg C! |
| ! ! ! ! ! ! ! /%N1 ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.3.9! 232 ! M programmed limit ! 10 ! 10 ! 10 ! ! |
| +-----------------------------------------------------------------------------+ |
(2) A321: CFMI Engines 56-5-B1, 56-5-B2, 56-5-B3
| +-----------------------------------------------------------------------------+ |
| !Report! Limit ! Description of Report Item !56-5-B1!56-5-B2!56-5-B3! Unit ! |
| !Item N! No. ! ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.1.1! 212 ! EGTdivT1 limit ! 25 ! 25 ! 25 ! deg C! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.1.2! 213 ! EGTdivT2 limit ! 30 ! 30 ! 30 ! deg C! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.1.3! 214 ! EGTdivT3 limit ! 35 ! 35 ! 35 ! deg C! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.1.4! 215 ! EGTdivT4 limit ! 40 ! 40 ! 40 ! deg C! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.1.5! 216 ! TNdivT1 limit ! 40 ! 40 ! 40 ! deg C! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.1.6! 217 ! TNdivT2 limit ! 50 ! 50 ! 50 ! deg C! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.1.7! 218 ! TNdivT3 limit ! 60 ! 60 ! 60 ! deg C! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.1.8! 219 ! TNdivT4 limit ! 70 ! 70 ! 70 ! deg C! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.2.1! 220 ! N1L1 limit ! 90 ! 90 ! 90 ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.2.2! 221 ! N1L2 limit ! 115 ! 115 ! 115 ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.2.3! 222 ! N1L3 limit ! 3 ! 3 ! 3 ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.2.5! 224 ! IVVL limit valid during PH 4 ! 150 ! 150 ! 150 !feet/m! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.2.6! 223 ! ALTL limit valid during PH 5.1! 5000 ! 5000 ! 5000 ! feet ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.2.7! 225 ! TATL limit ! 5 ! 5 ! 5 ! deg C! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.2.8! 226 ! N1RL limit ! 2 ! 2 ! 2 ! %rpm/! |
| ! ! ! ! ! ! ! sec ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.2.9! 228 ! Y09: time interval ! 10 ! 10 ! 10 ! sec ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| !4.2.10! 227 ! PFLdelta limit ! .1 ! .1 ! .1 ! kg/s ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.3.6! 229 ! KL limit ! 14 ! 14 ! 14 ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.3.7! 230 ! C09.1 limit for climb (ph 5.1)! 7.7 ! 7.7 ! 7.7 ! deg C! |
| ! ! ! ! ! ! ! /%N1 ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.3.8! 231 ! C09.2 limit for climb (ph 6) ! 7 ! 7 ! 7 ! deg C! |
| ! ! ! ! ! ! ! /%N1 ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.3.9! 232 ! M programmed limit ! 10 ! 10 ! 10 ! ! |
| +-----------------------------------------------------------------------------+ |
(3) A319: CFMI Engines 56-5-A5, 56-5-B6, 56-5-B5, 56-5A4
| +-----------------------------------------------------------------------------+ |
| !Report! Limit ! Description of Report !56-5-A5!56-5-B6!56-5-B5!56-5A4! Unit ! |
| !Item N! No. ! Item ! ! ! ! ! ! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! 4.1.1! 212 ! EGTdivT1 limit ! 25 ! 25 ! 25 ! 25 ! deg C! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! 4.1.2! 213 ! EGTdivT2 limit ! 30 ! 30 ! 30 ! 30 ! deg C! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! 4.1.3! 214 ! EGTdivT3 limit ! 35 ! 35 ! 35 ! 35 ! deg C! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! 4.1.4! 215 ! EGTdivT4 limit ! 40 ! 40 ! 40 ! 40 ! deg C! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! 4.1.5! 216 ! TNdivT1 limit ! 40 ! 40 ! 40 ! 40 ! deg C! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! 4.1.6! 217 ! TNdivT2 limit ! 50 ! 50 ! 50 ! 50 ! deg C! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! 4.1.7! 218 ! TNdivT3 limit ! 60 ! 60 ! 60 ! 60 ! deg C! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! 4.1.8! 219 ! TNdivT4 limit ! 70 ! 70 ! 70 ! 70 ! deg C! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! 4.2.1! 220 ! N1L1 limit ! 90 ! 90 ! 90 ! 90 ! ! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! 4.2.2! 221 ! N1L2 limit ! 115 ! 115 ! 115 ! 115 ! ! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! 4.2.3! 222 ! N1L3 limit ! 3 ! 3 ! 3 ! 3 ! ! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! 4.2.5! 224 ! IVVL limit valid ! 150 ! 150 ! 150 ! 150 !feet/m! |
| ! ! ! during PH 4 ! ! ! ! ! ! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! 4.2.6! 223 ! ALTL limit valid ! 5000 ! 5000 ! 5000 ! 5000 ! feet ! |
| ! ! ! during PH 5.1 ! ! ! ! ! ! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! 4.2.7! 225 ! TATL limit ! 5 ! 5 ! 5 ! 5 ! deg C! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! 4.2.8! 226 ! N1RL limit ! 2 ! 2 ! 2 ! 2 ! %rpm/! |
| ! ! ! ! ! ! ! ! sec ! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! 4.2.9! 228 ! Y09: time interval ! 10 ! 10 ! 10 ! 10 ! sec ! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| !4.2.10! 227 ! PFLdelta limit ! .1 ! .1 ! .1 ! .1 ! kg/s ! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! 4.3.6! 229 ! KL limit ! 14 ! 14 ! 14 ! 14 ! ! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! 4.3.7! 230 ! C09.1 limit for climb ! 7.7 ! 7.7 ! 7.7 ! 7.7 ! deg C! |
| ! ! ! (ph 5.1) ! ! ! ! ! /%N1 ! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! 4.3.8! 231 ! C09.2 limit for climb ! 7 ! 7 ! 7 ! 7 ! deg C! |
| ! ! ! (ph 6) ! ! ! ! ! /%N1 ! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! 4.3.9! 232 ! M programmed limit ! 10 ! 10 ! 10 ! 10 ! ! |
| +-----------------------------------------------------------------------------+ |
(4) A319: CFMI Engines 56-5-B7
| +-----------------------------------------------------------------------------+ |
| !Report! Limit ! Description of Report Item !56-5-B7! SPARE ! SPARE ! Unit ! |
| !Item N! No. ! ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.1.1! 212 ! EGTdivT1 limit ! 25 ! ! ! deg C! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.1.2! 213 ! EGTdivT2 limit ! 30 ! ! ! deg C! |
| !------!-------!--------- ---------------------!-------!-------!-------!------! |
| ! 4.1.3! 214 ! EGTdivT3 limit ! 35 ! ! ! deg C! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.1.4! 215 ! EGTdivT4 limit ! 40 ! ! ! deg C! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.1.5! 216 ! TNdivT1 limit ! 40 ! ! ! deg C! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.1.6! 217 ! TNdivT2 limit ! 50 ! ! ! deg C! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.1.7! 218 ! TNdivT3 limit ! 60 ! ! ! deg C! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.1.8! 219 ! TNdivT4 limit ! 70 ! ! ! deg C! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.2.1! 220 ! N1L1 limit ! 90 ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.2.2! 221 ! N1L2 limit ! 115 ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.2.3! 222 ! N1L3 limit ! 3 ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.2.5! 224 ! IVVL limit valid during PH 4 ! 150 ! ! !feet/m! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.2.6! 223 ! ALTL limit valid during PH 5.1! 5000 ! ! ! feet ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.2.7! 225 ! TATL limit ! 5 ! ! ! deg C! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.2.8! 226 ! N1RL limit ! 2 ! ! ! %rpm/! |
| ! ! ! ! ! ! ! sec ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.2.9! 228 ! Y09: time interval ! 10 ! ! ! sec ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| !4.2.10! 227 ! PFLdelta limit ! .1 ! ! ! kg/s ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.3.6! 229 ! KL limit ! 14 ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.3.7! 230 ! C09.1 limit for climb (ph 5.1)! 7.7 ! ! ! deg C! |
| ! ! ! ! ! ! ! /%N1 ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.3.8! 231 ! C09.2 limit for climb (ph 6) ! 7 ! ! ! deg C! |
| ! ! ! ! ! ! ! /%N1 ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 4.3.9! 232 ! M programmed limit ! 10 ! ! ! ! |
| +-----------------------------------------------------------------------------+ |
(5) A320: CFMI Engines 56-5-A1, 56-5-A3, 56-5-B4, 56-5-B5, 56-5-B6
| +-----------------------------------------------------------------------------+ |
| !Report!Limit! Description of ! CFM ! CFM ! CFM ! CFM ! CFM ! Unit ! |
| !Item !No. ! Report Item !56-5-A1!56-5-A3!56-5-B4!56-5-B5!56-5-B6! ! |
| ! ! ! !-------!-------!-------!-------!-------!------! |
| ! ! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! ! |
| ! ! ! ! CFM #1! CFM #2! CFM #3! CFM #4! CFM #8! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.1.1! 212 !EGTdivT1 ! 25 ! 25 ! 25 ! 25 ! 25 ! deg C! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.1.2! 213 !EGTdivT2 ! 30 ! 30 ! 30 ! 30 ! 30 ! deg C! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.1.3! 214 !EGTdivT3 ! 35 ! 35 ! 35 ! 35 ! 35 ! deg C! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.1.4! 215 !EGTdivT4 ! 40 ! 40 ! 40 ! 40 ! 40 ! deg C! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.1.5! 216 !TNdivT1 ! 40 ! 40 ! 40 ! 40 ! 40 ! deg C! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.1.6! 217 !TNdivT2 ! 50 ! 50 ! 50 ! 50 ! 50 ! deg C! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.1.7! 218 !TNdivT3 ! 60 ! 60 ! 60 ! 60 ! 60 ! deg C! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.1.8! 219 !TNdivT4 ! 70 ! 70 ! 70 ! 70 ! 70 ! deg C! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.2.1! 220 !N1L1 ! 90 ! 90 ! 90 ! 90 ! 90 ! % ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.2.2! 221 !N1L2 ! 115 ! 115 ! 115 ! 115 ! 115 ! % ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.2.3! 222 !N1L3 ! 3 ! 3 ! 3 ! 3 ! 3 ! % ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.2.5! 224 !IVVL ! 150 ! 150 ! 150 ! 150 ! 150 !ft/min! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.2.6! 223 !ALTL ! 5000 ! 5000 ! 5000 ! 5000 ! 5000 ! ft ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.2.7! 225 !TATL ! 5 ! 5 ! 5 ! 5 ! 5 ! deg C! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.2.8! 226 !N1RRL ! 2 ! 2 ! 2 ! 2 ! 2 ! %/sec! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.2.9! 228 !'Y09'time ! 10 ! 10 ! 10 ! 10 ! 10 ! sec ! |
| ! ! !interval ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| !4.2.10! 227 !PFLdelta ! 0.1 ! 0.1 ! 0.1 ! 0.1 ! 0.1 ! kg/s ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.3.6! 229 !KL flight leg ! 14 ! 14 ! 14 ! 14 ! 14 ! ! |
| ! ! !counter limit ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.3.7! 230 !C09.1 limit for ! 7.7 ! 7.7 ! 7.7 ! 7.7 ! 7.7 ! deg C! |
| ! ! !climb (PH 5.1) ! ! ! ! ! ! /%! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.3.8! 231 !C09.2 limit for ! 7.0 ! 7.0 ! 7.0 ! 7.0 ! 7.0 ! deg C! |
| ! ! !cruise (PH 6) ! ! ! ! ! ! /%N1 ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.3.9! 232 !M ! 10 ! 10 ! 10 ! 10 ! 10 ! ! |
| +-----------------------------------------------------------------------------+ |
(6) A321: CFMI Engines 56-5-B1, 56-5-B2, 56-5-B3, 56-5-B4
| +-----------------------------------------------------------------------------+ |
| !Report!Limit! Description of ! CFM ! CFM ! CFM ! CFM ! Unit ! |
| !Item !No. ! Report Item !56-5-B1!56-5-B2!56-5-B3!56-5 ! ! |
| ! ! ! !-------!-------!-------!-------!------! |
| ! ! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! ! |
| ! ! ! ! CFM #5! CFM #6! CFM #7! CFM #3! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.1.1! 212 !EGTdivT1 ! 25 ! 25 ! 25 ! 25 ! deg C! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.1.2! 213 !EGTdivT2 ! 30 ! 30 ! 30 ! 30 ! deg C! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.1.3! 214 !EGTdivT3 ! 35 ! 35 ! 35 ! 35 ! deg C! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.1.4! 215 !EGTdivT4 ! 40 ! 40 ! 40 ! 40 ! deg C! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.1.5! 216 !TNdivT1 ! 40 ! 40 ! 40 ! 40 ! deg C! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.1.6! 217 !TNdivT2 ! 50 ! 50 ! 50 ! 50 ! deg C! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.1.7! 218 !TNdivT3 ! 60 ! 60 ! 60 ! 60 ! deg C! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.1.8! 219 !TNdivT4 ! 70 ! 70 ! 70 ! 70 ! deg C! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.2.1! 220 !N1L1 ! 90 ! 90 ! 90 ! 90 ! % ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.2.2! 221 !N1L2 ! 115 ! 115 ! 115 ! 115 ! % ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.2.3! 222 !N1L3 ! 3 ! 3 ! 3 ! 3 ! % ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.2.5! 224 !IVVL ! 150 ! 150 ! 150 ! 150 !ft/min! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.2.6! 223 !ALTL ! 5000 ! 5000 ! 5000 ! 5000 ! ft ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.2.7! 225 !TATL ! 5 ! 5 ! 5 ! 5 ! deg C! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.2.8! 226 !N1RRL ! 2 ! 2 ! 2 ! 2 ! %/sec! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.2.9! 228 !'Y09' time interval ! 10 ! 10 ! 10 ! 10 ! sec ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| !4.2.10! 227 !PFLdelta ! 0.1 ! 0.1 ! 0.1 ! 0.1 ! kg/s ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.3.6! 229 !KL flight leg counter ! 14 ! 14 ! 14 ! 14 ! ! |
| ! ! !limit ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.3.7! 230 !C09.1 limit for climb ! 7.7 ! 7.7 ! 7.7 ! 7.7 ! deg C! |
| ! ! !(PH 5.1) ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.3.8! 231 !C09.2 limit for cruise ! 7.0 ! 7.0 ! 7.0 ! 7.0 ! deg C! |
| ! ! !(PH 6) ! ! ! ! ! /%N1 ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.3.9! 232 !M ! 10 ! 10 ! 10 ! 10 ! ! |
| +-----------------------------------------------------------------------------+ |
(7) A319: CFMI Engines 56-5-A5, 56-5-B6, 56-5-B5, 56-5-A4, 56-5-B7
| +-----------------------------------------------------------------------------+ |
| !Report!Limit! Description of ! CFM ! CFM ! CFM ! CFM ! CFM ! Unit ! |
| !Item !No. !Report Item !56-5-A5!56-5-B6!56-5-B5!56-5-A4!56-5-B7! ! |
| ! ! ! !-------!-------!-------!-------!-------!------! |
| ! ! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! ! |
| ! ! ! ! C7xxxx! C8xxxx! C4xxxx! C6xxxx! C5xxxx! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.1.1! 212 !EGTdivT1 ! 25 ! 25 ! 25 ! 25 ! 25 ! deg C! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.1.2! 213 !EGTdivT2 ! 30 ! 30 ! 30 ! 30 ! 30 ! deg C! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.1.3! 214 !EGTdivT3 ! 35 ! 35 ! 35 ! 35 ! 35 ! deg C! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.1.4! 215 !EGTdivT4 ! 40 ! 40 ! 40 ! 40 ! 40 ! deg C! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.1.5! 216 !TNdivT1 ! 40 ! 40 ! 40 ! 40 ! 40 ! deg C! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.1.6! 217 !TNdivT2 ! 50 ! 50 ! 50 ! 50 ! 50 ! deg C! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.1.7! 218 !TNdivT3 ! 60 ! 60 ! 60 ! 60 ! 60 ! deg C! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.1.8! 219 !TNdivT4 ! 70 ! 70 ! 70 ! 70 ! 70 ! deg C! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.2.1! 220 !N1L1 ! 90 ! 90 ! 90 ! 90 ! 90 ! % ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.2.2! 221 !N1L2 ! 115 ! 115 ! 115 ! 115 ! 115 ! % ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.2.3! 222 !N1L3 ! 3 ! 3 ! 3 ! 3 ! 3 ! % ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.2.5! 224 !IVVL ! 150 ! 150 ! 150 ! 150 ! 150 !ft/min! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.2.6! 223 !ALTL ! 5000 ! 5000 ! 5000 ! 5000 ! 5000 ! ft ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.2.7! 225 !TATL ! 5 ! 5 ! 5 ! 5 ! 5 ! deg C! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.2.8! 226 !N1RRL ! 2 ! 2 ! 2 ! 2 ! 2 ! %/sec! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.2.9! 228 !'Y09'time ! 10 ! 10 ! 10 ! 10 ! 10 ! sec ! |
| ! ! !interval ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| !4.2.10! 227 !PFLdelta limit ! 0.1 ! 0.1 ! 0.1 ! 0.1 ! 0.1 ! kg/s ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.3.6! 229 !KL flight leg ! 14 ! 14 ! 14 ! 14 ! 14 ! ! |
| ! ! !counter limit ! ! ! ! ! ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.3.7! 230 !C09.1 limit for ! 7.7 ! 7.7 ! 7.7 ! 7.7 ! 7.7 ! deg C! |
| ! ! !climb (PH 5.1) ! ! ! ! ! ! /%N1 ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.3.8! 231 !C09.2 limit for ! 7.0 ! 7.0 ! 7.0 ! 7.0 ! 7.0 ! deg C! |
| ! ! !cruise (PH 6) ! ! ! ! ! ! /%N1 ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 4.3.9! 232 !M ! 10 ! 10 ! 10 ! 10 ! 10 ! ! |
| +-----------------------------------------------------------------------------+ |
(8) A318: CFMI Engines 56-5-B8, 56-5-B9
| +-----------------------------------------------------------------------------+ |
| !Report!Limit! Description of ! CFM ! CFM ! SPARE ! SPARE ! Unit ! |
| !Item !No. ! Report Item !56-5-B8!56-5-B9! ! ! ! |
| ! ! ! !-------!-------!-------!-------!------! |
| ! ! ! !DMU/ID !DMU/ID ! ! ! ! |
| ! ! ! !C1xxxxx! C2xxxx! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.1.1! 212 !EGTdivT1 ! 25 ! 25 ! ! ! deg C! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.1.2! 213 !EGTdivT2 ! 30 ! 30 ! ! ! deg C! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.1.3! 214 !EGTdivT3 ! 35 ! 35 ! ! ! deg C! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.1.4! 215 !EGTdivT4 ! 40 ! 40 ! ! ! deg C! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.1.5! 216 !TNdivT1 ! 40 ! 40 ! ! ! deg C! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.1.6! 217 !TNdivT2 ! 50 ! 50 ! ! ! deg C! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.1.7! 218 !TNdivT3 ! 60 ! 60 ! ! ! deg C! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.1.8! 219 !TNdivT4 ! 70 ! 70 ! ! ! deg C! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.2.1! 220 !N1L1 ! 90 ! 90 ! ! ! % ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.2.2! 221 !N1L2 ! 115 ! 115 ! ! ! % ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.2.3! 222 !N1L3 ! 3 ! 3 ! ! ! % ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.2.5! 224 !IVVL ! 150 ! 150 ! ! !ft/min! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.2.6! 223 !ALTL ! 5000 ! 5000 ! ! ! ft ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.2.7! 225 !TATL ! 5 ! 5 ! ! ! deg C! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.2.8! 226 !N1RRL ! 2 ! 2 ! ! ! %/sec! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.2.9! 228 !'Y09' time interval ! 10 ! 10 ! ! ! sec ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| !4.2.10! 227 !PFLdelta limit ! 0.1 ! 0.1 ! ! ! kg/s ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.3.6! 229 !KL flight leg counter ! 14 ! 14 ! ! ! ! |
| ! ! !limit ! ! ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.3.7! 230 !C09.1 limit for climb ! 7.7 ! 7.7 ! ! ! deg C! |
| ! ! !(PH 5.1) ! ! ! ! ! /%N1 ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.3.8! 231 !C09.2 limit for climb ! 7.0 ! 7.0 ! ! ! deg C! |
| ! ! !(PH 6) ! ! ! ! ! /%N1 ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 4.3.9! 232 !M ! 10 ! 10 ! ! ! ! |
| +-----------------------------------------------------------------------------+ |
(9) A320: CFMI Engines 56-5-A1, 56-5-A3, 56-5-B4, 56-5-B5, 56-5-B6
| +-----------------------------------------------------------------------------+ |
| !Report! Description of ! CFM ! CFM ! CFM ! CFM ! CFM ! Unit ! |
| !Item ! Report Item !56-5-A1!56-5-A3!56-5-B4!56-5-B5!56-5-B6! ! |
| ! ! !-------!-------!-------!-------!-------!------! |
| ! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! ! |
| ! ! ! CFM #1! CFM #2! CFM #3! CFM #4! CFM #8! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.1.1! EGTdivT1 limit ! 25 ! 25 ! 25 ! 25 ! 25 ! deg C! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.1.2! EGTdivT2 limit ! 30 ! 30 ! 30 ! 30 ! 30 ! deg C! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.1.3! EGTdivT3 limit ! 35 ! 35 ! 35 ! 35 ! 35 ! deg C! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.1.4! EGTdivT4 limit ! 40 ! 40 ! 40 ! 40 ! 40 ! deg C! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.1.5! TNdivT1 limit ! 40 ! 40 ! 40 ! 40 ! 40 ! deg C! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.1.6! TNdivT2 limit ! 50 ! 50 ! 50 ! 50 ! 50 ! deg C! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.1.7! TNdivT3 limit ! 60 ! 60 ! 60 ! 60 ! 60 ! deg C! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.1.8! TNdivT4 limit ! 70 ! 70 ! 70 ! 70 ! 70 ! deg C! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.2.1! N1L1 limit ! 90 ! 90 ! 90 ! 90 ! 90 ! % ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.2.2! N1L2 limit ! 115 ! 115 ! 115 ! 115 ! 115 ! % ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.2.3! N1L3 limit ! 3 ! 3 ! 3 ! 3 ! 3 ! % ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.2.5! IVVL limit (valid ! 150 ! 150 ! 150 ! 150 ! 150 !ft/min! |
| ! ! during flight phase 4)! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.2.6! ALTL limit (valid du- ! 5000 ! 5000 ! 5000 ! 5000 ! 5000 ! ft ! |
| ! !ring flight phase 5.1) ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.2.7! TATL limit ! 5 ! 5 ! 5 ! 5 ! 5 ! deg C! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.2.8! N1RL limit ! 2 ! 2 ! 2 ! 2 ! 2 ! %/sec! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.2.9! 'Y09' time interval ! 10 ! 10 ! 10 ! 10 ! 10 ! sec ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| !4.2.10! PFdelta limit ! 0.1 ! 0.1 ! 0.1 ! 0.1 ! 0.1 ! kg/s ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.3.6! KL limit ! 14 ! 14 ! 14 ! 14 ! 14 ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.3.7! C09.1 limit for climb ! 7.7 ! 7.7 ! 7.7 ! 7.7 ! 7.7 ! deg C! |
| ! ! (PH 5.1) ! ! ! ! ! ! /%N1 ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.3.8! C09.2 limit for cruise! 7.0 ! 7.0 ! 7.0 ! 7.0 ! 7.0 ! deg C! |
| ! ! (PH 6) ! ! ! ! ! ! /%N1 ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.3.9! M programmed limit ! 10 ! 10 ! 10 ! 10 ! 10 ! ! |
| +-----------------------------------------------------------------------------+ |
(10) A321: CFMI Engines 56-5-B1, 56-5-B2, 56-5-B3, 56-5-B4
| +-----------------------------------------------------------------------------+ |
| !Report! Description of Report Item ! CFM ! CFM ! CFM ! CFM ! Unit ! |
| !Item ! !56-5-B1!56-5-B2!56-5-B3!56-5-B4! ! |
| ! ! !-------!-------!-------!-------!------! |
| ! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! ! |
| ! ! ! CFM #5! CFM #6! CFM #6! CFM #3! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.1.1! EGTdivT1 limit ! 25 ! 25 ! 25 ! 25 ! deg C! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.1.2! EGTdivT2 limit ! 30 ! 30 ! 30 ! 30 ! deg C! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.1.3! EGTdivT3 limit ! 35 ! 35 ! 35 ! 35 ! deg C! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.1.4! EGTdivT4 limit ! 40 ! 40 ! 40 ! 40 ! deg C! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.1.5! TNdivT1 limit ! 40 ! 40 ! 40 ! 40 ! deg C! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.1.6! TNdivT2 limit ! 50 ! 50 ! 50 ! 50 ! deg C! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.1.7! TNdivT3 limit ! 60 ! 60 ! 60 ! 60 ! deg C! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.1.8! TNdivT4 limit ! 70 ! 70 ! 70 ! 70 ! deg C! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.2.1! N1L1 limit ! 90 ! 90 ! 90 ! 90 ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.2.2! N1L2 limit ! 115 ! 115 ! 115 ! 115 ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.2.3! N1L3 limit ! 3 ! 3 ! 3 ! 3 ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.2.5! IVVL limit (valid during ! 150 ! 150 ! 150 ! 150 !ft/min! |
| ! ! flight phase 4) ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.2.6! ALTL limit (valid during ! 5000 ! 5000 ! 5000 ! 5000 ! ft ! |
| ! ! flight phase 5.1) ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.2.7! TATL limit ! 5 ! 5 ! 5 ! 5 ! deg C! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.2.8! N1RL limit ! 2 ! 2 ! 2 ! 2 ! %/sec! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.2.9! 'Y09' time interval ! 10 ! 10 ! 10 ! 10 ! sec ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !4.2.10! PFdelta limit ! 0.1 ! 0.1 ! 0.1 ! 0.1 ! kg/s ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.3.6! KL limit ! 14 ! 14 ! 14 ! 14 ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.3.7! C09.1 limit for climb (PH 5.1)! 7.7 ! 7.7 ! 7.7 ! 7.7 ! deg C! |
| ! ! ! ! ! ! ! /%N1 ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.3.8! C09.2 limit for cruise (PH 6) ! 7.0 ! 7.0 ! 7.0 ! 7.0 ! deg C! |
| ! ! ! ! ! ! ! /%N1 ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.3.9! M programmed limit ! 10 ! 10 ! 10 ! 10 ! ! |
| +-----------------------------------------------------------------------------+ |
(11) A319: CFMI Engines 56-5-A5, 56-5-B6, 56-5-B5, 56-5-A4, 56-5-B7
| +-----------------------------------------------------------------------------+ |
| !Report! Description of ! CFM ! CFM ! CFM ! CFM ! CFM ! Unit ! |
| !Item ! Report Item !56-5-A5!56-5-B6!56-5-B5!56-5-A4!56-5-B7! ! |
| ! ! !-------!-------!-------!-------!-------!------! |
| ! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! ! |
| ! ! ! C7xxxx! C8xxxx! C4xxxx! C6xxxx! C5xxxx! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.1.1! EGTdivT1 limit ! 25 ! 25 ! 25 ! 25 ! 25 ! deg C! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.1.2! EGTdivT2 limit ! 30 ! 30 ! 30 ! 30 ! 30 ! deg C! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.1.3! EGTdivT3 limit ! 35 ! 35 ! 35 ! 35 ! 35 ! deg C! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.1.4! EGTdivT4 limit ! 40 ! 40 ! 40 ! 40 ! 40 ! deg C! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.1.5! TNdivT1 limit ! 40 ! 40 ! 40 ! 40 ! 40 ! deg C! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.1.6! TNdivT2 limit ! 50 ! 50 ! 50 ! 50 ! 50 ! deg C! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.1.7! TNdivT3 limit ! 60 ! 60 ! 60 ! 60 ! 60 ! deg C! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.1.8! TNdivT4 limit ! 70 ! 70 ! 70 ! 70 ! 70 ! deg C! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.2.1! N1L1 limit ! 90 ! 90 ! 90 ! 90 ! 90 ! % ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.2.2! N1L2 limit ! 115 ! 115 ! 115 ! 115 ! 115 ! % ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.2.3! N1L3 limit ! 3 ! 3 ! 3 ! 3 ! 3 ! % ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.2.5! IVVL limit valid ! 150 ! 150 ! 150 ! 150 ! 150 !ft/min! |
| ! ! during flight phase 4 ! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.2.6! ALTL limit valid ! 5000 ! 5000 ! 5000 ! 5000 ! 5000 ! ft ! |
| ! !during flight phase 5.1! ! ! ! ! ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.2.7! TATL limit ! 5 ! 5 ! 5 ! 5 ! 5 ! deg C! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.2.8! N1RL limit ! 2 ! 2 ! 2 ! 2 ! 2 ! %/sec! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.2.9! 'Y09' time interval ! 10 ! 10 ! 10 ! 10 ! 10 ! sec ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| !4.2.10! PFdelta limit ! 0.1 ! 0.1 ! 0.1 ! 0.1 ! 0.1 ! kg/s ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.3.6! KL limit ! 14 ! 14 ! 14 ! 14 ! 14 ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.3.7! C09.1 limit for climb ! 7.7 ! 7.7 ! 7.7 ! 7.7 ! 7.7 ! deg C! |
| ! ! (PH 5.1) ! ! ! ! ! ! /%N1 ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.3.8! C09.2 limit for cruise! 7.0 ! 7.0 ! 7.0 ! 7.0 ! 7.0 ! deg C! |
| ! ! (PH 6) ! ! ! ! ! ! /%N1 ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 4.3.9! M programmed limit ! 10 ! 10 ! 10 ! 10 ! 10 ! ! |
| +-----------------------------------------------------------------------------+ |
(12) A318: CFMI Engines 56-5-B8, 56-5-B9
| +-----------------------------------------------------------------------------+ |
| !Report! Description of Report Item ! CFM ! CFM ! SPARE ! SPARE ! Unit ! |
| !Item ! !56-5-B8!56-5-B9! ! ! ! |
| ! ! !-------!-------!-------!-------!------! |
| ! ! !DMU/ID !DMU/ID ! ! ! ! |
| ! ! !C1xxxxx! C2xxxx! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.1.1! EGTdivT1 limit ! 25 ! 25 ! ! ! deg C! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.1.2! EGTdivT2 limit ! 30 ! 30 ! ! ! deg C! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.1.3! EGTdivT3 limit ! 35 ! 35 ! ! ! deg C! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.1.4! EGTdivT4 limit ! 40 ! 40 ! ! ! deg C! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.1.5! TNdivT1 limit ! 40 ! 40 ! ! ! deg C! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.1.6! TNdivT2 limit ! 50 ! 50 ! ! ! deg C! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.1.7! TNdivT3 limit ! 60 ! 60 ! ! ! deg C! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.1.8! TNdivT4 limit ! 70 ! 70 ! ! ! deg C! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.2.1! N1L1 limit ! 90 ! 90 ! ! ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.2.2! N1L2 limit ! 115 ! 115 ! ! ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.2.3! N1L3 limit ! 3 ! 3 ! ! ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.2.5! IVVL limit valid during ! 150 ! 150 ! ! !ft/min! |
| ! ! flight phase 4 ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.2.6! ALTL limit valid during ! 5000 ! 5000 ! ! ! ft ! |
| ! ! flight phase 5.1 ! ! ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.2.7! TATL limit ! 5 ! 5 ! ! ! deg C! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.2.8! N1RL limit ! 2 ! 2 ! ! ! %/sec! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.2.9! 'Y09' time interval ! 10 ! 10 ! ! ! sec ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| !4.2.10! PFdelta limit ! 0.1 ! 0.1 ! ! ! kg/s ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.3.6! KL limit ! 14 ! 14 ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.3.7! C09.1 limit for climb (PH 5.1)! 7.7 ! 7.7 ! ! ! deg C! |
| ! ! ! ! ! ! ! /%N1 ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.3.8! C09.2 limit for climb (PH 6) ! 7.0 ! 7.0 ! ! ! deg C! |
| ! ! ! ! ! ! ! /%N1 ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 4.3.9! M programmed limit ! 10 ! 10 ! ! ! ! |
| +-----------------------------------------------------------------------------+ |
Z. Report Limits for Engine Start Report <10>
(1) A320: CFMI Engines 56-5-A1, 56-5-A3, 56-5-B4
| +-----------------------------------------------------------------------------+ |
| !Report! Limit ! Description of Report Item !56-5-A1!56-5-A3!56-5-B4! Unit ! |
| !Item N! No. ! ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.1 ! 265 ! EGTL limit ! 725 ! 725 ! 725 ! deg ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 6.1 ! 266 ! F10.1 cycle ! 25 ! 25 ! 25 !nbcyc.! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 6.2 ! 267 ! N2 trigger value ! 40 ! 40 ! 40 ! % ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 7.2 ! 268 ! No of consecutive legs (X10) ! 5 ! 5 ! 5 ! ! |
| +-----------------------------------------------------------------------------+ |
(2) A321: CFMI Engines 56-5-B1, 56-5-B2, 56-5-B3
| +-----------------------------------------------------------------------------+ |
| !Report! Limit ! Description of Report Item !56-5-B1!56-5-B2!56-5-B3! Unit ! |
| !Item N! No. ! ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.1 ! 265 ! EGTL limit ! 725 ! 725 ! 725 ! deg ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 6.1 ! 266 ! F10.1 cycle ! 25 ! 25 ! 25 !nbcyc.! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 6.2 ! 267 ! N2 trigger value ! 40 ! 40 ! 40 ! % ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 7.2 ! 268 ! No of consecutive legs (X10) ! 5 ! 5 ! 5 ! ! |
| +-----------------------------------------------------------------------------+ |
(3) A319: CFMI Engines 56-5-A5, 56-5-B6, 56-5-B5, 56-5A4.
| +-----------------------------------------------------------------------------+ |
| !Report! Limit ! Description of Report !56-5-A5!56-5-B6!56-5-B5!56-5A4! Unit ! |
| !Item N! No. ! Item ! ! ! ! ! ! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! 5.1 ! 265 ! EGTL limit ! 725 ! 725 ! 725 ! 725 ! deg ! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! 6.1 ! 266 ! F10.1 cycle ! 25 ! 25 ! 25 ! 25 !nbcyc.! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! 6.2 ! 267 ! N2 trigger value ! 40 ! 40 ! 40 ! 40 ! % ! |
| !------!-------!------------------------!-------!-------!-------!------!------! |
| ! 7.2 ! 268 ! No of consecutive legs ! 5 ! 5 ! 5 ! 5 ! ! |
| ! ! ! (X10) ! ! ! ! ! ! |
| +-----------------------------------------------------------------------------+ |
(4) A319: CFMI Engines 56-5-B7
| +-----------------------------------------------------------------------------+ |
| !Report! Limit ! Description of Report Item !56-5-B7! SPARE ! SPARE ! Unit ! |
| !Item N! No. ! ! ! ! ! ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 5.1 ! 265 ! EGTL limit ! 725 ! ! ! deg ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 6.1 ! 266 ! F10.1 cycle ! 25 ! ! !nbcyc.! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 6.2 ! 267 ! N2 trigger value ! 40 ! ! ! % ! |
| !------!-------!-------------------------------!-------!-------!-------!------! |
| ! 7.2 ! 268 ! No of consecutive legs (X10) ! 5 ! ! ! ! |
| +-----------------------------------------------------------------------------+ |
(5) A320: CFMI Engines 56-5-A1, 56-5-A3, 56-5-B4, 56-5-B5, 56-5-B6
| +-----------------------------------------------------------------------------+ |
| !Report!Limit! Description of ! CFM ! CFM ! CFM ! CFM ! CFM ! Unit ! |
| !Item !No. ! Report Item !56-5-A1!56-5-A3!56-5-B4!56-5-B5!56-5-B6! ! |
| ! ! ! !-------!-------!-------!-------!-------!------! |
| ! ! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! ! |
| ! ! ! ! CFM #1! CFM #2! CFM #3! CFM #4! CFM #8! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.1 ! 265 !EGTL limit ! 725 ! 725 ! 725 ! 725 ! 725 ! deg C! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 6.1 ! 266 !'F10.1' ! 25 ! 25 ! 25 ! 25 ! 25 ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 6.2 ! 267 !N2 trigger ! 40 ! 40 ! 40 ! 40 ! 40 ! % ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 7.2 ! 268 !Nb. 'X10' for ! 5 ! 5 ! 5 ! 5 ! 5 ! ! |
| ! ! !consecutive legs ! ! ! ! ! ! ! |
| +-----------------------------------------------------------------------------+ |
(6) A321: CFMI Engines 56-5-B1, 56-5-B2, 56-5-B3, 56-5-B4
| +-----------------------------------------------------------------------------+ |
| !Report!Limit! Description of ! CFM ! CFM ! CFM ! CFM ! Unit ! |
| !Item !No. ! Report Item !56-5-B1!56-5-B2!56-5-B3!56-5-B4! ! |
| ! ! ! !-------!-------!-------!-------!------! |
| ! ! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! ! |
| ! ! ! ! CFM #5! CFM #6! CFM #7! CFM #3! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.1 ! 265 !EGTL limit ! 725 ! 725 ! 725 ! 725 ! deg C! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 6.1 ! 266 !'F10.1' ! 25 ! 25 ! 25 ! 25 ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 6.2 ! 267 !N2 trigger ! 40 ! 40 ! 40 ! 40 ! % ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 7.2 ! 268 !Nb. 'X10' for consecutive! 5 ! 5 ! 5 ! 5 ! ! |
| ! ! !legs ! ! ! ! ! ! |
| +-----------------------------------------------------------------------------+ |
(7) A319: CFMI Engines 56-5-A5, 56-5-B6, 56-5-B5, 56-5A4, 56-5-B7
| +-----------------------------------------------------------------------------+ |
| !Report!Limit! Description of ! CFM ! CFM ! CFM ! CFM ! CFM ! Unit ! |
| !Item !No. ! Report Item !56-5-A5!56-5-B6!56-5-B5!56-5-A4!56-5-B7! ! |
| ! ! ! !-------!-------!-------!-------!-------!------! |
| ! ! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! ! |
| ! ! ! ! C7xxxx! C8xxxx! C4xxxx! C6xxxx! C5xxxx! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 5.1 ! 265 !EGTL limit ! 725 ! 725 ! 725 ! 725 ! 725 ! deg C! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 6.1 ! 266 !'F10.1' ! 25 ! 25 ! 25 ! 25 ! 25 ! ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 6.2 ! 267 !N2 trigger ! 40 ! 40 ! 40 ! 40 ! 40 ! % ! |
| !------!-----!-----------------!-------!-------!-------!-------!-------!------! |
| ! 7.2 ! 268 !Nb. 'X10' for ! 5 ! 5 ! 5 ! 5 ! 5 ! ! |
| ! ! !consecutive legs ! ! ! ! ! ! ! |
| +-----------------------------------------------------------------------------+ |
(8) A318: CFMI Engines 56-5-B8, 56-5-B9
| +-----------------------------------------------------------------------------+ |
| !Report!Limit! Description of ! CFM ! CFM ! SPARE ! SPARE ! Unit ! |
| !Item !No. ! Report Item !56-5-B8!56-5-B9! ! ! ! |
| ! ! ! !-------!-------!-------!-------!------! |
| ! ! ! !DMU/ID !DMU/ID ! ! ! ! |
| ! ! ! !C1xxxxx! C2xxxx! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 5.1 ! 265 !EGTL limit ! 725 ! 725 ! ! ! deg C! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 6.1 ! 266 !'F10.1' ! 25 ! 25 ! ! ! ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 6.2 ! 267 !N2 trigger ! 40 ! 40 ! ! ! % ! |
| !------!-----!-------------------------!-------!-------!-------!-------!------! |
| ! 7.2 ! 268 !Nb. 'X10' for consecutive! 5 ! 5 ! ! ! ! |
| ! ! !legs ! ! ! ! ! ! |
| +-----------------------------------------------------------------------------+ |
(9) A320: CFMI Engines 56-5-A1, 56-5-A3, 56-5-B4, 56-5-B5, 56-5-B6
| +-----------------------------------------------------------------------------+ |
| !Report! Description of ! CFM ! CFM ! CFM ! CFM ! CFM ! Unit ! |
| !Item ! Report Item !56-5-A1!56-5-A3!56-5-B4!56-5-B5!56-5-B6! ! |
| ! ! !-------!-------!-------!-------!-------!------! |
| ! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! ! |
| ! ! ! CFM #1! CFM #2! CFM #3! CFM #4! CFM #8! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.1 ! EGTL limit ! 725 ! 725 ! 725 ! 725 ! 725 ! deg C! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 6.1 ! 'F10.1' cycle ! 25 ! 25 ! 25 ! 25 ! 25 ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 6.2 ! N2 trigger value ! 40 ! 40 ! 40 ! 40 ! 40 ! % ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 7.2 ! No. 'X10' for ! 5 ! 5 ! 5 ! 5 ! 5 ! ! |
| ! ! consecutive legs ! ! ! ! ! ! ! |
| +-----------------------------------------------------------------------------+ |
(10) A321: CFMI Engines 56-5-B1, 56-5-B2, 56-5-B3, 56-5-B4
| +-----------------------------------------------------------------------------+ |
| !Report! Description of Report Item ! CFM ! CFM ! CFM ! CFM ! Unit ! |
| !Item ! !56-5-B1!56-5-B2!56-5-B3!56-5-B4! ! |
| ! ! !-------!-------!-------!-------!------! |
| ! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! ! |
| ! ! ! CFM #5! CFM #6! CFM #7! CFM #3! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.1 ! EGTL limit ! 725 ! 725 ! 725 ! 725 ! deg C! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 6.1 ! 'F10.1' cycle ! 25 ! 25 ! 25 ! 25 ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 6.2 ! N2 trigger value ! 40 ! 40 ! 40 ! 40 ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 7.2 ! No. of 'X10' consecutive legs ! 5 ! 5 ! 5 ! 5 ! ! |
| +-----------------------------------------------------------------------------+ |
(11) A319: CFMI Engines 56-5-A5, 56-5-B6, 56-5-B5, 56-5A4, 56-5-B7
| +-----------------------------------------------------------------------------+ |
| !Report! Description of ! CFM ! CFM ! CFM ! CFM ! CFM ! Unit ! |
| !Item ! Report Item !56-5-A5!56-5-B6!56-5-B5!56-5-A4!56-5-B7! ! |
| ! ! !-------!-------!-------!-------!-------!------! |
| ! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! ! |
| ! ! ! C7xxxx! C8xxxx! C4xxxx! C6xxxx! C5xxxx! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 5.1 ! EGTL limit ! 725 ! 725 ! 725 ! 725 ! 725 ! deg C! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 6.1 ! 'F10.1' cycle ! 25 ! 25 ! 25 ! 25 ! 25 ! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 6.2 ! N2 trigger value ! 40 ! 40 ! 40 ! 40 ! 40 ! % ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! 7.2 ! No. 'X10' for ! 5 ! 5 ! 5 ! 5 ! 5 ! ! |
| ! ! consecutive legs ! ! ! ! ! ! ! |
| +-----------------------------------------------------------------------------+ |
(12) A318: CFMI Engines 56-5-B8, 56-5-B9
| +-----------------------------------------------------------------------------+ |
| !Report! Description of Report Item ! CFM ! CFM ! SPARE ! SPARE ! Unit ! |
| !Item ! !56-5-B8!56-5-B9! ! ! ! |
| ! ! !-------!-------!-------!-------!------! |
| ! ! !DMU/ID !DMU/ID ! ! ! ! |
| ! ! !C1xxxxx! C2xxxx! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 5.1 ! EGTL limit ! 725 ! 725 ! ! ! deg C! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 6.1 !'F10.1' cycle ! 25 ! 25 ! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 6.2 ! N2 trigger value ! 40 ! 40 ! ! ! % ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! 7.2 ! No. of 'X10' consecutive legs ! 5 ! 5 ! ! ! ! |
| +-----------------------------------------------------------------------------+ |
AA. Report Limits for Engine Run-up Report <11>
(1) A320: CFMI Engines 56-5-A1, 56-5-A3, 56-5-B4
| +-----------------------------------------------------------------------------+ |
| !Report! Description of Report Item !56-5-A1!56-5-A3!56-5-B4!SPARE ! Unit ! |
| !Item N! ! ! ! ! ! ! |
| !------!--------------------------------!-------!-------!-------!------!------! |
| ! ! |
| ! N O T A P P L I C A B L E ! |
| ! ! |
| +-----------------------------------------------------------------------------+ |
(2) A321: CFMI Engines 56-5-B1, 56-5-B2, 56-5-B3
| +-----------------------------------------------------------------------------+ |
| !Limit ! Description of Report Item !56-5-B1!56-5-B2!56-5-B3!SPARE ! Unit ! |
| !No ! ! ! ! ! ! ! |
| !------!--------------------------------!-------!-------!-------!------!------! |
| ! ! |
| ! N O T A P P L I C A B L E ! |
| ! ! |
| +-----------------------------------------------------------------------------+ |
(3) A319: CFMI Engines 56-5-A5, 56-5-B6, 56-5-B5, 56-5A4
| +-----------------------------------------------------------------------------+ |
| !Limit ! Description of Report Item !56-5-A5!56-5-B6!56-5-B5!56-5A4! Unit ! |
| !No ! ! ! ! ! ! ! |
| !------!--------------------------------!-------!-------!-------!------!------! |
| ! ! |
| ! N O T A P P L I C A B L E ! |
| ! ! |
| +-----------------------------------------------------------------------------+ |
(4) A319: CFMI Engines 56-5-B7
| +-----------------------------------------------------------------------------+ |
| !Limit ! Description of Report Item !56-5-B7! SPARE ! SPARE ! SPARE! Unit ! |
| !No ! ! ! ! ! ! ! |
| !------!--------------------------------!-------!-------!-------!------!------! |
| ! ! |
| ! N O T A P P L I C A B L E ! |
| ! ! |
| +-----------------------------------------------------------------------------+ |
(5) A320: CFMI Engines 56-5-A1, 56-5-A3, 56-5-B4, 56-5-B5, 56-5-B6
| +-----------------------------------------------------------------------------+ |
| !Report! Description of ! CFM ! CFM ! CFM ! CFM ! CFM ! Unit ! |
| !Item ! Report Item !56-5-A1!56-5-A3!56-5-B4!56-5-B5!56-5-B6! ! |
| ! ! !-------!-------!-------!-------!-------!------! |
| ! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! ! |
| ! ! ! CFM #1! CFM #2! CFM #3! CFM #4! CFM #8! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! ! |
| ! N O T A P P L I C A B L E ! |
| ! ! |
| +-----------------------------------------------------------------------------+ |
(6) A321: CFMI Engines 56-5-B1, 56-5-B2, 56-5-B3, 56-5-B4
| +-----------------------------------------------------------------------------+ |
| !Report! Description of Report Item ! CFM ! CFM ! CFM ! CFM ! Unit ! |
| !Item ! !56-5-B1!56-5-B2!56-5-B3!56-5-B4! ! |
| ! ! !-------!-------!-------!-------!------! |
| ! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! ! |
| ! ! ! CFM #5! CFM #6! CFM #7! CFM #3! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! ! |
| ! N O T A P P L I C A B L E ! |
| ! ! |
| +-----------------------------------------------------------------------------+ |
(7) A319: CFMI Engines 56-5-A5, 56-5-B6, 56-5-B5, 56-5A4, 56-5-B7
| +-----------------------------------------------------------------------------+ |
| !Report! Description of ! CFM ! CFM ! CFM ! CFM ! CFM ! Unit ! |
| !Item ! Report Item !56-5-A5!56-5-B6!56-5-B5!56-5-A4!56-5-B7! ! |
| ! ! !-------!-------!-------!-------!-------!------! |
| ! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! ! |
| ! ! ! C7xxxx! C8xxxx! C4xxxx! C6xxxx! C5xxxx! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! ! |
| ! N O T A P P L I C A B L E ! |
| ! ! |
| +-----------------------------------------------------------------------------+ |
(8) A318: CFMI Engines 56-5-B8, 56-5-B9
| +-----------------------------------------------------------------------------+ |
| !Report! Description of Report Item ! CFM ! CFM ! SPARE ! SPARE ! Unit ! |
| !Item ! !56-5-B8!56-5-B9! ! ! ! |
| ! ! !-------!-------!-------!-------!------! |
| ! ! !DMU/ID !DMU/ID ! ! ! ! |
| ! ! !C1xxxxx! C2xxxx! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! ! |
| ! N O T A P P L I C A B L E ! |
| ! ! |
| +-----------------------------------------------------------------------------+ |
(9) A320: CFMI Engines 56-5-A1, 56-5-A3, 56-5-B4, 56-5-B5, 56-5-B6
| +-----------------------------------------------------------------------------+ |
| !Report! Description of ! CFM ! CFM ! CFM ! CFM ! CFM ! Unit ! |
| !Item ! Report Item !56-5-A1!56-5-A3!56-5-B4!56-5-B5!56-5-B6! ! |
| ! ! !-------!-------!-------!-------!-------!------! |
| ! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! ! |
| ! ! ! CFM #1! CFM #2! CFM #3! CFM #4! CFM #8! ! |
| !------!-----------------------!-------!-------!-------!-------!-------!------! |
| ! ! |
| ! N O T A P P L I C A B L E ! |
| ! ! |
| +-----------------------------------------------------------------------------+ |
(10) A321: CFMI Engines 56-5-B1, 56-5-B2, 56-5-B3, 56-5-B4
| +-----------------------------------------------------------------------------+ |
| !Report! Description of Report Item ! CFM ! CFM ! CFM ! CFM ! Unit ! |
| !Item ! !56-5-B1!56-5-B2!56-5-B3!56-5-B4! ! |
| ! ! !-------!-------!-------!-------!------! |
| ! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! ! |
| ! ! ! CFM #5! CFM #6! CFM #7! CFM #3! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! ! |
| ! N O T A P P L I C A B L E ! |
| ! ! |
| +-----------------------------------------------------------------------------+ |
(11) A319: CFMI Engines 56-5-A5, 56-5-B6, 56-5-B5, 56-5A4, 56-5-B7
| +-----------------------------------------------------------------------------+ |
| !Report! Description of ! CFM ! CFM ! CFM ! CFM ! CFM ! Unit ! |
| !Item ! Report Item !56-5-A5!56-5-B6!56-5-B5!56-5-A4!56-5-B7! ! |
| ! ! !-------!-------!-------!-------!-------!------! |
| ! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! ! |
| ! ! ! C7xxxx! C8xxxx! C4xxxx! C6xxxx! C5xxxx! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! ! |
| ! N O T A P P L I C A B L E ! |
| ! ! |
| +-----------------------------------------------------------------------------+ |
(12) A318: CFMI Engines 56-5-B8, 56-5-B9
| +-----------------------------------------------------------------------------+ |
| !Report! Description of Report Item ! CFM ! CFM ! SPARE ! SPARE ! Unit ! |
| !Item ! !56-5-B8!56-5-B9! ! ! ! |
| ! ! !-------!-------!-------!-------!------! |
| ! ! !DMU/ID !DMU/ID ! ! ! ! |
| ! ! !C1xxxxx! C2xxxx! ! ! ! |
| !------!-------------------------------!-------!-------!-------!-------!------! |
| ! ! |
| ! N O T A P P L I C A B L E ! |
| ! ! |
| +-----------------------------------------------------------------------------+ |