W DOC AIRBUS | AMM A320F

AIDS - 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:
  • <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,
** ON A/C NOT FOR ALL
2. Reports
A. Engine Cruise Report <01>
F Engine Cruise Report <01> (Engine Type IAE) ** 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.
NOTE: For the standard header definition of the report refer to (Ref. AMM D/O 31-36-00-00).
NOTE: If the Engine Serial Number (ESN) printed out in the report is in the range between 13191 and 15000, then add 5000 to this value to get the actual ESN.
(1) Engine-Cruise-Report Data-Field-Description <01> (Engine Type IAE)
+---------------------------------------------------------------------+
! 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 !
! ! !
! ! NOTE: If the ESN printed out in the report is in !
! ! the range between 13191 and 15000, then add !
! ! 5000 to this value to get the actual ESN. !
!--------------!------------------------------------------------------!
! EHRS ! Engine Flight Hours !
! 99999 ! (00000 to 99999 hours) !
! ! DMU Engine 1 and 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. !
!--------------!------------------------------------------------------!
! ECYC ! Engine Cycle !
! 99999 ! (00000 to 99999) !
! ! DMU Engine 1 and 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 the ECYC through the MCDU if !
! ! the DMU is replaced on the A/C. !
!--------------!------------------------------------------------------!
! 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 !
! ! !
! ! Parameter for AP1 ! Parameter for AP2 !Definition: !
! ! Report Line EC: ! Report Line EE: ! !
! ! -------------------!-------------------!------------ !
! ! / ! / !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 !
! ! -------------------!-------------------!------------ !
! ! 01.2.274.00.24 = 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 !
! ! 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 !
! ! left 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 then 'E3' !
! ! appears bellow AP1 and AP2. !
!--------------!------------------------------------------------------!
! 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. !
! ! N VARe(i) !
! ! QE=SIGMA(We(i)*---------------) !
! ! i=A 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. !
!--------------!------------------------------------------------------!
! EPR ! EPR Actual !
! 9999 ! (0.6 to 1.8) !
! ! EEC 7C.1.340.01 Engine 1 !
! ! 7C.2.340.10 Engine 2 !
!--------------!------------------------------------------------------!
! EPRC ! EPR Command !
! 9999 ! (0.6 to 1.8) !
! ! EEC 7C.1.341.01 Engine 1 !
! ! 7C.2.341.10 Engine 2 !
!--------------!------------------------------------------------------!
! EGT ! Selected T495 (Exhaust Gas Temperature) !
! X999 ! (-80 to 999.9 deg 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. !
! ! EEC 7C.1.345.01 Engine 1 !
! ! 7C.2.345.10 Engine 2 !
!--------------!------------------------------------------------------!
! N1 ! Selected N1 Actual !
! 9999 ! (0 to 120.0 %rpm) !
! ! EEC 7C.1.346.01 Engine 1 !
! ! 7C.2.346.10 Engine 2 !
!--------------!------------------------------------------------------!
! N2 ! Selected N2 Actual !
! 9999 ! (0 to 120.0 %rpm) !
! ! EEC 7C.1.344.01 Engine 1 !
! ! 7C.2.344.10 Engine 2 !
!--------------!------------------------------------------------------!
! FF ! Engine Fuel Flow !
! 9999 ! 0 to 8500 kg/h (0 to 17000 p/h) !
! ! EEC 7C.1.244.01 Engine 1 !
! ! 7C.2.244.10 Engine 2 !
!--------------!------------------------------------------------------!
! P125 ! P125 Static Air Pressure at Position 12.5 !
! 99999 ! (0.0 to 30.000 psia) !
! ! EEC 7C.1.257.01 Engine 1 !
! ! 7C.2.257.10 Engine 2 !
!--------------!------------------------------------------------------!
! P25 ! P25 Total Air Pressure at Position 2.5 !
! 99999 ! (0.0 to 30.000 psia) !
! ! EEC 7C.1.262.01 Engine 1 !
! ! 7C.2.262.10 Engine 2 !
!--------------!------------------------------------------------------!
! T25 ! Selected T25 !
! X999 ! (-30 to 300.0 deg 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. !
! ! EEC 7C.1.263.01 Engine 1 !
! ! 7C.2.263.10 Engine 2 !
!--------------!------------------------------------------------------!
! P3 ! Selected PS3 (Burner Pressure) !
! 9999 ! (0.0 to 550.0 psia) !
! ! EEC 7C.1.264.01 Engine 1 !
! ! 7C.2.264.10 Engine 2 !
!--------------!------------------------------------------------------!
! T3 ! Selected T3 !
! X999 ! (-89.0 to 700.0 deg 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. !
! ! EEC 7C.1.265.01 Engine 1 !
! ! 7C.2.265.10 Engine 2 !
!--------------!------------------------------------------------------!
! P49 ! Pressure on position 4.9 !
! 99999 ! (1 to 25 psia) !
! ! EEC 7C.1.132.01 Engine 1 !
! ! 7C.2.132.10 Engine 2 !
!--------------!------------------------------------------------------!
! SVA ! Stator Vane Actuator Feedback !
! 999 ! (0 to 100 %) !
! ! EEC 7C.1.325.01 Engine 1 !
! ! 7C.2.325.10 Engine 2 !
!--------------!------------------------------------------------------!
! BAF ! 2.5 Bleed Actuator Feedback !
! X99 ! (-16 % to 128 %) !
! ! EEC 7C.1.335.01 Engine 1 !
! ! 7C.2.335.10 Engine 2 !
!--------------!------------------------------------------------------!
! ACC ! Active Clearance Control Feedback !
! 999 ! (0 to 100 %) !
! ! EEC 7C.1.330.01 Engine 1 !
! ! 7C.2.330.10 Engine 2 !
!--------------!------------------------------------------------------!
! LP ! LPT ACC Solenoid Position !
! 01 ! Bit status 1 = closed !
! ! EEC 7C.1.271.01.17 Engine 1 !
! ! 7C.2.271.10.17 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 6F.1.143.01 Engine 1 !
! ! 6F.2.143.10# !
! ! 6F.1.142.01 Engine 2 !
! ! 6F.2.142.10# !
!--------------!------------------------------------------------------!
! TN ! Nacelle Temperature !
! X99 ! (-55 to 300 deg 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# !
!--------------!------------------------------------------------------!
! P2 ! PT2 Total Air Pressure at Position 2 !
! 99999 ! (0.0 to 25.000 psia) !
! ! EEC 7C.1.131.01 Engine 1 !
! ! 7C.2.131.10 Engine 2 !
!--------------!------------------------------------------------------!
! T2 ! T2 Temperature !
! X999 ! (-80 to 90.0 deg 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. !
! ! EEC 7C.1.130.01 Engine 1 !
! ! 7C.2.130.10 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.270.XX.17 = 1 Manual Thrust Mode Active !
! ! 12 7C.X.270.XX.18 = 1 N1 Rated Mode Engaged !
! ! 13 7C.X.270.XX.20 = 1 Auto Thrust Mode Activated!
! ! 14 7C.X.270.XX.21 = 1 2.5 Bleed Failed !
! ! 15 7C.X.270.XX.23 = 1 Autothrust TLA Limited !
! ! 16 SPARE !
! ! 17 SPARE !
! ! 18 7C.X.270.XX.27 = 1 SVA Failed !
! ! 19 7C.X.271.XX.16 = 1 FDV Off !
! ! 20 SPARE !
! ! 21 7C.X.271.XX.19 = 1 7th Bleed #1 Solenoid !
! ! Closed !
! ! 22 7C.X.271.XX.20 = 1 7th Bleed #2 Solenoid !
! ! Closed !
! ! 23 7C.X.271.XX.21 = 1 10th Bleed Solenoid !
! ! Closed !
! ! 24 7C.X.271.XX.28 = 1 P2/T2 Probe Heater Relay !
! ! On !
! ! 25 7C.X.351.XX.14 = 1 Left ADC Link Failed !
! ! 26 7C.X.351.XX.15 = 1 Right ADC Link Failed !
! ! 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 ! 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.22 = 1 Bleed Config. K1 Selected !
! ! 12 7C.X.272.XX.23 = 1 Bleed Config. K2 Selected !
! ! 13 7C.X.272.XX.24 = 1 Bleed Config. K3 Selected !
! ! 14 7C.X.272.XX.25 = 1 Bleed Config. K4 Selected !
! ! 15 7C.X.272.XX.26 = 1 Bleed Config. K5 Selected !
! ! 16 7C.X.272.XX.27 = 1 Bleed Config. K6 Selected !
! ! 17 7C.X.272.XX.28 = 1 Bleed Config. Data Failed !
! ! 18 SPARE !
! ! 19 7C.X.272.XX.19 = 1 Bump Mode is selected !
! ! 20 7C.X.272.XX.20 = 1 Bump Mode is selected !
! ! 21 7C.X.272.XX.21 = 1 Bump Mode is selected !
! ! 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 !
!--------------!------------------------------------------------------!
! EVM ! Engine Vibration Status Word !
! XXXXX ! EVM 3D.1.035.01 Engine 1 !
! ! 3D.1.035.10 Engine 2 !
! ! 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) !
! ! 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) !
! ! 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 26.1.316.01 Engine 1 !
! ! 26.2.316.01# !
! ! 26.1.316.10 Engine 2 !
! ! 26.2.316.10# !
!--------------!------------------------------------------------------!
! 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 conditions !
! ! suffix a denotes taxi out conditions !
! ! 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*(1+(K1*OITa)+(K2*N2a)+(K3*P3a)) !
! ! OIKb=OIQb*(1+(K1*OITb)+(K2*N2b)+(K3*P3b)) !
! ! OIQ= measured oil quantity 29.1.073.11 Engine 1!
! ! 29.2.073.11# !
! ! 29.1.073.00 Engine 2!
! ! 29.2.073.00## !
! ! OIT= oil temperature 26.1.316.01 Engine 1!
! ! 26.2.316.01 !
! ! 26.1.316.10 Engine 2!
! ! 26.2.316.10# !
! ! N2= core speed 7C.1.344.01 Engine 1!
! ! 7C.2.344.10 Engine 2!
! ! P3= burner pressure 7C.1.264.01 Engine 1!
! ! 7C.2.264.10 Engine 2!
! ! UTC= universal time 17.1.150.00 !
! ! coordinated (BNR) !
! ! (attention to the date) !
! ! K1, K2, K3 = factors are as follows: !
! ! K1= -8.5*pow(10,-4); K2= pow(10,-6); K3= pow(10,-6)!
!--------------!------------------------------------------------------!
! VB1 ! N1 Vibration !
! 999 ! 0 to 10.0 (If the value is 10.0 then 99 is printed)!
! ! EVM 3D.1.135.01 Engine 1 !
! ! 3D.1.135.10 Engine 2 !
!--------------!------------------------------------------------------!
! VB2 ! N2 Vibration !
! 999 ! 0 to 10.0 (If the value is 10.0 then 99 is printed)!
! ! EVM 3D.1.136.01 Engine 1 !
! ! 3D.1.136.10 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 !
+---------------------------------------------------------------------+

(2) Parameter Logic
+---------------------------------------------------------------------+
! Param. ! Print Value (Standard Progr.) !
!--------------!------------------------------------------------------!
! ESN ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! EHRS ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! ECYC ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! AP ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! QE ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! EPR ! Arithmetic average for F01*20 sec !
!--------------!------------------------------------------------------!
! EPRC ! Arithmetic average for F01*20 sec !
!--------------!------------------------------------------------------!
! EGT ! Arithmetic average for F01*20 sec !
!--------------!------------------------------------------------------!
! N1 ! Arithmetic average for F01*20 sec !
!--------------!------------------------------------------------------!
! N2 ! Arithmetic average for F01*20 sec !
!--------------!------------------------------------------------------!
! FF ! Arithmetic average for F01*20 sec !
!--------------!------------------------------------------------------!
! P125 ! 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 !
!--------------!------------------------------------------------------!
! P49 ! Arithmetic average for F01*20 sec !
!--------------!------------------------------------------------------!
! SVA ! Arithmetic average for F01*20 sec !
!--------------!------------------------------------------------------!
! BAF ! Arithmetic average for F01*20 sec !
!--------------!------------------------------------------------------!
! ACC ! Arithmetic average for F01*20 sec !
!--------------!------------------------------------------------------!
! LP ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! GLE ! Arithmetic average for F01*20 sec !
!--------------!------------------------------------------------------!
! PD ! Arithmetic average for F01*20 sec !
!--------------!------------------------------------------------------!
! TN ! Arithmetic average for F01*20 sec !
!--------------!------------------------------------------------------!
! P2 ! Arithmetic average for F01*20 sec !
!--------------!------------------------------------------------------!
! T2 ! Arithmetic average for F01*20 sec !
!--------------!------------------------------------------------------!
! ECW1 ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! ECW2 ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! EVM ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! OIP ! Arithmetic average for F01*20 sec !
!--------------!------------------------------------------------------!
! OIT ! Arithmetic average for F01*20 sec !
!--------------!------------------------------------------------------!
! OIQH ! Value from the last calculation !
!--------------!------------------------------------------------------!
! VB1 ! Arithmetic average for F01*20 sec !
!--------------!------------------------------------------------------!
! VB2 ! Arithmetic average for F01*20 sec !
!--------------!------------------------------------------------------!
! PHA ! Arithmetic average for F01*20 sec !
+---------------------------------------------------------------------+

(3) Engine-Cruise-Report Logic <01> (Engine Type IAE)
+--------------------------------------------------------------------------+
!Code!Item ! ! Progr. !Standard !
! No.!No. ! Description of Function Item !----------!Value or !
! ! ! !GSE !MCDU !Table TXY!
!----!------!-----------------------------------------!----!-----!---------!
! !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 ! C ! see !
! ! ! ! ! ! separate!
! ! ! ! ! ! list !
! !E ! Transfer to ACARS MU ! C ! C ! see !
! ! ! ! ! ! separate!
! ! ! ! ! ! list !
! !F ! Increment of the report counter if the ! C ! C ! 1 !
! ! ! report was triggered by a logic number ! ! ! !
! ! ! > 1000; 1=yes, 0=no (standard ! ! ! !
! ! ! programming = 1) ! ! ! !
! !G ! Average intervals in seconds ! C ! ! 20 !
! !H ! Overall Average of 'F01' averages ! C ! C ! 5 !
! !I.1 ! 'Y01.5' for OIQ measurements (sec.) ! A ! A ! 5 !
! !I.2 ! 'Y01.4' for OIQ measurements (sec.) ! A ! A ! 10 !
!----!------!-----------------------------------------!----!-----!---------!
!1000!1 ! Manual selection through MCDU ! ! ! !
!----!------!-----------------------------------------!----!-----!---------!
!2000!2 ! Flight phase dependent manual ! ! ! !
! ! ! selection through remote print ! ! ! !
! ! ! button if programmed. ! ! ! !
! !2.1 ! Flight Phase (no standard programming) ! C ! C ! not !
! ! ! ! ! ! assign. !
!----!------!-----------------------------------------!----!-----!---------!
!3000!3 ! Programmable Start Logic ! ! ! !
! !3.1 ! Logic algorithm ! C ! ! !
! !3.2 ! Logic criteria values ! C ! ! not !
! ! ! ! ! ! progr. !
!----!------!-----------------------------------------!----!-----!---------!
!4000! ! The DMU generates the Engine Cruise ! ! ! !
! ! ! Report based on 'Flight Hours' or ! ! ! !
! ! ! Flight Legs' programmable through GSE. ! ! ! !
! ! ! ! ! ! !
! ! ! Logic based on Flight Hours: ! ! ! !
! ! ! ! ! ! !
! ! ! If, after starting each new time period ! ! ! !
! ! ! of 'Y01.1' flight hours and during the ! ! ! !
! ! ! entry into flight phase 6 after 'Y01.2' ! ! ! !
! ! ! minutes, the stable frame criteria ! ! ! !
! ! ! are not met then an Engine Cruise ! ! ! !
! ! ! Report is generated and stored in the ! ! ! !
! ! ! report buffer. The report gives the ! ! ! !
! ! ! subsequent message in the last line: ! ! ! !
! ! ! 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 ! ! ! !
! ! ! gives the subsequent message in the last! ! ! !
! ! ! line: ! ! ! !
! ! ! NO STABLE FRAME CONDITION ! ! ! !
! ! ! ! ! ! !
! ! ! In this case the average interval is ! ! ! !
! ! ! fixed to 20 seconds. ! ! ! !
!----!------!-----------------------------------------!----!-----!---------!
! !4 ! The default programming is 'Flight ! C ! C ! Hours !
! ! ! Hours' ! ! ! !
! ! ! ! ! ! !
! !4.1 ! 'Y01.1' flight hours ! C ! C ! T23 !
! !4.2 ! 'Y01.2' minutes after cruise ! C ! C ! T23 !
! !4.3 ! 'Y01.3' flight legs ! C ! C ! T23 !
!----!------!-----------------------------------------!----!-----!---------!
!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 '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 which ! ! ! !
! ! ! is stored according to logic 4000 is ! ! ! !
! ! ! then deleted. ! ! ! !
! ! ! ! ! ! !
! ! ! Logic based on Flight Legs: ! ! ! !
! ! ! ! ! ! !
! ! ! Every 'Y01.3' flight legs the DMU ! ! ! !
! ! ! searches in the flight phase 6 for a ! ! ! !
! ! ! report generation with stable frame ! ! ! !
! ! ! criteria where the best aircraft quality! ! ! !
! ! ! number QE is calculated. The report with! ! ! !
! ! ! the best quality number is stored in the! ! ! !
! ! ! report buffer and the report which is ! ! ! !
! ! ! stored according to logic 4000 is then ! ! ! !
! ! ! deleted. ! ! ! !
!----!------!-----------------------------------------!----!-----!---------!
! !5 ! The default programming is 'Flight ! C ! C ! Hours !
! ! ! hours'. ! ! ! !
!----!------!-----------------------------------------!----!-----!---------!
! ! ! Parameter for stable frame criteria ! ! ! !
! !5.1 ! 'P01' stable period ! C ! C ! T23 !
! ! ! (5 subperiodes = 100 sec.) ! ! ! !
! !5.2 ! 78% < ACC < 100% ! C ! C ! T23 !
! ! ! ACC = 7C.1.330.01 Engine 1 ! ! ! !
! ! ! 7C.2.330.10 Engine 2 ! ! ! !
! ! ! ! ! ! !
! ! ! Stable frame conditions: ! ! ! !
! ! ! During 'P01' seconds the following ! ! ! !
! ! ! parameters are stable as given below: ! ! ! !
! ! ! ! ! ! !
! !5.3 ! IALT 04.1.361.XX ft ! C ! C ! T23 !
! ! ! 04.2.361.XX ! ! ! !
! ! ! ! ! ! !
! !5.3.1 ! Wa of IALT ! C ! C ! T23 !
! ! ! ! ! ! !
! !5.4 ! GS 04.1.312.01 kts ! C ! C ! T23 !
! ! ! 04.2.312.10 ! ! ! !
! ! ! ! ! ! !
! !5.4.1 ! Wa of GS ! C ! C ! T23 !
! ! ! ! ! ! !
! ! ! ! ! ! !
! !5.5 ! ROLL 04.1.325.01 degr. ! C ! C ! T23 !
! ! ! ANGLE 04.2.325.10 ! ! ! !
! ! ! ! ! ! !
! !5.5.1 ! Wa of ROLL ! C ! C ! T23 !
! ! ! ! ! ! !
! !5.6 ! TAT 06.1.211.01 degrees C ! C ! C ! T23 !
! ! ! 06.2.211.10 ! ! ! !
! ! ! ! ! ! !
! !5.6.1 ! Wa of TAT ! C ! C ! T23 !
! ! ! ! ! ! !
! !5.7 ! N2 7C.1.344.01 Eng.1 % ! C ! C ! T23 !
! ! ! 7C.2.344.10 Eng.2 ! ! ! !
! ! ! ! ! ! !
! !5.7.1 ! Wa of N2 ! C ! C ! T23 !
! ! ! ! ! ! !
! !5.8 ! EGT 7C.1.345.01 Eng.1 C ! C ! C ! T23 !
! ! ! 7C.2.345.10 Eng.2 ! ! ! !
! ! ! ! ! ! !
! !5.8.1 ! Wa of EGT ! C ! C ! T23 !
! ! ! ! ! ! !
! !5.9 ! VACC 04.1.364.01 g ! C ! C ! T23 !
! ! ! 04.2.364.10 ! ! ! !
! ! ! ! ! ! !
! !5.9.1 ! Wa of VACC ! C ! C ! T23 !
! ! ! ! ! ! !
!----!------!-----------------------------------------!----!-----!---------!
! !5.10 ! MN 06.1.205.01 Mach ! C ! C ! T23 !
! ! ! 06.2.205.10 ! ! ! !
! ! ! ! ! ! !
! !5.10.1! Wa of MN ! C ! C ! T23 !
! ! ! ! ! ! !
! !5.11 ! N1 7C.1.346.01 Eng.1 % ! C ! C ! T23 !
! ! ! 7C.2.346.10 Eng.2 ! ! ! !
! ! ! ! ! ! !
! !5.11.1! Wa of N1 ! C ! C ! T23 !
! ! ! ! ! ! !
! !5.12 ! PT2 7C.1.131.01 Eng.1 psia ! C ! C ! T23 !
! ! ! 7C.2.131.10 Eng.2 ! ! ! !
! ! ! ! ! ! !
! !5.12.1! Wa of PT2 ! C ! C ! T23 !
! ! ! ! ! ! !
! !5.13 ! FF 7C.1.244.01 Eng.1 kg/h ! C ! ! T23 !
! ! ! 7C.2.244.10 Eng.2 ! ! ! !
! !5.13.1! Wa of FF ! C ! C ! T23 !
! ! ! ! ! ! !
! !5.14 ! EPR 7C.1.340.01 Eng.1 ! C ! C ! T23 !
! ! ! 7C.2.340.10 Eng.2 ! ! ! !
! ! ! ! ! ! !
! !5.14.1! Wa of EPR ! C ! C ! T23 !
! ! ! ! ! ! !
!----!------!-----------------------------------------!----!-----!---------!
!6001!6 ! Independently of the other logic a ! ! ! !
!6002! ! stable search logic for an Engine ! ! ! !
!6003! ! Cruise Rep.<01> is started as long as ! ! ! !
!. ! ! 'X01' is not zero (once per leg only). ! ! ! !
!. ! ! Each time an Engine Cruise Report <01> ! ! ! !
!. ! ! is generated by this logic, the number ! ! ! !
!. ! ! 'X01' decreases until zero. ! ! ! !
!. ! ! ! ! ! !
!600X! ! The number 'X01' is programmable. ! ! ! !
! ! ! ! ! ! !
! ! ! If an engine serial number is changed, ! ! ! !
! ! ! 'X01' is automatically set to 5. ! ! ! !
! ! ! ! ! ! !
! !6.1 ! Logic algorithm ! ! ! !
! ! ! ! ! ! !
! !6.2 ! Number 'X01' for consecutive reports (up! C ! C ! T23 !
! ! ! to 9). ! ! ! !
! ! ! ! ! ! !
! !6.3 ! Number 5 in case of ESN change ! C ! C ! 5 !
!----!------!-----------------------------------------!----!-----!---------!
!7000!7 ! In case the ENGINE DIVERGENCE REPORT ! ! ! !
! ! ! <09> was generated, the stable frame ! ! ! !
! ! ! search logic for the ENGINE CRUISE ! ! ! !
! ! ! REPORT <01> is started immediately ! ! ! !
! ! ! independently of the best stable frame ! ! ! !
! ! ! logic and the report is generated with ! ! ! !
! ! ! code 7000. ! ! ! !
! ! ! ! ! ! !
!----!------!-----------------------------------------!----!-----!---------!
!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 !
+--------------------------------------------------------------------------+

B. AIDS Reports Print Rules - Default Values for Report <01>
+-------------------------------------------------------------------------+
!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 !
+-------------------------------------------------------------------------+

C. Cruise Performance Report <02>
F Cruise Performance Report <02> (Engine Type IAE) ** 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.
NOTE: For the standard header definition of the report refer to (Ref. AMM D/O 31-36-00-00).
NOTE: If the ESN printed out in the report is in the range between 13191 and 15000, then add 5000 to this value to get the actual ESN.
(1) Cruise-Performance-Report Data-Field-Description <02> (Engine Type IAE)
NOTE: Only the parts of the ENGINE 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 ! (-60.0 to 99.9 deg C) !
! ! NOTE: Negative values are shown with '-' on the !
! ! first position. Otherwise the first position !
! ! contains a '0'. !
! ! ADIRU 06.1.211.01 !
! ! 06.2.211.10 !
!--------------!------------------------------------------------------!
! ALT ! Standard Altitude (1013mbar) !
! X9999 ! (-2000 to 50000 ft) !
! ! Negative values are indicated by '-' on the first !
! ! position. Otherwise the first position is used for !
! ! the value. !
! ! ADIRU 06.1.203.01 !
! ! 06.2.203.10# !
!--------------!------------------------------------------------------!
! CAS ! Computed Air Speed !
! 999 ! (30 to 450 kts) !
! ! ADIRU 06.1.206.01 !
! ! 06.2.206.10# !
!--------------!------------------------------------------------------!
! MN ! Mach Number !
! 999 ! (0.100 to 0.999) !
! ! ADIRU 06.1.205.01 !
! ! 06.2.205.10# !
!--------------!------------------------------------------------------!
! GW ! Gross Weight !
! 9999 ! (0 to 9000*10 kg) (0 to 1980*100 lbs) !
! ! FMGC 02.1.075.00 !
! ! 02.2.075.00# !
!--------------!------------------------------------------------------!
! CG ! Center of Gravity !
! 999 ! (0 to 35.0 %MAC) !
! ! FMGC 02.1.077.00 !
! ! 02.2.077.00# !
!--------------!------------------------------------------------------!
! QA ! Aircraft 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. !
! ! N VARa(i) !
! ! QA=SIGMA(Wa(i)*---------------) !
! ! i=A 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 ! (0 to 99999 kg) !
! ! FQIC param. 5A.2.257.10 Left Inner Cell !
! ! param. 5A.2.261.19 Right Inner Cell !
! ! Remark: Report line 'X1' shows Left Inner Cell !
! ! Fuel Quantity. !
! ! Report line 'X2' shows Right Inner Cell !
! ! Fuel Quantity. !
!--------------!------------------------------------------------------!
! ELEV ! Elevator Position !
! X999 ! (-30 to 15 deg) !
! ! FCDC param. 6C.1.314.01 Left Elevator Position !
! ! param. 6C.2.314.10 !
! ! param. 6C.1.334.01 Right Elevator Position !
! ! param. 6C.2.334.10 !
! ! Negative values are shown with '-' on the first !
! ! position. Otherwise the first position contains a !
! ! '0'. !
! ! Remark: Report line 'X1' shows the Left Elevator !
! ! Position. !
! ! Report line 'X2' shows the Right Elevator !
! ! Position. !
!--------------!------------------------------------------------------!
! AOA ! Corrected Angle of Attack !
! X999 ! (-30.0 to 85.0 deg) !
! ! ADIRU param. 06.1.241.01 AOA System 1 !
! ! param. 06.2.241.10 AOA System 2 !
! ! Negative values are shown with '-' on the first !
! ! position. Otherwise the first position contains a !
! ! '0'. !
! ! Remark: Report line 'X1' shows AOA System 1. !
! ! Report line 'X2' shows AOA System 2. !
!--------------!------------------------------------------------------!
! SLP ! Side Slip Angle !
! X999 ! (-32.0 to 32.0 deg) !
! ! FAC param. 0A.1.226.00 SLP System 1 !
! ! param. 0A.2.226.00 SLP System 2 !
! ! Negative values are shown with '-' on the first !
! ! position. Otherwise the first position contains a !
! ! '0'. !
! ! Remark: Report line 'X1' shows SLP System 1. !
! ! Report line 'X2' shows SLP System 2. !
!--------------!------------------------------------------------------!
! CFPG ! Calculated Flight Path Acceleration !
! X9999 ! DMU (-0.9999 to 4.0000 g) !
! ! Negative values are shown with '-' on the first !
! ! position. Otherwise the first is used for the !
! ! value. !
! ! 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 !
! ! FPG=----------------------------------------------*!
! ! 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 ! DMU (-999 to 999 ft/min) !
! ! Negative values are shown with '-' on the first !
! ! position. Otherwise the first position contains a !
! ! '0'. !
! ! 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 ! (-30.0 to 30.0 deg) !
! ! SDAC param. 29.1.312.00 !
! ! param. 29.2.312.00# !
! ! Negative values are shown with '-' on the first !
! ! position. Otherwise the first position contains a !
! ! '0'. !
!--------------!------------------------------------------------------!
! RUDT ! Rudder Trim Position !
! X999 ! (-25.0 to 25.0 deg) !
! ! FAC param. 0A.1.313.00 !
! ! param. 0A.2.313.00# !
! ! Negative values are shown with '-' on the first !
! ! position. Otherwise the first position contains a !
! ! '0'. !
!--------------!------------------------------------------------------!
! AILL ! Left Aileron Position !
! X999 ! (-25.0 to 25.0 deg) !
! ! FCDC param. 6C.1.310.01 !
! ! param. 6C.2.310.10# !
! ! Negative values are shown with '-' on the first !
! ! position. Otherwise the first position contains a !
! ! '0'. !
!--------------!------------------------------------------------------!
! AILR ! Right Aileron Position !
! X999 ! (-25.0 to 25.0 deg) !
! ! FCDC param. 6C.1.330.01 !
! ! param. 6C.2.330.10# !
! ! Negative values are shown with '-' on the first !
! ! position. Otherwise the first position contains a !
! ! '0'. !
!--------------!------------------------------------------------------!
! STAB ! Stabilizer Position #1 !
! X999 ! (-13.5 to 4.0 deg) !
! ! FCDC param. 6C.1.315.01 !
! ! param. 6C.2.315.10# !
! ! Negative values are shown with '-' on the first !
! ! position. Otherwise the first position contains a !
! ! '0'. !
!--------------!------------------------------------------------------!
! ROLL ! Roll Angle !
! X999 ! (-90.0 to 90.0 deg) !
! ! ADIRU param. 04.1.325.01 !
! ! param. 04.2.325.10# !
! ! Negative values are shown with '-' on the first !
! ! position. Otherwise the first position contains a !
! ! '0'. !
!--------------!------------------------------------------------------!
! YAW ! Body Axis Yaw Rate !
! X999 ! (-45.0 to 45.0 deg/sec) !
! ! ADIRU param. 04.1.330.01 !
! ! param. 04.2.330.10# !
! ! Negative values are shown with '-' on the first !
! ! position. Otherwise the first position contains a !
! ! '0'. !
!--------------!------------------------------------------------------!
! RSP2 ! Roll Spoiler 2 Position !
! X999 ! (-45.0 to 0 deg ) !
! ! param. 6C.1.362.01 Left Spoiler !
! ! param. 6C.2.362.10# !
! ! param. 6C.1.372.01 Right Spoiler !
! ! param. 6C.2.372.10# !
! ! Negative values are shown with '-' on the first !
! ! position. Otherwise the first position contains a !
! ! '0'. !
! ! Remark: Report line X4 shows RSP2 left spoiler. !
! ! Report line X5 shows RSP2 right spoiler. !
!--------------!------------------------------------------------------!
! RSP3 ! Roll Spoiler 3 Position !
! X999 ! (-45.0 to 0 deg ) !
! ! param. 6C.1.363.01 Left Spoiler !
! ! param. 6C.2.363.10# !
! ! param. 6C.1.373.01 Right Spoiler !
! ! param. 6C.2.373.10# !
! ! Negative values are shown with '-' on the first !
! ! position. Otherwise the first position contains a !
! ! '0'. !
! ! Remark: Report line X4 shows RSP3 left spoiler. !
! ! Report line X5 shows RSP3 right spoiler. !
!--------------!------------------------------------------------------!
! RSP4 ! Roll Spoiler 4 Position !
! X999 ! (-45.0 to 0 deg ) !
! ! param. 6C.1.364.01 Left Spoiler !
! ! param. 6C.2.364.10# !
! ! param. 6C.1.374.01 Right Spoiler !
! ! param. 6C.2.374.10# !
! ! Negative values are shown with '-' on the first !
! ! position. Otherwise the first position contains a !
! ! '0'. !
! ! Remark: Report line X4 shows RSP4 left spoiler. !
! ! Report line X5 shows RSP4 right spoiler. !
!--------------!------------------------------------------------------!
! RSP5 ! Roll Spoiler 5 Position !
! X999 ! (-45.0 to 0 deg ) !
! ! param. 6C.1.365.01 Left Spoiler !
! ! param. 6C.2.365.10# !
! ! param. 6C.1.375.01 Right Spoiler !
! ! param. 6C.2.375.10# !
! ! Negative values are shown with '-' on the first !
! ! position. Otherwise the first position contains a !
! ! '0'. !
! ! Remark: Report line X4 shows RSP5 left spoiler. !
! ! Report line X5 shows RSP5 right spoiler. !
!--------------!------------------------------------------------------!
! FLAP ! Flap Actual Position !
! X999 ! (-9.0 to 40.0 deg) !
! ! SFFC 1B.1.137.01 FLAP System 1 !
! ! 1B.2.137.10 FLAP System 2 !
! ! Negative values are shown with '-' on the first !
! ! position. Otherwise the first position contains a !
! ! '0'. !
! ! Remark: Report line X4 shows FLAP System 1. !
! ! Report line X5 shows FLAP System 2. !
!--------------!------------------------------------------------------!
! SLAT ! Slat Actual Position !
! X999 ! (0.0 to 27.0 deg) !
! ! SFFC 1B.1.127.01 System 1 !
! ! SFFC 1B.2.127.10 System 2 !
! ! Negative values are shown with '-' on the first !
! ! position. Otherwise the first position contains a !
! ! '0'. !
! ! Remark: Report line X4 shows SLAT System 1. !
! ! Report line X5 shows SLAT System 2. !
!--------------!------------------------------------------------------!
! THDG ! True Heading (BCD) !
! X9999 ! (0 to 359.9 deg) !
! ! ADIRU 04.1.044.01 THDG System 1 !
! ! 04.2.044.10 THDG System 2 !
! ! Remark: Report line X6 shows THDG System 1. !
! ! Report line X7 shows THDG System 2. !
!--------------!------------------------------------------------------!
! LONP ! Longitude Position !
! X9999 ! (East 179.9 deg to West 179.9 deg) !
! ! ADIRU 04.1.311.XX LONP System 1 !
! ! 04.2.311.XX LONP System 2 !
! ! The first position shows east or west. 'E' for an !
! ! East position and 'W' for a West position. !
! ! Remark: Report line X6 shows LONP System 1. !
! ! Report line X7 shoes LONP System 2. !
!--------------!------------------------------------------------------!
! LATP ! Latitude Position !
! X9999 ! (North 89.9 to South 89.9 deg) !
! ! ADIRU 04.1.310.XX System 1 !
! ! 04.2.310.XX System 2 !
! ! The first position shows north or south. 'N' for a !
! ! North position and 'S' for a South position !
! ! Remark: Report line X6 shows LATP System 1. !
! ! Report line X7 shows LATP System 2. !
!--------------!------------------------------------------------------!
! WS ! Wind Speed !
! 999 ! (0 to 100 kts) !
! ! 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 ! (0 to 359 deg) !
! ! 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 ! Fuel Temperature !
! X999 ! (-60.0 to 170.0 C) !
! ! FQIC 5A.2.177.10 Fuel Temp. Left Wing Tank !
! ! 5A.2.201.10 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 ! (0 to 0.999 kg/l) !
! ! 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) are transmitted one after !
! ! another on label 272. The adequate tank !
! ! identification is as follows: !
! ! Report Line X6 shows the Fuel Density value!
! ! of the Left Wing Tank. !
! ! (Bit 29 28 27 = 0 0 1). !
! ! Report Line X7 shows the Fuel Density value!
! ! of the Right Wing Tank. !
! ! (Bit 29 28 27 = 0 1 1) !
! ! The center Tank (Bit 29 28 27 = 1 1 0) !
! ! is not taken into account. !
! ! The update rate of label 272 will be 1 !
! ! second. Due to this fact the Fuel Density !
! ! value of the dedicated tank is available !
! ! every 3 seconds. !
+---------------------------------------------------------------------+

(2) 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 !
!--------------!------------------------------------------------------!
! ECYC ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! AP ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! QA ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! QE ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! EPR ! Arithmetic average for F02 * 20 sec !
!--------------!------------------------------------------------------!
! EPRC ! Arithmetic average for F02 * 20 sec !
!--------------!------------------------------------------------------!
! EGT ! Arithmetic average for F02 * 20 sec !
!--------------!------------------------------------------------------!
! N1 ! Arithmetic average for F02 * 20 sec !
!--------------!------------------------------------------------------!
! N2 ! Arithmetic average for F02 * 20 sec !
!--------------!------------------------------------------------------!
! FF ! Arithmetic average for F02 * 20 sec !
!--------------!------------------------------------------------------!
! P125 ! 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 !
!--------------!------------------------------------------------------!
! P49 ! Arithmetic average for F02 * 20 sec !
!--------------!------------------------------------------------------!
! SVA ! Arithmetic average for F02 * 20 sec !
!--------------!------------------------------------------------------!
! BAF ! Arithmetic average for F02 * 20 sec !
!--------------!------------------------------------------------------!
! ACC ! Arithmetic average for F02 * 20 sec !
!--------------!------------------------------------------------------!
! LP ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! GLE ! Arithmetic average for F02 * 20 sec !
!--------------!------------------------------------------------------!
! PD ! Arithmetic average for F02 * 20 sec !
!--------------!------------------------------------------------------!
! TN ! Arithmetic average for F02 * 20 sec !
!--------------!------------------------------------------------------!
! P2 ! Arithmetic average for F02 * 20 sec !
!--------------!------------------------------------------------------!
! T2 ! Arithmetic average for F02 * 20 sec !
!--------------!------------------------------------------------------!
! ECW1 ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! ECW2 ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! EVM ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! OIP ! Arithmetic average for F02 * 20 sec !
!--------------!------------------------------------------------------!
! OIT ! Arithmetic average for F02 * 20 sec !
!--------------!------------------------------------------------------!
! OIQH ! Value from the last calculation !
!--------------!------------------------------------------------------!
! VB1 ! Arithmetic average for F02 * 20 sec !
!--------------!------------------------------------------------------!
! VB2 ! Arithmetic average for F02 * 20 sec !
!--------------!------------------------------------------------------!
! PHA ! Arithmetic average for F02 * 20 sec !
!--------------!------------------------------------------------------!
! WFQ ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! ELEV ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! AOA ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! SLP ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! CFPG ! Last DMU calculated !
!--------------!------------------------------------------------------!
! CIVV ! Last DMU calculated !
!--------------!------------------------------------------------------!
! 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 trigger !
!--------------!------------------------------------------------------!
! LONP ! Value at moment trigger !
!--------------!------------------------------------------------------!
! LATP ! Value at moment 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 !
!--------------!------------------------------------------------------!

(3) Cruise Performance Report Logic (Engine Type IAE)
+--------------------------------------------------------------------------+
!Code!Item ! !Progr. !Standard !
! No.!No. ! Description of Function Item !----------!Value or !
! ! ! !GSE !MCDU !Table !
!----!------!-----------------------------------------!----!-----!---------!
! !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 ! C ! see !
! ! ! ! ! ! separate!
! ! ! ! ! ! list !
! !E ! Transfer to ACARS MU ! C ! C ! see !
! ! ! ! ! ! separate!
! ! ! ! ! ! list !
! !F ! Increment of the report counter if the ! C ! 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 ! A ! 5 !
! !I ! OIQ values taken from 'taxi in' and ! ! ! !
! ! ! 'taxi out' for OIQH calculation. The ! ! ! !
! ! ! same programming as for Report <01> ! ! ! !
! ! ! applies. ! ! ! !
!----!------!-----------------------------------------!----!-----!---------!
!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 ! C ! not !
! ! ! ! ! ! assigned!
!----!------!-----------------------------------------!----!-----!---------!
!3000!3 ! Programmable Start Logic ! ! ! !
! !3.1 ! Logic algorithm ! C ! ! !
! !3.2 ! Trigger condition ! C ! ! not !
! ! ! ! ! ! progr. !
!----!------!-----------------------------------------!----!-----!---------!
!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 where the best ! ! ! !
! ! ! aircraft quality number QA is calculated! ! ! !
! ! ! 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 ! C ! C ! Hours !
! ! ! Hours'. ! ! ! !
! ! ! ! ! ! !
! !5.1 ! Logic algorithm ! ! ! !
! ! ! ! ! ! !
! !5.2 ! 'Y02.1' flight hours ! C ! C ! T23 !
! ! ! ! ! ! !
! !5.3 ! 'Y02.2' flight legs ! C ! C ! T23 !
! ! ! ! ! ! !
! !5.4 ! 'PO2' stable periods ! A ! ! T23 !
! ! ! (5 subperiods = 100 sec) ! ! ! !
! ! ! Stable frame basic condition in order ! ! ! !
! ! ! avoid report triggering in flight phases! ! ! !
! ! ! where parameters are of no use. ! ! ! !
! ! ! ! ! ! !
! !5.5 ! 78% < ACC < 100% ! C ! C ! T23 !
! ! ! ACC 7C.1.330.01 Eng.1 ! ! ! !
! ! ! 7C.2.330.10 Eng.2 ! ! ! !
! ! ! ! ! ! !
! ! ! Stable frame conditions: ! ! ! !
! ! ! During 'P02' seconds the following ! ! ! !
! ! ! parameters are stable as defined below: ! ! ! !
! ! ! ! ! ! !
! ! ! The stable frame variation is customer ! ! ! !
! ! ! programmable, but only in the range ! ! ! !
! ! ! defined in the column for standard ! ! ! !
! ! ! values. ! ! ! !
! ! ! ! ! ! !
! !5.6 ! IALT 04.1.361.XX ft ! A ! A ! T23 !
! ! ! 04.2.361.XX ! ! ! T23 !
! ! ! ! ! ! !
! !5.6.1 ! Wa of IALT ! C ! C ! T23 !
! ! ! ! ! ! !
! ! ! ! ! ! !
! !5.7 ! GS 04.1.312.01 kts ! A ! A ! T23 !
! ! ! 04.2.312.10 ! ! ! !
! ! ! ! ! ! !
! !5.7.1 ! Wa of GS ! C ! C ! T23 !
! ! ! ! ! ! !
! ! ! ! ! ! !
! !5.8 ! ROLL ANGLE 04.1.325.01 degr. ! A ! A ! T23 !
! ! ! 04.2.325.10 ! ! ! !
! ! ! ! ! ! !
! !5.8.1 ! Wa of ROLL ANGLE ! C ! C ! T23 !
! ! ! ! ! ! !
! ! ! ! ! ! !
! !5.9 ! TAT 06.1.211.01 degrees C ! A ! A ! T23 !
! ! ! 06.2.211.10 ! ! ! !
! ! ! ! ! ! !
! !5.9.1 ! Wa of TAT ! C ! C ! T23 !
! ! ! ! ! ! !
! ! ! ! ! ! !
! !5.10 ! N2 7C.1.344.01 Eng.1 % ! A ! A ! T23 !
! ! ! 7C.2.344.10 Eng.2 ! ! ! !
! ! ! ! ! ! !
! !5.10.1! Wa of N2 ! C ! C ! T23 !
! ! ! ! ! ! !
! ! ! ! ! ! !
! !5.11 ! EGT 7C.1.345.01 Eng.1 C ! A ! A ! T23 !
! ! ! 7C.2.345.10 Eng 2 ! ! ! !
! ! ! ! ! ! !
! !5.11.1! Wa of EGT ! C ! C ! T23 !
! ! ! ! ! ! !
! ! ! ! ! ! !
! !5.12 ! VACC 04.1.364.01 g ! A ! A ! T23 !
! ! ! 04.2.364.10 ! ! ! !
! ! ! ! ! ! !
! !5.12.1! Wa of VACC ! C ! C ! T23 !
! ! ! ! ! ! !
! ! ! ! ! ! !
! !5.13 ! MN 06.1.205.01 Mach ! A ! A ! T23 !
! ! ! 06.2.205.10 ! ! ! !
! ! ! ! ! ! !
! !5.13.1! Wa of MN ! C ! C ! T23 !
! ! ! ! ! ! !
! ! ! ! ! ! !
! !5.14 ! N1 7C.1.346.01 Eng.1 % ! A ! A ! T23 !
! ! ! 7C.2.346.10 Eng.2 ! ! ! !
! ! ! ! ! ! !
! !5.14.1! Wa of N1 ! C ! C ! T23 !
! ! ! ! ! ! !
! ! ! ! ! ! !
! !5.15 ! PT2 7C.1.131.01 Eng.1 psia ! A ! A ! T23 !
! ! ! 7C.2.131.10 Eng.2 ! ! ! !
! ! ! ! ! ! !
! !5.15.1! Wa of PT2 ! C ! C ! T23 !
! ! ! ! ! ! !
! !5.16 ! FF 7C.1.244.01 Eng.1 kg/h ! A ! A ! T23 !
! ! ! 7C.2.244.10 Eng.2 ! ! ! !
! ! ! ! ! ! !
! !5.16.1! Wa of FF ! C ! C ! T23 !
! ! ! ! ! ! !
! ! ! ! ! ! !
! !5.17 ! EPR 7C.1.340.01 Eng.1 ! A ! A ! T23 !
! ! ! 7C.2.340.10 Eng.2 ! ! ! !
! ! ! ! ! ! !
! !5.17.1! Wa of EPR ! C ! C ! T23 !
! ! ! ! ! ! !
!----!------!-----------------------------------------!----!-----!---------!
!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 IMI 'G02' ! ! ! !
! ! ! The report <02> 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 !
+--------------------------------------------------------------------------+

D. AIDS Reports Print Rules - Default Values for Report <02>
+-------------------------------------------------------------------------+
!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 !
+-------------------------------------------------------------------------+

E. Engine Take-Off Report <04>
F Take Off Delta EPR Summary (Engine Type IAE) ** ON A/C NOT FOR ALL
F Engine Take-Off Report <04> (Engine Type IAE) ** 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.
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 IAE)
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.
NOTE: The Number 4 Bearing Engine Pressure (PSB) is missing in Engine Take-Off Report <04> on aircrafts fitted with FWC H2F7 standard (PN 350E053021212).
NOTE: If the ESN printed out in the report is in the range between 13191 and 15000, then add 5000 to this value to get the actual ESN.
+---------------------------------------------------------------------+
! Value ! Content Description !
!--------------!------------------------------------------------------!
! EGTM ! Maximum EGT during Take Off observing time period !
! X999 ! (-55 to 999.9 C) !
! ! EEC ENG 1 7C.1.345.01 !
! ! ENG 2 7C.2.345.10 !
! ! Negative values are shown with '-' on the first !
! ! position. Otherwise the first position contains a !
! ! '0'. !
!--------------!------------------------------------------------------!
! EGTB ! Unbiased EGT !
! X999 ! (-55 to 999.9 C) !
! ! EEC ENG 1 7C.1.321.01 !
! ! ENG 2 7C.2.321.10 !
! ! Negative values are shown with '-' on the first !
! ! position. Otherwise the first position is used for !
! ! the value. !
! ! Remark: Parameter EGTB is not for IAE engine !
! ! V2530-A5 specified. !
!--------------!------------------------------------------------------!
! EPRT ! EPR Take Off !
! 9999 ! (0.6 to 1.8) !
! ! EEC ENG 1 7C.1.342.01 !
! ! ENG 2 7C.2.342.10 !
!--------------!------------------------------------------------------!
! EPRC ! EPR Command !
! 9999 ! (0.6 to 1.8) !
! ! EEC ENG 1 7C.1.341.01 !
! ! ENG 2 7C.2.341.10 !
!--------------!------------------------------------------------------!
! FT ! Wing Fuel Temperature !
! X999 ! (-60.0 to 170.0 C) !
! ! FQIC 5A.1.177.10 Fuel Temp. Left Wing Tank !
! ! 5A.1.201.10 Fuel Temp. Right Wing Tank !
! ! Remark: Report line 'V1' shows Fuel Left Wing !
! ! Temperature. !
! ! Report line 'V2' shows Fuel Right Wing !
! ! Temperature. !
!--------------!------------------------------------------------------!
! 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 !
! ! SDAC ENG 1 29.1.001.01.16 Oil filter !
! ! 29.2.001.01.16# !
! ! ENG 2 29.1.001.10.16 Oil filter !
! ! 29.2.001.10.16# !
! ! SDCA ENG 1 29.1.001.01.17 Fuel filter !
! ! 29.2.001.01.17# !
! ! ENG 2 29.1.001.10.17 Fuel filter !
! ! 29.2.001.10.17# !
!--------------!------------------------------------------------------!
! PSB ! Number 4 Bearing Engine Pressure !
! 999 ! (0 to 400 psia) !
! ! FWC 26.1.320.01 Engine 1 !
! ! 26.2.320.01# !
! ! 26.1.320.10 Engine 2 !
! ! 26.2.320.10# !
!--------------!------------------------------------------------------!
! TLA ! Throttle Lever Angle Position !
! X999 ! (-24.0 to 48.0 deg) !
! ! EEC ENG 1 7C.1.133.01 !
! ! ENG 2 7C.2.133.10 !
! ! Negative values are shown with '-' on the first !
! ! position. Otherwise the first position is for the !
! ! value. !
!--------------!------------------------------------------------------!
! BVP ! Engine Scavange Valve Position !
! 1 ! (Bit Status 1 = open) !
! ! FWC ENG 1 26.1.031.01.26 !
! ! 26.2.031.01.26# !
! ! ENG 2 26.1.031.10.26 !
! ! 26.2.031.10.26# !
+---------------------------------------------------------------------+

(2) Parameter Logic
+---------------------------------------------------------------------+
! Param. ! Print Value (Standard Progr.) !
!--------------!------------------------------------------------------!
! ESN ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! EHRS ! 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 PH 4 !
!--------------!------------------------------------------------------!
! EGTM ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! EGTB ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! EPR ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! EGT ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! N1 ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! N2 ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! FF ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! EPRT ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! EPRC ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! P3 ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! T3 ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! GLE ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! P2 ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! T2 ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! P49 ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! ECW1 ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! ECW2 ! 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 !
!--------------!------------------------------------------------------!
! FT ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! O/F ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! VB1 ! Arithmetic average for Y04.2 seconds !
!--------------!------------------------------------------------------!
! VB2 ! Arithmetic average for Y04.2 seconds !
!--------------!------------------------------------------------------!
! PHA ! Arithmetic average for Y04.2 seconds !
!--------------!------------------------------------------------------!
! PSB ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! TLA ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! BVP ! Value at moment of trigger !
+---------------------------------------------------------------------+

(3) Engine Take Off Report Logic <04> (Engine Type IAE)
+--------------------------------------------------------------------------+
!Code!Item ! ! Progr. !Standard !
! No.!No. ! Description of Function Item !----------!Value or !
! ! ! !GSE !MCDU !Table TXY!
!----!------!-----------------------------------------!----!-----!---------!
! !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 ! C ! see !
! ! ! ! ! ! separate!
! ! ! ! ! ! list !
! !E ! Transfer to ACARS MU ! C ! C ! see !
! ! ! ! ! ! separate!
! ! ! ! ! ! list !
! !F ! Increment of the report counter if the ! C ! C ! 1 !
! ! ! report was triggered by a code number ! ! ! !
! ! ! > 1000; 1=yes, 0=no ! ! ! !
! !G ! 'Y04.2' Average intervals in seconds ! C ! C ! 2 !
! ! ! for OIT, OIP, VB1, VB2 and PHA. ! ! ! !
! ! ! 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 ! Logic algorithm ! ! ! !
! !2.2 ! Remote Print Button assignment. ! C ! C ! not !
! ! ! ! ! ! assigned!
!----!------!-----------------------------------------!----!-----!---------!
!3000!3 ! Programmable Start Logic ! ! ! !
! !3.1 ! Logic algorithm ! C ! ! !
! !3.2 ! 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 both engine EGT ! ! ! !
! ! ! is maximal. The searching time period ! ! ! !
! ! ! is started 'Y04.1' seconds after enter- ! ! ! !
! ! ! ing flight phase 4. ! ! ! !
! ! ! The trigger stays armed also during ! ! ! !
! ! ! flight phase 5. ! ! ! !
! !4.1 ! Logic algorithm ! ! ! !
! ! ! ! ! ! !
! !4.1.2 ! The report is postponed to the next ! ! ! !
! ! ! flight leg if at least one of the EGT ! ! ! !
! ! ! values of Eng 1 or Eng 2 is below EGTL ! ! ! !
! ! ! when the starter air valve switches from! ! ! !
! ! ! the closed to the open position at ! ! ! !
! ! ! engine start. ! ! ! !
! ! ! Starter Air Valve open: ! ! ! !
! ! ! 7C.1.270.01.13 = 1 Engine 1 ! ! ! !
! ! ! 7C.1.270.10.13 = 2 Engine 2 ! ! ! !
! ! ! ! ! ! !
! ! ! 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: ! ! ! !
! ! ! 5D.2.061.10.28 = 0 Engine 1 ! ! ! !
! ! ! 5D.2.061.10.27 = 0 Engine 2 ! ! ! !
!----!------!-----------------------------------------!----!-----!---------!
!4100!4.1.3 ! The same rules as described for Log. No.! C ! C !disarmed !
! ! ! 4000 are 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 disarmed and armed ! ! ! !
! ! ! through the MCDU menu 'AIDS DISCRET ! ! ! !
! ! ! TRIGGER INHIBIT'. ! ! ! !
!----!------!-----------------------------------------!----!-----!---------!
! !4.1.4 ! 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)'. ! ! ! !
! ! ! ! ! ! !
! !4.1.5 ! EGTL = EGT + TAT ! C ! C ! T23 !
! ! ! ! ! ! !
! !4.2 ! 'F04'th Take Off ! C ! C ! T23 !
! ! ! ! ! ! !
! !4.3 ! 'Y04.1' seconds after PH 4 entry ! C ! C ! T23 !
! ! ! ! ! ! !
! !4.4 ! T/O Delta EPR summary limits ! ! ! !
! ! ! deltaEPR = EPRmaxT/O - EPRactual ! ! ! !
! ! ! EPRmaxT/O = 7C.1.342.01 Eng 1 ! ! ! !
! ! ! 7C.2.342.10 Eng 2 ! ! ! !
! ! ! EPRactual = 7C.1.340.01 Eng 1 ! ! ! !
! ! ! 7C.2.340.10 Eng 2 ! ! ! !
! ! ! ! ! ! !
! !4.4.1 ! deltaEPR > 0.1 ! A ! ! T23 !
! ! ! ! ! ! !
! !4.4.2 ! deltaEPR > 0.075 and <=0.1 ! A ! ! T23 !
! ! ! ! ! ! !
! !4.4.3 ! deltaEPR > 0.05 and <=0.075 ! A ! ! T23 !
! ! ! ! ! ! !
! !4.4.4 ! deltaEPR > 0.03 and <=0.05 ! A ! ! T23 !
! ! ! ! ! ! !
! !4.4.5 ! deltaEPR > 0.02 and <=0.03 ! A ! ! T23 !
! ! ! ! ! ! !
! !4.4.6 ! deltaEPR > 0.01 and <=0.02 ! A ! ! T23 !
! ! ! ! ! ! !
! !4.4.7 ! deltaEPR <= 0.01 ! A ! ! T23 !
! ! ! ! ! ! !
! !4.5 ! The calculation is made 'Y04.3' seconds ! ! ! !
! ! ! after entry into flight phase 4. ! ! ! !
! ! ! ! ! ! !
! !4.5.1 ! 'Y04.3' seconds after PH 4 entry. ! C ! C ! T23 !
! ! ! ! ! ! !
!----!------!-----------------------------------------!----!-----!---------!
!5001!5 ! Each time when a report is generated by ! ! ! !
!5002! ! this logic the number (X) is decreased ! ! ! !
!5003! ! until zero. The conditions are described! ! ! !
! ! ! under code No. 40000 (without item 4.2).! ! ! !
!5004! ! ! ! ! !
!5005! ! The number (X) is programmable. ! ! ! !
! . ! ! ! ! ! !
! . ! ! In case of change the engine serial ! ! ! !
! . ! ! number, (X) is automatically set to ! ! ! !
! . ! ! five. ! ! ! !
!500X! ! The code appears in an increasing order,! ! ! !
! ! ! i.e. the first report has the code 5001,! ! ! !
! ! ! the next code is 5002 and so on until ! ! ! !
! ! ! 5005. ! ! ! !
! ! ! ! ! ! !
! !5.1 ! Logic algorithm ! ! ! !
! ! ! ! ! ! !
! !5.2 ! Number 'X' for consecutive legs up to 9.! C ! C ! T23 !
! ! ! ! ! ! !
! !5.3 ! Number 'X' 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 at the next! ! ! !
! ! ! take-off according to code 4000 without ! ! ! !
! ! ! performing the logic for the report ! ! ! !
! ! ! postponement. ! ! ! !
!--------------------------------------------------------------------------!
! A = Programmable by Airbus !
! C = Programmable by Customer !
+--------------------------------------------------------------------------+

F. AIDS Reports Print Rules - Default Values for Report <04>
+-------------------------------------------------------------------------+
!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 !
+-------------------------------------------------------------------------+

G. Engine Report On Request <05>
F Engine Report On Request <05> (Engine Type IAE) ** 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.
NOTE: For the standard header definition of the report refer to (Ref. AMM D/O 31-36-00-00).
NOTE: If the ESN printed out in the report is in the range between 13191 and 15000, then add 5000 to this value to get the actual ESN.
(1) Engine Report O/R Data Field Description <05> (Engine Type IAE)
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 !
!--------------!------------------------------------------------------!
! ECW3 ! Engine Control Word 3 !
! 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.19 = 1 Reverser System Failed !
! ! 12 7C.X.271.XX.14 = 1 Reverser deploy Solenoid- !
! ! Deploy !
! ! 13 7C.X.271.XX.22 = 1 Overspeed Solenoid On !
! ! 14 7C.X.271.XX.28 = 1 P2/T2 Probe Heater Relay !
! ! On !
! ! 15 7C.X.272.XX.22 = 1 Bleed Config. K1 Selected !
! ! 16 7C.X.272.XX.23 = 1 Bleed Config. K2 Selected !
! ! 17 7C.X.272.XX.24 = 1 Bleed Config. K3 Selected !
! ! 18 7C.X.272.XX.25 = 1 Bleed Config. K4 Selected !
! ! 19 7C.X.272.XX.26 = 1 Bleed Config. K5 Selected !
! ! 20 7C.X.272.XX.27 = 1 Bleed Config. K6 Selected !
! ! 21 7C.X.272.XX.28 = 1 Bleed Config. Data Failed !
! ! 22 7C.X.276.XX.25 = 1 Continuous Ignition Active!
! ! 23 7C.X.276.XX.27 = 1 Engine Blowout !
! ! 24 7C.X.351.XX.14 = 1 Left ADC Input Failed !
! ! 25 7C.X.351.XX.15 = 1 Right ADC Input Failed !
! ! 26 7C.X.155.XX.28 = 1 EEC Overheat !
! ! 27 SPARE !
! ! 28 SPARE !
! ! 29 SPARE !
!--------------!------------------------------------------------------!
! ECW4 ! Engine Control Word 4 !
! 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 SPARE !
! ! 12 7C.X.272.XX.16 = 1 FDV Off !
! ! 13 SPARE !
! ! 14 SPARE !
! ! 15 SPARE !
! ! 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 !
!--------------!------------------------------------------------------!
! 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 !
! ! '0'. !
! ! ADIRU 06.1.211.01 !
! ! 06.2.211.10# !
!--------------!------------------------------------------------------!
! ALT ! Standard Altitude (1013mbar) !
! 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 ! 99 1111 1 1111 99!
! ! LH Pack Flow 8E.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 is 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'. !
+---------------------------------------------------------------------+

(2) Parameter Logic
+---------------------------------------------------------------------+
! Param. ! Print Value (Standard Progr.) !
!--------------!------------------------------------------------------!
! ESN ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! EHRS ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! ECYC ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! AP ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! ECW3 ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! ECW4 ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! EVM ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! EPR ! Snapshot at 1 sec. intervals !
!--------------!------------------------------------------------------!
! EGT ! Snapshot at 1 sec. intervals !
!--------------!------------------------------------------------------!
! N1 ! Snapshot at 1 sec. intervals !
!--------------!------------------------------------------------------!
! N2 ! Snapshot at 1 sec. intervals !
!--------------!------------------------------------------------------!
! FF ! Snapshot at 1 sec. intervals !
!--------------!------------------------------------------------------!
! VB1 ! Snapshot at 1 sec. intervals !
!--------------!------------------------------------------------------!
! VB2 ! Snapshot at 1 sec. intervals !
!--------------!------------------------------------------------------!
! TAT ! Report line CE at 5 seconds pre-event !
! ! Report line C3 at 5 seconds post-event !
!--------------!------------------------------------------------------!
! ALT ! Report line CE at 5 seconds pre-event !
! ! Report line C3 at 5 seconds post-event !
!--------------!------------------------------------------------------!
! MN ! Report line CE at 5 seconds pre-event !
! ! Report line C3 at 5 seconds post-event !
!--------------!------------------------------------------------------!
! BLEED ! Report line CE at 5 seconds pre-event !
! STATUS ! Report line C3 at 5 seconds post-event !
+---------------------------------------------------------------------+

(3) Engine Report O/R Logic <05> (Engine Type IAE)
+--------------------------------------------------------------------------+
!Code!Item ! !Progr. !Standard !
! No.!No. ! Description of Function Item !----------!Value or !
! ! ! !GSE !MCDU !Table TXY!
!----!------!-----------------------------------------!----!-----!---------!
! !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 (3) ! C ! C ! see !
! ! ! ! ! ! separate!
! ! ! ! ! ! list !
! !E ! Transfer to ACARS MU ! C ! C ! see !
! ! ! ! ! ! separate!
! ! ! ! ! ! list !
! !F ! Increment of the report counter if the ! C ! C ! 1 !
! ! ! report was triggered by a code number ! ! ! !
! ! ! > 1000; 1=yes, 0=no (standard ! ! ! !
! ! ! programming = 1) ! ! ! !
!----!------!-----------------------------------------!----!-----!---------!
!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 ! Flight Phase: ! C ! C ! 4,5,5.1,!
! ! ! ! ! ! 6,7,7.1,!
! ! ! ! ! ! 8,9,10 !
!----!------!-----------------------------------------!----!-----!---------!
!3000!3 ! Programmable Start Logic ! ! ! !
! !3.1 ! Logic algorithm ! C ! ! !
! !3.2 ! Logic criteria values ! 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>
+-------------------------------------------------------------------------+
!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 !
+-------------------------------------------------------------------------+

I. Engine Gas Path Advisory Report <06>
F Engine Gas Path Advisory Report <06> (Engine Type IAE) ** ON A/C NOT FOR ALL
The Engine Gas 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.
NOTE: For the standard header definition of the report refer to (Ref. AMM D/O 31-36-00-00).
NOTE: If the ESN printed out in the report is in the range between 13191 and 15000, then add 5000 to this value to get the actual ESN.
(1) Engine-Gas-Path-Advisory-Report Data-Field-Description <06> (Engine Type IAE)
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 !
!--------------!------------------------------------------------------!
! HPT ! Selected HPTC Position !
! X99 ! ECU (-10 to 100%) !
! ! 7C.1.306.01 Engine 1 !
! ! 7C.2.306.10 Engine 2 !
!--------------!------------------------------------------------------!
! E ! Exceedance Engine Position !
! 9 ! No. of engine where the exceedence occurs. !
! ! DMU !
! ! NOTE: If the report is not triggered by a limit !
! ! exceedence then this field contains zero's. !
!--------------!------------------------------------------------------!
! MAX ! Maximal Value of the Exceeded Parameter !
! 9999 ! !
! ! NOTE: If the report is not triggered by a limit !
! ! exceedence then this field contains zero's. !
!--------------!------------------------------------------------------!
! LIM ! Programmable Limit, which was exceeded !
! 9999 ! !
! ! NOTE: If the report is not triggered by a limit !
! ! exceedence then this field contains zero's. !
!--------------!------------------------------------------------------!
! REF ! N2 at Stall Detection !
! 9999 ! (0.0 to 120.0% rpm) !
! ! ECU Engine 1 7C.1.344.01 !
! ! Engine 2 7C.2.344.10 !
! ! NOTE: For all other exceedence zero's are printed. !
!--------------!------------------------------------------------------!
! TOL ! Time Over Limit !
! 999 ! DMU (Time at least 60 seconds) !
! ! NOTE: If the report is not triggered by a limit !
! ! exceedence then this field contains zero's. !
!--------------!------------------------------------------------------!
! TTP ! Time To Peak !
! 999 ! DMU (Time to maximum of exceeded value) !
! ! NOTE: If the report is not triggered by a limit !
! ! exceedence then this field contains zero's. !
!--------------!------------------------------------------------------!
! Y1 ! 'Y06.1' Second Programmed Pre-event Intervals !
! 99 ! DMU (1 to 6 sec) !
!--------------!------------------------------------------------------!
! Y2 ! 'Y06.2' Second Programmed Pre-event Intervals !
! 99 ! DMU (1 to 60 sec) !
!--------------!------------------------------------------------------!
! PARA ! Label of the Exceeded Parameter !
! 999 ! !
!--------------!------------------------------------------------------!
! MN ! Mach Number !
! 999 ! (0.100 to 0.999) !
! ! ADIRU 06.1.205.01 !
! ! 06.2.205.10# !
!--------------!------------------------------------------------------!
! ECW3 ! Engine Control Word 3 !
! 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.19 = 1 Reverser System Failed !
! ! 12 7C.X.271.XX.14 = 1 Reverser deploy Solenoid- !
! ! Deploy !
! ! 13 7C.X.271.XX.22 = 1 Overspeed Solenoid On !
! ! 14 7C.X.271.XX.28 = 1 P2/T2 Probe Heater Relay !
! ! On !
! ! 15 7C.X.272.XX.22 = 1 Bleed Config. K1 Selected !
! ! 16 7C.X.272.XX.23 = 1 Bleed Config. K2 Selected !
! ! 17 7C.X.272.XX.24 = 1 Bleed Config. K3 Selected !
! ! 18 7C.X.272.XX.25 = 1 Bleed Config. K4 Selected !
! ! 19 7C.X.272.XX.26 = 1 Bleed Config. K5 Selected !
! ! 20 7C.X.272.XX.27 = 1 Bleed Config. K6 Selected !
! ! 21 7C.X.272.XX.28 = 1 Bleed Config. Data Failed !
! ! 22 7C.X.276.XX.25 = 1 Continuous Ignition Active!
! ! 23 7C.X.276.XX.27 = 1 Engine Blowout !
! ! 24 7C.X.351.XX.14 = 1 Left ADC Input Failed !
! ! 25 7C.X.351.XX.15 = 1 Right ADC Input Failed !
! ! 26 7C.X.155.XX.28 = 1 EEC Overheat !
! ! 27 SPARE !
! ! 28 SPARE !
! ! 29 SPARE !
!--------------!------------------------------------------------------!
! ECW4 ! Engine Control Word 4 !
! 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 SPARE !
! ! 12 7C.X.272.XX.16 = 1 FDV Off !
! ! 13 SPARE !
! ! 14 SPARE !
! ! 15 SPARE !
! ! 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 !
!--------------!------------------------------------------------------!
! TRP ! Thrust Reverser Position !
! 999 ! (0 to 100 %) !
! ! ECU 7C.1.137.01 Engine 1 !
! ! 7C.2.137.10 Engine 2 !
+---------------------------------------------------------------------+

(2) Parameter Logic
+---------------------------------------------------------------------+
! Param. ! Print Value (Standard Progr.) !
!--------------!------------------------------------------------------!
! ESN ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! EHRS ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! ECYC ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! AP ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! HPT ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! SVA ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! BAF ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! LP ! 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' post-event intervals !
!--------------!------------------------------------------------------!
! PARA ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! EPR ! Snapshot at Y06.1 and Y06.2 sec. intervals !
!--------------!------------------------------------------------------!
! EGT ! Snapshot at Y06.1 and Y06.2 sec. intervals !
!--------------!------------------------------------------------------!
! N1 ! Snapshot at Y06.1 and Y06.2 sec. intervals !
!--------------!------------------------------------------------------!
! N2 ! 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 !
!--------------!------------------------------------------------------!
! EPRC ! Snapshot at Y06.1 and Y06.2 sec. intervals !
!--------------!------------------------------------------------------!
! T2 ! Snapshot at Y06.1 and Y06.2 sec. intervals !
!--------------!------------------------------------------------------!
! P2 ! Snapshot at Y06.1 and Y06.2 sec. intervals !
!--------------!------------------------------------------------------!
! MN ! Snapshot at Y06.1 and Y06.2 sec. intervals !
!--------------!------------------------------------------------------!
! ECW3 ! Snapshot at Y06.1 and Y06.2 sec. intervals !
!--------------!------------------------------------------------------!
! ECW4 ! Snapshot at Y06.1 and Y06.2 sec. intervals !
!--------------!------------------------------------------------------!
! TRP ! Snapshot at Y06.1 and Y06.2 sec. intervals !
+---------------------------------------------------------------------+

(3) Engine Gas Path Advisory Report Logic <06> (Engine Type IAE)
+--------------------------------------------------------------------------+
!Code!Item ! ! Progr. !Standard !
! No.!No. ! Description of Function Item !----------!Value or !
! ! ! !GSE !MCDU !Table TXY!
!----!------!-----------------------------------------!----!-----!---------!
! !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 (2) ! C ! C ! see !
! ! ! ! ! ! separate!
! ! ! ! ! ! list !
! !E ! Transfer to ACARS MU ! C ! C ! see !
! ! ! ! ! ! separate!
! ! ! ! ! ! list !
! !F ! Increment of the report counter if the ! C ! C ! 1 !
! ! ! report was triggered by a code number ! ! ! !
! ! ! > 1000; 1=yes, 0=no ! ! ! !
! ! ! (standard programming = 1) ! ! ! !
! !G ! 'Y06.1' Pre-event print intervals ! C ! ! 6 !
! !H ! 'Y06.2' Post-event print intervals ! C ! ! 5 !
! !I ! 'M06.1' Number of Post-event data set ! C ! ! 5 !
! ! ! (up to 16). ! ! ! !
! !J ! Max. No. of reports per trigger, engine ! C ! ! 10 !
! ! ! and flight leg ! ! ! !
! !K ! 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 ! Logic algorithm ! ! ! !
! !2.2 ! Flight Phases (no standard prog.) ! C ! C ! not !
! ! ! ! ! ! assigned!
!----!------!-----------------------------------------!----!-----!---------!
!3000!3 ! Programmable Start Logic ! ! ! !
! !3.1 ! Logic algorithm ! C ! ! !
! !3.2 ! Logic criteria values ! C ! ! not !
! ! ! ! ! ! progr. !
!----!------!-----------------------------------------!----!-----!---------!
!4000!4 ! Report generation, if Stall bit is set ! ! ! !
! ! ! to '1'. ! ! ! !
! ! ! 7C.1.145.01.19 = 1 Engine 1 ! ! ! !
! ! ! 7C.2.145.01.19 = 1 Engine 2 ! ! ! !
!----!------!-----------------------------------------!----!-----!---------!
!5100!5 ! (EGT > EGTL1) AND ! ! ! !
! ! ! ( (PH == 3) OR ! ! ! !
! ! ! (PH == 4) OR ! ! ! !
! ! ! (PH == 5) OR ! ! ! !
! ! ! (PH == 6) OR ! ! ! !
! ! ! (Alpha Floor protection active ==1) ) ! ! ! !
! ! ! AND ! ! ! !
! ! ! (EGT limit exceedance indicated by ! ! ! !
! ! ! FWC == 1) ! ! ! !
! ! ! ! ! ! !
! ! ! Alpha Floor protection active ! ! ! !
! ! ! 7C.1.155.01.25 = 1 Engine 1 ! ! ! !
! ! ! 7C.2.155.10.25 = 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 ! ! ! !
!5200! ! ( (PH !=1.1) AND ! ! ! !
! ! ! (PH !=3) AND ! ! ! !
! ! ! (PH !=4) AND ! ! ! !
! ! ! (PH !=5) ) AND ! ! ! !
! ! ! (EGT limit exceedance indicated by ! ! ! !
! ! ! FWC == 1) ! ! ! !
! ! ! or ! ! ! !
!5300! ! Not applicable ! ! ! !
! ! ! ! ! ! !
!5400! ! Not applicable ! ! ! !
!5500! ! N1 > N1L1.1 in all PH ! ! ! !
!5600! ! Not applicable ! ! ! !
!5700! ! N2 > N2L1.1 in all PH ! ! ! !
!----!------!-----------------------------------------!----!-----!---------!
! !5.1 ! EGTL1 (red limit) ! C ! C ! T23 !
! ! ! ! ! ! !
! !5.2 ! EGTL2 (yellow limit) ! C ! C ! T23 !
! ! ! ! ! ! !
! !5.3 ! Not applicable ! C ! C ! T23 !
! ! ! ! ! ! !
! !5.4 ! Not applicable ! ! ! !
! ! ! ! ! ! !
! !5.5 ! N1L1.2 (red limit) ! C ! C ! T23 !
! ! ! ! ! ! !
! !5.6 ! Not applicable ! ! ! !
! ! ! ! ! ! !
! !5.7 ! N2L1.2 (red limit) ! C ! C ! T23 !
! ! ! ! ! ! !
! !5.8 ! If trigger code 5100 is activated and ! ! ! !
! ! ! report code 5200 has already been acti- ! ! ! !
! ! ! vated before but not closed yet, report ! ! ! !
! ! ! code 5100 only is 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.1.145.01.16 = 1 ! ! ! !
! ! ! or 7C.2.145.19.16 = 1) ! ! ! !
!----!------!-----------------------------------------!----!-----!---------!
! !7 ! Report Generation stops when exceedance ! ! ! !
! ! ! parameter within limits are 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 !
+--------------------------------------------------------------------------+

J. AIDS Reports Print Rules - Default Values for Report <06>
+-------------------------------------------------------------------------+
!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 ! Not applicable !
!-------!-----------------------------------------------------------------!
! 5500 ! NO ! YES ! NO ! NO ! YES ! NO ! YES !
!-------!-----------------------------------------------------------------!
! 5600 ! Not applicable !
!-------!-----------------------------------------------------------------!
! 5700 ! NO ! YES ! NO ! NO ! ! NO ! YES !
!-------!-------!--------!-------!-------! Y !--------!--------------!
! 6000 ! NO ! YES ! NO ! NO ! E ! NO ! YES !
!-------!-------!--------!-------!-------! S !--------!--------------!
! 8100 ! NO ! YES ! NO ! NO ! ! NO ! YES !
+-------------------------------------------------------------------------+

K. Engine Mechanical Advisory Report <07>
F Engine Mechanical Advisory Report <07> (Engine Type IAE) ** 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.
NOTE: For the standard header definition of the report refer to (Ref. AMM D/O 31-36-00-00).
NOTE: If the ESN printed out in the report is in the range between 13191 and 15000, then add 5000 to this value to get the actual ESN.
(1) Engine Mechanical Advisory Report Data Field Description <07> (Engine Type IAE)
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.
NOTE: The Number 4 Bearing Engine pressure (PSB) parameter is missing in Engine Mechanical Advisory Report <07> on aircrafts fitted with FWC H2F7 standard (PN 350E053021212).
The Report <07> is not given in case of PSB exceedance (code 4400).
+---------------------------------------------------------------------+
! Value ! Content Description !
!--------------!------------------------------------------------------!
! ECW4 ! Engine Control Word 4 !
! 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 SPARE !
! ! 12 7C.X.272.XX.16 = 1 FDV Off !
! ! 13 SPARE !
! ! 14 SPARE !
! ! 15 SPARE !
! ! 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 !
!--------------!------------------------------------------------------!
! Y1 ! 'Y07.1' seconds programmed Pre-event Intervals !
! 99 ! DMU (1 to 4 sec.) !
!--------------!------------------------------------------------------!
! Y2 ! 'Y07.2' seconds programmed Post-event Intervals !
! 99 ! DMU (1 to 60 sec.) !
!--------------!------------------------------------------------------!
! E ! Exceedance Engine Position !
! 9 ! DMU !
! ! No. of engine where the exceedence occurs or in !
! ! case of discrete trigger the related No. of engine.!
!--------------!------------------------------------------------------!
! MAX ! Maximal Value of the Exceeded Parameter !
! 9999 ! !
! ! NOTE: In case of OIPL1.1 or OIPL1.2 exceedance the !
! ! minimal value is printed. !
! ! NOTE: If the report is not triggered by a limit !
! ! exceedance but by a discrete signal the value!
! ! is calculated indirect. !
!--------------!------------------------------------------------------!
! LIM ! Programmable Limit, which was exceeded !
! 9999 ! !
! ! NOTE: If the report is not triggered by a limit !
! ! exceedance this field has zero's. !
!--------------!------------------------------------------------------!
! REF ! N1 is taken at exceedance of VB1. For all other !
! 9999 ! exceedance N2 is taken. !
! ! (0.0 to 120.0% rpm) !
! ! ECU ENGINE 1 N1 7C.1.346.01 !
! ! ENGINE 2 7C.2.346.10 !
! ! !
! ! ENGINE 1 N2 7C.1.344.01 !
! ! ENGINE 2 7C.2.344.10 !
! ! !
!--------------!------------------------------------------------------!
! TOL ! Time Over Limit !
! 999 ! DMU (Time at lease 60 seconds) !
! ! NOTE: If the report was not triggered by a limit !
! ! exceedance but be a discrete signal, the !
! ! value is calculated indirect. !
!--------------!------------------------------------------------------!
! TTP ! Time To Peak !
! 999 ! DMU (Time to maximum of exceeded value) !
! ! NOTE: If the report is not triggered by a limit !
! ! exceedance but by a discrete signal, the !
! ! value is calculated indirect. !
!--------------!------------------------------------------------------!
! PARA ! Label of the Exceeded Parameter !
! 999 ! !
!--------------!------------------------------------------------------!
! PSB ! Number 4 Bearing Engine Pressure !
! 999 ! (0 to 400 psia) !
! ! FWC Engine 1 26.1.320.01 !
! ! 26.2.320.01# !
! ! Engine 2 26.1.320.10 !
! ! 26.2.320.10# !
!--------------!------------------------------------------------------!
! BVP ! Engine Scavange Valve Position !
! 1 ! (Bit Status 1 = open) !
! ! FWC Engine 1 26.1.031.01.26 !
! ! 26.2.031.01.26# !
! ! Engine 2 26.1.031.10.26 !
! ! 26.2.031.10.26# !
+---------------------------------------------------------------------+

(2) Parameter Logic
+---------------------------------------------------------------------+
! Param. ! Print Value (Standard Progr.) !
!--------------!------------------------------------------------------!
! ESN ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! EHRS ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! ECYC ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! AP ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! ECW4 ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! Y1 ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! Y2 ! 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 !
!--------------!------------------------------------------------------!
! PARA ! 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 !
!--------------!------------------------------------------------------!
! VB1 ! Snapshot at Y07.1 and Y07.2 sec. intervals !
!--------------!------------------------------------------------------!
! VB2 ! Snapshot at Y07.1 and Y07.2 sec. intervals !
!--------------!------------------------------------------------------!
! PHA ! 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 !
!--------------!------------------------------------------------------!
! PSB ! Snapshot at Y07.1 and Y07.2 sec. intervals !
!--------------!------------------------------------------------------!
! BVP ! Snapshot at Y07.1 and Y07.2 sec. intervals !
+---------------------------------------------------------------------+

(3) Engine Mechanical Advisory Report Logic <07> (Engine Type IAE)
+--------------------------------------------------------------------------+
!Code!Item ! ! Progr. !Standard !
! No.!No. ! Description of Function Item !----------!Value or !
! ! ! !GSE !MCDU !Table TXY!
!----!------!-----------------------------------------!----!-----!---------!
! !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 (2) ! C ! C ! see !
! ! ! ! ! ! separate!
! ! ! ! ! ! list !
! !E ! Transfer to ACARS MU ! C ! C ! see !
! ! ! ! ! ! separate!
! ! ! ! ! ! list !
! !F ! Increment of the report counter if the ! C ! C ! 1 !
! ! ! report was triggered by a logig number ! ! ! !
! ! ! > 1000; 1 = yes, 0 = no ! ! ! !
! ! ! (standard programming = 1) ! ! ! !
! !G ! 'Y07.1' Pre-event print intervals ! C ! ! 4 !
! ! ! (4 seconds). ! ! ! !
! !H ! 'Y07.2' After-event print intervals ! C ! ! 5 !
! ! ! (5 seconds). ! ! ! !
! !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 ! Logic algorithm ! ! ! !
! !2.2 ! Flight Phase (no standard programming) ! C ! C ! not !
! ! ! ! ! ! assigned!
!----!------!-----------------------------------------!----!-----!---------!
!3000!3 ! Programmable Start Logic ! ! ! !
! !3.1 ! Logic algorithm ! C ! ! !
! !3.2 ! Logic criteria values ! C ! ! not !
! ! ! ! ! ! progr. !
!----!------!-----------------------------------------!----!-----!---------!
!4110!4 ! OIT > OITL1 in all PH ! ! ! !
! ! ! or ! ! ! !
!4120! ! OIT > OITL2 in all PH ! ! ! !
! ! ! or ! ! ! !
!4130! ! Not applicable ! ! ! !
! ! ! or ! ! ! !
!4210! ! OIP < OIPL1 at N2L2.1 in PH 2, 3, 9 ! ! ! !
! ! ! or ! ! ! !
!4220! ! OIP < OIPL2 at N2L2.2 in phases 4 to 8 ! ! ! !
! ! ! or ! ! ! !
!4230! ! OIP > OIPL3 in all PH ! ! ! !
! ! ! or ! ! ! !
!4310! ! VB1 is above Advisory LVL in all PH ! ! ! !
! ! ! (EVM 3D.1.035.01.11 or ! ! ! !
! ! ! 3D.1.035.10.11) ! ! ! !
! ! ! Remark: Refer also to item 4.5 ! ! ! !
! ! ! or ! ! ! !
!4320! ! VB2 is above Advisory LVL in all PH ! ! ! !
! ! ! (EVM, 3D.1.035.01.12 or ! ! ! !
! ! ! 3D.1.035.10.12) ! ! ! !
! ! ! Remark: Refer also to item 4.6 ! ! ! !
! ! ! or ! ! ! !
!4400! ! PSB > PSBlim ! ! ! !
! ! ! ! ! ! !
! !4.1.1 ! OITL1 in Degrees C (yellow limit) ! C ! C ! T23 !
! ! ! ! ! ! !
! !4.1.2 ! OITL2 in Degrees C (red limit) ! C ! C ! T23 !
! ! ! ! ! ! !
! !4.1.3 ! Not applicable ! ! ! !
! !4.1.4 ! 'Y07.3' = 15 min. ! C ! C ! T23 !
! ! ! ! ! ! !
! !4.2.1 ! OIPL1.1 ! A ! ! T23 !
! ! ! defined in the following table: ! ! ! !
! ! ! (linear interpolation and linear ! ! ! !
! ! ! extrapolation below 50% and above 100%)! ! ! !
! ! ! OIPL1.1 (psia) ! N2L2.1 (%rpm) ! ! ! !
! ! ! ________________!_______________ ! ! ! !
! ! ! 0 ! 0 ! ! ! !
! ! ! 0 ! 59 ! ! ! !
! ! ! 80 ! 60 ! ! ! !
! ! ! 80 ! 90 ! ! ! !
! ! ! 80 ! 100 ! ! ! !
! ! ! ! ! ! !
! !4.2.2 ! OIPL1.2 ! A ! ! T23 !
! ! ! defined in the following table: ! ! ! !
! ! ! (linear interpolation and linear ! ! ! !
! ! ! extrapolation below 50% and above 100%)! ! ! !
! ! ! OIPL1.1 (psia) ! N2L2.1 (%rpm) ! ! ! !
! ! ! ________________!_______________ ! ! ! !
! ! ! 80 ! 60 ! ! ! !
! ! ! 80 ! 70 ! ! ! !
! ! ! 80 ! 80 ! ! ! !
! ! ! 80 ! 90 ! ! ! !
! ! ! 80 ! 100 ! ! ! !
! ! ! ! ! ! !
! !4.2.3 ! OIPL2 ! C ! C ! T23 !
! ! ! ! ! ! !
! !4.3 ! PSBlim ! C ! C ! T23 !
! ! ! ! ! ! !
! !4.4 ! Logic algorithm ! ! ! !
! !4.5 ! For code 4310 the value for Max and TTP ! ! ! !
! ! ! is calculated indirectly 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 ! ! ! !
! ! ! also counts the seconds while the above ! ! ! !
! ! ! named discrete is set to '1'and the ! ! ! !
! ! ! Maximum is not reached and use the coun-! ! ! !
! ! ! ted seconds for TIP. ! ! ! !
! ! ! The value for TOL is the time while the ! ! ! !
! ! ! discrete for code 4310 is set to '1'. ! ! ! !
! ! ! In case the discrete is set to '1' for ! ! ! !
! ! ! more than 60 seconds the calculation ! ! ! !
! ! ! of the values TOL, TTP and MAX stops. ! ! ! !
! ! ! ! ! ! !
! !4.6 ! The same algorithm - as described in i- ! ! ! !
! ! ! tem 4.5 - is used for TOL, MAX and TTP, ! ! ! !
! ! ! if code 4320 with the related 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. ! ! ! !
! !5.1 ! Logic algorithm ! ! ! !
!----!------!-----------------------------------------!----!-----!---------!
!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>
+-------------------------------------------------------------------------+
!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 !
!-------!-------!--------!-------!-------! Y !--------!--------------!
! 3000 ! NO ! NO ! NO ! NO ! E ! NO ! YES !
!-------!-------!--------!------ !-------! S !--------!--------------!
! 4110 ! NO ! YES ! NO ! NO ! ! NO ! YES !
!-------!-------!--------!-------!-------! !--------!--------------!
! 4120 ! NO ! YES ! NO ! NO ! ! NO ! YES !
!-------!-----------------------------------------------------------------!
! 4130 ! Not applicable !
!-------!-----------------------------------------------------------------!
! 4210 ! NO ! YES ! NO ! NO ! ! NO ! YES !
!-------!-------!--------!-------!-------! !--------!--------------!
! 4220 ! NO ! YES ! NO ! NO ! ! NO ! YES !
!-------!-------!--------!-------!-------! !--------!--------------!
! 4230 ! NO ! YES ! NO ! NO ! Y ! NO ! YES !
!-------!-------!--------!-------!-------! E !--------!--------------!
! 4310 ! NO ! YES ! NO ! NO ! S ! NO ! YES !
!-------!-------!--------!-------!-------! !--------!--------------!
! 4320 ! NO ! YES ! NO ! NO ! ! NO ! YES !
!-------!-------!--------!-------!-------! !--------!--------------!
! 4400 ! NO ! YES ! NO ! NO ! ! NO ! YES !
!-------!-------!--------!-------!-------! !--------!--------------!
! 8100 ! NO ! YES ! NO ! NO ! ! NO ! YES !
+-------------------------------------------------------------------------+

M. Engine Divergence Report <09>
F Engine Divergence Report <09> (Engine Type IAE) ** 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.
NOTE: For the standard header definition of the report refer to (Ref. AMM D/O 31-36-00-00).
NOTE: If the ESN printed out in the report is in the range between 13191 and 15000, then add 5000 to this value to get the actual ESN.
(1) Engine Divergence Report Data Field Description <09> (Engine Type IAE)
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 in PH 5.1 or PH 6 !
! 9999 ! Depending of divergent parameter !
!--------------!------------------------------------------------------!
! REF ! Actual deltaEGT or deltaTN value of PH 5.1 or PH 6 !
! 9999 ! DMU (-999 to 999 °C) !
! ! Negative values are shown with '-' in the first !
! ! position. !
!--------------!------------------------------------------------------!
! K ! Actual Value of K in PH5.1 or PH6 !
! 99 ! DMU (0 to 99) !
!--------------!------------------------------------------------------!
! ECW3 ! Engine Control Word 3 !
! 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.19 = 1 Reverser System Failed !
! ! 12 7C.X.271.XX.14 = 1 Reverser deploy Solenoid- !
! ! Deploy !
! ! 13 7C.X.271.XX.22 = 1 Overspeed Solenoid On !
! ! 14 7C.X.271.XX.28 = 1 P2/T2 Probe Heater Relay !
! ! On !
! ! 15 7C.X.272.XX.22 = 1 Bleed Config. K1 Selected !
! ! 16 7C.X.272.XX.23 = 1 Bleed Config. K2 Selected !
! ! 17 7C.X.272.XX.24 = 1 Bleed Config. K3 Selected !
! ! 18 7C.X.272.XX.25 = 1 Bleed Config. K4 Selected !
! ! 19 7C.X.272.XX.26 = 1 Bleed Config. K5 Selected !
! ! 20 7C.X.272.XX.27 = 1 Bleed Config. K6 Selected !
! ! 21 7C.X.272.XX.28 = 1 Bleed Config. Data Failed !
! ! 22 7C.X.276.XX.25 = 1 Continuous Ignition Active!
! ! 23 7C.X.276.XX.27 = 1 Engine Blowout !
! ! 24 7C.X.351.XX.14 = 1 Left ADC Input Failed !
! ! 25 7C.X.351.XX.15 = 1 Right ADC Input Failed !
! ! 26 7C.X.155.XX.28 = 1 EEC Overheat !
! ! 27 SPARE !
! ! 28 SPARE !
! ! 29 SPARE !
!--------------!------------------------------------------------------!
! ECW4 ! Engine Control Word 4 !
! 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 SPARE !
! ! 12 7C.X.272.XX.16 = 1 FDV Off !
! ! 13 SPARE !
! ! 14 SPARE !
! ! 15 SPARE !
! ! 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 !
!--------------!------------------------------------------------------!
! PARA ! Label of the Exceeded Parameter !
! 999 ! !
+---------------------------------------------------------------------+

(2) Parameter Logic
+---------------------------------------------------------------------+
! Param. ! Print Value (Standard Progr.) !
!--------------!------------------------------------------------------!
! ESN ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! EHRS ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! ECYC ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! AP ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! ECW4 ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! SVA ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! BAF ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! E ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! DIV ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! K ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! REF ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! ECW3 ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! PARA ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! EPR ! Snapshot at 2 seconds interval !
!--------------!------------------------------------------------------!
! EGT ! Snapshot at 2 seconds interval !
!--------------!------------------------------------------------------!
! N1 ! Snapshot at 2 seconds interval !
!--------------!------------------------------------------------------!
! N2 ! Snapshot at 2 seconds interval !
!--------------!------------------------------------------------------!
! FF ! Snapshot at 2 seconds interval !
!--------------!------------------------------------------------------!
! TN ! Snapshot at 2 seconds interval !
!--------------!------------------------------------------------------!
! EPRC ! Snapshot at 2 seconds interval !
+---------------------------------------------------------------------+

(3) Engine Divergence Report Logic <09> (Engine Type IAE)
+--------------------------------------------------------------------------+
!Code!Item ! ! Progr. !Standard !
! No.!No. ! Description of Function Item !MCDU !Value or !
! ! ! !GSE !MCDU !Table TXY!
!----!------!-----------------------------------------!----!-----!---------!
! !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 (2) ! C ! C ! see !
! ! ! ! ! ! separate!
! ! ! ! ! ! list !
! !E ! Transfer to ACARS MU ! C ! C ! see !
! ! ! ! ! ! separate!
! ! ! ! ! ! list !
! !F ! Increment of the report counter if the ! C ! C ! 1 !
! ! ! report was triggered by a code number ! ! ! !
! ! ! > 1000; 1=yes, 0=no ! ! ! !
! ! ! (Standard programming = 1) ! ! ! !
!----!------!-----------------------------------------!----!-----!---------!
!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 ! Flight Phases (no standard programming) ! C ! C ! not !
! ! ! ! ! ! assigned!
!----!------!-----------------------------------------!----!-----!---------!
!3000!3 ! Programmable Start Logic ! ! ! !
! !3.1 ! Logic algorithm ! C ! ! !
! !3.2 ! Logic criteria values ! C ! ! not !
! ! ! ! ! ! progr. !
!----!------!-----------------------------------------!----!-----!---------!
! !4 ! If during flight phase climb and cruise ! ! ! !
! ! ! (5.1 and 6) the condition as defined ! ! ! !
! ! ! under 4.2 are met the EGT Divergence ! ! ! !
! ! ! (EGTdiv) and TN Divergence (TNdiv) ! ! ! !
! ! ! monitoring function are performed as ! ! ! !
! ! ! defined under item 4.3 to 4.4. ! ! ! !
! ! ! A divergence report is generated each ! ! ! !
! ! ! time the value of EGTdiv or TNdiv ! ! ! !
! ! ! exceeds the defined threshold values ! ! ! !
! ! ! defined below. ! ! ! !
! !4.1 ! Threshold values: ! ! ! !
!4110!4.1.1 ! EGTdivT1 ! C ! C ! T23 !
! ! ! ! ! ! !
!4120!4.1.2 ! EGTdivT2 ! C ! C ! T23 !
! ! ! ! ! ! !
!4130!4.1.3 ! EGTdivT3 ! C ! C ! T23 !
! ! ! ! ! ! !
!4140!4.1.4 ! EGTdivT4 ! C ! C ! T23 !
! ! ! ! ! ! !
!4150!4.1.5 ! TNdivT1 ! C ! C ! T23 !
! ! ! ! ! ! !
!4160!4.1.6 ! TNdivT2 ! C ! C ! T23 !
! ! ! ! ! ! !
!4170!4.1.7 ! TNdivT3 ! C ! C ! T23 !
! ! ! ! ! ! !
!4180!4.1.8 ! TNdivT4 ! C ! C ! T23 !
! ! ! ! ! ! !
! ! ! ! ! ! !
! !4.2 ! Divergence Monitoring Conditions ! ! ! !
! ! ! 1. EPRactual of both engines > EPRL1 ! ! ! !
! ! ! 2. EPRactual of both engines < EPRL2 ! ! ! !
! ! ! 3. EPRactual of both engines is within ! ! ! !
! ! ! EPRL3 of each other. ! ! ! !
! ! ! 4. Bleed loads for both engines are ! ! ! !
! ! ! symmetrical and the crossfeed valve ! ! ! !
! ! ! is closed. ! ! ! !
! ! ! 5. IVV stable within IVVL, (valid during! ! ! !
! ! ! PH 6 only). ! ! ! !
! ! ! 6. ALT < ALTL (valid during PH 5.1 only)! ! ! !
! ! ! 7. Delta TAT within TATL ! ! ! !
! ! ! The Delta TAT is the difference of ! ! ! !
! ! ! TATmin (during last Y09 seconds) and ! ! ! !
! ! ! the TATmax (during last Y09 seconds).! ! ! !
! ! ! 8. EPRrate within EPRRL ! ! ! !
! ! ! The EPRrate is computed by checking ! ! ! !
! ! ! the diference between two samples at ! ! ! !
! ! ! 1 Hz. ! ! ! !
! ! ! 9. SSMS valid during the whole 'Y09.1' ! ! ! !
! ! !10. Conditions 1-9 TRUE for > 'Y09.1' ! ! ! !
! ! ! ! ! ! !
! !4.2.1 ! EPRL1 ! C ! C ! T23 !
! ! ! ! ! ! !
! !4.2.2 ! EPRL2 ! C ! C ! T23 !
! ! ! ! ! ! !
! !4.2.3 ! EPRL3 ! C ! C ! T23 !
! ! ! ! ! ! !
! !4.2.4 ! Symmetrical bleed loads: ! ! ! !
! ! ! ((Valve positions LH and RH must be ! ! ! !
! ! ! identical) AND ! ! ! !
! ! ! (cross feed valve must be closed) AND ! ! ! !
! ! ! (APU valve must be closed OR not ! ! ! !
! ! ! transmitted) AND ! ! ! !
! ! ! (pack flows must be within PFLdelta of ! ! ! !
! ! ! each other)) ! ! ! !
! ! ! 99 1111 1 1111 99 ! ! ! !
! ! ! ! ! ! ! !__ RH Pack Flow ! ! ! !
! ! ! ! ! ! !______ RH Valve pos. ! ! ! !
! ! ! ! ! !_________ Cross feed Valve pos.! ! ! !
! ! ! ! !_____________ LH Valve pos. ! ! ! !
! ! ! !_________________ LH Pack Flow ! ! ! !
! ! ! ! ! ! !
! !4.2.5 ! IVVL ! C ! C ! T23 !
! ! ! ! ! ! !
! !4.2.6 ! ALTL ! C ! C ! T23 !
! ! ! ! ! ! !
! !4.2.7 ! TATL ! C ! C ! T23 !
! ! ! ! ! ! !
! !4.2.8 ! EPRRL ! C ! C ! T23 !
! ! ! ! ! ! !
! !4.2.9 ! 'Y09' ! C ! C ! T23 !
! ! ! ! ! ! !
! !4.2.10! PFLdelta ! C ! C ! T23 !
! ! ! ! ! ! !
! !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 ! The calculations 4.3.2.1 and 4.3.2.2 are! ! ! !
! ! ! performed when the Divergence Monito- ! ! ! !
! ! ! ring Conditions (Item 4.2) are met. ! ! ! !
! !4.3.2.! delta EGTref5 is calculated if the A/C ! ! ! !
! !1 ! has entered flight phase 5.1: ! ! ! !
! ! ! deltaEGTref5 = deltaEGTref5old+ ! ! ! !
! ! ! (deltaEGTm - deltaEGTref5old)! ! ! !
! ! ! -----------------------------! ! ! !
! ! ! K5 + 1 ! ! ! !
! ! ! deltaEGTref5old is the deltaEGTref5 va- ! ! ! !
! ! ! lue from previous flight. ! ! ! !
! ! ! ! ! ! !
! !4.3.2.! delta EGTref6 is calculated if the A/C ! ! ! !
! !2 ! has entered flight phase 6: ! ! ! !
! ! ! deltaEGTref6 = deltaEGTref6old+ ! ! ! !
! ! ! (deltaEGTm - deltaEGTref6old)! ! ! !
! ! ! -----------------------------! ! ! !
! ! ! K6 + 1 ! ! ! !
! ! ! deltaEGTref6old is the deltaEGTref6 va- ! ! ! !
! ! ! lue from previous flight. ! ! ! !
! ! ! ! ! ! !
! ! ! Once the calculation (4.3.2) is per- ! ! ! !
! ! ! formed deltaEGTref5 and deltaEGTref6 ! ! ! !
! ! ! is stored and used for the EGTdiv ! ! ! !
! ! ! calculation (item 4.3.1). ! ! ! !
! !4.3.3 ! M ! ! ! !
! ! ! SIGMA EGTdiff(n) ! ! ! !
! ! ! n=1 ! ! ! !
! ! !deltaEGTm = ---------------- ! ! ! !
! ! ! M ! ! ! !
! ! ! this calculation is done 'M' consecuti- ! ! ! !
! ! ! ve times once per second i.e. during 10 ! ! ! !
! ! ! seconds. ! ! ! !
! !4.3.4 ! EGTdiff = CEGT#1 - EGT#2 ! ! ! !
! ! ! ! ! ! !
! !4.3.5 ! CEGT#1 = EGT#1 + (EPR#2 - EPR#1) * C09.1! ! ! !
! ! ! (or C09.2) ! ! ! !
! ! ! ! ! ! !
! !4.3.6 ! KL ! C ! C ! T23 !
! ! ! ! ! ! !
! !4.3.7 ! C09.1 limit for climb (PH5.1) = 3.2 ! C ! C ! T23 !
! ! ! Deg. C/0.01EPR ! ! ! !
! ! ! ! ! ! !
! !4.3.8 ! C09.2 limit for cruise (PH6) = 3.2 ! C ! C ! T23 !
! ! ! Deg. C/0.01EPR ! ! ! !
! ! ! ! ! ! !
! !4.3.9 ! M = 10 ! C ! C ! T23 !
! ! ! ! ! ! !
! ! ! ! ! ! !
! !4.3.10! - K5 and K6 are incremented by one for ! ! ! !
! ! ! each flight leg until KL is reached. ! ! ! !
! ! ! Then K5 and/or K6 = KL is remained as ! ! ! !
! ! ! long as: ! ! ! !
! ! ! - Engine S/N is not changed ! ! ! !
! ! ! - A/C-ID is not changed ! ! ! !
! ! ! - KL, C and values defined in ! ! ! !
! ! ! 4.1.1 and 4.1.8 are not changed.! ! ! !
! ! ! ! ! ! !
! ! ! - If there is a change as a.m. the K5, ! ! ! !
! ! ! K6, deltaEGTref5old and ! ! ! !
! ! ! deltaEGTref6old will be set to 0. ! ! ! !
! ! ! ! ! ! !
! ! ! - K5, K6, deltaEGTref5old, 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 calculation! ! ! !
! ! ! in flight phase 6 during the entire ! ! ! !
! ! ! flight. ! ! ! !
! ! ! ! ! ! !
! !4.3.11! actual K5 value for PH5.1 printed in ! ! ! !
! ! ! AIDS report limit list. ! ! ! !
! !4.3.12! actual K6 value for PH6 printed in AIDS ! ! ! !
! ! ! report limit list. ! ! ! !
! !4.3.13! actual EGT ref value for PH 5.1 printed ! ! ! !
! ! ! in AIDS report limit list. ! ! ! !
! !4.3.14! actual EGT ref value for PH 6 printed ! ! ! !
! ! ! in AIDS report limit list. ! ! ! !
! !4.3.15! actual TN ref value for PH 5.1 printed ! ! ! !
! ! ! in AIDS report limit list ! ! ! !
! !4.3.16! actual TN ref value for PH 6 printed ! ! ! !
! ! ! in AIDS report limit list. ! ! ! !
! !4.4 ! TN Divergence Calculation ! ! ! !
! !4.4.1 ! TNdiv = deltaTNdiff - deltaTNref ! ! ! !
! !4.4.2 ! deltaTNdiff = TN#1 - TN#2 ! ! ! !
! !4.4.3 ! The calculations4.4.3.1 and 4.4.3.2 ! ! ! !
! ! ! are performed when the Divergence Moni- ! ! ! !
! ! ! toring Conditions (Item 4.2) are met. ! ! ! !
! !4.4.3 ! delta TNref5 is calculated if the A/C ! ! ! !
! !1 ! has entered flight phase 5.1: ! ! ! !
! ! ! ! ! ! !
! ! ! deltaTNref5 = deltaTNref5old+ ! ! ! !
! ! ! (deltaTNm - deltaTNref5old) ! ! ! !
! ! ! -----------------------------! ! ! !
! ! ! K5 + 1 ! ! ! !
! ! ! deltaTNref5old = deltaTNref5 from pre- ! ! ! !
! ! ! vious flight leg. ! ! ! !
! !4.4.3.! ! ! ! !
! !2 ! deltaTNref6 is calculated if the A/C ! ! ! !
! ! ! has entered flight phase 6: ! ! ! !
! ! ! deltaTNref6 = deltaTNref6old+ ! ! ! !
! ! ! (deltaTNm - deltaTNref6old)! ! ! !
! ! ! ---------------------------! ! ! !
! ! ! K6 + 1 ! ! ! !
! ! ! deltaTNref6old = deltaTNref6 from the ! ! ! !
! ! ! previous flight leg. ! ! ! !
! ! ! Once calculation (4.4.3) is performed ! ! ! !
! ! ! deltaTNref5 and deltaTNref6 are stored ! ! ! !
! ! ! and used for the TNdiv calculation ! ! ! !
! ! ! (item 4.4.1). ! ! ! !
! ! ! ! ! ! !
! !4.4.4 ! M ! ! ! !
! ! ! SIGMA TNdiff(n) ! ! ! !
! ! ! n=1 ! ! ! !
! ! !deltaTNTm = ---------------- ! ! ! !
! ! ! M ! ! ! !
! ! ! this calculation is done 'M' consecutive! ! ! !
! ! ! times once per second i.e. during 10 ! ! ! !
! ! ! seconds. ! ! ! !
! ! ! The same rules as (analogue to 4.3.10) ! ! ! !
! ! ! for EGT divergence are applied, except ! ! ! !
! ! ! TN#1 is not correct for deviations in ! ! ! !
! ! ! EPR. ! ! ! !
!----!------!-----------------------------------------!----!-----!---------!
! !5 ! In case of divergence detection and ! ! ! !
! ! ! report generation, the search logic for ! ! ! !
! ! ! the engine cruise report stable frames ! ! ! !
! ! ! is started immediately. ! ! ! !
! ! ! ! ! ! !
! !5.1 ! Logic algorithm ! ! ! !
!----!------!-----------------------------------------!----!-----!---------!
!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>
+-------------------------------------------------------------------------+
!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 !
+-------------------------------------------------------------------------+

O. Engine Start Report <10>
F Engine Start Report <10> (Engine Type IAE) ** 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.
NOTE: For the standard header definition of the report refer to (Ref. AMM D/O 31-36-00-00).
NOTE: If the ESN printed out in the report is in the range between 13191 and 15000, then add 5000 to this value to get the actual ESN.
(1) Engine Start Report Data Field Description <10> (Engine Type IAE)
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 5 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 ! ECU (-55 to 999.9 C) !
! ! Engine 1 7C.1.345.01 !
! ! Engine 2 7C.2.345.10 !
! ! Negative values are shown with '-' on 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 '-' on 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) !
! ! SAV open 7C.1.270.01.15 = 1 Engine 1 !
! ! 7C.2.270.10.15 = 1 Engine 2# !
!--------------!------------------------------------------------------!
! TTP ! Time from SAV open to max EGT or to start abort !
! 999 ! DMU (Time in seconds) !
! ! SAV open 7C.1.270.01.15 = 1 Engine 1 !
! ! 7C.2.270.10.15 = 1 Engine 2 !
!--------------!------------------------------------------------------!
! TTF ! Time from SAV open to Fuel Shut-Off Valve = open !
! 999 ! (Time in seconds) !
! ! Engine 1 7C.1.270.01.15 = 1 = SAV open !
! ! Engine 2 7C.2.270.10.15 = 1 !
! ! Engine 2 7C.1.145.01.16 = 1 = Fuel Shut-Off !
! ! Engine 2 7C.2.145.10.16 = 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 (0 to 15000 p/h) !
! ! EEC Engine 1 7C.1.244.01 !
! ! Engine 2 7C.2.244.10# !
!--------------!------------------------------------------------------!
! PD ! Precooler Inlet Pressure !
! 99 ! !
! ! Report Line N1: Precooler Inlet Pressure at !
! ! 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 !
! ! EEC 7C.1.276.01.28 Engine 1 !
! ! 7C.1.276.10.28 Engine 2# !
!--------------!------------------------------------------------------!
! 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.276.XX.16 = 1 Ignition Failure !
! ! 12 7C.X.276.XX.21 = 1 EIU Start Data Failed !
! ! 13 7C.X.276.XX.25 = 1 Continuous Ignition Active !
! ! 14 7C.X.276.XX.26 = 1 Starter Air Valve Failed !
! ! 15 7C.X.271.XX.19 = 1 7th Bleed #1 Solenoid !
! ! closed !
! ! 16 7C.X.271.XX.20 = 1 7th Bleed #2 Solenoid !
! ! closed !
! ! 17 7C.X.271.XX.21 = 1 10th Bleed Solenoid closed !
! ! 18 7C.X.271.XX.23 = 1 Fuel On Solenoid !
! ! 19 7C.X.271.XX.24 = 1 Fuel Off Solenoid !
! ! 20 7C.X.271.XX.25 = 1 Starter Air Valve Solenoid !
! ! open !
! ! 21 7C.X.271.XX.26 = 1 Ignition Relay #1 De- !
! ! energize. !
! ! 22 7C.X.271.XX.27 = 1 Ignition Relay #2 De- !
! ! energize. !
! ! 23 7C.X.270.XX.15 = 1 Starter Air Valve Position !
! ! not closed !
! ! 24 7C.X.145.XX.15 = 1 Starter Air Valve Position !
! ! failed !
! ! 25 7C.X.145.XX.16 = 1 Fuel On/Off Valve Position !
! ! off !
! ! 26 7C.X.145.XX.17 = 1 Fuel On/Off Valve Position !
! ! failed !
! ! 27 SPARE !
! ! 28 SPARE !
! ! 29 SPARE !
+---------------------------------------------------------------------+

(2) Parameter Logic
+---------------------------------------------------------------------+
! Param. ! Print Value (Standard Progr.) !
!--------------!------------------------------------------------------!
! ESN ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! EHRS ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! ECYC ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! AP ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! Y1 ! Programmed 'Y10.1' pre-event !
!--------------!------------------------------------------------------!
! Y2 ! Programmed 'Y10.2' post-event !
!--------------!------------------------------------------------------!
! E ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! MAX ! Highest value during the 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 !
!--------------!------------------------------------------------------!
! EGT ! Snapshot at Y10.1 and Y10.2 sec. intervals !
!--------------!------------------------------------------------------!
! N1 ! Snapshot at Y10.1 and Y10.2 sec. intervals !
!--------------!------------------------------------------------------!
! N2 ! Snapshot at Y10.1 and Y10.2 sec. intervals !
!--------------!------------------------------------------------------!
! FF ! Snapshot at Y10.1 and Y10.2 sec. intervals !
!--------------!------------------------------------------------------!
! P2 ! Snapshot at Y10.1 and Y10.2 sec. intervals !
!--------------!------------------------------------------------------!
! T25 ! Snapshot at Y10.1 and Y10.2 sec. intervals !
!--------------!------------------------------------------------------!
! PD ! Snapshot at Y10.1 and Y10.2 sec. intervals !
!--------------!------------------------------------------------------!
! P3 ! Snapshot at Y10.1 and Y10.2 sec. intervals !
!--------------!------------------------------------------------------!
! T3 ! Snapshot at Y10.1 and Y10.2 sec. intervals !
!--------------!------------------------------------------------------!
! SVA ! Snapshot at Y10.1 and Y10.2 sec. intervals !
!--------------!------------------------------------------------------!
! BAF ! Snapshot at Y10.1 and Y10.2 sec. intervals !
!--------------!------------------------------------------------------!
! T2 ! Snapshot at Y10.1 and Y10.2 sec. intervals !
!--------------!------------------------------------------------------!
! OIT ! Snapshot at Y10.1 and Y10.2 sec. intervals !
!--------------!------------------------------------------------------!
! ECW5 ! Snapshot at Y10.1 and Y10.2 sec. intervals !
+---------------------------------------------------------------------+

(3) Engine Start Report Logic <10> (Engine Type IAE)
+--------------------------------------------------------------------------+
!Code!Item ! ! Progr .!Standard !
! No.!No. ! Description of Function Item !----------!Value or !
! ! ! !GSE !MCDU !Table TXY!
!----!------!-----------------------------------------!----!-----!---------!
! !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 (2) ! C ! C ! see !
! ! ! ! ! ! separate!
! ! ! ! ! ! list !
! !E ! Transfer to ACARS MU ! C ! C ! see !
! ! ! ! ! ! separate!
! ! ! ! ! ! list !
! !F ! Increment of the report counter if the ! C ! C ! 1 !
! ! ! report was triggered by a code number ! ! ! !
! ! ! > 1000; 1=yes, 0=no ! ! ! !
! ! ! (standard programming = 1) ! ! ! !
! !G ! 'Y10.1' Pre-event print intervals (sec.)! C ! ! 5 !
! !H ! 'Y10.2'Post-event print intervals (sec.)! C ! ! 2 !
! !I ! 'Y10.3' time when Fuel Flow is measured ! A ! A ! 20 !
! ! ! (sec.) ! ! ! !
!----!------!-----------------------------------------!----!-----!---------!
!1000!1 ! Manual selection via MCDU ! ! ! !
!----!------!-----------------------------------------!----!-----!---------!
!2000!2 ! Flight phase dependent manual ! ! ! !
! ! ! selection via remote print button ! ! ! !
! ! ! if programmed. ! ! ! !
! !2.1 ! Logic algorithm ! ! ! !
! !2.2 ! Flight Phase : Engine Start ! C ! ! 1.1 !
!----!------!-----------------------------------------!----!-----!---------!
!3000!3 ! Programmable Start Logic ! ! ! !
! !3.1 ! Logic algorithm ! C ! ! !
! !3.2 ! Logic criteria values ! C ! ! not !
! ! ! ! ! ! progr. !
!----!------!-----------------------------------------!----!-----!---------!
! !4 ! Aborted engine 1 or 2 start detected ! ! ! !
! ! ! by FADEC: ! ! ! !
! ! ! 7C.1.276.01.14 and 7C.2.276.10.14 are ! ! ! !
! ! ! observed. If they are set to 1, then the! ! ! !
! ! ! reason is detected by one of the bits ! ! ! !
! ! ! described as follows: ! ! ! !
! ! ! ! ! ! !
! !4.1 ! Logic algorithm ! ! ! !
! ! ! ! ! ! !
!4410!4.1.1 ! Start Abort ->SAV Fault ! ! ! !
! ! ! param. 7C.1.276.01.26 ! ! ! !
! ! ! param. 7C.2.276.10.26 ! ! ! !
! ! ! or ! ! ! !
!4420!4.1.2 ! Start Abort ->HPSOV Failed ! ! ! !
! ! ! param. 7C.1.276.01.18 ! ! ! !
! ! ! param. 7C.2.276.10.18 ! ! ! !
! ! ! or ! ! ! !
!4430!4.1.3 ! Start Abort ->EGT Overtemperature ! ! ! !
! ! ! param. 7C.1.276.01.17 ! ! ! !
! ! ! param. 7C.2.276.10.17 ! ! ! !
! ! ! or ! ! ! !
!4440!4.1.4 ! Start Abort ->Stall ! ! ! !
! ! ! param. 7C.1.145.01.19 ! ! ! !
! ! ! param. 7C.2.145.10.19 ! ! ! !
! ! ! or ! ! ! !
!4450!4.1.5 ! Start Abort ->Ignition failure ! ! ! !
! ! ! param. 7C.1.276.01.16 ! ! ! !
! ! ! param. 7C.2.276.10.16 ! ! ! !
! ! ! or ! ! ! !
!4460!4.1.6 ! Hung Start ! ! ! !
! ! ! param. 7C.1.276.01.19 ! ! ! !
! ! ! param. 7C.2.276.10.19 ! ! ! !
! ! ! or ! ! ! !
!4470!4.1.7 ! Start Abort ->Start data failed ! ! ! !
! ! ! param. 7C.1.276.01.21 ! ! ! !
! ! ! param. 7C.2.276.10.21 ! ! ! !
! ! ! or ! ! ! !
!4480!4.1.8 ! Slow Start ! ! ! !
! ! ! param. 7C.1.145.01.18 ! ! ! !
! ! ! param. 7C.2.145.10.18 ! ! ! !
!----!------!-----------------------------------------!----!-----!---------!
!5000!5 ! In case of exceedance of EGTL during ! ! ! !
! ! ! appropriate engine start. ! ! ! !
! !5.1 ! EGTL ! C ! C ! T23 !
! ! ! ! ! ! !
!----!------!-----------------------------------------!----!-----!---------!
!6000!6 ! Every 'F10.1'th cycle at the moment when! ! ! !
! ! ! N2 >= N2 trigger during engine start. ! ! ! !
! ! ! 7C.1.344.01 ! ! ! !
! ! ! 7C.2.344.10 ! ! ! !
! !6.1 ! 'F10.1'th cycle ! C ! C ! T23 !
! ! ! ! ! ! !
! !6.2 ! N2 trigger ! C ! C ! T23 !
! ! ! ! ! ! !
! !6.3 ! In this case 4 pre and 7 post event data! ! ! !
! ! ! sets are printed out. ! ! ! !
!----!------!-----------------------------------------!----!-----!---------!
!7001!7 ! A programmable number 'X10' of ! ! ! !
! ! ! consecutive legs. ! ! ! !
!7002! ! ! ! ! !
!7003! ! ! ! ! !
!7004! ! This means: During the next 'X10' legs ! ! ! !
!7005! ! the engine start report is automatically! ! ! !
!. ! ! generated when N2 >= N2trigger during ! ! ! !
!. ! ! appropriate engine start. ! ! ! !
!. ! ! Counter modification and report logic ! ! ! !
!. ! ! are individually for each engine. ! ! ! !
!700X! ! ! ! ! !
! !7.1 ! Logic algorithm ! ! ! !
! !7.2 ! Number 'X10' for consecutive legs ! C ! ! T23 !
! ! ! programmable (up to 9). ! ! ! !
! ! ! ! ! ! !
! !7.3 ! In this case 4 pre and 7 post event data! ! ! !
! ! ! sets are printed out. ! ! ! !
!----!------!-----------------------------------------!----!-----!---------!
!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 >= N2trigger 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>
+-------------------------------------------------------------------------+
!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 !
+-------------------------------------------------------------------------+

Q. Engine Run Up Report <11>
F Engine Run Up Report <11> (Engine Type IAE) ** 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 Remote 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.
NOTE: For the standard header definition of the report refer to (Ref. AMM D/O 31-36-00-00).
NOTE: If the ESN printed out in the report is in the range between 13191 and 15000, then add 5000 to this value to get the actual ESN.
(1) Engine Run Up Report Data Field Description <11> (Engine Type IAE)
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) (0 to 15000 p/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 !
+---------------------------------------------------------------------+

(2) Parameter Logic
+---------------------------------------------------------------------+
! Param. ! Print Value (Standard Progr.) !
!--------------!------------------------------------------------------!
! ESN ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! EHRS ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! ECYC ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! AP ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! EPR ! Arithmetic average for 20 sec. !
!--------------!------------------------------------------------------!
! EGT ! Arithmetic average for 20 sec. !
!--------------!------------------------------------------------------!
! N1 ! Arithmetic average for 20 sec. !
!--------------!------------------------------------------------------!
! N2 ! Arithmetic average for 20 sec. !
!--------------!------------------------------------------------------!
! FF ! Arithmetic average for 20 sec. !
!--------------!------------------------------------------------------!
! P125 ! Arithmetic average for 20 sec. !
!--------------!------------------------------------------------------!
! P25 ! Arithmetic average for 20 sec. !
!--------------!------------------------------------------------------!
! T25 ! Arithmetic average for 20 sec. !
!--------------!------------------------------------------------------!
! P3 ! Arithmetic average for 20 sec. !
!--------------!------------------------------------------------------!
! T3 ! Arithmetic average for 20 sec. !
!--------------!------------------------------------------------------!
! P49 ! Arithmetic average for 20 sec. !
!--------------!------------------------------------------------------!
! SVA ! Arithmetic average for 20 sec. !
!--------------!------------------------------------------------------!
! BAF ! Arithmetic average for 20 sec. !
!--------------!------------------------------------------------------!
! HPT ! Arithmetic average for 20 sec. !
!--------------!------------------------------------------------------!
! LP ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! GLE ! Arithmetic average for 20 sec. !
!--------------!------------------------------------------------------!
! PD ! Arithmetic average for 20 sec. !
!--------------!------------------------------------------------------!
! TN ! Arithmetic average for 20 sec. !
!--------------!------------------------------------------------------!
! P2 ! Arithmetic average for 20 sec. !
!--------------!------------------------------------------------------!
! T2 ! Arithmetic average for 20 sec. !
!--------------!------------------------------------------------------!
! ECW1 ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! ECW2 ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! EVM ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! VB1 ! Arithmetic average for 20 sec. !
!--------------!------------------------------------------------------!
! VB2 ! Arithmetic average for 20 sec. !
!--------------!------------------------------------------------------!
! PHA ! Arithmetic average for 20 sec. !
!--------------!------------------------------------------------------!
! OIP ! Arithmetic average for 20 sec. !
!--------------!------------------------------------------------------!
! OIT ! Arithmetic average for 20 sec. !
!--------------!------------------------------------------------------!
! EGTK ! Arithmetic average for 20 sec. !
!--------------!------------------------------------------------------!
! N1K ! Arithmetic average for 20 sec. !
!--------------!------------------------------------------------------!
! N2K ! Arithmetic average for 20 sec. !
!--------------!------------------------------------------------------!
! FFK ! Arithmetic average for 20 sec. !
+---------------------------------------------------------------------+

(3) Engine Run Up Report Logic <11> (Engine Type IAE)
+--------------------------------------------------------------------------+
!Code!Item ! ! Progr. !Standard !
! No.!No. ! Description of Function Item !----------!Value or !
! ! ! !GSE !MCDU !Table TXY!
!----!------!-----------------------------------------!----!-----!---------!
! !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 ! C ! Blank !
! !D ! Print Out Rules (3) ! C ! C ! see !
! ! ! ! ! ! separate!
! ! ! ! ! ! list !
! !E ! Transfer to ACARS MU ! C ! C ! see !
! ! ! ! ! ! separat !
! ! ! ! ! ! list !
! !F ! Increment of the report counter if the ! C ! C ! 1 !
! ! ! report was triggered by a logic number ! ! ! !
! ! ! > 1000; 1=yes, 0=no ! ! ! !
! ! ! (standard programming = 1) ! ! ! !
! ! ! ! ! ! !
! ! ! Exponents for correction of N1, N2, EGT ! ! ! !
! ! ! and FF ! ! ! !
! ! ! Standard programming: ! ! ! !
! !G1 ! n1 ! A ! ! 0.5 !
! !G2 ! n2 ! A ! ! 1.05 !
! !G3 ! n3 ! A ! ! 0.5 !
! !G4 ! n4 ! A ! ! 0.63 !
!----!------!-----------------------------------------!----!-----!---------!
!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 ! Flight Phases (standard programming: PH ! C ! ! 2 and 3 !
! ! ! 2 and 3) ! ! ! !
!----!------!-----------------------------------------!----!-----!---------!
!3000!3 ! Programmable Start Logic ! ! ! !
! !3.1 ! Logic algorithm ! C ! ! !
! !3.2 ! Logic criteria values ! 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>
+-------------------------------------------------------------------------+
!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 !
+-------------------------------------------------------------------------+

S. Report Limits for Engine Cruise Report <01>
(1) A320: IAE Engines V2500-A1, V2527-A5, V2527E-A5, V2524-A5
+-----------------------------------------------------------------------------+
!Report! Description of Report Item !V2500- !V2527- !V2527E-!V2524- ! Unit !
!Item ! !A1 !A5 !A5 !A5 ! !
! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! !
! ! ! I10001! I20001! I30001! I80001! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.1 ! 'Y01.1' flight hours ! 4 ! 4 ! 4 ! 4 ! hours!
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.2 ! 'Y01.1' minutes after ! 10 ! 10 ! 10 ! 10 ! min !
! ! cruise entry ! ! ! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.3 ! 'Y01.3' flight legs ! 0 ! 0 ! 0 ! 0 ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.1 ! 'P01' stable periods ! 5 ! 5 ! 5 ! 5 ! !
! ! (1 period = 20 seconds) ! ! ! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 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 ! 0.8 ! 0.8 ! 0.8 ! 0.8 ! deg !
! ! variation ! ! ! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.5.1! Weighting Factor WA of the ! 1 ! 1 ! 1 ! 1 ! !
! ! ROLL ANGLE ! ! ! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.6 ! TAT stable frame variation ! 1.1 ! 1.1 ! 1.1 ! 1.1 ! 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 ! 18 ! 18 ! 18 ! deg C!
!------!-------------------------------!-------!-------!-------!-------!------!
!5.8.1 ! Weighting Factor WA of EGT ! 1 ! 1 ! 1 ! 1 ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.9 ! VACC stable frame variation ! 0.03 ! 0.03 ! 0.03 ! 0.03 ! g !
!------!-------------------------------!-------!-------!-------!-------!------!
!5.9.1 ! Weighting Factor WA of VACC ! 1 ! 1 ! 1 ! 1 ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.10 ! MN stable frame variation ! 0.008! 0.008! 0.008! 0.008! Mach !
!------!-------------------------------!-------!-------!-------!-------!------!
!5.10.1! Weighting Factor WA of MN ! 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 ! P2 stable frame variation ! 0.05 ! 0.05 ! 0.05 ! 0.05 ! psia !
!------!-------------------------------!-------!-------!-------!-------!------!
!5.12.1! Weighting Factor WA of P2 ! 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 ! EPR stable frame variation ! 0.035! 0.035! 0.035! 0.035! !
!------!-------------------------------!-------!-------!-------!-------!------!
!5.14.1! Weighting Factor WA of EPR ! 1 ! 1 ! 1 ! 1 ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 6.2 ! Number 'X01' for consecutive ! 5 ! 5 ! 5 ! 5 ! !
! ! reports ! ! ! ! ! !
+-----------------------------------------------------------------------------+

(2) A321: IAE Engines V2530-A5, V2533-A5
+-----------------------------------------------------------------------------+
!Report! Description of Report Item !V2530- !V2533- ! SPARE ! SPARE ! Unit !
!Item ! !A5 !A5 ! ! ! !
! ! !DMU/ID !DMU/ID ! ! ! !
! ! ! I50001! I60001! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.1 ! 'Y01.1' flight hours ! 4 ! 4 ! ! ! hours!
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.2 ! 'Y01.2' minutes after ! 10 ! 10 ! ! ! min !
! ! cruise entry ! ! ! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.3 ! 'Y01.3' flight legs ! 0 ! 0 ! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.1 ! 'P01' stable periods ! 5 ! 5 ! ! ! !
! ! (1 period = 20 seconds) ! ! ! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 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 ! 0.8 ! 0.8 ! ! ! deg !
! ! variation ! ! ! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.5.1! Weighting Factor WA of the ! 1 ! 1 ! ! ! !
! ! ROLL ANGLE ! ! ! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.6 ! TAT stable frame variation ! 1.1 ! 1.1 ! ! ! 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 ! 18 ! ! ! deg C!
!------!-------------------------------!-------!-------!-------!-------!------!
!5.8.1 ! Weighting Factor WA of EGT ! 1 ! 1 ! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.9 ! VACC stable frame variation ! 0.03 ! 0.03 ! ! ! g !
!------!-------------------------------!-------!-------!-------!-------!------!
!5.9.1 ! Weighting Factor WA of VACC ! 1 ! 1 ! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.10 ! MN stable frame variation ! 0.008! 0.008! ! ! Mach !
!------!-------------------------------!-------!-------!-------!-------!------!
!5.10.1! Weighting Factor WA of MN ! 1 ! 1 ! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.11 ! N1 stable frame variation ! 1.6 ! 1.6 ! ! ! % !
!------!-------------------------------!-------!-------!-------!-------!------!
!5.11.1! Weighting Factor WA of N1 ! 1 ! 1 ! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.12 ! P2 stable frame variation ! 0.05 ! 0.05 ! ! ! psia !
!------!-------------------------------!-------!-------!-------!-------!------!
!5.12.1! Weighting Factor WA of P2 ! 1 ! 1 ! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.13 ! FF stable frame variation ! 100 ! 100 ! ! ! kg/h !
!------!-------------------------------!-------!-------!-------!-------!------!
!5.13.1! Weighting Factor WA of FF ! 1 ! 1 ! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.14 ! EPR stable frame variation ! 0.035! 0.035! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
!5.14.1! Weighting Factor WA of EPR ! 1 ! 1 ! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 6.2 ! Number 'X01' for consecutive ! 5 ! 5 ! ! ! !
! ! reports ! ! ! ! ! !
+-----------------------------------------------------------------------------+


(3) A319: IAE Engines V2522-A5, V2524-A5, V2527M-A5
+-----------------------------------------------------------------------------+
!Report! Description of Report Item !V2522- !V2524- !V2527M-! SPARE ! Unit !
!Item ! !A5 !A5 !A5 ! ! !
! ! !DMU/ID !DMU/ID !DMU/ID ! ! !
! ! ! I70001! I80001! I60001! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.1 ! 'Y01.1' flight hours ! 4 ! 4 ! 4 ! ! hours!
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.2 ! 'Y01.2' minutes after ! 10 ! 10 ! 10 ! ! min !
! ! cruise entry ! ! ! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.3 ! 'Y01.3' flight legs ! 0 ! 0 ! 0 ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.1 ! 'P01' stable periods ! 5 ! 5 ! 5 ! ! !
! ! (1 period = 20 seconds) ! ! ! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.3 ! IALT stable frame variation ! 150 ! 150 ! 150 ! ! ft !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.3.1! Weighting Factor WA of IALT ! 1 ! 1 ! 1 ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.4 ! GS stable frame variation ! 6 ! 6 ! 6 ! ! kts !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.4.1! Weighting Factor WA of GS ! 1 ! 1 ! 1 ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.5 ! ROLL ANGLE stable frame ! 0.8 ! 0.8 ! 0.8 ! ! deg !
! ! variation ! ! ! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.5.1! Weighting Factor WA of the ! 1 ! 1 ! 1 ! ! !
! ! ROLL ANGLE ! ! ! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.6 ! TAT stable frame variation ! 1.1 ! 1.1 ! 1.1 ! ! deg C!
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.6.1! Weighting Factor WA of TAT ! 1 ! 1 ! 1 ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.7 ! N2 stable frame variation ! 0.9 ! 0.9 ! 0.9 ! ! % !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.7.1! Weighting Factor WA of N2 ! 1 ! 1 ! 1 ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.8 ! EGT stable frame variation ! 18 ! 18 ! 18 ! ! deg C!
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.8.1! Weighting Factor WA of EGT ! 1 ! 1 ! 1 ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.9 ! VACC stable frame variation ! 0.03 ! 0.03 ! 0.03 ! ! g !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.9.1! Weighting Factor WA of VACC ! 1 ! 1 ! 1 ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.10 ! MN stable frame variation ! 0.008! 0.008! 0.008! ! Mach !
!------!-------------------------------!-------!-------!-------!-------!------!
!5.10.1! Weighting Factor WA of MN ! 1 ! 1 ! 1 ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.11 ! N1 stable frame variation ! 1.6 ! 1.6 ! 1.6 ! ! % !
!------!-------------------------------!-------!-------!-------!-------!------!
!5.11.1! Weighting Factor WA of N1 ! 1 ! 1 ! 1 ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.12 ! P2 stable frame variation ! 0.05 ! 0.05 ! 0.05 ! ! psia !
!------!-------------------------------!-------!-------!-------!-------!------!
!5.12.1! Weighting Factor WA of P2 ! 1 ! 1 ! 1 ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.13 ! FF stable frame variation ! 100 ! 100 ! 100 ! ! kg/h !
!------!-------------------------------!-------!-------!-------!-------!------!
!5.13.1! Weighting Factor WA of FF ! 1 ! 1 ! 1 ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.14 ! EPR stable frame variation ! 0.035! 0.035! 0.035! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
!5.14.1! Weighting Factor WA of EPR ! 1 ! 1 ! 1 ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 6.2 ! Number 'X01' for consecutive ! 5 ! 5 ! 5 ! ! !
! ! reports ! ! ! ! ! !
+-----------------------------------------------------------------------------+

T. Report Limits for Cruise Performance Report <02>
(1) A320: IAE Engines V2500-A1, V2527-A5, V2527E-A5, V2524-A5
+-----------------------------------------------------------------------------+
!Report! Description of Report Item !V2500- !V2527- !V2527E-!V2524- ! Unit !
!Item ! !A1 !A5 !A5 !A5 ! !
! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! !
! ! ! I10001! I20001! I30001! I80001! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.2 ! 'Y02.1' flight hours ! 1 ! 1 ! 1 ! 1 ! hours!
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.4 ! 'P02' stable periods ! 5 ! 5 ! 5 ! 5 ! !
! ! (1 period = 20 seconds) ! ! ! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.6 ! IALT stable frame variation ! 150 ! 150 ! 150 ! 150 ! ft !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.6.1! Weighting Factor WA of IALT ! 1 ! 1 ! 1 ! 1 ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.7 ! GS stable frame variation ! 6 ! 6 ! 6 ! 6 ! kts !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.7.1! Weighting Factor WA of GS ! 1 ! 1 ! 1 ! 1 ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.8 ! ROLL ANGLE stable frame ! 0.8 ! 0.8 ! 0.8 ! 0.8 ! deg !
! ! variation ! ! ! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.8.1! Weighting Factor WA of the ! 1 ! 1 ! 1 ! 1 ! !
! ! ROLL ANGLE ! ! ! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.9 ! TAT stable frame variation ! 1.1 ! 1.1 ! 1.1 ! 1.1 ! deg C!
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.9.1! Weighting Factor WA of TAT ! 1 ! 1 ! 1 ! 1 ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.10 ! N2 stable frame variation ! 0.9 ! 0.9 ! 0.9 ! 0.9 ! % !
!------!-------------------------------!-------!-------!-------!-------!------!
!5.10.1! Weighting Factor WA of N2 ! 1 ! 1 ! 1 ! 1 ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.11 ! EGT stable frame variation ! 18 ! 18 ! 18 ! 18 ! deg C!
!------!-------------------------------!-------!-------!-------!-------!------!
!5.11.1! Weighting Factor WA of EGT ! 1 ! 1 ! 1 ! 1 ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.12 ! VACC stable frame variation ! 0.03 ! 0.03 ! 0.03 ! 0.03 ! g !
!------!-------------------------------!-------!-------!-------!-------!------!
!5.12.1! Weighting Factor WA of VACC ! 1 ! 1 ! 1 ! 1 ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.13 ! MN stable frame variation ! 0.008! 0.008! 0.008! 0.008! Mach !
!------!-------------------------------!-------!-------!-------!-------!------!
!5.13.1! Weighting Factor WA of MN ! 1 ! 1 ! 1 ! 1 ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.14 ! N1 stable frame variation ! 1.6 ! 1.6 ! 1.6 ! 1.6 ! % !
!------!-------------------------------!-------!-------!-------!-------!------!
!5.14.1! Weighting Factor WA of N1 ! 1 ! 1 ! 1 ! 1 ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.15 ! P2 stable frame variation ! 0.05 ! 0.05 ! 0.05 ! 0.05 ! psia !
!------!-------------------------------!-------!-------!-------!-------!------!
!5.15.1! Weighting Factor WA of P2 ! 1 ! 1 ! 1 ! 1 ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.16 ! FF stable frame variation ! 100 ! 100 ! 100 ! 100 ! kg/h !
!------!-------------------------------!-------!-------!-------!-------!------!
!5.16.1! Weighting Factor WA of FF ! 1 ! 1 ! 1 ! 1 ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.17 ! EPR stable frame variation ! 0.035! 0.035! 0.035! 0.035! !
!------!-------------------------------!-------!-------!-------!-------!------!
!5.17.1! Weighting Factor WA of EPR ! 1 ! 1 ! 1 ! 1 ! !
+-----------------------------------------------------------------------------+

(2) A321: IAE Engines V2530-A5, V2533-A5
+-----------------------------------------------------------------------------+
!Report! Description of Report Item !V2530- !V2533- ! SPARE ! SPARE ! Unit !
!Item ! !A5 !A5 ! ! ! !
! ! !DMU/ID !DMU/ID ! ! ! !
! ! ! I50001! I60001! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.2 ! 'Y02.1' flight hours ! 1 ! 1 ! ! ! hours!
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.4 ! 'P02' stable periods ! 5 ! 5 ! ! ! !
! ! (1 period = 20 seconds) ! ! ! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.6 ! IALT stable frame variation ! 150 ! 150 ! ! ! ft !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.6.1! Weighting Factor WA of IALT ! 1 ! 1 ! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.7 ! GS stable frame variation ! 6 ! 6 ! ! ! kts !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.7.1! Weighting Factor WA of GS ! 1 ! 1 ! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.8 ! ROLL ANGLE stable frame ! 0.8 ! 0.8 ! ! ! deg !
! ! variation ! ! ! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.8.1! Weighting Factor WA of the ! 1 ! 1 ! ! ! !
! ! ROLL ANGLE ! ! ! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.9 ! TAT stable frame variation ! 1.1 ! 1.1 ! ! ! deg C!
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.9.1! Weighting Factor WA of TAT ! 1 ! 1 ! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.10 ! N2 stable frame variation ! 0.9 ! 0.9 ! ! ! % !
!------!-------------------------------!-------!-------!-------!-------!------!
!5.10.1! Weighting Factor WA of N2 ! 1 ! 1 ! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.11 ! EGT stable frame variation ! 18 ! 18 ! ! ! deg C!
!------!-------------------------------!-------!-------!-------!-------!------!
!5.11.1! Weighting Factor WA of EGT ! 1 ! 1 ! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.12 ! VACC stable frame variation ! 0.03 ! 0.03 ! ! ! g !
!------!-------------------------------!-------!-------!-------!-------!------!
!5.12.1! Weighting Factor WA of VACC ! 1 ! 1 ! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.13 ! MN stable frame variation ! 0.008! 0.008! ! ! Mach !
!------!-------------------------------!-------!-------!-------!-------!------!
!5.13.1! Weighting Factor WA of MN ! 1 ! 1 ! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.14 ! N1 stable frame variation ! 1.6 ! 1.6 ! ! ! % !
!------!-------------------------------!-------!-------!-------!-------!------!
!5.14.1! Weighting Factor WA of N1 ! 1 ! 1 ! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.15 ! P2 stable frame variation ! 0.05 ! 0.05 ! ! ! psia !
!------!-------------------------------!-------!-------!-------!-------!------!
!5.15.1! Weighting Factor WA of P2 ! 1 ! 1 ! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.16 ! FF stable frame variation ! 100 ! 100 ! ! ! kg/h !
!------!-------------------------------!-------!-------!-------!-------!------!
!5.16.1! Weighting Factor WA of FF ! 1 ! 1 ! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.17 ! EPR stable frame variation ! 0.035! 0.035! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
!5.17.1! Weighting Factor WA of EPR ! 1 ! 1 ! ! ! !
+-----------------------------------------------------------------------------+

(3) A319: IAE Engines V2522-A5, V2524-A5, V2527M-A5
+-----------------------------------------------------------------------------+
!Report! Description of Report Item !V2522- !V2524- !V2527M-! SPARE ! Unit !
!Item ! !A5 !A5 !A5 ! ! !
! ! !DMU/ID !DMU/ID !DMU/ID ! ! !
! ! ! I70001! I80001! I60001! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.2 ! 'Y02.1' flight hours ! 1 ! 1 ! 1 ! ! hours!
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.4 ! 'P02' stable periods ! 5 ! 5 ! 5 ! ! !
! ! (1 period = 20 seconds) ! ! ! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.6 ! IALT stable frame variation ! 150 ! 150 ! 150 ! ! ft !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.6.1! Weighting Factor WA of IALT ! 1 ! 1 ! 1 ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.7 ! GS stable frame variation ! 6 ! 6 ! 6 ! ! kts !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.7.1! Weighting Factor WA of GS ! 1 ! 1 ! 1 ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.8 ! ROLL ANGLE stable frame ! 0.8 ! 0.8 ! 0.8 ! ! deg !
! ! variation ! ! ! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.8.1! Weighting Factor WA of the ! 1 ! 1 ! 1 ! ! !
! ! ROLL ANGLE ! ! ! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.9 ! TAT stable frame variation ! 1.1 ! 1.1 ! 1.1 ! ! deg C!
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.9.1! Weighting Factor WA of TAT ! 1 ! 1 ! 1 ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.10 ! N2 stable frame variation ! 0.9 ! 0.9 ! 0.9 ! ! % !
!------!-------------------------------!-------!-------!-------!-------!------!
!5.10.1! Weighting Factor WA of N2 ! 1 ! 1 ! 1 ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.11 ! EGT stable frame variation ! 18 ! 18 ! 18 ! ! deg C!
!------!-------------------------------!-------!-------!-------!-------!------!
!5.11.1! Weighting Factor WA of EGT ! 1 ! 1 ! 1 ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.12 ! VACC stable frame variation ! 0.03 ! 0.03 ! 0.03 ! ! g !
!------!-------------------------------!-------!-------!-------!-------!------!
!5.12.1! Weighting Factor WA of VACC ! 1 ! 1 ! 1 ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.13 ! MN stable frame variation ! 0.008! 0.008! 0.008! ! Mach !
!------!-------------------------------!-------!-------!-------!-------!------!
!5.13.1! Weighting Factor WA of MN ! 1 ! 1 ! 1 ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.14 ! N1 stable frame variation ! 1.6 ! 1.6 ! 1.6 ! ! % !
!------!-------------------------------!-------!-------!-------!-------!------!
!5.14.1! Weighting Factor WA of N1 ! 1 ! 1 ! 1 ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.15 ! P2 stable frame variation ! 0.05 ! 0.05 ! 0.05 ! ! psia !
!------!-------------------------------!-------!-------!-------!-------!------!
!5.15.1! Weighting Factor WA of P2 ! 1 ! 1 ! 1 ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.16 ! FF stable frame variation ! 100 ! 100 ! 100 ! ! kg/h !
!------!-------------------------------!-------!-------!-------!-------!------!
!5.16.1! Weighting Factor WA of FF ! 1 ! 1 ! 1 ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.17 ! EPR stable frame variation ! 0.035! 0.035! 0.035! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
!5.17.1! Weighting Factor WA of EPR ! 1 ! 1 ! 1 ! ! !
+-----------------------------------------------------------------------------+

U. Report Limits for Engine T/O Report <04>
(1) A320: IAE V2500-A1, V2527-A5, V2527E-A5, V2524-A5
+-----------------------------------------------------------------------------+
!Report! Description of Report Item !V2500- !V2527- !V2527E-!V2524- ! Unit !
!Item ! !A1 !A5 !A5 !A5 ! !
! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! !
! ! ! I10001! I20001! I30001! I80001! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.1.5! EGTL temperature limit cold ! 0 ! 0 ! 0 ! 0 ! deg C!
! ! engine start detection ! ! ! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.2 ! 'F04'th Take Off ! 5 ! 5 ! 5 ! 5 ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.3 ! 'Y04.1' seconds after PH4 ! 50 ! 50 ! 50 ! 50 ! sec !
! ! entry ! ! ! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.4.1! Delta EPR ! >0.1 ! >0.1 ! >0.1 ! >0.1 ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.4.2! Delta EPR ! 0.075 ! 0.075 ! 0.075 ! 0.075 ! !
! ! ! ...0.1! ...0.1! ...0.1! ...0.1! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.4.3! Delta EPR !0.05...!0.05...!0.05...!0.05...! !
! ! ! 0.075 ! 0.075 ! 0.075 ! 0.075! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.4.4! Delta EPR !0.03...!0.03...!0.03...!0.03...! !
! ! ! 0.05 ! 0.05 ! 0.05 ! 0.05 ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.4.5! Delta EPR !0.02...!0.02...!0.02...!0.02...! !
! ! ! 0.03 ! 0.03 ! 0.03 ! 0.03 ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.4.6! Delta EPR !0.01...!0.01...!0.01...!0.01...! !
! ! ! 0.02 ! 0.02 ! 0.02 ! 0.02 ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.4.7! Delta EPR !</=0.01!</=0.01!</=0.01!</=0.01! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.5.1! 'Y04.3' seconds after PH4 ! 5 ! 5 ! 5 ! 5 ! sec !
! ! entry ! ! ! ! ! !
! ! calculation of EPR summary ! ! ! ! ! !
! ! limits ! ! ! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.2 ! Number 'X04' for consecutive ! 5 ! 5 ! 5 ! 5 ! !
! ! legs ! ! ! ! ! !
+-----------------------------------------------------------------------------+

(2) A321: IAE V2530-A5, V2533-A5
+-----------------------------------------------------------------------------+
!Report! Description of Report Item !V2530- !V2533- ! SPARE ! SPARE ! Unit !
!Item ! !A5 !A5 ! ! ! !
! ! !DMU/ID !DMU/ID ! ! ! !
! ! ! I50001! I60001! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.1.5! EGTL temperature limit cold ! 0 ! 0 ! ! ! deg C!
! ! engine start detection ! ! ! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.2 ! 'F04'th Take Off ! 5 ! 5 ! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.3 ! 'Y04.1' seconds after PH4 ! 50 ! 50 ! ! ! sec !
! ! entry ! ! ! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.4.1! Delta EPR ! >0.1 ! >0.1 ! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.4.2! Delta EPR ! 0.075 ! 0.075 ! ! ! !
! ! ! ...0.1! ...0.1! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.4.3! Delta EPR !0.05...!0.05...! ! ! !
! ! ! 0.075 ! 0.075 ! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.4.4! Delta EPR !0.03...!0.03...! ! ! !
! ! ! 0.05 ! 0.05 ! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.4.5! Delta EPR !0.02...!0.02...! ! ! !
! ! ! 0.03 ! 0.03 ! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.4.6! Delta EPR !0.01...!0.01...! ! ! !
! ! ! 0.02 ! 0.02 ! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.4.7! Delta EPR !</=0.01!</=0.01! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.5.1! 'Y04.2' seconds after PH4 ! 5 ! 5 ! ! ! sec !
! ! entry ! ! ! ! ! !
! ! calculation of EPR summary ! ! ! ! ! !
! ! limits ! ! ! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.2 ! Number 'X04' for consecutive ! 5 ! 5 ! ! ! !
! ! legs ! ! ! ! ! !
+-----------------------------------------------------------------------------+

(3) A319: IAE V2522-A5, V2524-A5, V2527M-A5
+-----------------------------------------------------------------------------+
!Report! Description of Report Item !V2522- !V2524- !V2527M-! SPARE ! Unit !
!Item ! !A5 !A5 !A5 ! ! !
! ! !DMU/ID !DMU/ID !DMU/ID ! ! !
! ! ! I70001! I80001! I60001! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.1.5! EGTL temperature limit cold ! 0 ! 0 ! 0 ! ! deg C!
! ! engine start detection ! ! ! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.2 ! 'F04'th Take Off ! 5 ! 5 ! 5 ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.3 ! 'Y04.1' seconds after PH4 ! 50 ! 50 ! 50 ! ! sec !
! ! entry ! ! ! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.4.1! Delta EPR ! >0.1 ! >0.1 ! >0.1 ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.4.2! Delta EPR ! 0.075 ! 0.075 ! 0.075 ! ! !
! ! ! ...0.1! ...0.1! ...0.1! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.4.3! Delta EPR !0.05...!0.05...!0.05...! ! !
! ! ! 0.075 ! 0.075 ! 0.075 ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.4.4! Delta EPR !0.03...!0.03...!0.03...! ! !
! ! ! 0.05 ! 0.05 ! 0.05 ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.4.5! Delta EPR !0.02...!0.02...!0.02...! ! !
! ! ! 0.03 ! 0.03 ! 0.03 ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.4.6! Delta EPR !0.01...!0.01...!0.01...! ! !
! ! ! 0.02 ! 0.02 ! 0.02 ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.4.7! Delta EPR !</=0.01!</=0.01!</=0.01! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.5.1! 'Y04.2' seconds after PH4 ! 5 ! 5 ! 5 ! ! sec !
! ! entry ! ! ! ! ! !
! ! calculation of EPR summary ! ! ! ! ! !
! ! limits ! ! ! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.2 ! Number 'X04' for consecutive ! 5 ! 5 ! 5 ! ! !
! ! legs ! ! ! ! ! !
+-----------------------------------------------------------------------------+

V. Report Limits for Engine Report On Request <05>
(1) A320: IAE Engines V2500-A1, V2527-A5, V2527E-A5, V2524-A5
+-----------------------------------------------------------------------------+
!Report! Description of Report Item !V2500- !V2527- !V2527E-!V2524- ! Unit !
!Item ! !A1 !A5 !A5 !A5 ! !
! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! !
! ! ! I10001! I20001! I30001! I80001! !
!------!-------------------------------!-------!-------!-------!-------!------!
! !
! Not Applicable !
! !
+-----------------------------------------------------------------------------+

(2) A321: IAE Engines V2530-A5, V2533-A5
+-----------------------------------------------------------------------------+
!Report! Description of Report Item !V2530- !V2533- ! SPARE ! SPARE ! Unit !
!Item ! !A5 !A5 ! ! ! !
! ! !DMU/ID !DMU/ID ! ! ! !
! ! ! I50001! I60001! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! !
! Not Applicable !
! !
+-----------------------------------------------------------------------------+

(3) A319: IAE Engines V2522-A5, V2524-A5, V2527M-A5
+-----------------------------------------------------------------------------+
!Report! Description of Report Item !V2522- !V2524- !V2527M-! SPARE ! Unit !
!Item ! !A5 !A5 !A5 ! ! !
! ! !DMU/ID !DMU/ID !DMU/ID ! ! !
! ! ! I70001! I80001! I60001! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! !
! Not Applicable !
! !
+-----------------------------------------------------------------------------+

W. Report Limits for Engine Gas Path Advisory Report <06>
(1) A320: IAE Engines V2500-A1, V2527-A5, V2527E-A5, V2524-A5
+-----------------------------------------------------------------------------+
!Report! Description of Report Item !V2500- !V2527- !V2527E-!V2524- ! Unit !
!Item ! !A1 !A5 !A5 !A5 ! !
! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! !
! ! ! I10001! I20001! I30001! I80001! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.1 ! EGTL1 limit (red limit) ! 635 ! 635 ! 635 ! 635 ! deg C!
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.2 ! EGTL2 limit (yellow limit) ! 610 ! 610 ! 610 ! 635 ! deg C!
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.3 ! Not applicable ! ! ! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.5 ! N1L1.1 limit (red limit) ! 100 ! 100 ! 100 ! 100 ! %rpm !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.7 ! N2L1.1 limit (red limit) ! 100 ! 100 ! 100 ! 100 ! %rpm !
+-----------------------------------------------------------------------------+

(2) A321: IAE Engines V2530-A5, V2533-A5
+-----------------------------------------------------------------------------+
!Report! Description of Report Item !V2530- !V2533- ! SPARE ! SPARE ! Unit !
!Item ! !A5 !A5 ! ! ! !
! ! !DMU/ID !DMU/ID ! ! ! !
! ! ! I50001! I60001! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.1 ! EGTL1 limit (red limit) ! 650 ! 650 ! ! ! deg C!
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.2 ! EGTL2 limit (amber limit) ! 610 ! 610 ! ! ! deg C!
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.3 ! Not applicable ! ! ! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.5 ! N1L1.1 limit (red limit) ! 100 ! 100 ! ! ! %rpm !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.7 ! N2L1.1 limit (red limit) ! 100 ! 100 ! ! ! %rpm !
+-----------------------------------------------------------------------------+

(3) A319: IAE Engines V2522-A5, V2524-A5, V2527M-A5
+-----------------------------------------------------------------------------+
!Report! Description of Report Item !V2522- !V2524- !V2527M-! SPARE ! Unit !
!Item ! !A5 !A5 !A5 ! ! !
! ! !DMU/ID !DMU/ID !DMU/ID ! ! !
! ! ! I70001! I80001! I60001! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.1 ! EGTL1 limit (red limit) ! 635 ! 635 ! 635 ! ! deg C!
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.2 ! EGTL2 limit (amber limit) ! 610 ! 610 ! 610 ! ! deg C!
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.3 ! Not applicable ! ! ! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.5 ! N1L1.1 limit (red limit) ! 100 ! 100 ! 100 ! ! %rpm !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.7 ! N2L1.1 limit (red limit) ! 100 ! 100 ! 100 ! ! %rpm !
+-----------------------------------------------------------------------------+

X. Report Limits for Engine Mechanical Advisory Report <07>
(1) A320: IAE Engines V2500-A1, V2527-A5, V2527E-A5, V2524-A5
+-----------------------------------------------------------------------------+
!Report! Description of Report Item !V2500- !V2527- !V2527E-!V2524- ! Unit !
!Item ! !A1 !A5 !A5 !A5 ! !
! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! !
! ! ! I10001! I20001! I30001! I80001! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.1.1! OITL1 limit (red limit) ! 165 ! 165 ! 165 ! 165 ! deg C!
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.1.2! OITL2 limit (yellow limit) ! 155 ! 155 ! 155 ! 155 ! deg C!
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.1.4! 'Y07.3' time limit ! 15 ! 15 ! 15 ! 15 ! min. !
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.2.1! OIPL1.1 limits ! ! ! ! ! !
! ! N2L2.1: 0% rpm ! 0 ! 0 ! 0 ! 0 ! psia !
! ! 59% rpm ! 0 ! 0 ! 0 ! 0 ! psia !
! ! 60% rpm ! 80 ! 80 ! 80 ! 80 ! psia !
! ! 90% rpm ! 80 ! 80 ! 80 ! 80 ! psia !
! ! 100% rpm ! 80 ! 80 ! 80 ! 80 ! psia !
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.2.2! OIPL1.2 limits ! ! ! ! ! !
! ! N2L2.2: 60% rpm ! 80 ! 80 ! 80 ! 80 ! psia !
! ! 70% rpm ! 80 ! 80 ! 80 ! 80 ! psia !
! ! 80% rpm ! 80 ! 80 ! 80 ! 80 ! psia !
! ! 90% rpm ! 80 ! 80 ! 80 ! 80 ! psia !
! ! 100% rpm ! 80 ! 80 ! 80 ! 80 ! psia !
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.2.3! OIPL2 limit ! 390 ! 390 ! 390 ! 390 ! psi !
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.3 ! PSBLim ! 175 ! 175 ! 175 ! 175 ! psia !
+-----------------------------------------------------------------------------+

(2) A321: IAE Engines V2530-A5, V2533-A5
+-----------------------------------------------------------------------------+
!Report! Description of Report Item !V2530- !V2533- ! SPARE ! SPARE ! Unit !
!Item ! !A5 !A5 ! ! ! !
! ! !DMU/ID !DMU/ID ! ! ! !
! ! ! I50001! I60001! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.1.1! OITL1 limit (red limit) ! 165 ! 165 ! ! ! deg C!
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.1.2! OITL2 limit (yellow limit) ! 155 ! 155 ! ! ! deg C!
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.1.4! 'Y07.3' time limit ! 15 ! 15 ! ! ! min. !
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.2.1! OIPL1.1 limits ! ! ! ! ! !
! ! N2L2.1: 0% rpm ! 0 ! 0 ! ! ! psia !
! ! 59% rpm ! 0 ! 0 ! ! ! psia !
! ! 60% rpm ! 80 ! 80 ! ! ! psia !
! ! 90% rpm ! 80 ! 80 ! ! ! psia !
! ! 100% rpm ! 80 ! 80 ! ! ! psia !
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.2.2! OIPL1.2 limits ! ! ! ! ! !
! ! N2L2.2: 60% rpm ! 80 ! 80 ! ! ! psia !
! ! 70% rpm ! 80 ! 80 ! ! ! psia !
! ! 80% rpm ! 80 ! 80 ! ! ! psia !
! ! 90% rpm ! 80 ! 80 ! ! ! psia !
! ! 100% rpm ! 80 ! 80 ! ! ! psia !
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.2.3! OIPL2 limit ! 390 ! 390 ! ! ! psi !
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.3 ! PSBLim ! 175 ! 175 ! ! ! psia !
+-----------------------------------------------------------------------------+

(3) A319: IAE Engines V2522-A5, V2524-A5, V2527M-A5
+-----------------------------------------------------------------------------+
!Report! Description of Report Item !V2522- !V2524- !V2527M-! SPARE ! Unit !
!Item ! !A5 !A5 !A5 ! ! !
! ! !DMU/ID !DMU/ID !DMU/ID ! ! !
! ! ! I70001! I80001! I60001! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.1.1! OITL1 limit (red limit) ! 165 ! 165 ! 165 ! ! deg C!
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.1.2! OITL2 limit (yellow limit) ! 155 ! 155 ! 155 ! ! deg C!
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.1.4! 'Y07.3' time limit ! 15 ! 15 ! 15 ! ! min. !
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.2.1! OIPL1.1 limits ! ! ! ! ! !
! ! N2L2.1: 0% rpm ! 0 ! 0 ! 0 ! ! psia !
! ! 59% rpm ! 0 ! 0 ! 0 ! ! psia !
! ! 60% rpm ! 80 ! 80 ! 80 ! ! psia !
! ! 90% rpm ! 80 ! 80 ! 80 ! ! psia !
! ! 100% rpm ! 80 ! 80 ! 80 ! ! psia !
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.2.2! OIPL1.2 limits ! ! ! ! ! !
! ! N2L2.2: 60% rpm ! 80 ! 80 ! 80 ! ! psia !
! ! 70% rpm ! 80 ! 80 ! 80 ! ! psia !
! ! 80% rpm ! 80 ! 80 ! 80 ! ! psia !
! ! 90% rpm ! 80 ! 80 ! 80 ! ! psia !
! ! 100% rpm ! 80 ! 80 ! 80 ! ! psia !
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.2.3! OIPL2 limit ! 390 ! 390 ! 390 ! ! psi !
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.3 ! PSBLim ! 544 ! 544 ! 544 ! ! psia !
+-----------------------------------------------------------------------------+

Y. Report Limits for Engine Divergence Report <09>
(1) A320: IAE Engines V2500-A1, V2527-A5, V2527E-A5, V2524-A5
+-----------------------------------------------------------------------------+
!Report! Description of Report Item !V2500- !V2527- !V2527E-!V2524 - Unit !
!Item ! !A1 !A5 !A5 !A5 ! !
! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! !
! ! ! I10001! I20001! I30001! I80001! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.1.1! EGTdivT1 limit ! 15 ! 15 ! 15 ! 15 ! deg C!
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.1.2! EGTdivT2 limit ! 20 ! 20 ! 20 ! 20 ! deg C!
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.1.3! EGTdivT3 limit ! 30 ! 30 ! 30 ! 30 ! deg C!
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.1.4! EGTdivT4 limit ! 40 ! 40 ! 40 ! 40 ! deg C!
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.1.5! TNdivT1 limit ! 100 ! 100 ! 100 ! 100 ! deg C!
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.1.6! TNdivT2 limit ! 150 ! 150 ! 150 ! 150 ! deg C!
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.1.7! TNdivT3 limit ! 200 ! 200 ! 200 ! 200 ! deg C!
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.1.8! TNdivT4 limit ! 250 ! 250 ! 250 ! 250 ! deg C!
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.2.1! EPRL1 limit ! 1.05 ! 1.05 ! 1.05 ! 1.05 ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.2.2! EPRL2 limit ! 1.45 ! 1.45 ! 1.45 ! 1.45 ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.2.3! EPRL3 limit ! 0.025! 0.025! 0.025! 0.025! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.2.5! IVVL limit (valid during ! 150 ! 150 ! 150 ! 150 !ft/min!
! ! flight phase 6) ! ! ! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 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! EPRRL limit ! 2 ! 2 ! 2 ! 2 ! 1/sec!
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.2.9! 'Y09' time interval ! 10 ! 10 ! 10 ! 10 ! sec. !
!------!-------------------------------!-------!-------!-------!-------!------!
!4.2.10! PF delta limit ! 0.1 ! 0.1 ! 0.1 ! 01 !kg/sec!
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.3.6! KL limit ! 14 ! 14 ! 14 ! 14 ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.3.7! C09.1 limit for climb (PH5.1) ! 3.2 ! 3.2 ! 3.2 ! 3.2 !deg C/!
! ! ! ! ! ! !.01EPR!
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.3.8! C09.2 limit for climb (PH6) ! 3.2 ! 3.2 ! 3.2 ! 3.2 !deg C/!
! ! ! ! ! ! !.01EPR!
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.3.9! M programmed limit ! 10 ! 10 ! 10 ! 10 !ft/min!
+-----------------------------------------------------------------------------+

(2) A321: IAE Engines V2530-A5, V2533-A5
+-----------------------------------------------------------------------------+
!Report! Description of Report Item !V2530- !V2533- ! SPARE ! SPARE ! Unit !
!Item ! !A5 !A5 ! ! ! !
! ! !DMU/ID !DMU/ID ! ! ! !
! ! ! I50001! I60001! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.1.1! EGTdivT1 limit ! 15 ! 15 ! ! ! deg C!
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.1.2! EGTdivT2 limit ! 20 ! 20 ! ! ! deg C!
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.1.3! EGTdivT3 limit ! 30 ! 30 ! ! ! deg C!
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.1.4! EGTdivT4 limit ! 40 ! 40 ! ! ! deg C!
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.1.5! TNdivT1 limit ! 100 ! 100 ! ! ! deg C!
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.1.6! TNdivT2 limit ! 150 ! 150 ! ! ! deg C!
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.1.7! TNdivT3 limit ! 200 ! 200 ! ! ! deg C!
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.1.8! TNdivT4 limit ! 250 ! 250 ! ! ! deg C!
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.2.1! EPRL1 limit ! 1.05 ! 1.05 ! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.2.2! EPRL2 limit ! 1.45 ! 1.45 ! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.2.3! EPRL3 limit ! 0.025! 0.025! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.2.5! IVVL limit (valid during ! 150 ! 150 ! ! !ft/min!
! ! flight phase 6) ! ! ! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 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! EPRRL limit ! 2 ! 2 ! ! ! 1/sec!
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.2.9! 'Y09' time interval ! 10 ! 10 ! ! ! sec. !
!------!-------------------------------!-------!-------!-------!-------!------!
!4.2.10! PF delta limit ! 0.1 ! 0.1 ! ! !kg/sec!
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.3.6! KL limit ! 14 ! 14 ! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.3.7! C09.1 limit for climb (PH5.1) ! 3.2 ! 3.2 ! ! !deg C/!
! ! ! ! ! ! !.01EPR!
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.3.8! C09.2 limit for climb (PH6) ! 3.2 ! 3.2 ! ! !deg C/!
! ! ! ! ! ! !.01EPR!
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.3.9! M programmed limit ! 10 ! 10 ! ! !ft/min!
+-----------------------------------------------------------------------------+

(3) A319: IAE Engines V2522-A5, V2524-A5, V2527M-A5
+-----------------------------------------------------------------------------+
!Report! Description of Report Item !V2522- !V2524- !V2527M-! SPARE ! Unit !
!Item ! !A5 !A5 !A5 ! ! !
! ! !DMU/ID !DMU/ID !DMU/ID ! ! !
! ! ! I70001! I80001! I60001! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.1.1! EGTdivT1 limit ! 15 ! 15 ! 15 ! ! deg C!
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.1.2! EGTdivT2 limit ! 20 ! 20 ! 20 ! ! deg C!
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.1.3! EGTdivT3 limit ! 30 ! 30 ! 30 ! ! deg C!
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.1.4! EGTdivT4 limit ! 40 ! 40 ! 40 ! ! deg C!
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.1.5! TNdivT1 limit ! 100 ! 100 ! 100 ! ! deg C!
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.1.6! TNdivT2 limit ! 150 ! 150 ! 150 ! ! deg C!
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.1.7! TNdivT3 limit ! 200 ! 200 ! 200 ! ! deg C!
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.1.8! TNdivT4 limit ! 250 ! 250 ! 250 ! ! deg C!
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.2.1! EPRL1 limit ! 1.05 ! 1.05 ! 1.05 ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.2.2! EPRL2 limit ! 1.45 ! 1.45 ! 1.45 ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.2.3! EPRL3 limit ! 0.025! 0.025! 0.025! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.2.5! IVVL limit (valid during ! 150 ! 150 ! 150 ! !ft/min!
! ! flight phase 6) ! ! ! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.2.6! ALTL limit (valid during ! 5000 ! 5000 ! 5000 ! ! ft !
! ! flight phase 5.1) ! ! ! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.2.7! TATL limit ! 5 ! 5 ! 5 ! ! deg C!
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.2.8! EPRRL limit ! 2 ! 2 ! 2 ! ! 1/sec!
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.2.9! 'Y09' time interval ! 10 ! 10 ! 10 ! ! sec. !
!------!-------------------------------!-------!-------!-------!-------!------!
!4.2.10! PF delta limit ! 0.1 ! 0.1 ! 0.1 ! !kg/sec!
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.3.6! KL limit ! 14 ! 14 ! 14 ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.3.7! C09.1 limit for climb (PH5.1) ! 3.2 ! 3.2 ! 3.2 ! !deg C/!
! ! ! ! ! ! !.01EPR!
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.3.8! C09.2 limit for climb (PH6) ! 3.2 ! 3.2 ! 3.2 ! !deg C/!
! ! ! ! ! ! !.01EPR!
!------!-------------------------------!-------!-------!-------!-------!------!
! 4.3.9! M programmed limit ! 10 ! 10 ! 10 ! !ft/min!
+-----------------------------------------------------------------------------+

Z. Report Limits for Engine Start Report <10>
(1) A320: IAE Engines V2500-A1, V2527-A5, V2527E-A5, V2524-A5
+-----------------------------------------------------------------------------+
!Report! Description of !V2500- !V2527- !V2527E- !V2524- ! SPARE ! Unit !
!Item ! Report Item !A1 !A5 !A5 !A5 ! ! !
! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! ! !
! ! ! I10001! I20001! I30001 ! I80001! ! !
!------!----------------------!-------!-------!--------!-------!-------!------!
! 5.1 ! EGTL limit ! 635 ! 635 ! 635 ! 635 ! ! deg C!
!------!----------------------!-------!-------!--------!-------!-------!------!
! 6.1 ! 'F10.1'th cycle ! 25 ! 25 ! 25 ! 25 ! ! !
!------!----------------------!-------!-------!--------!-------!-------!------!
! 6.2 ! N2 trigger value ! 35 ! 35 ! 35 ! 35 ! ! % !
!------!----------------------!-------!-------!--------!-------!-------!------!
! 7.2 ! Number 'X10' for ! 5 ! 5 ! 5 ! 5 ! ! !
! ! consecutive legs ! ! ! ! ! ! !
+-----------------------------------------------------------------------------+

(2) A321: IAE Engines V2530-A5, V2533-A5
+-----------------------------------------------------------------------------+
!Report! Description of Report Item !V2530- !V2533- ! SPARE ! SPARE ! Unit !
!Item ! !A5 !A5 ! ! ! !
! ! !DMU/ID !DMU/ID ! ! ! !
! ! ! I50001! I60001! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.1 ! EGTL limit ! 635 ! 635 ! ! ! deg C!
!------!-------------------------------!-------!-------!-------!-------!------!
! 6.1 ! 'F10.1'th cycle ! 25 ! 25 ! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 6.2 ! N2 trigger value ! 35 ! 35 ! ! ! % !
!------!-------------------------------!-------!-------!-------!-------!------!
! 7.2 ! Number 'X10' for consecutive ! 5 ! 5 ! ! ! !
! ! legs ! ! ! ! ! !
+-----------------------------------------------------------------------------+

(3) A319: IAE Engines V2522-A5, V2524-A5, V2527M-A5
+-----------------------------------------------------------------------------+
!Report! Description of Report Item !V2522- !V2524- !V2527M-! SPARE ! Unit !
!Item ! !A5 !A5 !A5 ! ! !
! ! !DMU/ID !DMU/ID !DMU/ID ! ! !
! ! ! I70001! I80001! I60001! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 5.1 ! EGTL limit ! 635 ! 635 ! 635 ! ! deg C!
!------!-------------------------------!-------!-------!-------!-------!------!
! 6.1 ! 'F10.1'th cycle ! 25 ! 25 ! 25 ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! 6.2 ! N2 trigger value ! 35 ! 35 ! 35 ! ! % !
!------!-------------------------------!-------!-------!-------!-------!------!
! 7.2 ! Number 'X10' for consecutive ! 5 ! 5 ! 5 ! ! !
! ! legs ! ! ! ! ! !
+-----------------------------------------------------------------------------+

AA. Report Limits for Engine Run-up Report <11>
(1) A320: IAE Engines V2500-A1, V2527-A5, V2527E-A5, V2524-A5
+-----------------------------------------------------------------------------+
!Report! Description of Report Item !V2500- !V2527- !V2527E-!V2524- ! Unit !
!Item ! !A1 !A5 !A5 !A5 ! !
! ! !DMU/ID !DMU/ID !DMU/ID !DMU/ID ! !
! ! ! I10001! I20001! I30001! I80001! !
!------!-------------------------------!-------!-------!-------!-------!------!
! !
! Not Applicable !
! !
+-----------------------------------------------------------------------------+

(2) A321: IAE Engines V2530-A5, V2533-A5
+-----------------------------------------------------------------------------+
!Report! Description of Report Item !V2530- !V2533- ! SPARE ! SPARE ! Unit !
!Item ! !A5 !A5 ! ! ! !
! ! !DMU/ID !DMU/ID ! ! ! !
! ! ! I50001! I60001! ! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! !
! Not Applicable !
! !
+-----------------------------------------------------------------------------+

(3) A319: IAE Engines V2522-A5, V2524-A5, V2527M-A5
+-----------------------------------------------------------------------------+
!Report! Description of Report Item !V2522- !V2524- !V2527M-! SPARE ! Unit !
!Item ! !A5 !A5 !A5 ! ! !
! ! !DMU/ID !DMU/ID !DMU/ID ! ! !
! ! ! I70001! I80001! I60001! ! !
!------!-------------------------------!-------!-------!-------!-------!------!
! !
! Not Applicable !
! !
+-----------------------------------------------------------------------------+

[Rev.10 from 2021] 2026.04.01 00:36:23 UTC
"Aviabrain" 2025