W DOC AIRBUS | AMM A320F

AIDS - STRUCTURE 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).
These load AIDS report is available:
  • <15> Load Report.
** ON A/C NOT FOR ALL
2. Load Reports
A. Load Report <15>
F Load Report <15>
F Load Report <15>
F Load Report <15> ** ON A/C NOT FOR ALL
F Load Report <15> ** ON A/C NOT FOR ALL
F Load Report <15> ** ON A/C NOT FOR ALL
F Load Report <15> ** ON A/C NOT FOR ALL
F Load Report <15> ** ON A/C NOT FOR ALL
F Load Report <15> ** ON A/C NOT FOR ALL
The Load report is a collection of aircraft data before, at, and after an abnormal Load condition either in the air or at touchdown. The report is generated when one of the logic conditions (for detail see Load report logic) is present.
NOTE: For the standard header definition of the report refer to (Ref. AMM D/O 31-36-00-00).
NOTE: For the IAE engines, 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) Load Report Data Field Description
NOTE: Reports that are transmitted from the ACARS system do not have report lines without a line identifier.
+---------------------------------------------------------------------+
! Value ! Content Description !
!--------------!------------------------------------------------------!
! ESN ! Engine Serial Number !
! 999999 ! (000000 to 999999) !
! ! Eng 1 param. 7C.1.046.01 digit 3, 2, 1 !
! ! 7C.1.047.01 digit 6, 5, 4 !
! ! Eng 2 param. 7C.2.046.01 digit 3, 2, 1 !
! ! 7C.2.047.01 digit 6, 5, 4 !
! ! NOTE: For IAE engines: 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 !
!--------------!------------------------------------------------------!
! AP ! Auto Pilot Status !
! 99 ! (00 to G8) !
! ! FMGC 1 and 2 (FGC part) for Auto Pilot AP1 and AP2 !
! ! !
! ! XX Auto Pilot Modes: !
! ! !! !
! ! !!__Lateral Modes: 0 = NO MODE !
! ! ! 1 = HEADING !
! ! ! 2 = TRACK !
! ! ! 3 = NAV !
! ! ! 4 = LOC CAPTURE !
! ! ! 5 = LOC TRACK !
! ! ! 6 = LAND TRACK !
! ! ! 7 = RUNWAY !
! ! ! 8 = ROLL GO AROUND !
! ! ! !
! ! !__Longitudinal Modes: 0 = NO MODE !
! ! 1 = PITCH G/A !
! ! 2 = PITCH T/O !
! ! 3 = G/S TRACK !
! ! 4 = G/S CAPTURE !
! ! 5 = V/S !
! ! 6 = FPA !
! ! 7 = ALT !
! ! 8 = ALT ACQ !
! ! 9 = OPEN CLB !
! ! A = OPEN DES !
! ! B = IM CLB !
! ! C = IM DES !
! ! D = CLB !
! ! E = DES !
! ! F = FINAL DES !
! ! G = EXPEDITE !
! ! !
! ! AP1 ! AP2 !
! ! Report Line EC: ! Report Line EE: !Definition: !
! ! -------------------!-------------------!------------ !
! ! / ! / !No Mode Act. !
! ! -------------------!-------------------!------------ !
! ! 01.1.275.00.11 = 1 ! 01.2.275.00.11 = 1!RUNWAY Mode !
! ! -------------------!-------------------!------------ !
! ! 01.1.275.00.12 = 1 ! 01.2.275.00.12 = 1!NAV Mode !
! ! -------------------!-------------------!------------ !
! ! 01.1.275.00.13 = 1 ! 01.2.275.00.13 = 1!LOC CAPTURE !
! ! ! !Mode !
! ! -------------------!-------------------!------------ !
! ! 01.1.275.00.14 = 1 ! 01.2.275.00.14 = 1!LOC TRACK !
! ! ! !Mode !
! ! -------------------!-------------------!------------ !
! ! 01.1.275.00.15 = 1 ! 01.2.275.00.15 = 1!Roll GO !
! ! ! !AROUND Mode !
! ! -------------------!-------------------!------------ !
! ! 01.1.275.00.16 = 1 ! 01.2.275.00.16 = 1!HEADING Mode !
! ! -------------------!-------------------!------------ !
! ! 01.1.275.00.17 = 1 ! 01.2.275.00.17 = 1!TRACK Mode !
! ! -------------------!-------------------!------------ !
! ! 01.1.274.00.15 = 1 ! 01.2.274.00.15 = 1!PITCH TO Mode!
! ! -------------------!-------------------!------------ !
! ! 01.1.274.00.16 = 1 ! 01.2.274.00.16 = 1!PITCH GA Mode!
! ! -------------------!-------------------!------------ !
! ! 01.1.274.00.17 = 1 ! 01.2.274.00.17 = 1!V/S Mode !
! ! -------------------!-------------------!------------ !
! ! 01.1.274.00.18 = 1 ! 01.2.274.00.18 = 1!FPA Mode !
! ! -------------------!-------------------!-------------!
! ! 01.1.274.00.19 = 1 ! 01.2.274.00.19 = 1!ALT Mode !
! ! AND ! AND ! !
! ! 01.1.274.00.20 = 1 ! 01.2.274.00.20 = 1! !
! ! -------------------!-------------------!------------ !
! ! 01.1.274.00.19 = 1 ! 01.2.274.00.19 = 1!ALT ACQ !
! ! AND ! AND !Mode !
! ! 01.1.274.00.21 = 1 ! 01.2.274.00.21 = 1! !
! ! -------------------!-------------------!------------ !
! ! 01.1.274.00.20 = 1 ! 01.2.274.00.20 = 1!G/S TRACK !
! ! AND ! AND !Mode !
! ! 01.1.274.00.22 = 1 ! 01.2.274.00.22 = 1! !
! ! -------------------!-------------------!------------ !
! ! 01.1.274.00.21 = 1 ! 01.2.274.00.21 = 1!G/S CAPTURE !
! ! AND ! AND !Mode !
! ! 01.1.274.00.22 = 1 ! 01.2.274.00.22 = 1! !
! ! -------------------!-------------------!------------ !
! ! 01.1.274.00.23 = 1 ! 01.2.274.00.23 = 1!FINAL DES !
! ! ! !Mode !
! ! -------------------!-------------------!------------ !
! ! 01.2.274.00.24 = 1 ! 01.2.274.00.24 = 1!EXPED. Mode !
! ! -------------------!-------------------!------------ !
! ! 01.1.146.00.14 = 1 ! 01.2.146.00.14 = 1!LAND TRACK !
! ! ! !Mode !
! ! -------------------!-------------------!------------ !
! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!CLB Mode !
! ! AND ! AND ! !
! ! 01.1.274.00.13 = 0 ! 01.2.274.00.13 = 0! !
! ! OR ! OR ! !
! ! 01.1.274.00.14 = 0 ! 01.2.274.00.14 = 0! !
! ! OR ! OR ! !
! ! 01.1.274.00.24 = 0 ! 01.2.274.00.24 = 0! !
! ! -------------------!-------------------!------------ !
! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!DES Mode !
! ! AND ! AND ! !
! ! 01.1.274.00.13 = 0 ! 01.2.274.00.13 = 0! !
! ! OR ! OR ! !
! ! 01.1.274.00.14 = 0 ! 01.2.274.00.14 = 0! !
! ! OR ! OR ! !
! ! 01.1.274.00.24 = 0 ! 01.2.274.00.24 = 0! !
! ! -------------------!-------------------!------------ !
! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!IM. CLIMB !
! ! AND ! AND !Mode !
! ! 01.1.274.00.13 = 1 ! 01.2.274.00.13 = 1! !
! ! -------------------!-------------------!------------ !
! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!IM. DES Mode !
! ! AND ! AND ! !
! ! 01.1.274.00.13 = 1 ! 01.2.274.00.13 = 1! !
! ! -------------------!-------------------!------------ !
! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!OPEN CLB !
! ! AND ! AND !Mode !
! ! 01.1.274.00.14 = 1 ! 01.2.274.00.14 = 1! !
! ! -------------------!-------------------!------------ !
! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!OPEN DES !
! ! AND ! AND !Mode !
! ! 01.1.274.00.14 = 1 ! 01.2.274.00.14 = 1! !
! ! ---------------------------------------------------- !
! ! Auto Pilot Status DMU: !
! ! AP1 printed in report line EC !
! ! AP2 printed in report line EE !
!--------------!------------------------------------------------------!
! FLAP ! FLAP Actual Position !
! X999 ! (0 to 40.0 deg) !
! ! param. 1B.1.137.01 FLAP System 1 !
! ! 1B.2.137.10 FLAP System 2 !
!--------------!------------------------------------------------------!
! SLAT ! SLAT Actual Position !
! X999 ! (0 to 27.0 deg) !
! ! param. 1B.1.127.01 SLAT System 1 !
! ! 1B.2.127.10 SLAT System 2 !
!--------------!------------------------------------------------------!
! MAX ! Maximum Value of the exceedance parameter from !
! X999 ! time interval 0.5 sec. before 'landing detection' !
! ! till 0.5 sec. after 'landing detection'. !
!--------------!------------------------------------------------------!
! LIM ! Programmable limit which was exceeded !
! X999 ! !
!--------------!------------------------------------------------------!
! COUNTS ! Counter for spoiler 4 extensions !
! 5 x 9999 ! (0 to 9999) !
! ! 999 999 999 999 999 !
! ! I I I I I___Spoiler < -20 Deg !
! ! I I I I_______-15 Deg > Spoiler >= -20 !
! ! I I I____________-10 Deg > Spoiler >= -15 !
! ! I I__________________-5 Deg > Spoiler >= -10 !
! ! I_______________________ 0 Deg > Spoiler >= -5 !
! ! !
! ! 6C.1.364.01 LH Spoiler 4 Position !
! ! 6C.2.364.10 !
! ! 6C.1.374.01 RH Spoiler 4 Position !
! ! 6C.2.374.10 !
! ! 6C.1.044.01.24 = 1 Spoiler 4 Fault !
! ! 6C.2.044.10.24 = 1 !
! ! 6C.1.365.01 LH Spoiler 5 Position !
! ! 6C.2.365.10 !
! ! 6C.1.375.01 RH Spoiler 5 Position !
! ! 6C.2.375.10 !
! ! 6C.1.044.01.25 = 1 Spoiler 5 Fault !
! ! 6C.2.044.10.25 = 1 !
! ! 6C.1.041.01.21 = 1 Load Alleviation Active (LAF) !
! ! 6C.2.041.10.21 = 1 !
!--------------!------------------------------------------------------!
! REASON ! Reason for exceedance !
! XXXXXXXXXX ! Up to 10 characters !
! ! RALR Code: 4100 !
! ! VRTA Code: 4400, 4500, 5100, 5200 and 5300 !
! ! GW Code: 4800, 4900 !
! ! SPCT Code: 5400 !
!--------------!------------------------------------------------------!
! RALT ! Radio Height !
! X999 ! (-20 to 2500 ft) !
! ! param 25.1.164.01 Radio Altimeter #1 printed in !
! ! 25.2.164.01 report line X1 !
! ! param 25.1.164.10 Radio Altimeter #2 printed in !
! ! 25.2.164.10 report line X2 !
!--------------!------------------------------------------------------!
! RALR ! Radio Altitude Rate !
! X999 ! (-99.9 to 99.9 ft/sec) !
!--------------!------------------------------------------------------!
! PTCH ! Pitch Angle !
! X999 ! (-90.0 to 90.0 deg) !
! ! param. 04.1.324.01 !
! ! 04.2.324.10 !
!--------------!------------------------------------------------------!
! PTCR ! Body Pitch Rate !
! X999 ! (-45.0 to 45.0 deg/sec) !
! ! param. 04.1.326.01 !
! ! 04.2.326.10 !
!--------------!------------------------------------------------------!
! ROLL ! Roll Angle !
! X999 ! (-90.0 to 90.0 deg) !
! ! param. 04.1.325.01 !
! ! 04.2.325.10 !
!--------------!------------------------------------------------------!
! ROLR ! Body Roll Rate !
! X999 ! (-45.0 to 45.0 deg/sec) !
! ! param. 04.1.327.01 !
! ! 04.2.327.10 !
!--------------!------------------------------------------------------!
! YAW ! YAW Rate !
! X999 ! (-45.0 to 45.0 deg/sec) !
! ! param. 04.1.330.01 !
! ! 04.2.330.10 !
!--------------!------------------------------------------------------!
! VRTA ! Normal Acceleration !
! X999 ! (-3.00 to 6.00 g) !
! ! param. 29.1.333.01 !
! ! 29.2.333.10 !
!--------------!------------------------------------------------------!
! LONA ! Longitudinal Acceleration !
! X999 ! (-1.00 to 1.00 g) !
! ! param. 29.1.331.01 !
! ! 29.2.331.10 !
!--------------!------------------------------------------------------!
! LATA ! Lateral Acceleration !
! X999 ! (-1.00 to 1.00 g) !
! ! param. 29.1.332.01 !
! ! 29.2.332.10 !
+---------------------------------------------------------------------+

(2) Load Report Data Field Description
NOTE: Reports that are transmitted from the ACARS system do not have report lines without a line identifier.
+---------------------------------------------------------------------+
! Value ! Content Description !
!--------------!------------------------------------------------------!
! ESN ! Engine Serial Number !
! 999999 ! (000000 to 999999) !
! ! Eng 1 param. 7C.1.046.01 digit 3, 2, 1 !
! ! 7C.1.047.01 digit 6, 5, 4 !
! ! Eng 2 param. 7C.2.046.10 digit 3, 2, 1 !
! ! 7C.2.047.10 digit 6, 5, 4 !
!--------------!------------------------------------------------------!
! EHRS ! Engine Flight Hours !
! 99999 ! (00000 to 99999 hours) !
! ! DMU Engine 1 0D.1.060.01 !
! ! Engine 2 0D.1.060.10 !
!--------------!------------------------------------------------------!
! AP ! Auto Pilot Status !
! 99 ! (00 to 24) !
! ! FMGC 1 and 2 (FGC part) for Auto Pilot AP1 and AP2 !
! ! !
! ! XX Auto Pilot Modes: !
! ! !! !
! ! !!__Lateral Modes: 0 = NO MODE !
! ! ! 1 = HEADING !
! ! ! 2 = TRACK !
! ! ! 3 = NAV !
! ! ! 4 = LOC CAPTURE !
! ! ! 5 = LOC TRACK !
! ! ! 6 = LAND TRACK !
! ! ! 7 = RUNWAY !
! ! ! 8 = ROLL GO AROUND !
! ! ! !
! ! !__Longitudinal Modes: 0 = NO MODE !
! ! 1 = PITCH G/A !
! ! 2 = PITCH T/O !
! ! 3 = G/S TRACK !
! ! 4 = G/S CAPTURE !
! ! 5 = V/S !
! ! 6 = FPA !
! ! 7 = ALT !
! ! 8 = ALT ACQ !
! ! 9 = OPEN CLB !
! ! A = OPEN DES !
! ! B = IM CLB !
! ! C = IM DES !
! ! D = CLB !
! ! E = DES !
! ! F = FINAL DES !
! ! G = EXPEDITE !
! ! !
! ! AP1 ! AP2 !
! ! Report Line EC: ! Report Line EE: !Difinition: !
!--------------! -------------------!-------------------!------------ !
!00 ! / ! / !No Mode Act. !
!--------------! -------------------!-------------------!------------ !
!01 ! 01.1.275.00.11 = 1 ! 01.2.275.00.11 = 1!RUNWAY Mode !
!--------------! -------------------!-------------------!------------ !
!02 ! 01.1.275.00.12 = 1 ! 01.2.275.00.12 = 1!NAV Mode !
!--------------! -------------------!-------------------!------------ !
!03 ! 01.1.275.00.13 = 1 ! 01.2.275.00.13 = 1!LOC CAPTURE !
! ! ! !Mode !
!--------------! -------------------!-------------------!------------ !
!04 ! 01.1.275.00.14 = 1 ! 01.2.275.00.14 = 1!LOC TRACK !
! ! ! !Mode !
!--------------! -------------------!-------------------!------------ !
!05 ! 01.1.275.00.15 = 1 ! 01.2.275.00.15 = 1!Roll GO !
! ! ! !AROUND Mode !
!--------------! -------------------!-------------------!------------ !
!06 ! 01.1.275.00.16 = 1 ! 01.2.275.00.16 = 1!HEADING Mode !
!--------------! -------------------!-------------------!------------ !
!07 ! 01.1.275.00.17 = 1 ! 01.2.275.00.17 = 1!TRACK Mode !
!--------------! -------------------!-------------------!------------ !
!08 ! 01.1.274.00.15 = 1 ! 01.2.274.00.15 = 1!PITCH TO Mode!
!--------------! -------------------!-------------------!------------ !
!09 ! 01.1.274.00.16 = 1 ! 01.2.274.00.16 = 1!PITCH GA Mode!
!--------------! -------------------!-------------------!------------ !
!10 ! 01.1.274.00.17 = 1 ! 01.2.274.00.17 = 1!V/S Mode !
!--------------! -------------------!-------------------!------------ !
!11 ! 01.1.274.00.18 = 1 ! 01.2.274.00.18 = 1!FPA Mode !
!--------------! -------------------!-------------------!-------------!
!12 ! 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! !
!--------------! -------------------!-------------------!------------ !
!13 ! 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! !
!--------------! -------------------!-------------------!------------ !
!14 ! 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! !
!--------------! -------------------!-------------------!------------ !
!15 ! 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! !
!--------------! -------------------!-------------------!------------ !
!16 ! 01.1.274.00.23 = 1 ! 01.2.274.00.23 = 1!FINAL DES !
! ! ! !Mode !
!--------------! -------------------!-------------------!------------ !
!17 ! 01.1.274.00.24 = 1 ! 01.2.274.00.24 = 1!EXPED. Mode !
!--------------! -------------------!-------------------!------------ !
!18 ! 01.1.146.00.14 = 1 ! 01.2.146.00.14 = 1!LAND TRACK !
! ! ! !Mode !
!--------------! -------------------!-------------------!------------ !
!19 ! 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! !
!--------------! -------------------!-------------------!------------ !
!20 ! 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! !
!--------------! -------------------!-------------------!------------ !
!21 ! 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! !
!--------------! -------------------!-------------------!------------ !
!22 ! 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! !
!--------------! -------------------!-------------------!------------ !
!23 ! 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! !
!--------------! -------------------!-------------------!------------ !
!24 ! 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: !
! ! 0D.1.274.01 AP1 printed in report line EC !
! ! 0D.1.274.10 AP2 printed in report line EE !
!--------------!------------------------------------------------------!
! FLAP ! FLAP Actual Position !
! 9999 ! (0 to 40.0 deg) !
! ! param. 1B.1.137.01 FLAP System 1 !
! ! 1B.2.137.10 FLAP System 2 !
!--------------!------------------------------------------------------!
! SLAT ! SLAT Actual Position !
! 9999 ! (0 to 27.0 deg) !
! ! param. 1B.1.127.01 SLAT System 1 !
! ! 1B.2.127.10 SLAT System 2 !
!--------------!------------------------------------------------------!
! MAX ! Maximum Value of the exceedance parameter from !
! X999 ! time interval 0.5 sec. before 'landing detection' !
! ! until 0.5 sec. after 'landing detection'. !
!--------------!------------------------------------------------------!
! LIM ! Programmable limit which was exceeded !
! X999 ! !
!--------------!------------------------------------------------------!
! COUNTS ! Counter for spoiler 4 extensions !
! 5 x 9999 ! (0 to 9999) !
! ! 999 999 999 999 999 !
! ! I I I I I___Spoiler < -20 Deg !
! ! I I I I_______-15 Deg > Spoiler >= -20 !
! ! I I I____________-10 Deg > Spoiler >= -15 !
! ! I I__________________-5 Deg > Spoiler >= -10 !
! ! I_______________________ 0 Deg > Spoiler >= -5 !
! ! !
! ! 6C.1.364.01 LH Spoiler 4 Position !
! ! 6C.2.364.10 !
! ! 6C.1.374.01 RH Spoiler 4 Position !
! ! 6C.2.374.10 !
! ! 6C.1.044.01.24 = 1 Spoiler 4 Fault !
! ! 6C.2.044.10.24 = 1 !
! ! 6C.1.365.01 LH Spoiler 5 Position !
! ! 6C.2.365.10 !
! ! 6C.1.375.01 RH Spoiler 5 Position !
! ! 6C.2.375.10 !
! ! 6C.1.044.01.25 = 1 Spoiler 5 Fault !
! ! 6C.2.044.10.25 = 1 !
! ! 6C.1.041.01.21 = 1 Load Alleviation Active (LAF) !
! ! 6C.2.041.10.21 = 1 !
!--------------!------------------------------------------------------!
! REASON ! Reason for exceedance !
! XXXXXXXXXX ! Up to 10 characters !
! ! RALR Code: 4100 !
! ! VRTA Code: 4400, 4500, 5100, 5200 and 5300 !
! ! GW Code: 4800, 4900 !
! ! SPCT Code: 5400 !
!--------------!------------------------------------------------------!
! RALT ! Radio Altitude !
! X999 ! DMC (-20 to 2500 ft) !
! ! 25.1.164.01 !
! ! 25.1.164.10 !
!--------------!------------------------------------------------------!
! RALR ! Radio Altitude Rate !
! X999 ! Format: Negative values are indicated by 'N' in the !
! ! first position. Otherwise the first position is !
! ! used for the value. !
! ! -99.9 to 99.9 ft/sec !
! ! !
! ! Source: DMU !
! ! Remark: The calculation of Radio Altitude Rate is !
! ! started when: RALT<RALTL1 !
! ! - The calculation is performed with 16 Hz cycles !
! ! (T=0.0625 s) !
! ! - The calculation uses the current calculation !
! ! cycle current and data values. These data are !
! ! named as follows: !
! ! e.g. !
! ! IVV = IVV actual sample n !
! ! IVV1 = IVV previous sample n-1 !
! ! !
! ! PTCHACC = PTCHACC actual sample n !
! ! PTCHACC1 = PTCHACC previous sample n-1 !
! ! PTCHACC2 = PTCHACC previous sample n-2 !
! ! !
! ! - The calculation uses the following programmable !
! ! constants: !
! ! D geometrical correction factor for ROLR ft/deg!
! ! DX lever arm correction (x-axis) for R/A RALT ft!
! ! DZ lever arm correction (z-axis) for R/A RALT ft!
! ! DXTPIR lever arm correction (x-axis) for PTCH ft!
! ! FC filter frequency Hz!
! ! K1 filter constant !
! ! K2 filter constant !
! ! K3 filter constant !
! ! THETA0 average PTCH at touchdown deg!
! ! !
! ! Radio Altitude Rate calculation: !
! ! 1. Start Values !
! ! !
! ! For the very first calculation the start values are !
! ! defined as follows: !
! ! PTCHRAW1 = 0.0 !
! ! PTCHACC1 = 0.0 !
! ! PTCHACC2 = 0.0 !
! ! PTCR1 = 0.0 !
! ! EN1 = 0.0 !
! ! VZN1 = IVV/60.0 !
! ! ZN1 = RALT !
! ! !
! ! 2. Algorithm with KALMAN filter !
! ! The algorithm comprises of the following equations: !
! ! PTCHRAW = (PTCR-PTCR1)/T !
! ! PTCHACC = PTCHACC1+T*(2*PI*FC)*(PTCHRAW+PTCHRAW1- !
! ! PTCHACCI-PTCHACC2)/2 !
! ! NZTCOR = VACC*9.81/0.3048-DXTPIR*PTCHACC/57.3*cos !
! ! (PTCH/57.3) !
! ! HRACOR = RALT+DX*(sin(PTCH/57.3)-sin(THEATA0/57.3))!
! ! -DZ*(cos(PTCH/57.3)-cos(THEATA0/57.3)) !
! ! EPSN = ZN1-HRACOR !
! ! EN = EN1+T*(VZN-K2*EPSN) !
! ! VZN = VZN1+T*(VZN-K2*EPSN) !
! ! VZNU = VZN-D*ABS(ROLR) !
! ! RALR = VZNU !
!--------------!------------------------------------------------------!
! PTCH ! Pitch Angle !
! X999 ! (-99.0 to 90.0 deg) !
! ! param. 04.1.324.01 !
! ! 04.2.324.10 !
!--------------!------------------------------------------------------!
! PTCR ! Body Pitch Rate !
! X999 ! (-45.0 to 45.0 deg/sec) !
! ! param. 04.1.326.01 !
! ! 04.2.326.10 !
!--------------!------------------------------------------------------!
! ROLL ! Roll Angle !
! X999 ! (-90.0 to 90.0 deg) !
! ! param. 04.1.325.01 !
! ! 04.2.325.10 !
!--------------!------------------------------------------------------!
! ROLR ! Body Roll Rate !
! X999 ! (-45.0 to 45.0 deg/sec) !
! ! param. 04.1.327.01 !
! ! 04.2.327.10 !
!--------------!------------------------------------------------------!
! YAW ! YAW Rate !
! X999 ! (-45.0 to 45.0 deg/sec) !
! ! param. 04.1.330.01 !
! ! 04.2.330.10 !
!--------------!------------------------------------------------------!
! VRTA ! Normal Acceleration !
! X999 ! (-3.00 to 6.00 g) !
! ! param. 29.1.333.01 !
! ! 29.2.333.10 !
!--------------!------------------------------------------------------!
! LONA ! Longitudinal Acceleration !
! X999 ! (-1.00 to 1.00 g) !
! ! param. 29.1.331.01 !
! ! 29.2.331.10 !
!--------------!------------------------------------------------------!
! LATA ! Lateral Acceleration !
! X999 ! (-1.00 to 1.00 g) !
! ! param. 29.1.332.01 !
! ! 29.2.332.10 !
+---------------------------------------------------------------------+

(3) Load Report Data Field Description <15>
NOTE: Reports that are transmitted from the ACARS system do not have report lines without a line identifier.
+---------------------------------------------------------------------+
! Value ! Content Description !
!--------------!------------------------------------------------------!
! ESN ! Engine Serial Number !
! 999999 ! (000000 to 999999) !
! ! ECU Eng 1 param. 7C.1.046.01 digit 3, 2, 1 !
! ! 7C.1.047.01 digit 6, 5, 4 !
! ! Eng 2 param. 7C.2.046.10 digit 3, 2, 1 !
! ! 7C.2.047.10 digit 6, 5, 4 !
!--------------!------------------------------------------------------!
! EHRS ! Engine Flight Hours !
! 99999 ! (00000 to 99999 hours) !
! ! DMU Engine 1 0D.1.060.01 !
! ! Engine 2 0D.1.060.10 !
! ! !
! ! Time between "Main (LH and RH) Landing Gear !
! ! Decompressed" and "Main (LH and RH) Landing Gear !
! ! "Compressed". The EHRS is set to zero if a new ESN !
! ! is recognized by the DMU. It is possible to set the!
! ! EHRS via the MCDU, e.g. if the DMU is changed on !
! ! the A/C. !
!--------------!------------------------------------------------------!
! AP ! Auto Pilot Status !
! 99 ! (00 to 24) !
! ! FMGC 1 and 2 (FGC part) for Auto Pilot AP1 and AP2 !
!--------------! -------------------!-------------------!------------ !
! Auto Pilot ! AP1 ! AP2 ! !
! Status ! Report Line EC: ! Report Line EE: ! Definition: !
!--------------! -------------------!-------------------!------------ !
!00 ! -------------------! ------------------! No Mode Act.!
!--------------! -------------------!-------------------!------------ !
!01 ! 01.1.275.00.11 = 1 ! 01.2.275.00.11 = 1!RUNWAY Mode !
!--------------! -------------------!-------------------!------------ !
!02 ! 01.1.275.00.12 = 1 ! 01.2.275.00.12 = 1!NAV Mode !
!--------------! -------------------!-------------------!------------ !
!03 ! 01.1.275.00.13 = 1 ! 01.2.275.00.13 = 1!LOC CAPTURE !
! ! ! !Mode !
!--------------! -------------------!-------------------!------------ !
!04 ! 01.1.275.00.14 = 1 ! 01.2.275.00.14 = 1!LOC TRACK !
! ! ! !Mode !
!--------------! -------------------!-------------------!------------ !
!05 ! 01.1.275.00.15 = 1 ! 01.2.275.00.15 = 1!Roll GO !
! ! ! !AROUND Mode !
!--------------! -------------------!-------------------!------------ !
!06 ! 01.1.275.00.16 = 1 ! 01.2.275.00.16 = 1!HEADING Mode !
!--------------! -------------------!-------------------!------------ !
!07 ! 01.1.275.00.17 = 1 ! 01.2.275.00.17 = 1!TRACK Mode !
!--------------! -------------------!-------------------!------------ !
!08 ! 01.1.274.00.15 = 1 ! 01.2.274.00.15 = 1!PITCH TO Mode!
!--------------! -------------------!-------------------!------------ !
!09 ! 01.1.274.00.16 = 1 ! 01.2.274.00.16 = 1!PITCH GA Mode!
!--------------! -------------------!-------------------!------------ !
!10 ! 01.1.274.00.17 = 1 ! 01.2.274.00.17 = 1!V/S Mode !
!--------------! -------------------!-------------------!------------ !
!11 ! 01.1.274.00.18 = 1 ! 01.2.274.00.18 = 1!FPA Mode !
!--------------! -------------------!-------------------!-------------!
!12 ! 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! !
!--------------! -------------------!-------------------!------------ !
!13 ! 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! !
!--------------! -------------------!-------------------!------------ !
!14 ! 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! !
!--------------! -------------------!-------------------!------------ !
!15 ! 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! !
!--------------! -------------------!-------------------!------------ !
!16 ! 01.1.274.00.23 = 1 ! 01.2.274.00.23 = 1!FINAL DES !
! ! ! !Mode !
!--------------! -------------------!-------------------!------------ !
!17 ! 01.1.274.00.24 = 1 ! 01.2.274.00.24 = 1!EXPED. Mode !
!--------------! -------------------!-------------------!------------ !
!18 ! 01.1.146.00.14 = 1 ! 01.2.146.00.14 = 1!LAND TRACK !
! ! ! !Mode !
!--------------! -------------------!-------------------!------------ !
!19 ! 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! !
!--------------! -------------------!-------------------!------------ !
!20 ! 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! !
!--------------! -------------------!-------------------!------------ !
!21 ! 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! !
!--------------! -------------------!-------------------!------------ !
!22 ! 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! !
!--------------! -------------------!-------------------!------------ !
!23 ! 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! !
!--------------! -------------------!-------------------!------------ !
!24 ! 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: !
! ! 0D.1.274.01 AP1 printed in report line EC !
! ! 0D.1.274.10 AP2 printed in report line EE !
!--------------!------------------------------------------------------!
! FLAP ! FLAP Actual Position !
! 9999 ! (0 to 40.0 deg) !
!--------------!------------------------------------------------------!
! SLAT ! SLAT Position !
! 9999 ! (0 to 27.0 deg) !
! ! param. SFCC 1B.1.127.01 SLAT !
! ! 1B.2.127.10 SLAT !
!--------------!------------------------------------------------------!
! MAX ! Maximum Value of the exceedance parameter from !
! X999 ! time interval 0.5 sec. before 'landing detection' !
! ! until 0.5 sec. after 'landing detection'. !
! ! For logic 4100 see remark. !
! ! !
! ! Format: Depends on exceeded parameter !
! ! !
! ! Source: Depends on exceeded parameter !
! ! !
! ! Remark: If code = 4100 (exceedance RALR) the !
! ! maximum value is taken as an average value !
! ! from a window of RALR data between S1 and !
! ! S2 around the landing detection event. !
! ! If code = 4500 the highest maximum of the !
! ! exceeding parameter either at landing or at!
! ! bounce landing is displayed. !
! ! !
! ! !
!--------------!------------------------------------------------------!
! LIM ! Remark: If code = 4500 the limit which was exceeded !
! ! is displayed in reference to MAX either at !
! ! landing or at bounce landing. !
!--------------!------------------------------------------------------!
! COUNTS ! Counter for spoiler 4 extensions !
! ! Format (0 to 9999) !
! ! 999 999 999 999 999 !
! ! I I I I I___Spoiler < -20 Deg !
! ! I I I I_______-15 Deg > Spoiler >= -20 !
! ! I I I____________-10 Deg > Spoiler >= -15 !
! ! I I__________________-5 Deg > Spoiler >= -10 !
! ! I_______________________ 0 Deg > Spoiler >= -5 !
! ! !
! ! 6C.1.364.01 LH Spoiler 4 Position !
! ! 6C.2.364.10 !
! ! 6C.1.374.01 RH Spoiler 4 Position !
! ! 6C.2.374.10 !
! ! 6C.1.044.01.24 = 1 Spoiler 4 Fault !
! ! 6C.2.044.10.24 = 1 !
! ! 6C.1.365.01 LH Spoiler 5 Position !
! ! 6C.2.365.10 !
! ! 6C.1.375.01 RH Spoiler 5 Position !
! ! 6C.2.375.10 !
! ! 6C.1.044.01.25 = 1 Spoiler 5 Fault !
! ! 6C.2.044.10.25 = 1 !
! ! 6C.1.041.01.21 = 1 Load Alleviation Active (LAF) !
! ! 6C.2.041.10.21 = 1 !
!--------------!------------------------------------------------------!
! REASON ! Reason for exceedance XXXXXXXXXXXXXXXXXXXX !
! XXXXXXXXXX ! Format: Up to 10 characters !
! XXXXXXXXXX ! Source: DMU !
! ! !
! ! Remark: If the report was not triggered by a limit !
! ! exceedance this field contains blanks. !
! ! !
! ! RALR Code: 4100 !
! ! VRTA Code: 4400, 4500, 5100, 5200 and 5300 !
! ! GW Code: 4800, 4900 !
! ! SPCT Code: 5400 !
!--------------!------------------------------------------------------!
! RALT ! Radio Altitude !
! X999 ! Format: Negative values are indicated by '-' in the!
! ! first position. Otherwise the first position is !
! ! used for the value. !
! ! -20 to 2500 ft !
! ! DMC 25.1.164.01 !
! ! 25.1.164.10 !
!--------------!------------------------------------------------------!
! RALR ! Radio Altitude Rate
! X999 ! Format: Negative values are indicated by '-' in the !
! ! first position. Otherwise the first position is !
! ! used for the value. !
! ! -99.9 to 99.9 ft/sec !
! ! !
! ! Source: DMU !
! ! Remark: The calculation of Radio Altitude Rate is !
! ! started when: RALT<RALTL1 !
! ! - The calculation is performed with 16 Hz cycles !
! ! (T=0.0625 s) !
! ! - The calculation uses the current calculation !
! ! cycle current and data values. These data are !
! ! named as follows: !
! ! e.g. !
! ! IVV = IVV actual sample n !
! ! IVV1 = IVV previous sample n-1 !
! ! !
! ! PTCHACC = PTCHACC actual sample n !
! ! PTCHACC1 = PTCHACC previous sample n-1 !
! ! PTCHACC2 = PTCHACC previous sample n-2 !
! ! !
! ! - The calculation uses the following programmable !
! ! constants: !
! ! D geometrical correction factor for ROLR ft/deg!
! ! DX lever arm correction (x-axis) for R/A RALT ft!
! ! DZ lever arm correction (z-axis) for R/A RALT ft!
! ! DXTPIR lever arm correction (x-axis) for PTCH ft!
! ! FC filter frequency Hz!
! ! K1 filter constant !
! ! K2 filter constant !
! ! K3 filter constant !
! ! THETA0 average PTCH at touchdown deg!
! ! !
! ! Radio Altitude Rate calculation: !
! ! 1. Start Values !
! ! !
! ! For the very first calculation the start values are !
! ! defined as follows: !
! ! PTCHRAW1 = 0.0 !
! ! PTCHACC1 = 0.0 !
! ! PTCHACC2 = 0.0 !
! ! PTCR1 = 0.0 !
! ! EN1 = 0.0 !
! ! VZN1 = IVV/60.0 !
! ! ZN1 = RALT !
! ! !
! ! 2. Algorithm with KALMAN filter !
! ! The algorithm comprises of the following equations: !
! ! PTCHRAW = (PTCR-PTCR1)/T !
! ! PTCHACC = PTCHACC1+T*(2*PI*FC)*(PTCHRAW+PTCHRAW1- !
! ! PTCHACCI-PTCHACC2)/2 !
! ! NZTCOR = VACC*9.81/0.3048-DXTPIR*PTCHACC/57.3*cos !
! ! (PTCH/57.3) !
! ! HRACOR = RALT+DX*(sin(PTCH/57.3)-sin(THEATA0/57.3))!
! ! -DZ*(cos(PTCH/57.3)-cos(THEATA0/57.3)) !
! ! EPSN = ZN1-HRACOR !
! ! EN = EN1+T*(VZN-K2*EPSN) !
! ! VZN = VZN1+T*(VZN-K2*EPSN) !
! ! VZNU = VZN-D*ABS(ROLR) !
! ! RALR = VZNU !
!--------------!------------------------------------------------------!
! PTCH ! Pitch Angle !
! X999 ! Format: Negative values are indicated by '-' in the!
! ! first position. Otherwise the first position is !
! ! used for the value. !
! ! -99.0 to 90.0 deg !
! ! param. ADIRU 04.1.324.01 !
! ! 04.2.324.10 !
!--------------!------------------------------------------------------!
! PTCR ! Body Pitch Rate !
! X999 ! Format: Negative values are indicated by '-' in the!
! ! first position. Otherwise the first position is !
! ! used for the value. !
! ! -45.0 to 45.0 deg/sec !
! ! param. ADIRU 04.1.326.01 !
! ! 04.2.326.10 !
!--------------!------------------------------------------------------!
! ROLL ! Roll Angle !
! X999 ! Format: Negative values are indicated by '-' in the!
! ! first position. Otherwise the first position has a !
! ! '0'. !
! ! -90.0 to 90.0 deg !
! ! param. ADIRU 04.1.325.01 !
! ! 04.2.325.10 !
!--------------!------------------------------------------------------!
! ROLR ! Body Roll Rate !
! X999 ! Format: Negative values are indicated by '-' in the!
! ! first position. Otherwise the first position is !
! ! used for the value. !
! ! -45.0 to 45.0 deg/sec !
! ! param. ADIRU 04.1.327.01 !
! ! 04.2.327.10 !
!--------------!------------------------------------------------------!
! YAW ! YAW Rate !
! X999 ! Format: Negative values are indicated by '-' in the!
! ! first position. Otherwise the first position has a !
! ! '0'. !
! ! -45.0 to 45.0 deg/sec !
! ! param. ADIRU 04.1.330.01 !
! ! 04.2.330.10 !
!--------------!------------------------------------------------------!
! VRTA ! Normal Acceleration !
! X999 ! Format: Negative values are indicated by '-' in the!
! ! first position. Otherwise the first position is !
! ! used for the value. !
! ! -3.00 to 6.00 g !
! ! param. SDAC 29.1.333.01 !
! ! 29.2.333.10 !
!--------------!------------------------------------------------------!
! LONA ! Longitudinal Acceleration !
! X999 ! Format: Negative values are indicated by '-' in the!
! ! first position. Otherwise the first position is !
! ! used for the value. !
! ! (-1.00 to 1.00 g) !
! ! param. SDAC 29.1.331.01 !
! ! 29.2.331.10 !
!--------------!------------------------------------------------------!
! LATA ! Lateral Acceleration !
! X999 ! Format: Negative values are indicated by '-' in the!
! ! first position. Otherwise the first position is !
! ! used for the value. !
! ! (-1.00 to 1.00 g) !
! ! param. SDAC 29.1.332.01 !
! ! 29.2.332.10 !
+---------------------------------------------------------------------+

(4) Load Report Data Field Description <15>
NOTE: Reports that are transmitted from the ACARS system do not have report lines without a line identifier.
Report line S1 contains snapshot data at Y15.0 seconds before Land/Event.
Report line S2 contains snapshot data at Land/Event.
Report line S3 contains the "max-values" from the time interval Y15.1 seconds before Land/Event to 15.2 seconds after Land/Event.
Report line S4 contains the "min-values" from the time interval Y15.1 seconds before Land/Event to 15.2 seconds after Land/Event.
The report lines T1, T2, T3 and T4 is generated if the a/c bounced and the appropriate logic conditions are true. If not, these lines are omitted (inclusive header lines 46, 49, 53 and 54).
+--------------+------------------------------------------------------+
! Value ! Content Description !
!--------------+------------------------------------------------------!
! ESN ! Engine Serial Number !
! 999999 ! Format: 000000 to 999999 !
! ! Source: ECU Engine 1 7C.1.046.01 digit 3, 2, 1 !
! ! 7C.1.047.01 digit 6, 5, 4 !
! ! Engine 2 7C.2.046.10 digit 3, 2, 1 !
! ! 7C.2.047.10 digit 6, 5, 4 !
! ! !
! ! NOTE: For the IAE engines, 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 ! Format: 00000 to 99999 hours !
! ! Source: DMU 0D.1.060.01 Engine 1 !
! ! 0D.1.060.10 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 EHRS through the MCDU!
! ! e.g. if the DMU is changed on the A/C. !
!--------------!------------------------------------------------------!
! AP ! Auto Pilot Status !
! 99 ! Format: 00 to 24 !
! ! Source: FMGC 1 and 2 (FGC part) for Auto Pilot AP1 !
! ! and AP2 !
!+-------------+--------------------+-------------------+------------+!
!! Auto Pilot ! AP1 ! AP2 ! !!
!! Status ! Report Line EC: ! Report Line EE: ! Definition:!!
!!-------------+--------------------+-------------------+------------!!
!!00 ! -------------------!-------------------! No Mode !!
!! ! ! ! Active !!
!!-------------! -------------------!-------------------!------------!!
!!01 ! 01.1.275.00.11 = 1 ! 01.2.275.00.11 = 1!RUNWAY Mode !!
!!-------------! -------------------!-------------------!------------!!
!!02 ! 01.1.275.00.12 = 1 ! 01.2.275.00.12 = 1!NAV Mode !!
!!-------------! -------------------!-------------------!------------!!
!!03 ! 01.1.275.00.13 = 1 ! 01.2.275.00.13 = 1!LOC CAPTURE !!
!! ! ! !Mode !!
!!-------------! -------------------!-------------------!------------!!
!!04 ! 01.1.275.00.14 = 1 ! 01.2.275.00.14 = 1!LOC TRACK !!
!! ! ! !Mode !!
!!-------------! -------------------!-------------------!------------!!
!!05 ! 01.1.275.00.15 = 1 ! 01.2.275.00.15 = 1!Roll GO !!
!! ! ! !AROUND Mode !!
!!-------------! -------------------!-------------------!------------!!
!!06 ! 01.1.275.00.16 = 1 ! 01.2.275.00.16 = 1!HEADING Mode!!
!!-------------! -------------------!-------------------!------------!!
!!07 ! 01.1.275.00.17 = 1 ! 01.2.275.00.17 = 1!TRACK Mode !!
!!-------------! -------------------!-------------------!------------!!
!!08 ! 01.1.274.00.15 = 1 ! 01.2.274.00.15 = 1!PITCH TO !!
!! ! ! !Mode !!
!!-------------! -------------------!-------------------!------------!!
!!09 ! 01.1.274.00.16 = 1 ! 01.2.274.00.16 = 1!PITCH GA !!
!! ! ! !Mode !!
!!-------------! -------------------!-------------------!------------!!
!!10 ! 01.1.274.00.17 = 1 ! 01.2.274.00.17 = 1!V/S Mode !!
!!-------------! -------------------!-------------------!------------!!
!!11 ! 01.1.274.00.18 = 1 ! 01.2.274.00.18 = 1!FPA Mode !!
!!-------------! -------------------!-------------------!------------!!
!!12 ! 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! !!
!!-------------! -------------------!-------------------!------------!!
!!13 ! 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! !!
!!-------------! -------------------!-------------------!------------!!
!!14 ! 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! !!
!!-------------! -------------------!-------------------!------------!!
!!15 ! 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! !!
!!-------------! -------------------!-------------------!------------!!
!!16 ! 01.1.274.00.23 = 1 ! 01.2.274.00.23 = 1!FINAL DES !!
!! ! ! !Mode !!
!!-------------! -------------------!-------------------!------------!!
!!17 ! 01.1.274.00.24 = 1 ! 01.2.274.00.24 = 1!EXPED. Mode !!
!!-------------! -------------------!-------------------!------------!!
!!18 ! 01.1.146.00.14 = 1 ! 01.2.146.00.14 = 1!LAND TRACK !!
!! ! ! !Mode !!
!!-------------! -------------------!-------------------!------------!!
!!19 ! 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! !!
!!-------------! -------------------!-------------------!------------!!
!!20 ! 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! !!
!!-------------! -------------------!-------------------!------------!!
!!21 ! 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! !!
!!-------------! -------------------!-------------------!------------!!
!!22 ! 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! !!
!!-------------! -------------------!-------------------!------------!!
!!23 ! 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! !!
!!-------------! -------------------!-------------------!------------!!
!!24 ! 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: !
! ! 0D.1.274.01 AP1 printed in report line EC !
! ! 0D.1.274.10 AP2 printed in report line EE !
! ! Combined Auto Pilot Modes !
! ! The longitudinal auto pilot mode (1 to G) shows !
! ! the left position for the AP1 and AP2 print format !
! ! The lateral auto pilot mode (1 to 8) shows the right !
! ! position for the AP1 and AP2 print format. !
! ! In case of a combined auto pilot mode e.g. DES mode !
! ! and NAV mode are engaged simultaneously, then E3 !
! ! shows bellow AP1 and AP2. !
! ! XX Auto Pilot Modes: !
! ! !! !
! ! !!__Lateral Modes: 0 = NO MODE !
! ! ! 1 = HEADING !
! ! ! 2 = TRACK !
! ! ! 3 = NAV !
! ! ! 4 = LOCK CAPTURE !
! ! ! 5 = LOCK TRACK !
! ! ! 6 = LAND TRACK !
! ! ! 7 = RUNWAY !
! ! ! 8 = ROLL GO AROUND !
! ! ! !
! ! !__Longitudinal Modes: 0 = NO MODE !
! ! 1 = PITCH G/A !
! ! 2 = PITCH TO !
! ! 3 = G/S TRACK !
! ! 4 = G/S CAPTURE !
! ! 5 = V/S !
! ! 6 = FPA !
! ! 7 = ALT !
! ! 8 = ALT ACQ !
! ! 9 = OPEN CLB !
! ! A = OPEN DES !
! ! B = IM CLB !
! ! C = IM DES !
! ! D = CLB !
! ! E = DES !
! ! F = FINAL DES !
! ! G = EXPEDITE !
!--------------!------------------------------------------------------!
! FLAP ! FLAP Position !
! 9999 ! Format: 0 to 40.0 deg !
! ! Negative values are shown with - on the !
! ! first position. If not, the first position !
! ! contains a 0. !
! ! Source: SFCC 1B.1.137.01 FLAP System 1 !
! ! 1B.2.137.10 FLAP System 2 !
!--------------!------------------------------------------------------!
! SLAT ! SLAT Position !
! 9999 ! Format: 0 to 27.0 deg !
! ! Source: SFCC 1B.1.127.01 !
! ! 1B.2.127.10 !
!--------------!------------------------------------------------------!
! MAX ! Maximum value of the exceedance parameter from !
! X999 ! time interval 0.5 sec before landing detection !
! ! until 0.5 sec after landing detection. !
! ! For logic 4100 see remark. !
! ! !
! ! Format: Depends on exceeded parameter !
! ! !
! ! Source: Depends on exceeded parameter !
! ! !
! ! Remark: If code = 4100 (exceedance RALR) the !
! ! maximum value is taken as an average value !
! ! from a window of RALR data between S1 and !
! ! S2 around the landing detection event. If !
! ! code = 4500 the highest maximum of the !
! ! exceeding parameter either at landing or at!
! ! bounce landing is displayed. !
!--------------!------------------------------------------------------!
! LIM ! Programmable Limit which was exceeded !
! X999 ! Format: Depends of exceeded parameter !
! ! Source: Depends of exceeded parameter !
! ! Remark: If code = 4500 the limit which was exceeded!
! ! is displayed in reference to MAX either at !
! ! landing or at bounce landing. !
!--------------!------------------------------------------------------!
! COUNTS ! Counter for spoiler 4 extensions !
! ! Format: 0 to 9999 !
! ! 999 999 999 999 999 !
! ! --- --- --- --- --- !
! ! 0 > Spoiler >= -5 ______! ! ! ! ! !
! ! -5 > Spoiler >= -10 ___________! ! ! ! !
! ! -10 > Spoiler >= -15 ________________! ! ! !
! ! -15> Spoiler >= -20 _____________________! ! !
! ! Spoiler < -20 __________________________! !
! ! !
! ! Source: 6C.1.364.01 LH Spoiler 4 Position !
! ! 6C.2.364.10 !
! ! 6C.1.374.01 RH Spoiler 4 Position !
! ! 6C.2.374.10 !
! ! 6C.1.044.01.24 = 1 Spoiler 4 Fault !
! ! 6C.2.044.10.24 = 1 !
! ! 6C.1.365.01 LH Spoiler 5 Position !
! ! 6C.2.365.10 !
! ! 6C.1.375.01 RH Spoiler 5 Position !
! ! 6C.2.375.10 !
! ! 6C.1.044.01.25 = 1 Spoiler 5 Fault !
! ! 6C.2.044.10.25 !
! ! 6C.1.041.01.21 = 1 Load Alleviation Active !
! ! (LAF) !
! ! 6C.2.041.10.21 !
! ! Note: The max extension values of the LH Spoiler !
! ! 4 is counted as long as LAF is active and !
! ! Spoiler 4 is not fault. The value of LH !
! ! Spoiler 4 is compared with the value of RH !
! ! Spoiler 4, which are found at the same !
! ! time of max LH Spoiler 4. The lower one of !
! ! these values effects the counts as defined !
! ! above. If Spoiler 4 is fault and Spoiler 5 !
! ! is not fault, the Spoiler 5 LH and RH is !
! ! used for calculation and counts. !
!--------------!------------------------------------------------------!
! REASON ! Reason for exceedance !
! XXXXXXXXXX ! Format: Up to 10 characters !
! XX ! RALR Code: 4100 !
! ! VRTA Code: 4400, 4500, 5100,5200 and 5300!
! ! GW Code: 4800, 4900 !
! ! SPCT Code: 5400 !
! ! Source: DMU !
! ! Note: If the report was not triggered by a limit !
! ! exceedance, this field contains blanks. !
!--------------!------------------------------------------------------!
! RALT ! Radio Altitude !
! X999 ! Format: Negative values are shown with '-' in the !
! ! first position. If not, the first position !
! ! is used for the value. !
! ! -20 to 2500 ft !
! ! Source: DMC 25.1.164.01 !
! ! 25.1.164.10 !
!--------------!------------------------------------------------------!
! RALR ! Radio Altitude Rate !
! X999 ! Format: Negative values are shown with '-' in the !
! ! first position. If not, the first position !
! ! is used for the value. !
! ! -99.9 to +99.9 ft/sec !
! ! Source: DMU !
! ! Remark: The calculation of Radio Altitude Rate is !
! ! started when: RALT<RALTL1 !
! ! The calculation is performed with 16Hz cycles!
! ! (T=0.0625 s) !
! ! The calculation uses the current calculation !
! ! cycle current and data values. These data are!
! ! named as follows: !
! ! e.g. !
! ! IVV = IVV actual sample n !
! ! IVV1 = IVV previous sample n-1 !
! ! !
! ! PTCHACC = PTCHACC actual sample n !
! ! PTCHACC1 = PTCHACC previous sample n-1 !
! ! PTCHACC2 = PTCHACC previous sample n-2 !
! ! !
! ! The calculation uses the following !
! ! programmable constants: !
! ! D geometrical correction factor for ROLR ft/deg!
! ! DX lever arm correction (x-axis) for R/A RALT ft!
! ! DZ lever arm correction (z-axis) for R/A RALT ft!
! ! DXTPIR lever arm correction (x-axis) for PTCH ft!
! ! FC filter frequency Hz!
! ! K1 filter constant !
! ! K2 filter constant !
! ! K3 filter constant !
! ! THETA0 average PTCH at touchdown deg!
! ! !
! ! Radio Altitude Rate calculation: !
! ! 1. Start Values !
! ! !
! ! For the very first calculation the start values are !
! ! defined as follows: !
! ! PTCHRAW1 = 0.0 !
! ! PTCHACC1 = 0.0 !
! ! PTCHACC2 = 0.0 !
! ! PTCR1 = 0.0 !
! ! EN1 = 0.0 !
! ! VZN1 = IVV1/60.0 !
! ! ZN1 = RALT !
! ! !
! ! 2. Algorithm with KALMAN filter !
! ! The algorithm comprises of the following equations: !
! ! PTCHRAW = (PTCR-PTCR1)/T !
! ! PTCHACC = PTCHACC1+T*(2*PI*FC)*(PTCHRAW+PTCHRAW1- !
! ! PTCHACC1-PTCHACC2)/2 !
! ! NZTCOR = VACC*9.81/0.3048-DXTPIR*PTCHACC/57.3 !
! ! *cos(PTCH/57.3) !
! ! HRACOR = RALT+DX*(sin(PTCH/57.3)-sin(THEATA0/57.3))!
! ! -DZ*(cos(PTCH/57.3)-cos(THEATA0/57.3)) !
! ! EPSN = ZN1-HRACOR !
! ! EN = EN1+T*K3*EPSN !
! ! VZN = VZN1+T*(VZN-K2*EPSN) !
! ! VZNU = VZN-D*ABS(ROLR) !
! ! RALR = VZNU !
!--------------!------------------------------------------------------!
! PTCH ! Pitch Angle !
! X999 ! Format: Negative values are shown with '-' on the !
! ! first position. If not, the first position !
! ! is used for the value. !
! ! -99.0 to 90.0 deg !
! ! Source: ADIRU 04.1.324.01 !
! ! 04.2.324.10 !
!--------------!------------------------------------------------------!
! PTCR ! Body Pitch Rate !
! X999 ! Format: Negative values are shown with '-' on the !
! ! first position. If not,the first position !
! ! is used for the value. !
! ! -45.0 to 45.0 deg/sec !
! ! Source: ADIRU 04.1.326.01 !
! ! 04.2.326.10 !
!--------------!------------------------------------------------------!
! ROLL ! Roll Angle !
! X999 ! Format: Negative values are shown with '-' on the !
! ! first position. If not, the first position !
! ! contains a '0'. !
! ! -90.0 to 90.0 deg !
! ! Source: ADIRU 04.1.325.01 !
! ! 04.2.325.10 !
!--------------!------------------------------------------------------!
! ROLR ! Body Roll Rate !
! X999 ! Format: Negative values are shown with '-' on the !
! ! first position. If not, the first position !
! ! is used for the value. !
! ! -45.0 to 45.0 deg/sec !
! ! Source: ADIRU 04.1.327.01 !
! ! 04.2.327.10 !
!--------------!------------------------------------------------------!
! YAW ! YAW Rate !
! X999 ! Format: Negative values are shown with '-' on the !
! ! first position. If not, the first position !
! ! contains a '0'. !
! ! -45.0 to 45.0 deg/sec !
! ! Source: ADIRU 04.1.330.01 !
! ! 04.2.330.10 !
!--------------!------------------------------------------------------!
! VRTA ! Normal Acceleration !
! X999 ! Format: Negative values are shown with '-' on the !
! ! first position. If not, the first position !
! ! is used for the value. !
! ! -3.00 to 6.00 g !
! ! Source: SDAC 29.1.333.01 !
! ! 29.2.333.01 !
!--------------!------------------------------------------------------!
! LONA ! Longitudinal Acceleration !
! X999 ! Format: Negative values are shown with '-' on the !
! ! first position. If not, the first position !
! ! is used for the value. !
! ! -1.00 to 1.00 g !
! ! Source: SDAC 29.1.331.01 !
! ! 29.2.331.01 !
!--------------!------------------------------------------------------!
! LATA ! Lateral Acceleration !
! X999 ! Format: Negative values are shown with '-' on the !
! ! first position. If not, the first position !
! ! is used for the value. !
! ! -1.00 to 1.00 g !
! ! Source: SDAC 29.1.332.01 !
! ! 29.2.332.01 !
+--------------+------------------------------------------------------+

(5) Load Report Data Field Description <15>
NOTE: Reports that are transmitted from the ACARS system do not have report lines without a line identifier.
Report line S1 contains snapshot data at 'Y15.0' seconds before Land/Event.
Report line S2 contains snapshot data at Land/Event.
Report line S3 contains the "max-values" from the time interval 'Y15.1' seconds before Land/Event to '15.2' seconds after Land/Event.
Report line S4 contains the "min-values" from the time interval 'Y15.1' seconds before Land/Event to '15.2' seconds after Land/Event.
The report lines T1, T2, T3 and T4 is generated if the a/c bounced and the appropriate logic conditions are true. If not these lines are omitted (inclusive header lines 46, 49, 53 and 54).
+---------------------------------------------------------------------+
! Value ! Content Description !
!--------------!------------------------------------------------------!
! ESN ! Engine Serial Number !
! 999999 ! (000000 to 999999) !
! ! EECU/ECU Eng 1 param. 7C.1.046.01 digit 3, 2, 1 !
! ! 7C.1.047.01 digit 6, 5, 4 !
! ! Eng 2 param. 7C.2.046.10 digit 3, 2, 1 !
! ! 7C.2.047.10 digit 6, 5, 4 !
! ! !
! ! NOTE: For the IAE engines, 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 0D.1.060.01 !
! ! Engine 2 0D.1.060.10 !
! ! NOTE: 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 regonized by the DMU. It is possible to set the !
! ! EHRS through the MCDU, e.g. if the DMU is changed !
! ! on the a/c. !
!--------------!------------------------------------------------------!
! Auto Pilot Status 99 !
! !
! Format: ! Number of respective status 00 to 24 !!
! Source: ! FMGC 1 and 2 (FGC part) for Auto Pilot 1 and 2 !!
!!-------------!--------------------!-------------------!------------!!
!!Auto Pilot ! AP1 ! AP2 ! !!
!!Status ! Report line EC: ! Report line EE: ! Difinition:!!
!!-------------!--------------------!-------------------!------------!!
!!00 ! -------------------!-------------------! No Mode !!
!! ! ! ! Active !!
!!-------------! -------------------!-------------------!------------!!
!!01 ! 01.1.275.00.11 = 1 ! 01.2.275.00.11 = 1!RUNWAY Mode !!
!!-------------! -------------------!-------------------!------------!!
!!02 ! 01.1.275.00.12 = 1 ! 01.2.275.00.12 = 1!NAV Mode !!
!!-------------! -------------------!-------------------!------------!!
!!03 ! 01.1.275.00.13 = 1 ! 01.2.275.00.13 = 1!LOC CAPTURE !!
!! ! ! !Mode !!
!!-------------! -------------------!-------------------!------------!!
!!04 ! 01.1.275.00.14 = 1 ! 01.2.275.00.14 = 1!LOC TRACK !!
!! ! ! !Mode !!
!!-------------! -------------------!-------------------!------------!!
!!05 ! 01.1.275.00.15 = 1 ! 01.2.275.00.15 = 1!Roll GO !!
!! ! ! !AROUND Mode !!
!!-------------! -------------------!-------------------!------------!!
!!06 ! 01.1.275.00.16 = 1 ! 01.2.275.00.16 = 1!HEADING Mode!!
!!-------------! -------------------!-------------------!------------!!
!!07 ! 01.1.275.00.17 = 1 ! 01.2.275.00.17 = 1!TRACK Mode !!
!!-------------! -------------------!-------------------!------------!!
!!08 ! 01.1.274.00.15 = 1 ! 01.2.274.00.15 = 1!PITCH T/O !!
!! ! ! !Mode !!
!!-------------! -------------------!-------------------!------------!!
!!09 ! 01.1.274.00.16 = 1 ! 01.2.274.00.16 = 1!PITCH GA !!
!! ! ! !Mode !!
!!-------------! -------------------!-------------------!------------!!
!!10 ! 01.1.274.00.17 = 1 ! 01.2.274.00.17 = 1!V/S Mode !!
!!-------------! -------------------!-------------------!------------!!
!!11 ! 01.1.274.00.18 = 1 ! 01.2.274.00.18 = 1!FPA Mode !!
!!-------------! -------------------!-------------------!------------!!
!!12 ! 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! !!
!!-------------! -------------------!-------------------!------------!!
!!13 ! 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! !!
!!-------------! -------------------!-------------------!------------!!
!!14 ! 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! !!
!!-------------! -------------------!-------------------!------------!!
!!15 ! 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! !!
!!-------------! -------------------!-------------------!------------!!
!!16 ! 01.1.274.00.23 = 1 ! 01.2.274.00.23 = 1!FINAL DES !!
!! ! ! !Mode !!
!!-------------! -------------------!-------------------!------------!!
!!17 ! 01.1.274.00.24 = 1 ! 01.2.274.00.24 = 1!EXPED. Mode !!
!!-------------! -------------------!-------------------!------------!!
!!18 ! 01.1.146.00.14 = 1 ! 01.2.146.00.14 = 1!LAND TRACK !!
!! ! ! !Mode !!
!!-------------! -------------------!-------------------!------------!!
!!19 ! 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! !!
!!-------------! -------------------!-------------------!------------!!
!!20 ! 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! !!
!!-------------! -------------------!-------------------!------------!!
!!21 ! 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! !!
!!-------------! -------------------!-------------------!------------!!
!!22 ! 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! !!
!!-------------! -------------------!-------------------!------------!!
!!23 ! 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! !!
!!-------------! -------------------!-------------------!------------!!
!!24 ! 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: !
! ! 0D.1.274.01 AP1 printed in report line EC !
! ! 0D.1.274.10 AP2 printed in report line EE !
!--------------!------------------------------------------------------!
! FLAP ! FLAP Position !
! 9999 ! (0 to 40.0 deg) !
! ! SFCC 1B.1.137.01 !
! ! 1B.2.137.10 !
!--------------!------------------------------------------------------!
! SLAT ! SLAT Position !
! 9999 ! (0 to 27.0 deg) !
! ! SFCC 1B.1.127.01 !
! ! 1B.2.127.10 !
!--------------!------------------------------------------------------!
! MAX ! Maximum value of the exceedance parameter from !
! X999 ! time interval 0.5 sec. before 'landing detection' !
! ! until 0.5 sec. after 'landing detection'. !
! ! For logic 4100 see remark. !
! ! !
! ! Format: Depends on exceeded parameter !
! ! !
! ! Source: Depends on exceeded parameter !
! ! !
! ! NOTE: If code = 4100 (exceedance RALR) the !
! ! maximum value is taken as an average value from !
! ! a window of RALR data between S1 and S2 around !
! ! the landing detection event. !
! ! If code = 4500 the highest maximum of the exceeding!
! ! parameter either at landing or at bounce landing !
! ! is displayed. !
!--------------!------------------------------------------------------!
! LIM ! Programmable Limit which was exceeded !
! X999 ! Format: Depends of exceeded parameter !
! ! !
! ! Source: Depends of exceeded parameter !
! ! !
! ! NOTE: If code = 4500 the limit which was exceeded !
! ! is displayed in reference to MAX either at landing !
! ! or at bounce landing. !
!--------------!------------------------------------------------------!
! COUNTS ! Counter for spoiler 4 extensions !
! ! 999 999 999 999 999 !
! ! --- --- --- --- --- !
! ! 0 > Spoiler >= -5 ______! ! ! ! ! !
! ! -5 > Spoiler >= -10 ___________! ! ! ! !
! ! -10 > Spoiler >= -15 ________________! ! ! !
! ! -15 > Spoiler >= -20 ____________________! ! !
! ! Spoiler < -20 __________________________! !
! ! !
! ! Format: 0 to 9999 !
! ! !
! Source: ! 6C.1.364.01 LH Spoiler 4 Position !
! ! 6C.2.364.10 !
! ! 6C.1.374.01 RH Spoiler 4 Position !
! ! 6C.2.374.10 !
! ! 6C.1.044.01.24 = 1 Spoiler 4 Fault !
! ! 6C.2.044.10.24 = 1 !
! ! 6C.1.365.01 LH Spoiler 5 Position !
! ! 6C.2.365.10 !
! ! 6C.1.375.01 RH Spoiler 5 Position !
! ! 6C.2.375.10 !
! ! 6C.1.044.01.25 = 1 Spoiler 5 Fault !
! ! 6C.2.044.10.25 !
! ! 6C.1.041.01.21 = 1 Load Alleviation Active (LAF) !
! ! 6C.2.041.10.21 !
! ! Note: The max extension values of the LH Spoiler !
! ! 4 is counted as long as LAF is active and Spoiler 4!
! ! is not fault. The value of LH Spoiler 4 is compared!
! ! with the value of RH Spoiler 4, which are detected !
! ! at the same time of max LH Spoiler 4. The lower one!
! ! of these values effects the counts as defined above!
! ! If Spoiler 4 is fault and Spoiler 5 is not fault, !
! ! the Spoiler 5 LH and RH is used for calculation !
! ! and counts. !
!--------------!------------------------------------------------------!
! REASON ! Reason for exceedance !
! XXXXXXXXXX ! Format: Up to 10 characters !
! ! RALR Code: 4100 !
! ! VRTA Code: 4400, 4500,5100, 5200, 5300!
! ! GW Code: 4800, 4900 !
! ! SPCT Code: 5400 !
! ! Source: DMU !
! ! Remark: If the report was not triggered by a limit !
! ! exceedance, this field contains blanks. !
!--------------!------------------------------------------------------!
! RALT ! Radio Altitude !
! X999 ! Format: Negative values are shown with 'N' in the !
! ! first position. Otherwise the first position is !
! ! used for the value. !
! ! (-20 to 2500 ft) !
! ! DMC 25.1.164.01 !
! ! 25.1.164.10 !
!--------------!------------------------------------------------------!
! RALR ! Radio Altitude Rate !
! X999 ! Format: Negative values are shown with 'N' in the !
! ! first position. Otherwise the first position is used!
! ! for the value. !
! ! (-99.9 to 99.9 ft/sec) !
! ! Source: DMU !
! ! Note: The calculation of Radio Altitude Rate is !
! ! started when: RALT<RALTL1 !
! ! - The calculation is performed with 16 Hz cycles !
! ! (T=0.0625 s) !
! ! - The calculation uses the current calculation !
! ! cycle current and data values. These data are !
! ! named as follows: !
! ! e.g. !
! ! IVV = IVV actual sample n !
! ! IVV1 = IVV previous sample n-1 !
! ! !
! ! PTCHACC = PTCHACC actual sample n !
! ! PTCHACC1 = PTCHACC previous sample n-1 !
! ! PTCHACC2 = PTCHACC previous sample n-2 !
! ! !
! ! - The calculation uses the following programmable !
! ! constants: !
! ! D geometrical correction factor for ROLR ft/deg!
! ! DX lever arm correction (x-axis) for R/A RALT ft!
! ! DZ lever arm correction (z-axis) for R/A RALT ft!
! ! DXTPIR lever arm correction (x-axis) for PTCH ft!
! ! FC filter frequency Hz!
! ! K1 filter constant !
! ! K2 filter constant !
! ! K3 filter constant !
! ! THETA0 average PTCH at touchdown deg!
! ! !
! ! Radio Altitude Rate calculation: !
! ! 1. Start Values !
! ! !
! ! For the very first calculation the start values are !
! ! defined as follows: !
! ! PTCHRAW1 = 0.0 !
! ! PTCHACC1 = 0.0 !
! ! PTCHACC2 = 0.0 !
! ! PTCR1 = 0.0 !
! ! EN1 = 0.0 !
! ! VZN1 = IVV/60.0 !
! ! ZN1 = RALT !
! ! !
! ! 2. Algorithm with KALMAN filter !
! ! The algorithm comprises of the following equations: !
! ! PTCHRAW = (PTCR-PTCR1)/T !
! ! PTCHACC = PTCHACC1+T*(2*PI*FC)*(PTCHRAW+PTCHRAW1- !
! ! PTCHACC1-PTCHACC2)/2 !
! ! NZTCOR = VACC*9.81/0.3048-DXTPIR*PTCHACC/57.3 !
! ! *cos(PTCH/57.3) !
! ! HRACOR = RALT+DX*(sin(PTCH/57.3)-sin(THEATA0/57.3))!
! ! -DZ*(cos(PTCH/57.3)-cos(THEATA0/57.3)) !
! ! EPSN = ZN1-HRACOR !
! ! EN = EN1+T*K3*EPSN !
! ! VZN = VZN1+T*(VZN-K2*EPSN) !
! ! VZNU = VZN-D*ABS(ROLR) !
! ! RALR = VZNU !
!--------------!------------------------------------------------------!
! PTCH ! Pitch Angle !
! X999 ! Format: Negative values are shown with 'N' on the !
! ! first position. Otherwise the first position is !
! ! used for the value. !
! ! (-99.0 to 90.0 deg) !
! ! ADIRU 04.1.324.01 !
! ! 04.2.324.10 !
!--------------!------------------------------------------------------!
! PTCR ! Body Pitch Rate !
! X999 ! Format: Negative values are shown with 'N' on the !
! ! first position. Otherwise the first position is !
! ! used for the value. !
! ! (-45.0 to 45.0 deg/sec) !
! ! ADIRU 04.1.326.01 !
! ! 04.2.326.10 !
!--------------!------------------------------------------------------!
! ROLL ! Roll Angle !
! X999 ! Format: Negative values are shown with 'N' on the !
! ! first position. Otherwise the first position is !
! ! used for the value. !
! ! (-90.0 to 90.0 deg/sec) !
! ! ADIRU 04.1.325.01 !
! ! 04.2.325.10 !
!--------------!------------------------------------------------------!
! ROLR ! Body Roll Rate !
! X999 ! Format: Negative values are shown with 'N' on the !
! ! first position. Otherwise the first position is !
! ! used for the value. !
! ! (-45.0 to 45.0 deg/sec) !
! ! ADIRU 04.1.327.01 !
! ! 04.2.327.10 !
!--------------!------------------------------------------------------!
! YAW ! Yaw Rate !
! X999 ! Format: Negative values are shown with 'N' on the !
! ! first position. Otherwise the first position !
! ! is used for the value '0'. !
! ! (-45.0 to 45.0 deg/sec) !
! ! ADIRU 04.1.330.01 !
! ! 04.2.330.10 !
!--------------!------------------------------------------------------!
! VRTA ! Normal Acceleration !
! X999 ! Format: Negative values are shown with 'N' on the !
! ! first position. Otherwise the first position is !
! ! used for the value. !
! ! (-3.00 to 6.00 g) !
! ! SDAC 29.1.333.01 !
! ! 29.2.333.01 !
!--------------!------------------------------------------------------!
! LONA ! Longitudinal Acceleration !
! X999 ! Format: Negative values are shown with 'N' on the !
! ! first position. Otherwise the first position is !
! ! used for the value. !
! ! (-1.00 to 1.00 g) !
! ! SDAC 29.1.331.01 !
! ! 29.2.331.01 !
!--------------!------------------------------------------------------!
! LATA ! Lateral Acceleration !
! X999 ! Format: Negative values are shown with 'N' on the !
! ! first position. Otherwise the first position is !
! ! used for the value. !
! ! (-1.00 to 1.00 g) !
! ! SDAC 29.1.332.01 !
! ! 29.2.332.01 !
+---------------------------------------------------------------------+

(6) Load Report Data Field Description <15>
NOTE: Reports that are transmitted from the ACARS system do not have report lines without a line identifier.
Report line S1 contains snapshot data at 'Y15.0' seconds before Land/Event.
Report line S2 contains snapshot data at 'Land/Event.
Report line S3 contains the "max-values" from the time interval 'Y15.1' seconds before Land/Event to '15.2' seconds after Land/Event.
Report line S4 contains the "min-values" from the time interval 'Y15.1' seconds before Land/Event to '15.2' seconds after Land/Event..
The report lines T1, T2, T3 and T4 shall be generated if the a/c bounced and the appropriate logic conditions are true. Otherwise these lines shall be omitted (inclusive header lines 46, 49, 53 and 54).
+---------------------------------------------------------------------+
! Value ! Content Description !
!--------------!------------------------------------------------------!
! ESN ! Engine Serial Number !
! 999999 ! (000000 to 999999) !
! ! ECU Eng 1 param. 7C.1.046.01 digit 3, 2, 1 !
! ! 7C.1.047.01 digit 6, 5, 4 !
! ! Eng 2 param. 7C.2.046.10 digit 3, 2, 1 !
! ! 7C.2.047.10 digit 6, 5, 4 !
! ! !
! ! NOTE: For the IAE engines, 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 0D.1.060.01 !
! ! Engine 2 0D.1.060.10 !
! ! Remark: Time between "Main (LH and RH) Landing Gear!
! ! Decompressed" and "Main (LH and RH) Landing!
! ! Gear Compressed". The EHRS shall be set to !
! ! zero if a new ESN is recognized by the DMU.!
! ! It shall be possible to set the EHRS via !
! ! the MCDU, e.g. if the DMU is changed on the!
! ! A/C. !
!--------------!------------------------------------------------------!
! AP ! Auto Pilot Status !
! 99 ! (00 to 24) !
! ! FMGC 1 and 2 (FGC part) for Auto Pilot AP1 and AP2 !
!!-------------!--------------------!-------------------!------------!!
!!Auto Pilot ! AP1 ! AP2 ! !!
!!Status ! Report Line EC: ! Report Line EE: ! Definition:!!
!!-------------!--------------------!-------------------!------------!!
!!00 ! -------------------!-------------------! No Mode !!
!! ! ! ! Active !!
!!-------------! -------------------!-------------------!------------!!
!!01 ! 01.1.275.00.11 = 1 ! 01.2.275.00.11 = 1!RUNWAY Mode !!
!!-------------! -------------------!-------------------!------------!!
!!02 ! 01.1.275.00.12 = 1 ! 01.2.275.00.12 = 1!NAV Mode !!
!!-------------! -------------------!-------------------!------------!!
!!03 ! 01.1.275.00.13 = 1 ! 01.2.275.00.13 = 1!LOC CAPTURE !!
!! ! ! !Mode !!
!!-------------! -------------------!-------------------!------------!!
!!04 ! 01.1.275.00.14 = 1 ! 01.2.275.00.14 = 1!LOC TRACK !!
!! ! ! !Mode !!
!!-------------! -------------------!-------------------!------------!!
!!05 ! 01.1.275.00.15 = 1 ! 01.2.275.00.15 = 1!Roll GO !!
!! ! ! !AROUND Mode !!
!!-------------! -------------------!-------------------!------------!!
!!06 ! 01.1.275.00.16 = 1 ! 01.2.275.00.16 = 1!HEADING Mode!!
!!-------------! -------------------!-------------------!------------!!
!!07 ! 01.1.275.00.17 = 1 ! 01.2.275.00.17 = 1!TRACK Mode !!
!!-------------! -------------------!-------------------!------------!!
!!08 ! 01.1.274.00.15 = 1 ! 01.2.274.00.15 = 1!PITCH TO !!
!! ! ! !Mode !!
!!-------------! -------------------!-------------------!------------!!
!!09 ! 01.1.274.00.16 = 1 ! 01.2.274.00.16 = 1!PITCH GA !!
!! ! ! !Mode !!
!!-------------! -------------------!-------------------!------------!!
!!10 ! 01.1.274.00.17 = 1 ! 01.2.274.00.17 = 1!V/S Mode !!
!!-------------! -------------------!-------------------!------------!!
!!11 ! 01.1.274.00.18 = 1 ! 01.2.274.00.18 = 1!FPA Mode !!
!!-------------! -------------------!-------------------!------------!!
!!12 ! 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! !!
!!-------------! -------------------!-------------------!------------!!
!!13 ! 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! !!
!!-------------! -------------------!-------------------!------------!!
!!14 ! 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! !!
!!-------------! -------------------!-------------------!------------!!
!!15 ! 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! !!
!!-------------! -------------------!-------------------!------------!!
!!16 ! 01.1.274.00.23 = 1 ! 01.2.274.00.23 = 1!FINAL DES !!
!! ! ! !Mode !!
!!-------------! -------------------!-------------------!------------!!
!!17 ! 01.1.274.00.24 = 1 ! 01.2.274.00.24 = 1!EXPED. Mode !!
!!-------------! -------------------!-------------------!------------!!
!!18 ! 01.1.146.00.14 = 1 ! 01.2.146.00.14 = 1!LAND TRACK !!
!! ! ! !Mode !!
!!-------------! -------------------!-------------------!------------!!
!!19 ! 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! !!
!!-------------! -------------------!-------------------!------------!!
!!20 ! 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! !!
!!-------------! -------------------!-------------------!------------!!
!!21 ! 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! !!
!!-------------! -------------------!-------------------!------------!!
!!22 ! 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! !!
!!-------------! -------------------!-------------------!------------!!
!!23 ! 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! !!
!!-------------! -------------------!-------------------!------------!!
!!24 ! 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: !
! ! 0D.1.274.01 AP1 printed in report line EC !
! ! 0D.1.274.10 AP2 printed in report line EE !
! ! Combined Auto Pilot Modes !
! ! The longitudinal auto pilot mode (1 to G) shall !
! ! appear on the left position for the AP1 and AP2 print!
! ! format. !
! ! The lateral auto pilot mode (1 to 8) shall appear on !
! ! the right position for the AP1 and AP2 print format. !
! ! In case of a combined auto pilot mode e.g. DES mode !
! ! and NAV mode are engaged simultaneously, then 'E3' !
! ! shall appear bellow AP1 and AP2. !
! ! XX Auto Pilot Modes: !
! ! !! !
! ! !!__Lateral Modes: 0 = NO MODE !
! ! ! 1 = HEADING !
! ! ! 2 = TRACK !
! ! ! 3 = NAV !
! ! ! 4 = LOCK CAPTURE !
! ! ! 5 = LOCK TRACK !
! ! ! 6 = LAND TRACK !
! ! ! 7 = RUNWAY !
! ! ! 8 = ROLL GO AROUND !
! ! ! !
! ! !__Longitudinal Modes: 0 = NO MODE !
! ! 1 = PITCH G/A !
! ! 2 = PITCH TO !
! ! 3 = G/S TRACK !
! ! 4 = G/S CAPTURE !
! ! 5 = V/S !
! ! 6 = FPA !
! ! 7 = ALT !
! ! 8 = ALT ACQ !
! ! 9 = OPEN CLB !
! ! A = OPEN DES !
! ! B = IM CLB !
! ! C = IM DES !
! ! D = CLB !
! ! E = DES !
! ! F = FINAL DES !
! ! G = EXPEDITE !
!--------------!------------------------------------------------------!
! FLAP ! FLAP Actual Position !
! 9999 ! (0 to 40.0 deg) !
! ! (see table DT40 for special conversion)!
! ! Negative values are indicated by '-' on the !
! ! first position. Otherwise the first position !
! ! contains a '0'. !
! ! SFCC 1B.1.137.01 FLAP System 1 !
! ! 1B.2.137.10 FLAP System 2 !
!--------------!------------------------------------------------------!
! SLAT ! SLAT Position !
! 9999 ! (0 to 27.0 deg) !
! ! (see table DT41 for special conversion)!
! ! SFCC 1B.1.127.01 !
! ! 1B.2.127.10 !
!--------------!------------------------------------------------------!
! MAX ! Maximum Value of the exceedance parameter from !
! X999 ! time interval 0.5 sec. before 'landing detection' !
! ! until 0.5 sec. after 'landing detection'. !
! ! For logic 4100 see remark. !
! ! !
! ! Format: Depends on exceeded parameter !
! ! !
! ! Source: Depends on exceeded parameter !
! ! !
! ! Remark: If code = 4100 (exceedance RALR) the !
! ! maximum value shall be taken as an average !
! ! value from a window of RALR data between S1!
! ! and S2 around the landing detection event. !
! ! If code = 4500 the highest maximum of the !
! ! exceeding parameter either at landing or at!
! ! bounce landing is displayed. !
! ! !
!--------------!------------------------------------------------------!
! LIM ! Format: Depends on the parameter !
! X999 ! !
! ! Source: Depends on the parameter !
! ! !
! ! Remark: If code = 4500 the limit which was exceeded !
! ! shall be displayed in reference to MAX !
! ! either at landing or at bounce landing. !
!--------------!------------------------------------------------------!
! COUNTS ! Counter for spoiler 4 extensions !
! ! Format (0 to 9999) !
! ! 999 999 999 999 999 !
! ! --- --- --- --- --- !
! ! ! ! ! ! !___ 0 Deg > Spoiler >= - 5 !
! ! ! ! ! !________- 5 Deg > Spoiler >= -10 !
! ! ! ! !_____________-10 Deg > Spoiler >= -15 !
! ! ! !__________________-15 Deg > Spoiler >= -20 !
! ! !_______________________Spoiler < -20 !
! ! !
! ! 6C.1.364.01 LH Spoiler 4 Position !
! ! 6C.2.364.10 !
! ! 6C.1.374.01 RH Spoiler 4 Position !
! ! 6C.2.374.10 !
! ! 6C.1.044.01.24 = 1 Spoiler 4 Fault !
! ! 6C.2.044.10.24 = 1 !
! ! 6C.1.365.01 LH Spoiler 5 Position !
! ! 6C.2.365.10 !
! ! 6C.1.375.01 RH Spoiler 5 Position !
! ! 6C.2.375.10 !
! ! 6C.1.044.01.25 = 1 Spoiler 5 Fault !
! ! 6C.2.044.10.25 !
! ! 6C.1.041.01.21 = 1 Load Alleviation Active (LAF) !
! ! 6C.2.041.10.21 !
! ! Remark: The max extension values of the LH Spoiler !
! ! 4 is counted as long as LAF is active and !
! ! Spoiler 4 is not fault. The value of LH !
! ! Spoiler 4 is compared with the value of RH !
! ! Spoiler 4, which are detected at the same !
! ! time of max LH Spoiler 4. The lower one of !
! ! these values effects the counts as defined !
! ! above If Spoiler 4 is fault and Spoiler 5 !
! ! is not fault, the Spoiler 5 LH and RH is !
! ! used for calculation and counts. !
! ! !
!--------------!------------------------------------------------------!
! REASON ! Reason for exceedance XXXXXXXXXXXXXXXXXXXX !
! XXXXXXXXXX ! Format: Up to 10 characters !
! XXXXXXXXXX ! !
! ! RALR Code: 4100 !
! ! VRTA Code: 4400, 4500, 5100, 5200 and 5300 !
! ! GW Code: 4800, 4900 !
! ! SPCT Code: 5400 !
! ! Source: DMU !
! ! Remark: If the report was not triggered by a limit !
! ! exceedance, this field shall contain blanks. !
!--------------!------------------------------------------------------!
! RALT ! Radio Altitude !
! X999 ! Format: Negative values are indicated by '-' !
! ! in the first position. Otherwise the first position!
! ! shall be used for the value. !
! ! -20 to 2500 ft !
! ! DMC 25.1.164.01 !
! ! 25.1.164.10 !
!--------------!------------------------------------------------------!
! RALR ! Radio Altitude Rate !
! X999 ! Format: Negative values are indicated by '-' in !
! ! the first position. Otherwise the first position !
! ! are used for the value. !
! ! -99.9 to 99.9 ft/sec !
! ! !
! ! Source: DMU !
! ! Remark: The calculation of Radio Altitude Rate is !
! ! started when: RALT<RALTL1 !
! ! - The calculation is performed with 16 Hz cycles !
! ! (T=0.0625 s) !
! ! - The calculation uses the current calculation !
! ! cycle current and data values. These data are !
! ! named as follows: !
! ! e.g. !
! ! IVV = IVV actual sample n !
! ! IVV1 = IVV previous sample n-1 !
! ! !
! ! PTCHACC = PTCHACC actual sample n !
! ! PTCHACC1 = PTCHACC previous sample n-1 !
! ! PTCHACC2 = PTCHACC previous sample n-2 !
! ! !
! ! - The calculation uses the following programmable !
! ! constants: !
! ! D geometrical correction factor for ROLR ft/deg!
! ! DX lever arm correction (x-axis) for R/A RALT ft!
! ! DZ lever arm correction (z-axis) for R/A RALT ft!
! ! DXTPIR lever arm correction (x-axis) for PTCH ft!
! ! FC filter frequency Hz!
! ! K1 filter constant !
! ! K2 filter constant !
! ! K3 filter constant !
! ! THETA0 average PTCH at touchdown deg!
! ! !
! ! Radio Altitude Rate calculation: !
! ! 1. Start Values !
! ! !
! ! For the very first calculation the start values are !
! ! defined as follows: !
! ! PTCHRAW1 = 0.0 !
! ! PTCHACC1 = 0.0 !
! ! PTCHACC2 = 0.0 !
! ! PTCR1 = 0.0 !
! ! EN1 = 0.0 !
! ! VZN1 = IVV1/60.0 !
! ! ZN1 = RALT !
! ! !
! ! 2. Algorithm with KALMAN filter !
! ! The algorithm comprises of the following equations: !
! ! PTCHRAW = (PTCR-PTCR1)/T !
! ! PTCHACC = PTCHACC1+T*(2*PI*FC)*(PTCHRAW+PTCHRAW1- !
! ! PTCHACC1-PTCHACC2)/2 !
! ! NZTCOR = VACC*9.81/0.3048-DXTPIR*PTCHACC/57.3 !
! ! *cos(PTCH/57.3) !
! ! HRACOR = RALT+DX*(sin(PTCH/57.3)-sin(THEATA0/57.3))!
! ! -DZ*(cos(PTCH/57.3)-cos(THEATA0/57.3)) !
! ! EPSN = ZN1-HRACOR !
! ! EN = EN1+T*K3*EPSN !
! ! VZN = VZN1+T*(VZN-K2*EPSN) !
! ! VZNU = VZN-D*ABS(ROLR) !
! ! RALR = VZNU !
!--------------!------------------------------------------------------!
! PTCH ! Pitch Angle !
! X999 ! Format: Negative values are indicated by '-' !
! ! on the first position. Otherwise the first position!
! ! are used for the value. !
! ! -99.0 to 90.0 deg !
! ! param. ADIRU 04.1.324.01 !
! ! 04.2.324.10 !
!--------------!------------------------------------------------------!
! PTCR ! Body Pitch Rate !
! X999 ! Format: Negative values are indicated by '-' !
! ! on the first position. Otherwise the first position!
! ! are used for the value. !
! ! -45.0 to 45.0 deg/sec !
! ! param. ADIRU 04.1.326.01 !
! ! 04.2.326.10 !
!--------------!------------------------------------------------------!
! ROLL ! Roll Angle !
! X999 ! Format: Negative values are indicated by '-' !
! ! on the first position. Otherwise the first position!
! ! contains a '0'. !
! ! -90.0 to 90.0 deg !
! ! param. ADIRU 04.1.325.01 !
! ! 04.2.325.10 !
!--------------!------------------------------------------------------!
! ROLR ! Body Roll Rate !
! X999 ! Format: Negative values are indicated by '-' !
! ! on the first position. Otherwise the first position!
! ! are used for the value. !
! ! -45.0 to 45.0 deg/sec !
! ! param. ADIRU 04.1.327.01 !
! ! 04.2.327.10 !
!--------------!------------------------------------------------------!
! YAW ! YAW Rate !
! X999 ! Format: Negative values are indicated by '-' !
! ! on the first position. Otherwise the first position!
! ! contains a '0'. !
! ! -45.0 to 45.0 deg/sec !
! ! param. ADIRU 04.1.330.01 !
! ! 04.2.330.10 !
!--------------!------------------------------------------------------!
! VRTA ! Normal Acceleration !
! X999 ! Format: Negative values are indicated by '-' !
! ! on the first position. Otherwise the first position!
! ! are used for the value. !
! ! -3.00 to 6.00 g !
! ! param. SDAC 29.1.333.01 !
! ! 29.2.333.01 !
!--------------!------------------------------------------------------!
! LONA ! Longitudinal Acceleration !
! X999 ! Format: Negative values are indicated by '-' !
! ! on the first position. Otherwise the first position!
! ! are used for the value. !
! ! (-1.00 to 1.00 g) !
! ! param. SDAC 29.1.331.01 !
! ! 29.2.331.01 !
!--------------!------------------------------------------------------!
! LATA ! Lateral Acceleration !
! X999 ! Format: Negative values are indicated by '-' !
! ! on the first position. Otherwise the first position!
! ! are used for the value. !
! ! (-1.00 to 1.00 g) !
! ! param. SDAC 29.1.332.01 !
! ! 29.2.332.01 !
+---------------------------------------------------------------------+

(7) Load Report Data Field Description
NOTE: Reports that are transmitted from the ACARS system do not have report lines without a line identifier.
+---------------------------------------------------------------------+
! Value ! Content Description !
!--------------!------------------------------------------------------!
! ESN ! Engine Serial Number !
! 999999 ! (000000 to 999999) !
! ! EEC/ECU Eng 1 param. 7C.1.046.01 digit 3, 2, 1 !
! ! 7C.1.047.01 digit 6, 5, 4 !
! ! Eng 2 param. 7C.2.046.10 digit 3, 2, 1 !
! ! 7C.2.047.10 digit 6, 5, 4 !
!--------------!------------------------------------------------------!
! EHRS ! Engine Flight Hours !
! 99999 ! (00000 to 99999 hours) !
! ! DMU 0D.1.060.01 Engine 1 !
! ! 0D.1.060.10 Engine 2 !
! ! Remark: Time between "Main (LH and RH) Landing Gear!
! ! Decompressed" and "Main (LH and RH) Landing!
! ! Gear Compressed". The EHRS shall be set to !
! ! zero if a new ESN is regonized by the DMU. !
! ! It shall be possible to set the EHRS via !
! ! the MCDU, e.g. if the DMU is changed on the!
! ! A/C. !
!--------------!------------------------------------------------------!
! AP ! Auto Pilot Status !
! 99 ! (00 to 24) !
! ! 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 = LOCK CAPTURE !
! ! ! 5 = LOCK TRACK !
! ! ! 6 = LAND TRACK !
! ! ! 7 = RUNWAY !
! ! ! 8 = ROLL GO AROUND !
! ! ! !
! ! !__Longitudinal Modes: 0 = NO MODE !
! ! 1 = PITCH G/A !
! ! 2 = PITCH T/O !
! ! 3 = G/S TRACK !
! ! 4 = G/S CAPTURE !
! ! 5 = V/S !
! ! 6 = FPA !
! ! 7 = ALT !
! ! 8 = ALT ACQ !
! ! 9 = OPEN CLB !
! ! A = OPEN DES !
! ! B = IM CLB !
! ! C = IM DES !
! ! D = CLB !
! ! E = DES !
! ! F = FINAL DES !
! ! G = EXPEDITE !
! ! !
! ! AP1 ! AP2 !
! ! Report Line EC: ! Report Line EE: !Difinition: !
! ! -------------------!-------------------!------------ !
! ! / ! / !No Mode Act. !
! ! -------------------!-------------------!------------ !
! ! 01.1.275.00.11 = 1 ! 01.2.275.00.11 = 1!RUNWAY Mode !
! ! -------------------!-------------------!------------ !
! ! 01.1.275.00.12 = 1 ! 01.2.275.00.12 = 1!NAV Mode !
! ! -------------------!-------------------!------------ !
! ! 01.1.275.00.13 = 1 ! 01.2.275.00.13 = 1!LOC CAPTURE !
! ! ! !Mode !
! ! -------------------!-------------------!------------ !
! ! 01.1.275.00.14 = 1 ! 01.2.275.00.14 = 1!LOC TRACK !
! ! ! !Mode !
! ! -------------------!-------------------!------------ !
! ! 01.1.275.00.15 = 1 ! 01.2.275.00.15 = 1!Roll GO !
! ! ! !AROUND Mode !
! ! -------------------!-------------------!------------ !
! ! 01.1.275.00.16 = 1 ! 01.2.275.00.16 = 1!HEADING Mode !
! ! -------------------!-------------------!------------ !
! ! 01.1.275.00.17 = 1 ! 01.2.275.00.17 = 1!TRACK Mode !
! ! -------------------!-------------------!------------ !
! ! 01.1.274.00.15 = 1 ! 01.2.274.00.15 = 1!PITCH TO Mode!
! ! -------------------!-------------------!------------ !
! ! 01.1.274.00.16 = 1 ! 01.2.274.00.16 = 1!PITCH GA Mode!
! ! -------------------!-------------------!------------ !
! ! 01.1.274.00.17 = 1 ! 01.2.274.00.17 = 1!V/S Mode !
! ! -------------------!-------------------!------------ !
! ! 01.1.274.00.18 = 1 ! 01.2.274.00.18 = 1!FPA Mode !
! ! -------------------!-------------------!-------------!
! ! 01.1.274.00.19 = 1 ! 01.2.274.00.19 = 1!ALT Mode !
! ! AND ! AND ! !
! ! 01.1.274.00.20 = 1 ! 01.2.274.00.20 = 1! !
! ! -------------------!-------------------!------------ !
! ! 01.1.274.00.19 = 1 ! 01.2.274.00.19 = 1!ALT ACQ !
! ! AND ! AND !Mode !
! ! 01.1.274.00.21 = 1 ! 01.2.274.00.21 = 1! !
! ! -------------------!-------------------!------------ !
! ! 01.1.274.00.20 = 1 ! 01.2.274.00.20 = 1!G/S TRACK !
! ! AND ! AND !Mode !
! ! 01.1.274.00.22 = 1 ! 01.2.274.00.22 = 1! !
! ! -------------------!-------------------!------------ !
! ! 01.1.274.00.21 = 1 ! 01.2.274.00.21 = 1!G/S CAPTURE !
! ! AND ! AND !Mode !
! ! 01.1.274.00.22 = 1 ! 01.2.274.00.22 = 1! !
! ! -------------------!-------------------!------------ !
! ! 01.1.274.00.23 = 1 ! 01.2.274.00.23 = 1!FINAL DES !
! ! ! !Mode !
! ! -------------------!-------------------!------------ !
! ! 01.2.274.00.24 = 1 ! 01.2.274.00.24 = 1!EXPED. Mode !
! ! -------------------!-------------------!------------ !
! ! 01.1.146.00.14 = 1 ! 01.2.146.00.14 = 1!LAND TRACK !
! ! ! !Mode !
! ! -------------------!-------------------!------------ !
! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!CLB Mode !
! ! AND ! AND ! !
! ! 01.1.274.00.13 = 0 ! 01.2.274.00.13 = 0! !
! ! OR ! OR ! !
! ! 01.1.274.00.14 = 0 ! 01.2.274.00.14 = 0! !
! ! OR ! OR ! !
! ! 01.1.274.00.24 = 0 ! 01.2.274.00.24 = 0! !
! ! -------------------!-------------------!------------ !
! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!DES Mode !
! ! AND ! AND ! !
! ! 01.1.274.00.13 = 0 ! 01.2.274.00.13 = 0! !
! ! OR ! OR ! !
! ! 01.1.274.00.14 = 0 ! 01.2.274.00.14 = 0! !
! ! OR ! OR ! !
! ! 01.1.274.00.24 = 0 ! 01.2.274.00.24 = 0! !
! ! -------------------!-------------------!------------ !
! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!IM. CLIMB !
! ! AND ! AND !Mode !
! ! 01.1.274.00.13 = 1 ! 01.2.274.00.13 = 1! !
! ! -------------------!-------------------!------------ !
! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!IM. DES Mode !
! ! AND ! AND ! !
! ! 01.1.274.00.13 = 1 ! 01.2.274.00.13 = 1! !
! ! -------------------!-------------------!------------ !
! ! 01.1.274.00.11 = 1 ! 01.2.274.00.11 = 1!OPEN CLB !
! ! AND ! AND !Mode !
! ! 01.1.274.00.14 = 1 ! 01.2.274.00.14 = 1! !
! ! -------------------!-------------------!------------ !
! ! 01.1.274.00.12 = 1 ! 01.2.274.00.12 = 1!OPEN DES !
! ! AND ! AND !Mode !
! ! 01.1.274.00.14 = 1 ! 01.2.274.00.14 = 1! !
! ! ---------------------------------------------------- !
! ! Auto Pilot Status DMU: !
! !DMU 0D.1.274.01 AP1 printed in report line EC !
! ! 0D.1.274.10 AP2 printed in report line EE !
!--------------!------------------------------------------------------!
! FLAP ! FLAP Actual Position !
! 9999 ! (0 to 40.0 deg) see table DT40 for special !
! ! conversion !
! ! SFCC param. 1B.1.137.01 !
! ! 1B.2.137.10 !
!--------------!------------------------------------------------------!
! SLAT ! SLAT Actual Position !
! X999 ! (0 to 27.0 deg) see table DT41 for special convers.!
! ! SFCC param. 1B.1.127.01 !
! ! 1B.2.127.10 !
!--------------!------------------------------------------------------!
! MAX ! Maximum Value of the exceedance parameter from !
! X999 ! time interval 0.5 sec. before 'landing detection' !
! ! till 0.5 sec. after 'landing detection'. !
! ! For logic 4100 see remark. !
! ! !
! ! Format: Depends on exceeded parameter !
! ! !
! ! Source: Depends on exceeded parameter !
! ! !
! ! Remark: If code = 4100 (exceedance RALR) the !
! ! maximum value shall be taken as an average !
! ! value from a window of RALR data between S1!
! ! and S2 around the landing detection event. !
! ! If code = 4500 the highest maximum of the !
! ! exceeding parameter either at landing or at!
! ! bounce landing is displayed. !
! ! !
!--------------!------------------------------------------------------!
! LIM ! Format: Depends on the parameter !
! X999 ! !
! ! Source: Depends on the parameter !
! ! !
! ! Remark: If code = 4500 the limit which was exceeded !
! ! shall be displayed in reference to MAX !
! ! either at landing or at bounce landing. !
!--------------!------------------------------------------------------!
! COUNTS ! Counter for spoiler 4 extensions !
! 5 x 9999 ! (0 to 9999) !
! ! 999 999 999 999 999 !
! ! I I I I I___Spoiler < -20 Deg !
! ! I I I I_______-15 Deg > Spoiler >= -20 !
! ! I I I____________-10 Deg > Spoiler >= -15 !
! ! I I__________________-5 Deg > Spoiler >= -10 !
! ! I_______________________ 0 Deg > Spoiler >= -5 !
! ! !
! ! 6C.1.364.01 LH Spoiler 4 Position !
! ! 6C.2.364.10 !
! ! 6C.1.374.01 RH Spoiler 4 Position !
! ! 6C.2.374.10 !
! ! 6C.1.044.01.24 = 1 Spoiler 4 Fault !
! ! 6C.2.044.10.24 !
! ! 6C.1.365.01 LH Spoiler 5 Position !
! ! 6C.2.365.10 !
! ! 6C.1.375.01 RH Spoiler 5 Position !
! ! 6C.2.375.10 !
! ! 6C.1.044.01.25 = 1 Spoiler 5 Fault !
! ! 6C.2.044.10.25 !
! ! 6C.1.041.01.21 = 1 Load Alleviation Active (LAF) !
! ! 6C.2.041.10.21 !
! ! Remark: The max extension values of the LH Spoiler !
! ! 4 is counted as long as LAF is active and !
! ! Spoiler 4 is not fault.The value of LH !
! ! Spoiler 4 is compared with the value of RH !
! ! Spoiler 4, which are detected at the same !
! ! time of max LH Spoiler 4. The lower one of !
! ! these values effects the counts as defined !
! ! above If Spoiler 4 is fault and Spoiler 5 !
! ! is not fault, the Spoiler 5 LH and RH is !
! ! used for calculation and counts. !
! ! !
!--------------!------------------------------------------------------!
! REASON ! Reason for exceedance !
! XXXXXXXXXX ! Up to 10 characters !
! ! RALR Code: 4100 !
! ! VRTA Code: 4400, 4500, 5100, 5200 and 5300 !
! ! GW Code: 4800, 4900 !
! ! SPCT Code: 5400 !
! ! Source: DMU !
! ! Remark: If the report was not triggered by a limit !
! ! exceedance, this field shall contain blanks. !
!--------------!------------------------------------------------------!
! RALT ! Radio Altitude !
! X999 ! Format: Negative values are indicated by 'N' !
! ! in the first position. Otherwise the first position!
! ! are used for the value. !
! ! (-20 to 2500 ft) !
! ! DMC param 25.1.164.01 !
! ! 25.2.164.10 !
!--------------!------------------------------------------------------!
! RALR ! Radio Altitude Rate !
! X999 ! Format: Negative values are indicated by 'N' in !
! ! the first position. Otherwise the first position !
! ! are used for the value. !
! ! -99.9 to 99.9 ft/sec !
! ! !
! ! Source: DMU !
! ! Remark: The calculation of Radio Altitude Rate is !
! ! started when: RALT<RALTL1 !
! ! - The calculation is performed with 16 Hz cycles !
! ! (T=0.0625 s) !
! ! - The calculation uses the current calculation !
! ! cycle current and data values. These data are !
! ! named as follows: !
! ! e.g. !
! ! IVV = IVV actual sample n !
! ! IVV1 = IVV previous sample n-1 !
! ! !
! ! PTCHACC = PTCHACC actual sample n !
! ! PTCHACC1 = PTCHACC previous sample n-1 !
! ! PTCHACC2 = PTCHACC previous sample n-2 !
! ! !
! ! - The calculation uses the following programmable !
! ! constants: !
! ! D geometrical correction factor for ROLR ft/deg!
! ! DX lever arm correction (x-axis) for R/A RALT ft!
! ! DZ lever arm correction (z-axis) for R/A RALT ft!
! ! DXTPIR lever arm correction (x-axis) for PTCH ft!
! ! FC filter frequency Hz!
! ! K1 filter constant !
! ! K2 filter constant !
! ! K3 filter constant !
! ! THETA0 average PTCH at touchdown deg!
! ! !
! ! Radio Altitude Rate calculation: !
! ! 1. Start Values !
! ! !
! ! For the very first calculation the start values are !
! ! defined as follows: !
! ! PTCHRAW1 = 0.0 !
! ! PTCHACC1 = 0.0 !
! ! PTCHACC2 = 0.0 !
! ! PTCR1 = 0.0 !
! ! EN1 = 0.0 !
! ! VZN1 = IVV/60.0 !
! ! ZN1 = RALT !
! ! !
! ! 2. Algorithm with KALMAN filter !
! ! The algorithm comprises of the following equations: !
! ! PTCHRAW = (PTCR-PTCR1)/T !
! ! PTCHACC = PTCHACC1+T*(2*PI*FC)*(PTCHRAW+PTCHRAW1- !
! ! PTCHACC1-PTCHACC2)/2 !
! ! NZTCOR = VACC*9.81/0.3048-DXTPIR*PTCHACC/57.3 !
! ! *cos(PTCH/57.3) !
! ! EPSN = ZN1-HRACOR !
! ! EN = EN1+T*(VZN-K2*EPSN) !
! ! VZN = VZN1+T*(VZN-K2*EPSN) !
! ! VZNU = VZN-D*ABS(ROLR) !
! ! RALR = VZNU !
!--------------!------------------------------------------------------!
! PTCH ! Pitch Angle !
! X999 ! Format: Negative values shall be indicated by 'N' !
! ! on the first position. Otherwise the first position!
! ! shall be used for the value. !
! ! -99.0 to 90.0 deg !
! ! ADIRU param. 04.1.324.01 !
! ! 04.2.324.10 !
!--------------!------------------------------------------------------!
! PTCR ! Body Pitch Rate !
! X999 ! Format: Negative values shall be indicated by 'N' !
! ! on the first position. Otherwise the first position!
! ! shall be used for the value. !
! ! -45.0 to 45.0 deg/sec !
! ! param. ADIRU 04.1.326.01 !
! ! 04.2.326.10 !
!--------------!------------------------------------------------------!
! ROLL ! Roll Angle !
! X999 ! Format: Negative values are indicated by 'N' !
! ! on the first position. Otherwise the first position!
! ! contains a '0'. !
! ! -90.0 to 90.0 deg !
! ! param. ADIRU 04.1.325.01 !
! ! 04.2.325.10 !
!--------------!------------------------------------------------------!
! ROLR ! Body Roll Rate !
! X999 ! Format: Negative values are indicated by 'N' !
! ! on the first position. Otherwise the first position!
! ! are used for the value. !
! ! -45.0 to 45.0 deg/sec !
! ! param. ADIRU 04.1.327.01 !
! ! 04.2.327.10 !
!--------------!------------------------------------------------------!
! YAW ! YAW Rate !
! X999 ! Format: Negative values are indicated by 'N' !
! ! on the first position. Otherwise the first position!
! ! contains a '0'. !
! ! -45.0 to 45.0 deg/sec !
! ! param. ADIRU 04.1.330.01 !
! ! 04.2.330.10 !
!--------------!------------------------------------------------------!
! VRTA ! Normal Acceleration !
! X999 ! Format: Negative values are indicated by 'N' !
! ! on the first position. Otherwise the first position!
! ! are used for the value. !
! ! -3.00 to 6.00 g !
! ! param. SDAC 29.1.333.01 !
! ! 29.2.333.01 !
!--------------!------------------------------------------------------!
! LONA ! Longitudinal Acceleration !
! X999 ! (-1.00 to 1.00 g) !
! ! param. 29.1.331.01 !
! ! 29.2.331.01# !
!--------------!------------------------------------------------------!
! LONA ! Longitudinal Acceleration !
! X999 ! Format: Negative values are indicated by 'N' !
! ! on the first position. Otherwise the first position!
! ! are used for the value. !
! ! (-1.00 to 1.00 g) !
! ! param. SDAC 29.1.331.01 !
! ! 29.2.331.01 !
!--------------!------------------------------------------------------!
! LATA ! Lateral Acceleration !
! X999 ! Format: Negative values are indicated by 'N' !
! ! on the first position. Otherwise the first position!
! ! are used for the value. !
! ! (-1.00 to 1.00 g) !
! ! param. SDAC 29.1.332.01 !
! ! 29.2.332.01 !
+---------------------------------------------------------------------+

(8) Load Report Data Field Description <15>

Report line S1 contains snapshot data at 'Y15.0' seconds before Land/Event.
Report line S2 contains snapshot data at Land/Event.
Report line S3 contains the "max-values" from the time interval 'Y15.1' seconds before Land/Event to '15.2' seconds after Land/Event.
Report line S4 contains the "min-values" from the time interval 'Y15.1' seconds before Land/Event to '15.2' seconds after Land/Event.

Report lines T1, T2, T3 and T4 are generated if the A/C bounced and the appropriate logic conditions are true. If not these lines are omitted (inclusive header lines 46, 49, 53 and 54).
+---------------------------------------------------------------------+
! Value ! Content Description !
!--------------!------------------------------------------------------!
! ESN ! Engine Serial Number !
! 999999 ! Format: 000000 to 999999 !
! ! Source: !
! ! EIU Engine 1 param. 7B.1.046.xx digit 3, 2, 1 !
! ! 7B.1.047.xx digit 6, 5, 4 !
! ! Engine 2 param. 7B.2.046.xx digit 3, 2, 1 !
! ! 7B.2.047.xx digit 6, 5, 4 !
!--------------!------------------------------------------------------!
! EHRS ! Engine Flight Hours !
! 99999 ! Format: 00000 to 99999 hours !
! ! Source: DMU Engine 1 0D.1.060.01 !
! ! Engine 2 0D.1.060.10 !
! ! NOTE: 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. !
!--------------!------------------------------------------------------!
! AP ! Auto Pilot Status !
! 99 ! Format: Number of respective status 00 to 24 !
! ! Source: FMGC 1 and 2 (FGC part) for Auto Pilot 1 !
! ! and 2 !
! +------------!-----------------------------------------------------+!
! ! Auto Pilot ! Parameter for AP1 ! Parameter for AP2 ! Definition !!
! ! Status ! Report Line EC ! Report Line EE ! !!
! !------------!--------------------!-------------------!------------!!
! ! 00 !--------------------!-------------------! No Mode !!
! ! ! ! ! Active !!
! !------------!--------------------!-------------------!------------!!
! ! 01 ! 01.1.275.00.11 = 1 ! 01.2.275.00.11 = 1!RUNWAY Mode !!
! !------------!--------------------!-------------------!------------!!
! ! 02 ! 01.1.275.00.12 = 1 ! 01.2.275.00.12 = 1!NAV Mode !!
! !------------!--------------------!-------------------!------------!!
! ! 03 ! 01.1.275.00.13 = 1 ! 01.2.275.00.13 = 1!LOC CAPTURE !!
! ! ! ! !Mode !!
! !------------!--------------------!-------------------!------------!!
! ! 04 ! 01.1.275.00.14 = 1 ! 01.2.275.00.14 = 1!LOC TRACK !!
! ! ! ! !Mode !!
! !------------!--------------------!-------------------!------------!!
! ! 05 ! 01.1.275.00.15 = 1 ! 01.2.275.00.15 = 1!Roll GO !!
! ! ! ! !AROUND Mode !!
! !------------!--------------------!-------------------!------------!!
! ! 06 ! 01.1.275.00.16 = 1 ! 01.2.275.00.16 = 1!HEADING Mode!!
! !------------!--------------------!-------------------!------------!!
! ! 07 ! 01.1.275.00.17 = 1 ! 01.2.275.00.17 = 1!TRACK Mode !!
! !------------!--------------------!-------------------!------------!!
! ! 08 ! 01.1.274.00.15 = 1 ! 01.2.274.00.15 = 1!PITCH T/O !!
! ! ! ! !Mode !!
! !------------!--------------------!-------------------!------------!!
! ! 09 ! 01.1.274.00.16 = 1 ! 01.2.274.00.16 = 1!PITCH GA !!
! ! ! ! !Mode !!
! !------------!--------------------!-------------------!------------!!
! ! 10 ! 01.1.274.00.17 = 1 ! 01.2.274.00.17 = 1!V/S Mode !!
! !------------! -------------------!-------------------!------------!!
! ! 11 ! 01.1.274.00.18 = 1 ! 01.2.274.00.18 = 1!FPA Mode !!
! !------------! -------------------!-------------------!------------!!
! ! 12 ! 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! !!
! !------------! -------------------!-------------------!------------!!
! ! 13 ! 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! !!
! !------------!--------------------!-------------------!------------!!
! ! 14 ! 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! !!
! !------------!--------------------!-------------------!------------!!
! ! 15 ! 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! !!
! !------------!--------------------!-------------------!------------!!
! ! 16 ! 01.1.274.00.23 = 1 ! 01.2.274.00.23 = 1!FINAL DES !!
! ! ! ! !Mode !!
! !------------!--------------------!-------------------!------------!!
! ! 17 ! 01.1.274.00.24 = 1 ! 01.2.274.00.24 = 1!EXPED. Mode !!
! !------------!--------------------!-------------------!------------!!
! ! 18 ! 01.1.146.00.14 = 1 ! 01.2.146.00.14 = 1!LAND TRACK !!
! ! ! ! !Mode !!
! !------------!--------------------!-------------------!------------!!
! ! 19 ! 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! !!
! !------------!--------------------!-------------------!------------!!
! ! 20 ! 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! !!
! !------------!--------------------!-------------------!------------!!
! ! 21 ! 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! !!
! !------------! -------------------!-------------------!------------!!
! ! 22 ! 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! !!
! !------------! -------------------!-------------------!------------!!
! ! 23 ! 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! !!
! !------------! -------------------!-------------------!------------!!
! ! 24 ! 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 0D.1.274.01 AP1 printed in report line EC !
! ! 0D.1.274.10 AP2 printed in report line EE !
!--------------!------------------------------------------------------!
! FLAP ! FLAP Position !
! 9999 ! Format: 0 to 40.0 deg (see table DT40 for special !
! ! conversion) !
! ! Source: SFCC 1B.1.137.01 !
! ! 1B.2.137.10 !
!--------------!------------------------------------------------------!
! SLAT ! SLAT Position !
! 9999 ! Format: 0 to 27.0 deg (see table DT41 for special !
! ! conversion) !
! ! Source: SFCC 1B.1.127.01 !
! ! 1B.2.127.10 !
!--------------!------------------------------------------------------!
! MAX ! Maximum value of the exceedance parameter from !
! X999 ! time interval 0.5 sec before 'landing detection' !
! ! until 0.5 sec. after 'landing detection'. !
! ! For logic 4100 see note. !
! ! !
! ! Format: Depends on exceeded parameter !
! ! !
! ! Source: Depends on exceeded parameter !
! ! !
! ! NOTE: If code = 4100 (exceedance RALR), the !
! ! maximum value is taken as an average value from !
! ! a window of the RALR data between S1 and S2 around !
! ! the landing detection event. !
! ! If code = 4500, the highest maximum of the !
! ! exceeding parameter either at landing or at bounce !
! ! landing is displayed. !
!--------------!------------------------------------------------------!
! LIM ! Programmable Limit which was exceeded !
! X999 ! Format: Depends of exceeded parameter !
! ! !
! ! Source: Depends of exceeded parameter !
! ! !
! ! NOTE: If code = 4500, the limit which was exceeded !
! ! is displayed in reference to MAX either at landing !
! ! or at bounce landing. !
!--------------!------------------------------------------------------!
! COUNTS ! Counter for spoiler 4 extensions !
! ! 999 999 999 999 999 !
! ! --- --- --- --- --- !
! ! 0 > Spoiler >= -5 ______! ! ! ! ! !
! ! -5 > Spoiler >= -10 ___________! ! ! ! !
! ! -10 > Spoiler >= -15 ________________! ! ! !
! ! -15> Spoiler >= -20 _____________________! ! !
! ! Spoiler < -20 __________________________! !
! ! !
! ! Format: 0 to 9999 !
! ! !
! ! Source: 6C.1.364.01 LH Spoiler 4 Position !
! ! 6C.2.364.10 !
! ! 6C.1.374.01 RH Spoiler 4 Position !
! ! 6C.2.374.10 !
! ! 6C.1.044.01.24 = 1 Spoiler 4 Fault !
! ! 6C.2.044.10.24 = 1 !
! ! 6C.1.365.01 LH Spoiler 5 Position !
! ! 6C.2.365.10 !
! ! 6C.1.375.01 RH Spoiler 5 Position !
! ! 6C.2.375.10 !
! ! 6C.1.044.01.25 = 1 Spoiler 5 Fault !
! ! 6C.2.044.10.25 !
! ! 6C.1.041.01.21 = 1 Load Alleviation Active !
! ! 6C.2.041.10.21 (LAF) !
! ! !
! ! NOTE: The max extension values of the LH Spoiler !
! ! 4 is counted as long as LAF is active and Spoiler 4!
! ! is not fault. The value of LH Spoiler 4 is compared!
! ! with the value of RH Spoiler 4, which are detected !
! ! at the same time of max LH Spoiler 4. The lower one!
! ! of these values effects the counts as defined above!
! ! If Spoiler 4 is fault and Spoiler 5 is not fault, !
! ! the Spoiler 5 LH and RH is used for calculation !
! ! and counts. !
!--------------!------------------------------------------------------!
! REASON ! Reason for exceedance !
! XXXXXXXXXX ! Format: Up to 10 characters !
! ! RALR Code: 4100 !
! ! VRTA Code: 4400, 4500,5100, 5200, 5300!
! ! GW Code: 4800, 4900 !
! ! SPCT Code: 5400 !
! ! Source: DMU !
! ! NOTE: If the report was not triggered by a limit !
! ! exceedance, this field contains blanks. !
!--------------!------------------------------------------------------!
! RALT ! Radio Altitude !
! X999 ! Format: Negative values are shown with 'N' in the !
! ! first position. If not, the first position !
! ! is used for the value. !
! ! -20 to 2500 ft !
! ! Source: DMC 25.1.164.01 !
! ! 25.1.164.10 !
!--------------!------------------------------------------------------!
! RALR ! Radio Altitude Rate !
! X999 ! Format: Negative values are shown with 'N' in the !
! ! first position. If not, the first position !
! ! is used for the value. !
! ! -99.9 to 99.9 ft/sec !
! ! Source: DMU !
! ! NOTE: The calculation of Radio Altitude Rate is !
! ! started when RALT<RALTL1. !
! ! The calculation is performed with 16 Hz cycles !
! ! (T=0.0625 s) !
! ! The calculation uses the current calculation !
! ! cycle and data values. These data are named !
! ! as follows: !
! ! !
! ! IVV = IVV actual sample n !
! ! IVV1 = IVV previous sample n-1 !
! ! !
! ! PTCHACC = PTCHACC actual sample n !
! ! PTCHACC1 = PTCHACC previous sample n-1 !
! ! PTCHACC2 = PTCHACC previous sample n-2 !
! ! !
! ! The calculation uses the following !
! ! programmable constants: !
! ! D geometrical correction factor for ROLR (ft/deg) !
! ! DX lever arm correction (x-axis) for R/A RALT (ft) !
! ! DZ lever arm correction (z-axis) for R/A RALT ft!
! ! DXTPIR lever arm correction (x-axis) for PTCH ft!
! ! FC filter frequency Hz!
! ! K1 filter constant !
! ! K2 filter constant !
! ! K3 filter constant !
! ! THETA0 average PTCH at touchdown deg!
! ! !
! ! Radio Altitude Rate calculation: !
! ! 1. Start Values !
! ! !
! ! For the very first calculation the start values are !
! ! defined as follows: !
! ! PTCHRAW1 = 0.0 !
! ! PTCHACC1 = 0.0 !
! ! PTCHACC2 = 0.0 !
! ! PTCR1 = 0.0 !
! ! EN1 = 0.0 !
! ! VZN1 = IVV1/60.0 !
! ! ZN1 = RALT !
! ! !
! ! 2. Algorithm with KALMAN filter !
! ! The algorithm comprises of the following equations: !
! ! PTCHRAW = (PTCR-PTCR1)/T !
! ! PTCHACC = PTCHACC1+T*(2*PI*FC)*(PTCHRAW+PTCHRAW1- !
! ! PTCHACC1-PTCHACC2)/2 !
! ! NZTCOR = VACC*9.81/0.3048-DXTPIR*PTCHACC/57.3 !
! ! *cos(PTCH/57.3) !
! ! HRACOR = RALT+DX*(sin(PTCH/57.3)-sin(THEATA0/57.3))!
! ! -DZ*(cos(PTCH/57.3)-cos(THEATA0/57.3)) !
! ! EPSN = ZN1-HRACOR !
! ! EN = EN1+T*K3*EPSN !
! ! VZN = VZN1+T*(VZN-K2*EPSN) !
! ! VZNU = VZN-D*ABS(ROLR) !
! ! RALR = VZNU !
!--------------!------------------------------------------------------!
! PTCH ! Pitch Angle !
! X999 ! Format: Negative values are shown with 'N' on the !
! ! first position. If not the first position !
! ! is used for the value. !
! ! -99.0 to 90.0 deg !
! ! Source: ADIRU 04.1.324.01 !
! ! 04.2.324.10 !
!--------------!------------------------------------------------------!
! PTCR ! Body Pitch Rate !
! X999 ! Format: Negative values are shown with 'N' on the !
! ! first position. If not the first position !
! ! is used for the value. !
! ! -45.0 to 45.0 deg/sec !
! ! Source: ADIRU 04.1.326.01 !
! ! 04.2.326.10 !
!--------------!------------------------------------------------------!
! ROLL ! Roll Angle !
! X999 ! Format: Negative values are shown with 'N' on the !
! ! first position. If not the first position !
! ! is used for the value. !
! ! -90.0 to 90.0 deg/sec !
! ! Source: ADIRU 04.1.325.01 !
! ! 04.2.325.10 !
!--------------!------------------------------------------------------!
! ROLR ! Body Roll Rate !
! X999 ! Format: Negative values are shown with 'N' on the !
! ! first position. If not the first position !
! ! is used for the value. !
! ! -45.0 to 45.0 deg !
! ! Source: ADIRU 04.1.327.01 !
! ! 04.2.327.10 !
!--------------!------------------------------------------------------!
! YAW ! YAW Rate !
! X999 ! Format: Negative values are shown with 'N' on the !
! ! first position. If not the first position !
! ! is used for the value. !
! ! -45.0 to 45.0 deg !
! ! Source: ADIRU 04.1.330.01 !
! ! 04.2.330.10 !
!--------------!------------------------------------------------------!
! VRTA ! Normal Acceleration !
! X999 ! Format: Negative values are shown with 'N' on the !
! ! first position. If not the first position !
! ! is used for the value. !
! ! -3.00 to 6.00 g !
! ! Source: SDAC 29.1.333.01 !
! ! 29.2.333.01 !
!--------------!------------------------------------------------------!
! LONA ! Longitudinal Acceleration !
! X999 ! Format: Negative values are shown with 'N' on the !
! ! first position. If not the first position !
! ! is used for the value. !
! ! -1.00 to 1.00 g !
! ! Source: SDAC 29.1.331.01 !
! ! 29.2.331.01 !
!--------------!------------------------------------------------------!
! LATA ! Lateral Acceleration !
! X999 ! Format: Negative values are shown with 'N' on the !
! ! first position. If not the first position !
! ! is used for the value. !
! ! -1.00 to 1.00 g !
! ! Source: SDAC 29.1.332.01 !
! ! 29.2.332.01 !
+---------------------------------------------------------------------+

(9) Load Report Data Field Description <15>
+---------------------------------------------------------------------+
! Value ! Content Description !
!--------------!------------------------------------------------------!
! ESN ! Engine Serial Number !
! 999999 ! Format: 000000 to 999999 !
! ! Source: !
! ! EIU Engine 1 7B.1.046.xx digit 3, 2, 1 !
! ! 7B.1.047.xx digit 6, 5, 4 !
! ! Engine 2 7B.2.046.xx digit 3, 2, 1 !
! ! 7B.2.047.xx digit 6, 5, 4 !
!--------------!------------------------------------------------------!
! EHRS ! Engine Flight Hours !
! 99999 ! Format: 00000 to 99999 hours !
! ! Source: DMU Engine 1 0D.1.060.01 !
! ! Engine 2 0D.1.060.10 !
! ! NOTE: 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. !
!--------------!------------------------------------------------------!
! AP ! Auto Pilot Status !
! 99 ! Format: Number of respective status 00 to 24 !
! ! Source: FMGC 1 and 2 (FGC part) for Auto Pilot 1 !
! ! and 2 !
! +------------!-----------------------------------------------------+!
! ! Auto Pilot ! Parameter for AP1 ! Parameter for AP2 ! Definition !!
! ! Status ! Report Line EC ! Report Line EE ! !!
! !------------!--------------------!-------------------!------------!!
! ! 00 !--------------------!-------------------! No Mode !!
! ! ! ! ! Active !!
! !------------!--------------------!-------------------!------------!!
! ! 01 ! 01.1.275.00.11 = 1 ! 01.2.275.00.11 = 1!RUNWAY Mode !!
! !------------!--------------------!-------------------!------------!!
! ! 02 ! 01.1.275.00.12 = 1 ! 01.2.275.00.12 = 1!NAV Mode !!
! !------------!--------------------!-------------------!------------!!
! ! 03 ! 01.1.275.00.13 = 1 ! 01.2.275.00.13 = 1!LOC CAPTURE !!
! ! ! ! !Mode !!
! !------------!--------------------!-------------------!------------!!
! ! 04 ! 01.1.275.00.14 = 1 ! 01.2.275.00.14 = 1!LOC TRACK !!
! ! ! ! !Mode !!
! !------------!--------------------!-------------------!------------!!
! ! 05 ! 01.1.275.00.15 = 1 ! 01.2.275.00.15 = 1!Roll GO !!
! ! ! ! !AROUND Mode !!
! !------------!--------------------!-------------------!------------!!
! ! 06 ! 01.1.275.00.16 = 1 ! 01.2.275.00.16 = 1!HEADING Mode!!
! !------------!--------------------!-------------------!------------!!
! ! 07 ! 01.1.275.00.17 = 1 ! 01.2.275.00.17 = 1!TRACK Mode !!
! !------------!--------------------!-------------------!------------!!
! ! 08 ! 01.1.274.00.15 = 1 ! 01.2.274.00.15 = 1!PITCH T/O !!
! ! ! ! !Mode !!
! !------------!--------------------!-------------------!------------!!
! ! 09 ! 01.1.274.00.16 = 1 ! 01.2.274.00.16 = 1!PITCH GA !!
! ! ! ! !Mode !!
! !------------!--------------------!-------------------!------------!!
! ! 10 ! 01.1.274.00.17 = 1 ! 01.2.274.00.17 = 1!V/S Mode !!
! !------------! -------------------!-------------------!------------!!
! ! 11 ! 01.1.274.00.18 = 1 ! 01.2.274.00.18 = 1!FPA Mode !!
! !------------! -------------------!-------------------!------------!!
! ! 12 ! 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! !!
! !------------! -------------------!-------------------!------------!!
! ! 13 ! 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! !!
! !------------!--------------------!-------------------!------------!!
! ! 14 ! 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! !!
! !------------!--------------------!-------------------!------------!!
! ! 15 ! 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! !!
! !------------!--------------------!-------------------!------------!!
! ! 16 ! 01.1.274.00.23 = 1 ! 01.2.274.00.23 = 1!FINAL DES !!
! ! ! ! !Mode !!
! !------------!--------------------!-------------------!------------!!
! ! 17 ! 01.1.274.00.24 = 1 ! 01.2.274.00.24 = 1!EXPED. Mode !!
! !------------!--------------------!-------------------!------------!!
! ! 18 ! 01.1.146.00.14 = 1 ! 01.2.146.00.14 = 1!LAND TRACK !!
! ! ! ! !Mode !!
! !------------!--------------------!-------------------!------------!!
! ! 19 ! 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! !!
! !------------!--------------------!-------------------!------------!!
! ! 20 ! 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! !!
! !------------!--------------------!-------------------!------------!!
! ! 21 ! 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! !!
! !------------! -------------------!-------------------!------------!!
! ! 22 ! 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! !!
! !------------! -------------------!-------------------!------------!!
! ! 23 ! 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! !!
! !------------! -------------------!-------------------!------------!!
! ! 24 ! 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 0D.1.274.01 AP1 printed in report line EC !
! ! 0D.1.274.10 AP2 printed in report line EE !
!--------------!------------------------------------------------------!
! FLAP ! FLAP Position !
! X999 ! Format: 0 to 40.0 deg (see table DT40 for special !
! ! conversion) !
! ! Source: SFCC 1B.1.137.01 !
! ! 1B.2.137.10 !
!--------------!------------------------------------------------------!
! SLAT ! SLAT Position !
! X999 ! Format: 0 to 27.0 deg (see table DT41 for special !
! ! conversion) !
! ! Source: SFCC 1B.1.127.01 !
! ! 1B.2.127.10 !
!--------------!------------------------------------------------------!
! MAX ! Highest value (if the exceedance is positive) or !
! X999 ! lowest value (if the exceedance is negative) of !
! ! the exceeding parameter within a time interval of !
! ! 0.5 sec. before 'event detection' until 0.5 sec !
! ! after 'event detection'. !
! ! If case of RAG detection (Trigger code 4xxx), !
! ! manual trigger (code 1000) or standard trigger !
! ! (code 7000) the value is "0" !
! ! !
! ! Format: Depends on exceeded parameter !
! ! !
! ! Source: Depends on exceeded parameter !
! ! !
! ! NOTE: The exceedance value can be either negative !
! ! or positive depending on the exceeded limit. !
! ! In case of a negative limit, the lowest negative !
! ! value of the exceeding parameter must be taken. !
! ! !
!--------------!------------------------------------------------------!
! LIM ! Programmable limit, which was exceeded !
! X999 ! In case of RAG detection (Trigger code 4xxx) the !
! ! value is "0" !
! ! !
! ! Format: Depends on the parameter !
! ! !
! ! Source: Depends on the parameter !
! ! !
!--------------!------------------------------------------------------!
! COUNTS ! Counter for spoiler 4 extensions !
! ! 999 999 999 999 999 !
! ! --- --- --- --- --- !
! ! 0 > Spoiler >= -5 ______! ! ! ! ! !
! ! -5 > Spoiler >= -10 ___________! ! ! ! !
! ! -10 > Spoiler >= -15 ________________! ! ! !
! ! -15> Spoiler >= -20 _____________________! ! !
! ! Spoiler < -20 __________________________! !
! ! !
! ! Format: 0 to 9999 !
! ! !
! ! Source: 6C.1.364.01 LH Spoiler 4 Position !
! ! 6C.2.364.10 !
! ! 6C.1.374.01 RH Spoiler 4 Position !
! ! 6C.2.374.10 !
! ! 6C.1.044.01.24 = 1 Spoiler 4 Fault !
! ! 6C.2.044.10.24 = 1 !
! ! 6C.1.365.01 LH Spoiler 5 Position !
! ! 6C.2.365.10 !
! ! 6C.1.375.01 RH Spoiler 5 Position !
! ! 6C.2.375.10 !
! ! 6C.1.044.01.25 = 1 Spoiler 5 Fault !
! ! 6C.2.044.10.25 !
! ! 6C.1.041.01.21 = 1 Load Alleviation Active !
! ! 6C.2.041.10.21 (LAF) !
! ! !
! ! NOTE: The max extension values of the LH Spoiler !
! ! 4 is counted as long as LAF is active and Spoiler 4!
! ! is not fault. The value of LH Spoiler 4 is compared!
! ! with the value of RH Spoiler 4, which are detected !
! ! at the same time of max LH Spoiler 4. The lower one!
! ! of these values effects the counts as defined above!
! ! If Spoiler 4 is fault and Spoiler 5 is not fault, !
! ! the Spoiler 5 LH and RH is used for calculation !
! ! and counts. !
!--------------!------------------------------------------------------!
! REASON ! Reason for trigger !
! XXXXXXXXXX ! Format: Up to 20 characters !
! ! MANUAL TRIGGERING Code: 1000 !
! ! GW RED BOUNCE Code: 4310 !
! ! GW AMBER BOUNCE Code: 4320 !
! ! GW RED Code: 4410 !
! ! GW AMBER Code: 4420 !
! ! RED BOUNCE Code: 4510 !
! ! AMBER BOUNCE Code: 4520 !
! ! RED Code: 4610 !
! ! AMBER Code: 4620 !
! ! VRTA Code: 5100, 5200 and 5300 !
! ! SPCT Code: 5400 !
! ! LATA AMBER Code: 5600 !
! ! LATA RED Code: 5700 !
! ! STANDARD TRIGGER Code: 7000 !
! ! !
! ! Source: DMU !
! ! NOTE: For other codes not given above blanks must !
! ! be printed. !
!--------------!------------------------------------------------------!
! DNZKPI1 ! Computed Delta Vertical Acceleration (IMPACT1) !
! 999 ! Format: 0.00 to 5.00 g !
! ! !
! ! Source: DMU !
! ! !
! ! Computation Formula: !
! ! !
! ! DNZKPI1=(VRTAMA1-VRTAMI1)+(GWKG/1000*35)+ !
! ! +([|ROLLI1|^DNZCONST1]/9)-ACCONSTI1 !
! ! !
! ! If DNZKPI1 < 0 then DNZKPI1 = 0 !
! ! !
! ! NOTE: -The parameter can be calculated when the !
! ! maximum VRTAMA1, the minimum VRTAMI1 and !
! ! ROLLI1 are given. !
! ! !
! ! -The value of DNZKPI1 is set to 0 after the !
! ! related load report <15> was made. !
! ! !
! ! -The formula uses these parameters: !
! ! ACCONSTI1 Aircraft constant (IMPACT1) !
! ! (depending on A/C-type) !
! ! ROLLI1 Roll angle around first !
! ! touchdown (IMPACT1); !
! ! Refer to ROLLI1 description !
! ! DNZCONST1 Aircraft constant (IMPACT1) !
! ! (depending on A/C-type) !
! ! GWKG Gross weight in (KG); !
! ! Refer to GWKG description !
! ! VRTAMA1 Maximum vertical !
! ! acceleration around first !
! ! touchdown (IMPACT1); !
! ! Refer to VRTAMA1 description!
! ! VRTAMI1 Minimum vertical !
! ! acceleration around first !
! ! touchdown (IMPACT1); !
! ! Refer to VRTAMI1 description!
!--------------!------------------------------------------------------!
! VRTAMA1 ! Maximum vertical acceleration around first touchdown!
! 999 ! (IMPACT1) !
! ! Format: 0.00 to 6.00 g !
! ! !
! ! Maximum value of VRTA during the search !
! ! interval Y15.11 sec before and Y15.12 sec !
! ! after first touchdown (IMPACT1). !
! ! For definition of acquisition rate, make !
! ! sure that the every valid sample received !
! ! during search interval will be taken into !
! ! account for maximum search. !
! ! !
! ! Source: DMU !
! ! !
! ! NOTE: -If the detection of a bounce landing is done !
! ! before Y15.12, the calculation of VRTAMA1 must!
! ! be stopped and the maximum value which was !
! ! monitored until this time must be taken. !
! ! !
! ! -The value of VRTAMA1 is set to 0 after the !
! ! related load report <15> was made. !
! ! !
! ! -Refer to report <15> logic item No. 4.9.1 for !
! ! definition of landing detection (IMPACT1). !
!--------------!------------------------------------------------------!
! VRTAMI1 ! Minimum vertical acceleration around first touchdown!
! 999 ! (IMPACT1) !
! ! Format: 0.00 to 6.00 g !
! ! !
! ! Minimum value of VRTA during the search !
! ! interval Y15.51 sec before and Y15.52 sec !
! ! after the point in time when VRTAMA1 is !
! ! detected. !
! ! For definition of acquisition rate, make !
! ! sure that the every valid sample received !
! ! during search interval will be taken into !
! ! account for minimum search. !
! ! !
! ! Source: DMU !
! ! !
! ! NOTE: -The value for VRTAMI1 can be taken when the !
! ! VRTAMA1 is given. !
! ! !
! ! -If the detection of a bounce landing is done !
! ! before Y15.52, the calculation of VRTAMI1 must!
! ! be stopped and the maximum value which was !
! ! monitored until this time must be taken. !
! ! !
! ! -The value of VRTAMI1 is set to 0 after the !
! ! related load report <15> was made. !
! ! !
! ! -Refer to report <15> logic item No. 4.9.1 for !
! ! definition of landing detection (IMPACT1). !
!--------------!------------------------------------------------------!
! ROLLI1 ! Roll angle around first touchdown (IMPACT1) !
! X999 ! Format: Negative values are shown with '-' on the !
! ! first position. If not the first position !
! ! is used for the value. !
! ! -90.0 to 90.0 deg !
! ! !
! ! Source: DMU !
! ! !
! ! NOTE: -The value for ROLLI1 can be taken when the !
! ! VRTAMI1 is given. !
! ! !
! ! -To calculate ROLLI1 the parameter ROLL must be!
! ! monitored with a rate of 32Hz. !
! ! !
! ! -The value of ROLLI1 is set to 0 after the !
! ! related load report <15> was made. !
! ! !
! ! -Refer to report <15> logic item No. 4.9.1 for !
! ! definition of landing detection (IMPACT1) !
!--------------!------------------------------------------------------!
! NYKPI1 ! Computed Lateral Acceleration (IMPACT1) !
! 999 ! Format: 0.00 to 1.00 g !
! ! !
! ! Source: DMU !
! ! !
! ! Computation Formula: !
! ! !
! ! NYKPI1=(LATACONST1*|LATAMA1|) !
! ! !
! ! !
! ! NOTE: -The parameter can be calculated when the !
! ! maximum LATAMA1 is given. This means Y15.32 !
! ! seconds after the point in time when VRTAMA1 !
! ! is detected. !
! ! !
! ! -The value of NYKPI1 is set to 0 after the !
! ! related load report <15> was made. !
! ! !
! ! -The formula uses these parameters: !
! ! LATACONST1 Used for calculate the !
! ! Lateral Acceleration value !
! ! calculation (IMPACT1) !
! ! LATAMA1 Maximum absolute value of !
! ! Lateral Acceleration (LATA) !
! ! around first touchdown !
! ! (IMPACT1). !
!--------------!------------------------------------------------------!
! LATAMA1 ! Maximum absolute value of Lateral Acceleration !
! 999 ! around first touchdown (IMPACT1) !
! ! Format: 0.00 to 1.00 g !
! ! !
! ! Maximum absolute value of LATA during the !
! ! search interval of Y15.31 sec before and !
! ! Y15.32 sec after the point in time when !
! ! VRTAMA1 is detected. !
! ! For definition of acquisition rate, make !
! ! sure that the every valid sample received !
! ! during search interval will be taken into !
! ! account for maximum search. !
! ! !
! ! Source: DMU !
! ! !
! ! NOTE: -The value for LATAMA1 can be taken when the !
! ! VRTAMA1 is given. !
! ! !
! ! -If the detection of a bounce landing is done !
! ! before Y15.32, the calculation of LATAMA1 must!
! ! be stopped and the maximum value which was !
! ! monitored until this time must be taken. !
! ! !
! ! -The value of LATAMA1 is set to 0 after the !
! ! related load report <15> was made. !
! ! !
! ! -Refer to report <15> logic item No. 4.9.1 for !
! ! definition of landing detection (IMPACT1). !
!--------------!------------------------------------------------------!
! DNZKPI2 ! Computed Delta Vertical Acceleration (IMPACT2) !
! 999 ! Format: 0.00 to 5.00 g !
! ! !
! ! Source: DMU !
! ! !
! ! Computation Formula: !
! ! !
! ! DNZKPI2=(VRTAMA2-VRTAMI2)+(GWKG/1000*35)+ !
! ! +([|ROLLI2|^DNZCONST2]/9)-ACCONSTI2 !
! ! !
! ! If DNZKPI2 < 0 then DNZKPI2 = 0 !
! ! !
! ! NOTE: -The parameter can be calculated when the !
! ! maximum VRTAMA2, the minimum VRTAMI2 and !
! ! ROLLI2 are given. !
! ! !
! ! -The value of DNZKPI2 is set to 0 after the !
! ! related load report <15> was made. !
! ! !
! ! -The formula uses these parameters: !
! ! ACCONSTI2 Aircraft constant (IMPACT2) !
! ! (depending on A/C-type) !
! ! ROLLI2 Roll angle around second !
! ! touchdown (IMPACT2); !
! ! Refer to ROLLI2 description !
! ! DNZCONST2 Aircraft constant (IMPACT2) !
! ! (depending on A/C-type) !
! ! Refer to PTCHI2 description !
! ! GWKG Gross weight in (KG); !
! ! Refer to GWKG description !
! ! VRTAMA2 Maximum vertical !
! ! acceleration around second !
! ! touchdown (IMPACT2); !
! ! Refer to VRTAMA2 description!
! ! VRTAMI2 Minimum vertical !
! ! acceleration around second !
! ! touchdown (IMPACT2); !
! ! Refer to VRTAMI2 description!
!--------------!------------------------------------------------------!
! VRTAMA2 ! Maximum vertical acceleration around second touchdown!
! 999 ! (IMPACT2) !
! ! Format: 0.00 to 6.00 g !
! ! !
! ! Maximum value of VRTA during the search !
! ! interval Y15.21 sec before and Y15.22 sec !
! ! after second touchdown (IMPACT2). !
! ! For definition of acquisition rate, make !
! ! sure that the every valid sample received !
! ! during search interval will be taken into !
! ! account for maximum search. !
! ! !
! ! Source: DMU !
! ! !
! ! NOTE: -The value of VRTAMA2 is set to 0 after the !
! ! related load report <15> was made. !
! ! !
! ! -Refer to report <15> logic item No. 4.9.2 for !
! ! definition of landing detection (IMPACT2). !
!--------------!------------------------------------------------------!
! VRTAMI2 ! Minimum vertical acceleration around second touchdown!
! 999 ! (IMPACT2) !
! ! Format: 0.00 to 6.00 g !
! ! !
! ! Minimum value of VRTA during the search !
! ! interval Y15.61 sec before and Y15.62 sec !
! ! after the point in time when VRTAMA2 is !
! ! detected. !
! ! For definition of acquisition rate, make !
! ! sure that the every valid sample received !
! ! during search interval will be taken into !
! ! account for minimum search. !
! ! !
! ! Source: DMU !
! ! !
! ! NOTE: -The value for VRTAMI2 can be taken when the !
! ! VRTAMA2 is given. !
! ! !
! ! -The value of VRTAMI2 is set to 0 after the !
! ! related load report <15> was made. !
! ! !
! ! -Refer to report <15> logic item No. 4.9.2 for !
! ! definition of landing detection (IMPACT2). !
!--------------!------------------------------------------------------!
! ROLLI2 ! Roll angle around second touchdown (IMPACT2) !
! X999 ! Format: Negative values are shown with '-' on the !
! ! first position. If not the first position !
! ! is used for the value. !
! ! -90.0 to 90.0 deg !
! ! !
! ! Source: DMU !
! ! !
! ! NOTE: -The value for ROLLI2 can be taken when the !
! ! VRTAMI2 is given. !
! ! !
! ! -To calculate ROLLI2 the parameter ROLL must be!
! ! monitored with a rate of 32Hz. !
! ! !
! ! -The value of ROLLI2 is set to 0 after the !
! ! related load report <15> was made. !
! ! !
! ! -Refer to report <15> logic item No. 4.9.2 for !
! ! definition of landing detection (IMPACT2). !
!--------------!------------------------------------------------------!
! NYKPI2 ! Computed Lateral Acceleration (IMPACT2) !
! 999 ! Format: 0.00 to 1.00 g !
! ! !
! ! Source: DMU !
! ! !
! ! Computation Formula: !
! ! !
! ! NYKPI2=(LATACONST2*|LATAMA2|) !
! ! !
! ! !
! ! NOTE: -The parameter can be calculated when the !
! ! maximum LATAMA2 is given. This means Y15.42 !
! ! seconds after the point in time when VRTAMA2 !
! ! is detected. !
! ! !
! ! -The value of NYKPI2 is set to 0 after the !
! ! related load report <15> was made. !
! ! !
! ! -The formula uses these parameters: !
! ! LATACONST2 Used for calculate the !
! ! Lateral Acceleration value !
! ! calculation (IMPACT2) !
! ! LATAMA2 Maximum absolute value of !
! ! Lateral Acceleration (LATA) !
! ! around second touchdown !
! ! (IMPACT2). !
!--------------!------------------------------------------------------!
! LATAMA2 ! Maximum absolute value of Lateral Acceleration !
! 999 ! around second touchdown (IMPACT2) !
! ! Format: 0.00 to 1.00 g !
! ! !
! ! Maximum absolute value of LATA during the !
! ! search interval of Y15.41 sec before and !
! ! Y15.42 sec after the point in time when !
! ! VRTAMA2 is detected. !
! ! For definition of acquisition rate, make !
! ! sure that the every valid sample received !
! ! during search interval will be taken into !
! ! account for maximum search. !
! ! !
! ! Source: DMU !
! ! !
! ! NOTE: -The value for LATAMA2 can be taken when the !
! ! VRTAMA2 is given. !
! ! !
! ! NOTE: -The value of LATAMA2 is set to 0 after the !
! ! related load report <15> was made. !
! ! !
! ! -Refer to report <15> logic item No. 4.9.2 for !
! ! definition of landing detection (IMPACT2). !
!--------------!------------------------------------------------------!
! GWKG ! Gross Weight in kg !
! 99999 ! Format: 0 to 90000 kg !
! ! !
! ! Source: FMGC 02.1.075.00 !
! ! 02.2.075.00 !
! ! NOTE: The FMGC is sending the value with the unit !
! ! (lbs). The received value must be changed !
! ! into unit (kg). !
!--------------!------------------------------------------------------!
! LHLG ! Left Hand Landing Gear !
! 1 ! Format: Bit Status 1 = LH landing gear compressed !
! ! !
! ! Source: LGCIU 6D.1.021.01.13 !
! ! 6D.2.021.10.13 !
!--------------!------------------------------------------------------!
! RHLG ! Right Hand Landing Gear !
! 1 ! Format: Bit Status 1 = RH landing gear compressed !
! ! !
! ! Source: LGCIU 6D.1.021.01.14 !
! ! 6D.2.021.10.14 !
!--------------!------------------------------------------------------!
! MLG ! Main (LH and RH) Landing Gear !
! 1 ! Format: Bit Status 1 = Main (LH and RH) landing !
! ! gear compressed !
! ! !
! ! Source: LGCIU 6D.1.021.01.11 !
! ! 6D.2.021.10.11 !
!--------------!------------------------------------------------------!
! PTCH ! Pitch Angle !
! X999 ! Format: Negative values are shown with 'N' on the !
! ! first position. If not the first position !
! ! is used for the value. !
! ! -90.0 to 90.0 deg !
! ! Source: ADIRU 04.1.324.01 !
! ! 04.2.324.10 !
!--------------!------------------------------------------------------!
! PTCR ! Body Pitch Rate !
! X999 ! Format: Negative values are shown with 'N' on the !
! ! first position. If not the first position !
! ! is used for the value. !
! ! -45.0 to 45.0 deg/sec !
! ! Source: ADIRU 04.1.326.01 !
! ! 04.2.326.10 !
!--------------!------------------------------------------------------!
! ROLL ! Roll Angle !
! X999 ! Format: Negative values are shown with 'N' on the !
! ! first position. If not the first position !
! ! is used for the value. !
! ! -90.0 to 90.0 deg !
! ! Source: ADIRU 04.1.325.01 !
! ! 04.2.325.10 !
!--------------!------------------------------------------------------!
! ROLR ! Body Roll Rate !
! X999 ! Format: Negative values are shown with 'N' on the !
! ! first position. If not the first position !
! ! is used for the value. !
! ! -45.0 to 45.0 deg/sec !
! ! Source: ADIRU 04.1.327.01 !
! ! 04.2.327.10 !
!--------------!------------------------------------------------------!
! YAW ! YAW Rate !
! X999 ! Format: Negative values are shown with 'N' on the !
! ! first position. If not the first position !
! ! is used for the value. !
! ! -45.0 to 45.0 deg/sec !
! ! Source: ADIRU 04.1.330.01 !
! ! 04.2.330.10 !
!--------------!------------------------------------------------------!
! VRTA ! Normal Acceleration !
! X999 ! Format: Negative values are shown with 'N' on the !
! ! first position. If not the first position !
! ! is used for the value. !
! ! -3.00 to 6.00 g !
! ! Source: SDAC 29.1.333.01 !
! ! 29.2.333.01 !
!--------------!------------------------------------------------------!
! LATA ! Lateral Acceleration !
! X999 ! Format: Negative values are shown with 'N' on the !
! ! first position. If not the first position !
! ! is used for the value. !
! ! -1.00 to 1.00 g !
! ! Source: SDAC 29.1.332.01 !
! ! 29.2.332.01 !
!--------------!------------------------------------------------------!
! LONA ! Longitudinal Acceleration !
! X999 ! Format: Negative values are shown with 'N' on the !
! ! first position. If not the first position !
! ! is used for the value. !
! ! -1.00 to 1.00 g !
! ! Source: SDAC 29.1.331.01 !
! ! 29.2.331.01 !
!--------------!------------------------------------------------------!
! MN ! Mach Number !
! 999 ! Format: 0.100 to 0.999 !
! ! !
! ! Source: ADIRU 06.1.205.01 !
! ! 06.2.205.10 !
+---------------------------------------------------------------------+

(10) Load Report Data Field Description <15>
+---------------------------------------------------------------------+
! Value ! Content Description !
!--------------!------------------------------------------------------!
! ESN ! Engine Serial Number !
! 999999 ! Format: 000000 to 999999 !
! ! Source: !
! ! EEC/ECU Engine 1 7C.1.046.01 digit 3, 2, 1 !
! ! 7C.1.047.01 digit 6, 5, 4 !
! ! Engine 2 7C.2.046.10 digit 3, 2, 1 !
! ! 7C.2.047.10 digit 6, 5, 4 !
!--------------!------------------------------------------------------!
! EHRS ! Engine Flight Hours !
! 99999 ! Format: 00000 to 99999 hours !
! ! Source: DMU Engine 1 0D.1.060.01 !
! ! Engine 2 0D.1.060.10 !
! ! NOTE: 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. !
!--------------!------------------------------------------------------!
! AP ! Auto Pilot Status !
! 99 ! Format: Number of respective status 00 to 24 !
! ! Source: FMGC 1 and 2 (FGC part) for Auto Pilot 1 !
! ! and 2 !
! +------------!-----------------------------------------------------+!
! ! Auto Pilot ! Parameter for AP1 ! Parameter for AP2 ! Definition !!
! ! Status ! Report Line EC ! Report Line EE ! !!
! !------------!--------------------!-------------------!------------!!
! ! 00 !--------------------!-------------------! No Mode !!
! ! ! ! ! Active !!
! !------------!--------------------!-------------------!------------!!
! ! 01 ! 01.1.275.00.11 = 1 ! 01.2.275.00.11 = 1!RUNWAY Mode !!
! !------------!--------------------!-------------------!------------!!
! ! 02 ! 01.1.275.00.12 = 1 ! 01.2.275.00.12 = 1!NAV Mode !!
! !------------!--------------------!-------------------!------------!!
! ! 03 ! 01.1.275.00.13 = 1 ! 01.2.275.00.13 = 1!LOC CAPTURE !!
! ! ! ! !Mode !!
! !------------!--------------------!-------------------!------------!!
! ! 04 ! 01.1.275.00.14 = 1 ! 01.2.275.00.14 = 1!LOC TRACK !!
! ! ! ! !Mode !!
! !------------!--------------------!-------------------!------------!!
! ! 05 ! 01.1.275.00.15 = 1 ! 01.2.275.00.15 = 1!Roll GO !!
! ! ! ! !AROUND Mode !!
! !------------!--------------------!-------------------!------------!!
! ! 06 ! 01.1.275.00.16 = 1 ! 01.2.275.00.16 = 1!HEADING Mode!!
! !------------!--------------------!-------------------!------------!!
! ! 07 ! 01.1.275.00.17 = 1 ! 01.2.275.00.17 = 1!TRACK Mode !!
! !------------!--------------------!-------------------!------------!!
! ! 08 ! 01.1.274.00.15 = 1 ! 01.2.274.00.15 = 1!PITCH T/O !!
! ! ! ! !Mode !!
! !------------!--------------------!-------------------!------------!!
! ! 09 ! 01.1.274.00.16 = 1 ! 01.2.274.00.16 = 1!PITCH GA !!
! ! ! ! !Mode !!
! !------------!--------------------!-------------------!------------!!
! ! 10 ! 01.1.274.00.17 = 1 ! 01.2.274.00.17 = 1!V/S Mode !!
! !------------! -------------------!-------------------!------------!!
! ! 11 ! 01.1.274.00.18 = 1 ! 01.2.274.00.18 = 1!FPA Mode !!
! !------------! -------------------!-------------------!------------!!
! ! 12 ! 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! !!
! !------------! -------------------!-------------------!------------!!
! ! 13 ! 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! !!
! !------------!--------------------!-------------------!------------!!
! ! 14 ! 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! !!
! !------------!--------------------!-------------------!------------!!
! ! 15 ! 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! !!
! !------------!--------------------!-------------------!------------!!
! ! 16 ! 01.1.274.00.23 = 1 ! 01.2.274.00.23 = 1!FINAL DES !!
! ! ! ! !Mode !!
! !------------!--------------------!-------------------!------------!!
! ! 17 ! 01.1.274.00.24 = 1 ! 01.2.274.00.24 = 1!EXPED. Mode !!
! !------------!--------------------!-------------------!------------!!
! ! 18 ! 01.1.146.00.14 = 1 ! 01.2.146.00.14 = 1!LAND TRACK !!
! ! ! ! !Mode !!
! !------------!--------------------!-------------------!------------!!
! ! 19 ! 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! !!
! !------------!--------------------!-------------------!------------!!
! ! 20 ! 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! !!
! !------------!--------------------!-------------------!------------!!
! ! 21 ! 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! !!
! !------------! -------------------!-------------------!------------!!
! ! 22 ! 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! !!
! !------------! -------------------!-------------------!------------!!
! ! 23 ! 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! !!
! !------------! -------------------!-------------------!------------!!
! ! 24 ! 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 0D.1.274.01 AP1 printed in report line EC !
! ! 0D.1.274.10 AP2 printed in report line EE !
!--------------!------------------------------------------------------!
! FLAP ! FLAP Position !
! X999 ! Format: 0 to 40.0 deg (see table DT40 for special !
! ! conversion) !
! ! Source: SFCC 1B.1.137.01 !
! ! 1B.2.137.10 !
!--------------!------------------------------------------------------!
! SLAT ! SLAT Position !
! X999 ! Format: 0 to 27.0 deg (see table DT41 for special !
! ! conversion) !
! ! Source: SFCC 1B.1.127.01 !
! ! 1B.2.127.10 !
!--------------!------------------------------------------------------!
! MAX ! Highest value (if the exceedance is positive) or !
! X999 ! lowest value (if the exceedance is negative) of !
! ! the exceeding parameter within a time interval of !
! ! 0.5 sec before 'event detection' until 0.5 sec !
! ! after 'event detection'. !
! ! In case of RAG detection (Trigger code 4xxx), !
! ! manual trigger (code 1000) or standard trigger !
! ! (code 7000) the value is "0" !
! ! !
! ! Format: Depends on exceeded parameter !
! ! !
! ! Source: Depends on exceeded parameter !
! ! !
! ! NOTE: The exceedance value can be either negative !
! ! or positive depending on the exceeded limit. !
! ! In case of a negative limit, the lowest negative !
! ! value of the exceeding parameter must be taken. !
! ! !
!--------------!------------------------------------------------------!
! LIM ! Programmable limit, which was exceeded !
! X999 ! In case of RAG detection (Trigger code 4xxx) the !
! ! value is "0" !
! ! !
! ! Format: Depends on the parameter !
! ! !
! ! Source: Depends on the parameter !
! ! !
!--------------!------------------------------------------------------!
! COUNTS ! Counter for spoiler 4 extensions !
! ! 999 999 999 999 999 !
! ! --- --- --- --- --- !
! ! 0 > Spoiler >= -5 ______! ! ! ! ! !
! ! -5 > Spoiler >= -10 ___________! ! ! ! !
! ! -10 > Spoiler >= -15 ________________! ! ! !
! ! -15> Spoiler >= -20 _____________________! ! !
! ! Spoiler < -20 __________________________! !
! ! !
! ! Format: 0 to 9999 !
! ! !
! ! Source: 6C.1.364.01 LH Spoiler 4 Position !
! ! 6C.2.364.10 !
! ! 6C.1.374.01 RH Spoiler 4 Position !
! ! 6C.2.374.10 !
! ! 6C.1.044.01.24 = 1 Spoiler 4 Fault !
! ! 6C.2.044.10.24 = 1 !
! ! 6C.1.365.01 LH Spoiler 5 Position !
! ! 6C.2.365.10 !
! ! 6C.1.375.01 RH Spoiler 5 Position !
! ! 6C.2.375.10 !
! ! 6C.1.044.01.25 = 1 Spoiler 5 Fault !
! ! 6C.2.044.10.25 !
! ! 6C.1.041.01.21 = 1 Load Alleviation Active !
! ! 6C.2.041.10.21 (LAF) !
! ! !
! ! NOTE: The max extension values of the LH Spoiler !
! ! 4 is counted as long as LAF is active and Spoiler 4!
! ! is not fault. The value of LH Spoiler 4 is compared!
! ! with the value of RH Spoiler 4, which are detected !
! ! at the same time of max LH Spoiler 4. The lower one!
! ! of these values effects the counts as defined above!
! ! If Spoiler 4 is fault and Spoiler 5 is not fault, !
! ! the Spoiler 5 LH and RH is used for calculation !
! ! and counts. !
!--------------!------------------------------------------------------!
! REASON ! Reason for trigger !
! XXXXXXXXXX ! Format: Up to 20 characters !
! ! MANUAL TRIGGERING Code: 1000 !
! ! GW RED BOUNCE Code: 4310 !
! ! GW AMBER BOUNCE Code: 4320 !
! ! GW RED Code: 4410 !
! ! GW AMBER Code: 4420 !
! ! RED BOUNCE Code: 4510 !
! ! AMBER BOUNCE Code: 4520 !
! ! RED Code: 4610 !
! ! AMBER Code: 4620 !
! ! VRTA Code: 5100, 5200 and 5300 !
! ! SPCT Code: 5400 !
! ! LATA AMBER Code: 5600 !
! ! LATA RED Code: 5700 !
! ! STANDARD TRIGGER Code: 7000 !
! ! !
! ! Source: DMU !
! ! NOTE: For other codes not given above blanks must !
! ! be printed. !
!--------------!------------------------------------------------------!
! DNZKPI1 ! Computed Delta Vertical Acceleration (IMPACT1) !
! 999 ! Format: 0.00 to 5.00 g !
! ! !
! ! Source: DMU !
! ! !
! ! Computation Formula: !
! ! !
! ! DNZKPI1=(VRTAMA1-VRTAMI1)+(GWKG/1000*35)+ !
! ! +([|ROLLI1|^DNZCONST1]/9)-ACCONSTI1 !
! ! !
! ! If DNZKPI1 < 0 then DNZKPI1 = 0 !
! ! !
! ! NOTE: -The parameter can be calculated when the !
! ! maximum VRTAMA1, the minimum VRTAMI1 and !
! ! ROLLI1 are given. !
! ! !
! ! -The value of DNZKPI1 is set to 0 after the !
! ! related load report <15> was made. !
! ! !
! ! -The formula uses these parameters: !
! ! ACCONSTI1 Aircraft constant (IMPACT1) !
! ! (depending on A/C-type) !
! ! ROLLI1 Roll angle around first !
! ! touchdown (IMPACT1); !
! ! Refer to ROLLI1 description !
! ! DNZCONST1 Aircraft constant (IMPACT1) !
! ! (depending on A/C-type) !
! ! GWKG Gross weight in (KG); !
! ! Refer to GWKG description !
! ! VRTAMA1 Maximum vertical !
! ! acceleration around first !
! ! touchdown (IMPACT1); !
! ! Refer to VRTAMA1 description!
! ! VRTAMI1 Minimum vertical !
! ! acceleration around first !
! ! touchdown (IMPACT1); !
! ! Refer to VRTAMI1 description!
!--------------!------------------------------------------------------!
! VRTAMA1 ! Maximum vertical acceleration around first touchdown!
! 999 ! (IMPACT1) !
! ! Format: 0.00 to 6.00 g !
! ! !
! ! Maximum value of VRTA during the search !
! ! interval Y15.11 sec before and Y15.12 sec !
! ! after first touchdown (IMPACT1). !
! ! For definition of acquisition rate, make !
! ! sure that the every valid sample received !
! ! during search interval will be taken into !
! ! account for maximum search. !
! ! !
! ! Source: DMU !
! ! !
! ! NOTE: -If the detection of a bounce landing is done !
! ! before Y15.12, the calculation of VRTAMA1 must!
! ! be stopped and the maximum value which was !
! ! monitored until this time must be taken. !
! ! !
! ! -The value of VRTAMA1 is set to 0 after the !
! ! related load report <15> was made. !
! ! !
! ! -Refer to report <15> logic item No. 4.9.1 for !
! ! definition of landing detection (IMPACT1). !
!--------------!------------------------------------------------------!
! VRTAMI1 ! Minimum vertical acceleration around first touchdown!
! 999 ! (IMPACT1) !
! ! Format: 0.00 to 6.00 g !
! ! !
! ! Minimum value of VRTA during the search !
! ! interval Y15.51 sec before and Y15.52 sec !
! ! after the point in time when VRTAMA1 is !
! ! detected. !
! ! For definition of acquisition rate, make !
! ! sure that the every valid sample received !
! ! during search interval will be taken into !
! ! account for minimum search. !
! ! !
! ! Source: DMU !
! ! !
! ! NOTE: -The value for VRTAMI1 can be taken when the !
! ! VRTAMA1 is given. !
! ! !
! ! -If the detection of a bounce landing is done !
! ! before Y15.52, the calculation of VRTAMI1 must!
! ! be stopped and the maximum value which was !
! ! monitored until this time must be taken. !
! ! !
! ! -The value of VRTAMI1 is set to 0 after the !
! ! related load report <15> was made. !
! ! !
! ! -Refer to report <15> logic item No. 4.9.1 for !
! ! definition of landing detection (IMPACT1). !
!--------------!------------------------------------------------------!
! ROLLI1 ! Roll angle around first touchdown (IMPACT1) !
! X999 ! Format: Negative values are shown with '-' on the !
! ! first position. If not the first position !
! ! is used for the value. !
! ! -90.0 to 90.0 deg !
! ! !
! ! Source: DMU !
! ! !
! ! NOTE: -The value for ROLLI1 can be taken when the !
! ! VRTAMI1 is given. !
! ! !
! ! -To calculate ROLLI1 the parameter ROLL must be!
! ! monitored with a rate of 32Hz. !
! ! !
! ! -The value of ROLLI1 is set to 0 after the !
! ! related load report <15> was made. !
! ! !
! ! -Refer to report <15> logic item No. 4.9.1 for !
! ! definition of landing detection (IMPACT1). !
!--------------!------------------------------------------------------!
! NYKPI1 ! Computed Lateral Acceleration (IMPACT1) !
! 999 ! Format: 0.00 to 1.00 g !
! ! !
! ! Source: DMU !
! ! !
! ! Computation Formula: !
! ! !
! ! NYKPI1=(LATACONST1*|LATAMA1|) !
! ! !
! ! !
! ! NOTE: -The parameter can be calculated when the !
! ! maximum LATAMA1 is given. This means Y15.32 !
! ! seconds after the point in time when VRTAMA1 !
! ! is detected. !
! ! !
! ! -The value of NYKPI1 is set to 0 after the !
! ! related load report <15> was made. !
! ! !
! ! -The formula uses these parameters: !
! ! LATACONST1 Used for calculate the !
! ! Lateral Acceleration value !
! ! calculation (IMPACT1) !
! ! LATAMA1 Maximum absolute value of !
! ! Lateral Acceleration (LATA) !
! ! around first touchdown !
! ! (IMPACT1). !
!--------------!------------------------------------------------------!
! LATAMA1 ! Maximum absolute value of Lateral Acceleration !
! 999 ! around first touchdown (IMPACT1) !
! ! Format: 0.00 to 1.00 g !
! ! !
! ! Maximum absolute value of LATA during the !
! ! search interval of Y15.31 sec before and !
! ! Y15.32 sec after the point in time when !
! ! VRTAMA1 is detected. !
! ! For definition of acquisition rate, make !
! ! sure that the every valid sample received !
! ! during search interval will be taken into !
! ! account for maximum search. !
! ! !
! ! Source: DMU !
! ! !
! ! NOTE: -The value for LATAMA1 can be taken when the !
! ! VRTAMA1 is given. !
! ! !
! ! -If the detection of a bounce landing is done !
! ! before Y15.32, the calculation of LATAMA1 must!
! ! be stopped and the maximum value which was !
! ! monitored until this time must be taken. !
! ! !
! ! -The value of LATAMA1 is set to 0 after the !
! ! related load report <15> was made. !
! ! !
! ! -Refer to report <15> logic item No. 4.9.1 for !
! ! definition of landing detection (IMPACT1). !
!--------------!------------------------------------------------------!
! DNZKPI2 ! Computed Delta Vertical Acceleration (IMPACT2) !
! 999 ! Format: 0.00 to 5.00 g !
! ! !
! ! Source: DMU !
! ! !
! ! Computation Formula: !
! ! !
! ! DNZKPI2=(VRTAMA2-VRTAMI2)+(GWKG/1000*35)+ !
! ! +([|ROLLI2|^DNZCONST2]/9)-ACCONSTI2 !
! ! !
! ! If DNZKPI2 < 0 then DNZKPI2 = 0 !
! ! !
! ! NOTE: -The parameter can be calculated when the !
! ! maximum VRTAMA2, the minimum VRTAMI2 and !
! ! ROLLI2 are given. !
! ! !
! ! -The value of DNZKPI2 is set to 0 after the !
! ! related load report <15> was made. !
! ! !
! ! -The formula uses these parameters: !
! ! ACCONSTI2 Aircraft constant (IMPACT2) !
! ! (depending on A/C-type) !
! ! ROLLI2 Roll angle around second !
! ! touchdown (IMPACT2); !
! ! Refer to ROLLI2 description !
! ! DNZCONST2 Aircraft constant (IMPACT2) !
! ! (depending on A/C-type) !
! ! GWKG Gross weight in (KG); !
! ! Refer to GWKG description !
! ! VRTAMA2 Maximum vertical !
! ! acceleration around second !
! ! touchdown (IMPACT2); !
! ! Refer to VRTAMA2 description!
! ! VRTAMI2 Minimum vertical !
! ! acceleration around second !
! ! touchdown (IMPACT2); !
! ! Refer to VRTAMI2 description!
!--------------!------------------------------------------------------!
! VRTAMA2 ! Maximum vertical acceleration around second touchdown!
! 999 ! (IMPACT2) !
! ! Format: 0.00 to 6.00 g !
! ! !
! ! Maximum value of VRTA during the search !
! ! interval Y15.21 sec before and Y15.22 sec !
! ! after second touchdown (IMPACT2). !
! ! For definition of acquisition rate, make !
! ! sure that the every valid sample received !
! ! during search interval will be taken into !
! ! account for maximum search. !
! ! !
! ! Source: DMU !
! ! !
! ! NOTE: -The value of VRTAMA2 is set to 0 after the !
! ! related load report <15> was made. !
! ! !
! ! -Refer to report <15> logic item No. 4.9.2 for !
! ! definition of landing detection (IMPACT2). !
!--------------!------------------------------------------------------!
! VRTAMI2 ! Minimum vertical acceleration around second touchdown!
! 999 ! (IMPACT2) !
! ! Format: 0.00 to 6.00 g !
! ! !
! ! Minimum value of VRTA during the search !
! ! interval Y15.61 sec before and Y15.62 sec !
! ! after the point in time when VRTAMA2 is !
! ! detected. !
! ! For definition of acquisition rate, make !
! ! sure that the every valid sample received !
! ! during search interval will be taken into !
! ! account for minimum search. !
! ! !
! ! Source: DMU !
! ! !
! ! NOTE: -The value for VRTAMI2 can be taken when the !
! ! VRTAMA2 is given. !
! ! !
! ! -The value of VRTAMI2 is set to 0 after the !
! ! related load report <15> was made. !
! ! !
! ! -Refer to report <15> logic item No. 4.9.2 for !
! ! definition of landing detection (IMPACT2). !
!--------------!------------------------------------------------------!
! ROLLI2 ! Roll angle around second touchdown (IMPACT2) !
! X999 ! Format: Negative values are shown with '-' on the !
! ! first position. If not the first position !
! ! is used for the value. !
! ! -90.0 to 90.0 deg !
! ! !
! ! Source: DMU !
! ! !
! ! NOTE: -The value for ROLLI2 can be taken when the !
! ! VRTAMI2 is given. !
! ! !
! ! -To calculate ROLLI2 the parameter ROLL must be!
! ! monitored with a rate of 32Hz. !
! ! !
! ! -The value of ROLLI2 is set to 0 after the !
! ! related load report <15> was made. !
! ! !
! ! -Refer to report <15> logic item No. 4.9.2 for !
! ! definition of landing detection (IMPACT2) !
!--------------!------------------------------------------------------!
! NYKPI2 ! Computed Lateral Acceleration (IMPACT2) !
! 999 ! Format: 0.00 to 1.00 g !
! ! !
! ! Source: DMU !
! ! !
! ! Computation Formula: !
! ! !
! ! NYKPI2=(LATACONST2*|LATAMA2|) !
! ! !
! ! !
! ! NOTE: -The parameter can be calculated when the !
! ! maximum LATAMA2 is given. This means Y15.42 !
! ! seconds after the point in time when VRTAMA2 !
! ! is detected. !
! ! !
! ! -The value of NYKPI2 is set to 0 after the !
! ! related load report <15> was made. !
! ! !
! ! -The formula uses these parameters: !
! ! LATACONST2 Used for calculate the !
! ! Lateral Acceleration value !
! ! calculation (IMPACT2) !
! ! LATAMA2 Maximum absolute value of !
! ! Lateral Acceleration (LATA) !
! ! around second touchdown !
! ! (IMPACT2). !
!--------------!------------------------------------------------------!
! LATAMA2 ! Maximum absolute value of Lateral Acceleration !
! 999 ! around second touchdown (IMPACT2) !
! ! Format: 0.00 to 1.00 g !
! ! !
! ! Maximum absolute value of LATA during the !
! ! search interval of Y15.41 sec before and !
! ! Y15.42 sec after the point in time when !
! ! VRTAMA2 is detected. !
! ! For definition of acquisition rate, make !
! ! sure that the every valid sample received !
! ! during search interval will be taken into !
! ! account for maximum search. !
! ! !
! ! Source: DMU !
! ! !
! ! NOTE: -The value for LATAMA2 can be taken when the !
! ! VRTAMA2 is given. !
! ! !
! ! -The value of LATAMA2 is set to 0 after the !
! ! related load report <15> was made. !
! ! !
! ! -Refer to report <15> logic item No. 4.9.2 for !
! ! definition of landing detection (IMPACT2). !
!--------------!------------------------------------------------------!
! GWKG ! Gross Weight in kg !
! 99999 ! Format: 0 to 90000 kg !
! ! !
! ! Source: FMGC 02.1.075.00 !
! ! 02.2.075.00 !
! ! NOTE: The FMGC is sending the value with the unit !
! ! (lbs). The received value must be changed !
! ! into unit (kg). !
!--------------!------------------------------------------------------!
! LHLG ! Left Hand Landing Gear !
! 1 ! Format: Bit Status 1 = LH landing gear compressed !
! ! !
! ! Source: LGCIU 6D.1.021.01.13 !
! ! 6D.2.021.10.13 !
!--------------!------------------------------------------------------!
! RHLG ! Right Hand Landing Gear !
! 1 ! Format: Bit Status 1 = RH landing gear compressed !
! ! !
! ! Source: LGCIU 6D.1.021.01.14 !
! ! 6D.2.021.10.14 !
!--------------!------------------------------------------------------!
! MLG ! Main (LH and RH) Landing Gear !
! 1 ! Format: Bit Status 1 = Main (LH and RH) landing !
! ! gear compressed !
! ! !
! ! Source: LGCIU 6D.1.021.01.11 !
! ! 6D.2.021.10.11 !
!--------------!------------------------------------------------------!
! PTCH ! Pitch Angle !
! X999 ! Format: Negative values are shown with 'N' on the !
! ! first position. If not the first position !
! ! is used for the value. !
! ! -90.0 to 90.0 deg !
! ! Source: ADIRU 04.1.324.01 !
! ! 04.2.324.10 !
!--------------!------------------------------------------------------!
! PTCR ! Body Pitch Rate !
! X999 ! Format: Negative values are shown with 'N' on the !
! ! first position. If not the first position !
! ! is used for the value. !
! ! -45.0 to 45.0 deg/sec !
! ! Source: ADIRU 04.1.326.01 !
! ! 04.2.326.10 !
!--------------!------------------------------------------------------!
! ROLL ! Roll Angle !
! X999 ! Format: Negative values are shown with 'N' on the !
! ! first position. If not the first position !
! ! is used for the value. !
! ! -90.0 to 90.0 deg !
! ! Source: ADIRU 04.1.325.01 !
! ! 04.2.325.10 !
!--------------!------------------------------------------------------!
! ROLR ! Body Roll Rate !
! X999 ! Format: Negative values are shown with 'N' on the !
! ! first position. If not the first position !
! ! is used for the value. !
! ! -45.0 to 45.0 deg/sec !
! ! Source: ADIRU 04.1.327.01 !
! ! 04.2.327.10 !
!--------------!------------------------------------------------------!
! YAW ! YAW Rate !
! X999 ! Format: Negative values are shown with 'N' on the !
! ! first position. If not the first position !
! ! is used for the value. !
! ! -45.0 to 45.0 deg/sec !
! ! Source: ADIRU 04.1.330.01 !
! ! 04.2.330.10 !
!--------------!------------------------------------------------------!
! VRTA ! Normal Acceleration !
! X999 ! Format: Negative values are shown with 'N' on the !
! ! first position. If not the first position !
! ! is used for the value. !
! ! -3.00 to 6.00 g !
! ! Source: SDAC 29.1.333.01 !
! ! 29.2.333.01 !
!--------------!------------------------------------------------------!
! LATA ! Lateral Acceleration !
! X999 ! Format: Negative values are shown with 'N' on the !
! ! first position. If not the first position !
! ! is used for the value. !
! ! -1.00 to 1.00 g !
! ! Source: SDAC 29.1.332.01 !
! ! 29.2.332.01 !
!--------------!------------------------------------------------------!
! LONA ! Longitudinal Acceleration !
! X999 ! Format: Negative values are shown with 'N' on the !
! ! first position. If not the first position !
! ! is used for the value. !
! ! -1.00 to 1.00 g !
! ! Source: SDAC 29.1.331.01 !
! ! 29.2.331.01 !
!--------------!------------------------------------------------------!
! MN ! Mach Number !
! 999 ! Format: 0.100 to 0.999 !
! ! !
! ! Source: ADIRU 06.1.205.01 !
! ! 06.2.205.10 !
+---------------------------------------------------------------------+

(11) Parameter logic:
+---------------------------------------------------------------------+
! Param. ! Print Value (Standard Progr.) !
!--------------!------------------------------------------------------!
! FLAP ! Value at moment of trigger. !
!--------------!------------------------------------------------------!
! SLAT ! Value at moment of trigger. !
!--------------!------------------------------------------------------!
! MAX * ! Max value during 0.5 sec before until 0.5 sec after!
! ! landing. !
!--------------!------------------------------------------------------!
! LIM ! Value at moment of trigger. !
!--------------! -----------------------------------------------------!
! COUNTS ! Current value. !
!--------------! -----------------------------------------------------!
! REASON ! Reason of trigger. !
!--------------! -----------------------------------------------------!
! RALT ! Snapshot value. !
!--------------! -----------------------------------------------------!
! RALR ! Snapshot value. !
!--------------! -----------------------------------------------------!
! PTCH ! Snapshot value. !
!--------------! -----------------------------------------------------!
! PTCR ! Snapshot value. !
!--------------! -----------------------------------------------------!
! ROLL ! Snapshot value. !
!--------------! -----------------------------------------------------!
! ROLR ! Snapshot value. !
!--------------! -----------------------------------------------------!
! YAW ! Snapshot value. !
!--------------! -----------------------------------------------------!
! VRTA ! Max and Min values. !
!--------------!------------------------------------------------------!
! LONA ! Max and Min values. !
!--------------!------------------------------------------------------!
! LATA ! Max and Min values. !
+---------------------------------------------------------------------+
* NOTE: In case of report generation due to RALRL limit exceedance, the RALR value is taken at the dataset time fixed in item 'L' of the report logic.
(12) Parameter logic:
+---------------------------------------------------------------------+
! Param. ! Print Value (Standard Progr.) !
!--------------!------------------------------------------------------!
! ESN ! Value at moment of trigger. !
!--------------!------------------------------------------------------!
! EHRS ! Value at moment of trigger. !
!--------------!------------------------------------------------------!
! AP ! Value at moment of trigger. !
!--------------!------------------------------------------------------!
! FLAP ! Value at moment of trigger. !
!--------------!------------------------------------------------------!
! SLAT ! Value at moment of trigger. !
!--------------!------------------------------------------------------!
! MAX* ! Max value during 0.5 sec before until 0.5 sec after!
! ! landing. !
!--------------!------------------------------------------------------!
! LIM ! Value at moment of trigger. !
!--------------! -----------------------------------------------------!
! COUNTS ! Current value. !
!--------------! -----------------------------------------------------!
! REASON ! Reason of trigger. !
!--------------! -----------------------------------------------------!
! RALT ! Snapshot value. !
!--------------! -----------------------------------------------------!
! RALR ! Snapshot value. !
!--------------! -----------------------------------------------------!
! PTCH ! Snapshot value. !
!--------------! -----------------------------------------------------!
! PTCR ! Snapshot value. !
!--------------! -----------------------------------------------------!
! ROLL ! Snapshot value. !
!--------------! -----------------------------------------------------!
! ROLR ! Snapshot value. !
!--------------! -----------------------------------------------------!
! YAW ! Snapshot value. !
!--------------! -----------------------------------------------------!
! VRTA ! Max and Min values. !
!--------------!------------------------------------------------------!
! LONA ! Max and Min values. !
!--------------!------------------------------------------------------!
! LATA ! Max and Min values. !
+---------------------------------------------------------------------+

*Remark: In case of report generation due to RALRL limit exceedance the RALR value is taken at the dataset time fixed in item 'L' of report logic.
(13) Parameter logic:
+---------------------------------------------------------------------+
! Param. ! Print Value (Standard Progr.) !
!--------------+------------------------------------------------------!
! ESN ! Value at moment of trigger. !
!--------------!------------------------------------------------------!
! EHRS ! Value at moment of trigger. !
!--------------!------------------------------------------------------!
! AP ! Value at moment of trigger. !
!--------------!------------------------------------------------------!
! FLAP ! Value at moment of trigger. !
!--------------!------------------------------------------------------!
! SLAT ! Value at moment of trigger. !
!--------------!------------------------------------------------------!
! MAX * ! Max value during 0.5 sec before until 0.5 sec after!
! ! landing. !
!--------------!------------------------------------------------------!
! LIM ! Value at moment of trigger. !
!--------------! -----------------------------------------------------!
! COUNTS ! Current value. !
!--------------! -----------------------------------------------------!
! REASON ! Reason of trigger. !
!--------------! -----------------------------------------------------!
! RALT ! Snapshot value. !
!--------------! -----------------------------------------------------!
! RALR ! Snapshot value. !
!--------------! -----------------------------------------------------!
! PTCH ! Snapshot value. !
!--------------! -----------------------------------------------------!
! PTCR ! Snapshot value. !
!--------------! -----------------------------------------------------!
! ROLL ! Snapshot value. !
!--------------! -----------------------------------------------------!
! ROLR ! Snapshot value. !
!--------------! -----------------------------------------------------!
! YAW ! Snapshot value. !
!--------------! -----------------------------------------------------!
! VRTA ! Max and Min values . !
!--------------!------------------------------------------------------!
! LONA ! Max and Min values. !
!--------------!------------------------------------------------------!
! LATA ! Max and Min values. !
+---------------------------------------------------------------------+

*Remark: In case of report generation due to RALRL limit exceedance the RALR value must be taken at the dataset time fixed in item L of report logic.
(14) Parameter logic:
+---------------------------------------------------------------------+
! Param. ! Print Value (Standard Progr.) !
!--------------!------------------------------------------------------!
! FLAP ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! SLAT ! Value at moment of trigger !
!--------------!------------------------------------------------------!
! MAX * ! Max value during 0,5 sec before until 0,5 sec after!
! ! landing !
!--------------!------------------------------------------------------!
! LIM ! Value at moment of trigger !
!--------------! -----------------------------------------------------!
! COUNTS ! Current value !
!--------------! -----------------------------------------------------!
! REASON ! Reason of trigger !
!--------------! -----------------------------------------------------!
! RALT ! Snapshot value !
!--------------! -----------------------------------------------------!
! RALR ! Snapshot value !
!--------------! -----------------------------------------------------!
! PTCH ! Snapshot value !
!--------------! -----------------------------------------------------!
! PTCR ! Snapshot value !
!--------------! -----------------------------------------------------!
! ROLL ! Snapshot value !
!--------------! -----------------------------------------------------!
! ROLR ! Snapshot value !
!--------------! -----------------------------------------------------!
! YAW ! Snapshot value !
!--------------! -----------------------------------------------------!
! VRTA ! Max and Min values !
!--------------!------------------------------------------------------!
! LONA ! Max and Min values !
!--------------!------------------------------------------------------!
! LATA ! Max and Min values !
+---------------------------------------------------------------------+
*Remark: In case of report generation due to RALRL limit exceedance the RALR value is taken at the dataset time fixed in item 'L' of report logic.
(15) Parameter logic:
+---------------------------------------------------------------------+
! Param. ! Print Value (Standard Progr.) !
!--------------!------------------------------------------------------!
! ESN ! Value at moment of trigger. !
!--------------!------------------------------------------------------!
! EHRS ! Value at moment of trigger. !
!--------------!------------------------------------------------------!
! AP ! Value at moment of trigger. !
!--------------!------------------------------------------------------!
! FLAP ! Value at moment of trigger. !
!--------------!------------------------------------------------------!
! SLAT ! Value at moment of trigger. !
!--------------!------------------------------------------------------!
! MAX ! Max value during 0.5 sec before until 0.5 sec after!
! ! trigger. !
!--------------!------------------------------------------------------!
! LIM ! Value at moment of trigger. !
!--------------! -----------------------------------------------------!
! COUNTS ! Current value. !
!--------------! -----------------------------------------------------!
! REASON ! Reason of trigger. !
!--------------! -----------------------------------------------------!
! DNZKPI1 ! Calculated value for IMPACT1 !
!--------------! -----------------------------------------------------!
! NYKPI1 ! Calculated value for IMPACT1 !
!--------------! -----------------------------------------------------!
! PTCHI1 ! Snapshot at landing detection (IMPACT1) !
!--------------! -----------------------------------------------------!
! DNZKPI2 ! Calculated value for IMPACT2 !
!--------------! -----------------------------------------------------!
! NYKPI2 ! Calculated value for IMPACT2 !
!--------------! -----------------------------------------------------!
! PTCHI2 ! Snapshot at bounce landing detection (IMPACT2) !
!--------------! -----------------------------------------------------!
! PTCH ! Time History. !
!--------------! -----------------------------------------------------!
! PTCR ! Time History. !
!--------------! -----------------------------------------------------!
! ROLL ! Time History. !
!--------------! -----------------------------------------------------!
! ROLR ! Time History. !
!--------------! -----------------------------------------------------!
! YAW ! Time History. !
!--------------! -----------------------------------------------------!
! ! Max and Min values for lines S1, S2, T1 and T2 !
! ! Time History for lines: !
! VRTA ! G1 to G8, H0 to H8, I1 to I8, J1 to J8, K1 to K8, !
! ! L1 to L8, M1 to M8, N0 to N8, O1 to O8, P1 to P8, !
! ! Q1 to Q8, R1 to R8 !
!--------------!------------------------------------------------------!
! ! Max and Min values for lines S1, S2, T1 and T2 !
! ! Time History for lines: !
! LATA ! G1 to G8, H0 to H8, I1 to I8, J1 to J8, K1 to K8, !
! ! L1 to L8, M1 to M8, N0 to N8, O1 to O8, P1 to P8, !
! ! Q1 to Q8, R1 to R8 !
!--------------!------------------------------------------------------!
! LONA ! Max and Min values for lines S1, S2, T1 and T2. !
+---------------------------------------------------------------------+

(16) Load Report Logic
+----------------------------------------------------------------------+
!Code!Item ! !Progr.!Standard !
! No.!No. ! Description of Function Item !MCDU !Value or !
! ! ! !GSE !Table !
!----!------!-----------------------------------------!------!---------!
! !A ! Report Format ! ! !
! ! ! ! ! !
! !B ! Parameter Table ! ! !
! ! ! ! ! !
! !C ! First three lines of Report ! C ! Blank !
! ! ! ! ! !
! !D ! Print Out Rules ! C ! PH10 !
! ! ! (PH9,PH10, Immediately, Manually) ! ! !
! !E ! Transfer to ACARS MU (yes/no) ! C ! No !
! ! ! ! ! !
! !F ! Increment of the report counter (yes/no)! ! Yes !
! ! ! ! ! !
! !G ! Inhibit report triggers (yes/no) ! C ! No !
! ! ! ! ! !
! !H ! 'Y15.0' sec before land/event A320! C ! 1 !
! ! ! A321! C ! 1 !
! ! ! A319! C ! 1 !
! ! ! ! ! !
! !I ! 'Y15.1' sec before land/event A320! C ! 1 !
! ! ! A321! C ! 1 !
! ! ! A319! C ! 1 !
! ! ! ! ! !
! !J ! 'Y15.2' sec after land/event A320! C ! 3 !
! ! ! A321! C ! 3 !
! ! ! A319! C ! 3 !
! ! ! ! ! !
! !K ! 'Y15.3' sec before bounced A320! C ! 1 !
! ! ! A321! C ! 1 !
! ! ! A319! C ! 1 !
! ! ! ! ! !
! !L ! 'Y15.4' sec before bounced A320! C ! 1 !
! ! ! A321! C ! 1 !
! ! ! A319! C ! 1 !
! ! ! ! ! !
! !M ! 'Y15.5' sec after bounced A320! C ! 3 !
! ! ! A321! C ! 3 !
! ! ! A319! C ! 3 !
! ! ! ! ! !
! !N ! N dataset time sample at landing ! C ! 1 !
! ! ! to check for RALR trigger ! ! !
! ! ! Note: -N dataset time is programmable ! ! !
! ! ! from 0 to 5. ! ! !
! ! ! -1 sample is 1/16 second (16 Hz) ! ! !
!----!------!-----------------------------------------!------!---------!
!1000! ! Not Applicable ! ! !
!----!------!-----------------------------------------!------!---------!
!2000! ! Not Applicable ! ! !
!----!------!-----------------------------------------!------!---------!
!3000!3 ! Programmable Start Logic ! ! !
! !3.1 ! Logic algorithm ! C ! !
! !3.2 ! Logic criteria values ! C !not prog.!
! ! ! ! ! !
! ! ! The parameters which are used for logic ! ! !
! ! ! items described as follows shall be ! ! !
! ! ! observed with a rate of 16 Hz. ! ! !
! ! ! Exceptions: ! ! !
! ! ! At landing (0.5 sec before and 0.5 sec ! ! !
! ! ! after landing or bounce), the non- ! ! !
! ! ! filtered acceleration VRTA and the non- ! ! !
! ! ! filtered landing gear status (see to ! ! !
! ! ! item no. 4.7) shall be observed with ! ! !
! ! ! a rate of 32 Hz. ! ! !
!----!------!-----------------------------------------!------!---------!
! !4 ! Report will be generated if one of the ! ! !
! ! ! following logic items is present during ! ! !
! ! ! landing: ! ! !
!4100! ! RALR < RALRL ! ! !
! ! ! calculated between Start Sample Number ! ! !
! ! ! S1 and Stop Sample Number S2 ! ! !
! ! ! or ! ! !
!4400! ! VRTA > VRTAL1.1 ! ! !
! ! ! (during +/- 0.5 seconds before and after! ! !
! ! ! landing) calculated between Start ! ! !
! ! ! Sample Number S3 and Stop Sample ! ! !
! ! ! Number S4 ! ! !
! ! ! or ! ! !
!4800! ! GW > GWL (at landing) and RALR < RALRLG ! ! !
! ! ! (at dataset time at landing (see item ! ! !
! ! ! no. L)). ! ! !
! ! ! The appropriate GW (GWL1, GWL2, GWL3 or ! ! !
! ! ! GWL4) shall be taken depending if an ! ! !
! ! ! aircraft is equipped with or without ACT! ! !
! ! ! (Additional Center Tanks). ! ! !
! ! ! ! ! !
! ! ! Logic for ACT detection ! ! !
! ! ! ! ! !
! ! ! FWC 26.1.276.01 Bit 26 Bit 27 GW Limit! ! !
! ! ! 26.2.276.10 26 27 ! ! !
! ! ! 0 0 GWL1 ! ! !
! ! ! 1 0 GWL2 ! ! !
! ! ! 0 1 GWL3 ! ! !
! ! ! 1 1 GWL4 ! ! !
! ! ! ! ! !
! ! ! or ! ! !
! ! ! ! ! !
!4900! ! GW > GWL (at landing) and VRTA > VRTALG ! ! !
! ! ! (during +/- 0.5 sec before and after ! ! !
! ! ! landing). ! ! !
! ! ! The appropriate GW (GWL1, GWL2, GWL3 or ! ! !
! ! ! GWL4) shall be taken depending if an ! ! !
! ! ! aircraft is equipped with or without ACT! ! !
! ! ! (Additional Center Tanks). Logic for ACT! ! !
! ! ! detection like Code No. 4800. ! ! !
! ! ! ! ! !
!4500! ! Report will be generated if one of the ! ! !
! ! ! following logic items is present during ! ! !
! ! ! the bouncing: ! ! !
! ! ! ! ! !
! ! ! VRTA > VRTAL1.2 during +/- 0.5 sec at ! ! !
! ! ! landing (1st touchdown) ! ! !
! ! ! ! ! !
! ! ! or ! ! !
! ! ! ! ! !
! ! ! VRTA > VRTAL1.3 during +/- 0.5 sec at ! ! !
! ! ! bouncing (2nd touchdown). ! ! !
!----!------!-----------------------------------------!------!---------!
! !4.1 ! RALRL limit (ft/sec) A320 ! C ! -9.0 !
! ! ! A321 ! C ! -9.0 !
! ! A319 ! C ! -9.0 !
! !4.2 ! RALT ! ! !
! !4.2.1 ! RALTL1 limit (ft) A320 ! C ! 150.0 !
! ! ! A321 ! C ! 150.0 !
! ! ! A319 ! C ! 150.0 !
! !4.3 ! RALR ! ! !
! !4.3.1 ! D geometrical correction factor for ! ! !
! ! ! ROLR (ft/deg) A320 ! C ! 0.0 !
! ! ! A321 ! C ! 0.0 !
! ! ! A319 ! C ! 0.0 !
! !4.3.2 ! DX lever arm correction (x-axis) ! ! !
! ! ! for R/A RALT (ft) A320 ! C ! 18.0 !
! ! ! A321 ! C ! 28.8 !
! ! ! A319 ! C ! 18.5 !
! !4.3.3 ! DZ lever arm correction (z-axis) ! ! !
! ! ! for R/A RALT (ft) A320 ! C ! 7.1 !
! ! ! A321 ! C ! 7.8 !
! ! ! A319 ! C ! 7.2 !
! !4.3.4 ! DXTPIR lever arm correction (x-axis) ! ! !
! ! ! for PTCH (ft) A320 ! C ! 39.0 !
! ! ! A321 ! C ! 53.1 !
! ! ! A319 ! C ! 33.8 !
! ! ! ! ! !
! !4.3.5 ! FC filter frequency (Hz) A320 ! C ! 0.3 !
! ! ! A321 ! C ! 0.3 !
! ! ! A319 ! C ! 0.3 !
! ! ! ! ! !
! !4.3.6 ! K1 filter constant A320 ! C ! 5.2 !
! ! ! A321 ! C ! 5.2 !
! ! ! A319 ! C ! 5.2 !
! ! ! ! ! !
! !4.3.7 ! K2 filter constant A320 ! C ! 25.0 !
! ! ! A321 ! C ! 25.0 !
! ! ! A319 ! C ! 25.0 !
! ! ! ! ! !
! !4.3.8 ! K3 filter constant A320 ! C ! 5.0 !
! ! ! A321 ! C ! 5.0 !
! ! ! A319 ! C ! 5.0 !
! ! ! ! ! !
! !4.3.9 ! THETA0 (deg) A320 ! C ! 6.0 !
! ! ! A321 ! C ! 4.5 !
! ! ! A219 ! C ! 2.0 !
! ! ! ! ! !
! !4.3.10! S1 (sample) A320 ! C ! -4.0 !
! ! ! A321 ! C ! -4.0 !
! ! ! A319 ! C ! -4.0 !
! ! ! ! ! !
! !4.3.11! S2 (sample) A320 ! C ! 4.0 !
! ! ! A321 ! C ! 4.0 !
! ! ! A319 ! C ! 4.0 !
! ! ! ! ! !
! !4.4 ! VRTAL1.1 limit at landing (g) A320 ! C ! 2.6 !
! ! ! A321 ! C ! 2.6 !
! ! ! A319 ! C ! 2.6 !
! ! ! ! ! !
! !4.4.1 ! S3 (sample) A320 ! C ! -16 !
! ! ! A321 ! C ! -16 !
! ! ! A319 ! C ! -16 !
! !4.4.2 ! S4 (sample) A320 ! C ! 16 !
! ! ! A321 ! C ! 16 !
! ! ! A319 ! C ! 16 !
! ! ! ! ! !
! !4.5 ! VRTAL1.2 limit at landing (1st touchdown! ! !
! ! ! ) from bounced land/event (g) A320 ! C ! 2.6 !
! ! ! A321 ! C ! 2.6 !
! ! ! A319 ! C ! 2.6 !
! ! ! ! ! !
! !4.5.1 ! VRTAL1.3 limit at bounce (2nd touchdown)! ! !
! ! ! from bounced land/event (g) A320 ! C ! 2.6 !
! ! ! A321 ! C ! 2.6 !
! ! ! A319 ! C ! 2.6 !
! ! ! ! ! !
! !4.6 ! GW Overweight landing ! ! !
! !4.6.1 ! GWL1, GWL2, GWL3, GWL4 limit (kg) A320 ! C ! 64500 !
! ! ! A321 ! C ! 75500 !
! ! ! A319 ! C ! 61000 !
! ! ! ! ! !
! ! ! NOTE: The standard GWL value stored ! ! !
! ! ! in the DMU is not always in line with ! ! !
! ! ! the MLW. We recommend to set the GWL ! ! !
! ! ! value in line with the MLW (Ref: AMM ! ! !
! ! ! 31-36-00). ! ! !
! ! ! ! ! !
! !4.6.2 ! RALRLG limit (ft/sec) A320 ! C ! -6.0 !
! ! ! A321 ! C ! -6.0 !
! ! ! A319 ! C ! -6.0 !
! ! ! ! ! !
! !4.6.3 ! VRTALG limit (g) A320 ! C ! 1.7 !
! ! ! A321 ! C ! 1.7 !
! ! ! A319 ! C ! 1.7 !
! ! ! ! ! !
! !4.7 ! Landing detection ! ! !
! ! ! Landing is detected when in PH7 or PH8 ! ! !
! ! ! 6D.1.021.01 Bit 13 = 1 (LH gear) ! ! !
! ! ! or ! ! !
! ! ! 6D.1.021.01 Bit 14 = 1 (RH gear) ! ! !
! ! ! ! ! !
! !4.8 ! Bounced landing detection ! ! !
! ! ! A bounced landing is detected when in ! ! !
! ! ! PH7 or PH8 parameter 6D.1.021.01 Bit 11 ! ! !
! ! ! is set to 1 for longer than 'Y15.5' ! ! !
! ! ! seconds and ! ! !
! ! ! then one or both of 6D.1.021.01 Bit 13 ! ! !
! ! ! or Bit 14 is set to 0 for longer than ! ! !
! ! ! 'Y15.6' seconds and ! ! !
! ! ! then the one which was set to 0 or the ! ! !
! ! ! first one of 6D.1.021.01 Bit 13 or ! ! !
! ! ! Bit 14 is set to 1 again within 'Y15.7' ! ! !
! ! ! seconds. ! ! !
! ! ! ! ! !
! !4.9 ! 'Y15.5' landing gear compress time ! ! !
! ! ! (1st touchdown) (sample) A320 ! ! 16 !
! ! ! A321 ! ! 16 !
! ! ! A319 ! ! 16 !
! ! ! ! ! !
! !4.10 ! 'Y15.6' time between bounces (sample) ! ! !
! ! ! A320 ! ! 32 !
! ! ! A321 ! ! 32 !
! ! ! A319 ! ! 32 !
! ! ! ! ! !
! !4.11 ! 'Y15.7' landing gear compress time ! ! !
! ! ! (2nd touchdown) (sample) A320 ! ! 320 !
! ! ! A321 ! ! 320 !
! ! ! A319 ! ! 320 !
!----!------!-----------------------------------------!------!---------!
! !5 ! Report shall be generated if one of the ! ! !
! ! ! flight (PH5, 5.1, 6, 7, 7.1). There ! ! !
! ! ! shall be a spacing time TURBWAIT (sec) ! ! !
! ! ! to enable the trigger logic again after ! ! !
! ! ! the previous report generation. ! ! !
! ! ! ! ! !
!5100!5.1 ! VRTA > VRTAL2.1 if FLAPL < 0.5 deg ! ! !
! ! ! ! ! !
!5200!5.2 ! VRTA < VRTAL2.2 if FLAPL < 0.5 deg ! ! !
! ! ! ! ! !
!5300!5.3 ! VRTA > VRTAL2.3 if FLAPL >/= 0.5 deg or ! ! !
! ! ! VRTA < VRTAL2.4 if FLAPL >/= 0.5 deg ! ! !
! ! ! ! ! !
! ! ! Limitation for Code 5100, 5200, 5300: ! ! !
! ! ! W15 TURBWAIT spacing time for re- ! ! !
! ! ! activating the trigger logic after the ! ! !
! ! ! previous report generation within the ! ! !
! ! ! same flight leg. ! ! !
! ! ! ! ! !
!5400!5.4 ! If one of the 5 spoiler excursion ! ! !
! ! ! counters has an overflow (999 is ! ! !
! ! ! reached). ! ! !
! ! ! ! ! !
! !5.5 ! VRTAL2.1 limit (g) A320 ! C ! 2.5 !
! ! ! A321 ! C ! 2.5 !
! ! ! A319 ! C ! 2.5 !
! ! ! ! ! !
! !5.6 ! VRTAL2.2 limit (g) A320 ! C ! -1.0 !
! ! ! A321 ! C ! -1.0 !
! ! ! A319 ! C ! -1.0 !
! ! ! ! ! !
! !5.7 ! VRTAL2.3 limit (g) A320 ! C ! 2.0 !
! ! ! A321 ! C ! 2.0 !
! ! ! A319 ! C ! 2.0 !
! ! ! ! ! !
! !5.8 ! VRTAL2.4 limit (g) A320 ! C ! 0.0 !
! ! ! A321 ! C ! 0.0 !
! ! ! A319 ! C ! 0.0 !
! ! ! ! ! !
! !5.9 ! TURBWAIT (sec.) A320 ! C ! 10 !
! ! ! A321 ! C ! 10 !
! ! ! A319 ! C ! 10 !
! ! ! ! ! !
! !5.10 ! FLAPL (deg) A320 ! C ! 0.5 !
! ! ! A321 ! C ! 0.5 !
! ! ! A319 ! C ! 0.5 !
!----------------------------------------------------------------------!
! A = Programmable by Airbus !
! C = Programmable by Customer !
+----------------------------------------------------------------------+

(17) Load Report Logic
+----------------------------------------------------------------------+
!Code!Item ! !Progr.!Standard !
! No.!No. ! Description of Function Item !MCDU !Value or !
! ! ! !GSE !Table !
!----!------!-----------------------------------------!------!---------!
! !A ! Report Format ! ! !
! ! ! ! ! !
! !B ! Parameter Table ! ! !
! ! ! ! ! !
! !C ! First three lines of Report ! C ! Blank !
! ! ! ! ! !
! !D ! Print Out Rules ! C ! PH10 !
! ! ! (PH9,PH10, Immediately, Manually) ! ! !
! !E ! Transfer to ACARS MU (yes/no) ! C ! No !
! ! ! ! ! !
! !F ! Increment of the report counter (yes/no)! ! Yes !
! ! ! ! ! !
! !G ! Inhibit report triggers (yes/no) ! C ! No !
! ! ! ! ! !
! !H ! 'Y15.0' sec before land/event A320! C ! 1 !
! ! ! A321! C ! 1 !
! ! ! A319! C ! 1 !
! ! ! ! ! !
! !I ! 'Y15.1' sec before land/event A320! C ! 1 !
! ! ! A321! C ! 1 !
! ! ! A319! C ! 1 !
! ! ! ! ! !
! !J ! 'Y15.2' sec after land/event A320! C ! 3 !
! ! ! A321! C ! 3 !
! ! ! A319! C ! 3 !
! ! ! ! ! !
! !K ! 'Y15.3' sec before bounced A320! C ! 1 !
! ! ! A321! C ! 1 !
! ! ! A319! C ! 1 !
! ! ! ! ! !
! !L ! 'Y15.4' sec before bounced A320! C ! 1 !
! ! ! A321! C ! 1 !
! ! ! A319! C ! 1 !
! ! ! ! ! !
! !M ! 'Y15.5' sec after bounced A320! C ! 3 !
! ! ! A321! C ! 3 !
! ! ! A319! C ! 3 !
! ! ! ! ! !
! !N ! N dataset time sample at landing ! C ! 1 !
! ! ! to check for RALR trigger ! ! !
! ! ! Note: -N dataset time is programmable ! ! !
! ! ! from 0 to 5. ! ! !
! ! ! -1 sample is 1/16 second (16 Hz) ! ! !
!----!------!-----------------------------------------!------!---------!
!1000! ! Not applicable ! ! !
!----!------!-----------------------------------------!------!---------!
!2000! ! Not applicable ! ! !
!----!------!-----------------------------------------!------!---------!
!3000!3 ! Programmable Start Logic ! ! !
! !3.1 ! Logic algorithm ! C ! !
! !3.2 ! Logic criteria values ! C !not prog.!
! ! ! ! ! !
! ! ! The parameters which are used for logic ! ! !
! ! ! items described as follows shall be ! ! !
! ! ! observed with a rate of 16 Hz. ! ! !
! ! ! Exceptions: ! ! !
! ! ! At landing (0.5 sec before and 0.5 sec ! ! !
! ! ! after landing or bounce), the non- ! ! !
! ! ! filtered acceleration VRTA and the non- ! ! !
! ! ! filtered landing gear status (see to ! ! !
! ! ! item no. 4.7) shall be observed with ! ! !
! ! ! a rate of 32 Hz. ! ! !
!----!------!-----------------------------------------!------!---------!
! !4 ! Report is generated if one of the ! ! !
! ! ! following logic items is present during ! ! !
! ! ! landing: ! ! !
!4100! ! RALR < RALRL ! ! !
! ! ! calculated between Start Sample Number ! ! !
! ! ! S1 and Stop Sample Number S2 ! ! !
! ! ! or ! ! !
!4400! ! VRTA > VRTAL1.1 ! ! !
! ! ! (during +/- 0.5 seconds before and after! ! !
! ! ! landing) calculated between Start ! ! !
! ! ! Sample Number S3 and Stop Sample ! ! !
! ! ! Number S4 ! ! !
! ! ! or ! ! !
!4800! ! GW > GWL (at landing) and RALR > RALRLG ! ! !
! ! ! (at dataset time at landing (see item ! ! !
! ! ! no. L)). ! ! !
! ! ! The appropriate GW (GWL1, GWL2, GWL3 or ! ! !
! ! ! GWL4) is taken depending on if an ! ! !
! ! ! aircraft is equipped with or without ACT! ! !
! ! ! (Additional Center Tanks). ! ! !
! ! ! ! ! !
! ! ! Logic for ACT detection ! ! !
! ! ! ! ! !
! ! ! FWC 26.1.276.01 Bit 26 Bit 27 GW Limit! ! !
! ! ! 26.2.276.10 26 27 ! ! !
! ! ! 0 0 GWL1 ! ! !
! ! ! 1 0 GWL2 ! ! !
! ! ! 0 1 GWL3 ! ! !
! ! ! 1 1 GWL4 ! ! !
! ! ! ! ! !
! ! ! or ! ! !
! ! ! ! ! !
!4900! ! GW > GWL (at landing) and VRTA > VRTALG ! ! !
! ! ! (during +/- 0.5 sec before and after ! ! !
! ! ! landing). ! ! !
! ! ! The appropriate GW (GWL1, GWL2, GWL3 or ! ! !
! ! ! GWL4) is taken depending on if an ! ! !
! ! ! aircraft is equipped with or without ACT! ! !
! ! ! (Additional Center Tanks). Logic for ACT! ! !
! ! ! detection like Code No. 4800. ! ! !
! ! ! ! ! !
!4500! ! Report will be generated if one of the ! ! !
! ! ! following logic items is present during ! ! !
! ! ! the bouncing: ! ! !
! ! ! ! ! !
! ! ! VRTA > VRTAL1.2 during +/- 0.5 sec at ! ! !
! ! ! landing (1st touchdown) ! ! !
! ! ! ! ! !
! ! ! or ! ! !
! ! ! ! ! !
! ! ! VRTA > VRTAL1.3 during +/- 0.5 sec at ! ! !
! ! ! landing (2nd touchdown). ! ! !
!----!------!-----------------------------------------!------!---------!
! !4.1 ! RALRL limit (ft/sec) A320 ! C ! -9.0 !
! ! ! A321 ! C ! -9.0 !
! ! ! A319 ! C ! -9.0 !
! !4.2 ! RALT ! ! !
! !4.2.1 ! RALTL1 limit (ft) A320 ! C ! 150.0 !
! ! ! A321 ! C ! 150.0 !
! ! ! A319 ! C ! 150.0 !
! !4.3 ! RALR ! ! !
! !4.3.1 ! D geometrical correction factor for ! ! !
! ! ! ROLR (ft/deg) A320 ! C ! 0.0 !
! ! ! A321 ! C ! 0.0 !
! ! ! A319 ! C ! 0.0 !
! !4.3.2 ! DX lever arm correction (x-axis) ! ! !
! ! ! for R/A RALT (ft) A320 ! C ! 18.0 !
! ! ! A321 ! C ! 28.8 !
! ! ! A319 ! C ! 18.5 !
! !4.3.3 ! DZ lever arm correction (z-axis) ! ! !
! ! ! for R/A RALT (ft) A320 ! C ! 7.1 !
! ! ! A321 ! C ! 7.8 !
! ! ! A319 ! C ! 7.2 !
! !4.3.4 ! DXTPIR lever arm correction (x-axis) ! ! !
! ! ! for PTCH (ft) A320 ! C ! 39.0 !
! ! ! A321 ! C ! 53.1 !
! ! ! A319 ! C ! 33.8 !
! ! ! ! ! !
! !4.3.5 ! FC filter frequency (Hz) A320 ! C ! 0.3 !
! ! ! A321 ! C ! 0.3 !
! ! ! A319 ! C ! 0.3 !
! ! ! ! ! !
! !4.3.6 ! K1 filter constant A320 ! C ! 5.2 !
! ! ! A321 ! C ! 5.2 !
! ! ! A319 ! C ! 5.2 !
! ! ! ! ! !
! !4.3.7 ! K2 filter constant A320 ! C ! 25.0 !
! ! ! A321 ! C ! 25.0 !
! ! ! A319 ! C ! 25.0 !
! ! ! ! ! !
! !4.3.8 ! K3 filter constant A320 ! C ! 5.0 !
! ! ! A321 ! C ! 5.0 !
! ! ! A319 ! C ! 5.0 !
! ! ! ! ! !
! !4.3.9 ! THETA0 (deg) A320 ! C ! 6.0 !
! ! ! A321 ! C ! 4.5 !
! ! ! A219 ! C ! 2.0 !
! ! ! ! ! !
! !4.3.10! S1 (sample) A320 ! C ! -4.0 !
! ! ! A321 ! C ! -4.0 !
! ! ! A319 ! C ! -4.0 !
! ! ! ! ! !
! !4.3.11! S2 (sample) A320 ! C ! 4.0 !
! ! ! A321 ! C ! 4.0 !
! ! ! A319 ! C ! 4.0 !
! ! ! ! ! !
! !4.4 ! VRTAL1.1 limit at landing (g) A320 ! C ! 2.6 !
! ! ! A321 ! C ! 2.6 !
! ! ! A319 ! C ! 2.6 !
! ! ! ! ! !
! !4.4.1 ! S3 (sample) A320 ! C ! -16 !
! ! ! A321 ! C ! -16 !
! ! ! A319 ! C ! -16 !
! !4.4.2 ! S4 (sample) A320 ! C ! 16 !
! ! ! A321 ! C ! 16 !
! ! ! A319 ! C ! 16 !
! ! ! ! ! !
! !4.5 ! VRTAL1.2 limit at landing (1st touchdown! ! !
! ! ! ) from bounced land/event (g) A320 ! C ! 2.6 !
! ! ! A321 ! C ! 2.6 !
! ! ! A319 ! C ! 2.6 !
! ! ! ! ! !
! !4.5.1 ! VRTAL1.3 limit at bounce (2nd touchdown)! ! !
! ! ! from bounced land/event (g) A320 ! C ! 2.6 !
! ! ! A321 ! C ! 2.6 !
! ! ! A319 ! C ! 2.6 !
! ! ! ! ! !
! !4.6 ! GW Overweight landing ! ! !
! !4.6.1 ! GWL1, GWL2, GWL3, GWL4 limit (kg) A320 ! C ! 64500 !
! ! ! A321 ! C ! 75500 !
! ! ! A319 ! C ! 61000 !
! ! ! ! ! !
! ! ! NOTE: The standard GWL value stored ! ! !
! ! ! in the DMU is not always in line with ! ! !
! ! ! the MLW. We recommend to set the GWL ! ! !
! ! ! value in line with the MLW (Ref: AMM ! ! !
! ! ! 31-36-00). ! ! !
! ! ! ! ! !
! !4.6.2 ! RALRLG limit (ft/sec) A320 ! C ! -6.0 !
! ! ! A321 ! C ! -6.0 !
! ! ! A319 ! C ! -6.0 !
! ! ! ! ! !
! !4.6.3 ! VRTALG limit (g) A320 ! C ! 1.7 !
! ! ! A321 ! C ! 1.7 !
! ! ! A319 ! C ! 1.7 !
! ! ! ! ! !
! !4.7 ! Landing detection ! ! !
! ! ! Landing is detected when in PH7 or PH8 ! ! !
! ! ! 6D.1.021.01 Bit 13 = 1 (LH gear) ! ! !
! ! ! or ! ! !
! ! ! 6D.1.021.01 Bit 14 = 1 (RH gear) ! ! !
! ! ! ! ! !
! !4.8 ! Bounced landing detection ! ! !
! ! ! A bounced landing is detected when in ! ! !
! ! ! PH7 or PH8 parameter 6D.1.021.01 Bit 11 ! ! !
! ! ! is set to 1 for longer than 'Y15.5' ! ! !
! ! ! seconds and ! ! !
! ! ! then one or both of 6D.1.021.01 Bit 13 ! ! !
! ! ! or Bit 14 is set to 0 for longer than ! ! !
! ! ! 'Y15.6' seconds and ! ! !
! ! ! then the one which was set to 0 or the ! ! !
! ! ! first one of 6D.1.021.01 Bit 13 or ! ! !
! ! ! Bit 14 is set to 1 again within 'Y15.7' ! ! !
! ! ! seconds. ! ! !
! ! ! ! ! !
! !4.9 ! 'Y15.5' landing gear compress time ! ! !
! ! ! (1st touchdown) (sample) A320 ! ! 16 !
! ! ! A321 ! ! 16 !
! ! ! A319 ! ! 16 !
! ! ! ! ! !
! !4.10 ! 'Y15.6' time between bounces (sample) ! ! !
! ! ! A320 ! ! 32 !
! ! ! A321 ! ! 32 !
! ! ! A319 ! ! 32 !
! ! ! ! ! !
! !4.11 ! 'Y15.7' landing gear compress time ! ! !
! ! ! (2nd touchdown) (sample) A320 ! ! 320 !
! ! ! A321 ! ! 320 !
! ! ! A319 ! ! 320 !
! ! ! NOTE: 1 sample is 1/32 second (32 Hz) ! ! !
!----!------!-----------------------------------------!------!---------!
! !5 ! Report shall be generated if one of the ! ! !
! ! ! flight (PH5, 5.1, 6, 7, 7.1). There ! ! !
! ! ! shall be a spacing time TURBWAIT (sec.) ! ! !
! ! ! to enable the trigger logic again after ! ! !
! ! ! the previous report generation. ! ! !
! ! ! ! ! !
!5100!5.1 ! VRTA > VRTAL2.1 if FLAPL < 0.5 deg ! ! !
! ! ! ! ! !
!5200!5.2 ! VRTA < VRTAL2.2 if FLAPL < 0.5 deg ! ! !
! ! ! ! ! !
!5300!5.3 ! VRTA > VRTAL2.3 if FLAPL >/= 0.5 deg or ! ! !
! ! ! VRTA < VRTAL2.4 if FLAPL >/= 0.5 deg ! ! !
! ! ! ! ! !
! ! ! Limitation for Code 5100, 5200, 5300: ! ! !
! ! ! W15 TURBWAIT spacing time for re- ! ! !
! ! ! activating the trigger logic after the ! ! !
! ! ! previous report generation within the ! ! !
! ! ! same flight leg. ! ! !
! ! ! ! ! !
!5400!5.4 ! If one of the 5 spoiler excursion ! ! !
! ! ! counters has an overflow (999 is ! ! !
! ! ! reached). ! ! !
! ! ! ! ! !
! !5.5 ! VRTAL2.1 limit (g) A320 ! C ! 2.5 !
! ! ! A321 ! C ! 2.5 !
! ! ! A319 ! C ! 2.5 !
! ! ! ! ! !
! !5.6 ! VRTAL2.2 limit (g) A320 ! C ! -1.0 !
! ! ! A321 ! C ! -1.0 !
! ! ! A319 ! C ! -1.0 !
! ! ! ! ! !
! !5.7 ! VRTAL2.3 limit (g) A320 ! C ! 2.0 !
! ! ! A321 ! C ! 2.0 !
! ! ! A319 ! C ! 2.0 !
! ! ! ! ! !
! !5.8 ! VRTAL2.4 limit (g) A320 ! C ! 0.0 !
! ! ! A321 ! C ! 0.0 !
! ! ! A319 ! C ! 0.0 !
! ! ! ! ! !
! !5.9 ! TURBWAIT (sec.) A320 ! C ! 10 !
! ! ! A321 ! C ! 10 !
! ! ! A319 ! C ! 10 !
! ! ! ! ! !
! !5.10 ! FLAPL (deg) A320 ! C ! 0.5 !
! ! ! A321 ! C ! 0.5 !
! ! ! A319 ! C ! 0.5 !
!----------------------------------------------------------------------!
! A = Programmable by Airbus !
! C = Programmable by Customer !
+----------------------------------------------------------------------+

(18) Load Report Logic <15>
+----------------------------------------------------------------------+
!Code!Item ! !Progr.!Standard !
! No.!No. ! Description of Function Item !MCDU !Value or !
! ! ! !GSE !Table !
!----!------!-----------------------------------------!------!---------!
! !A ! Report Format ! ! !
! ! ! ! ! !
! !B ! Parameter Table ! ! !
! ! ! ! ! !
! !C ! First three lines of Report ! ! Blank !
! ! ! ! ! !
! !D ! Print Out Rules ! C ! PH10 !
! ! ! (PH9,PH10, Immediately, Manually) ! ! !
! !E ! Transfer to ACARS MU (yes/no) ! C ! No !
! ! ! ! ! !
! !F ! Increment of the report counter (yes/no)! C ! Yes !
! ! ! ! ! !
! !G ! Inhibit report triggers (yes/no) ! C ! No !
! ! ! ! ! !
! !H ! 'Y15.0' sec before land/event A320! C ! 1 !
! ! ! A321! C ! 1 !
! ! ! A319! C ! 1 !
! ! ! A318! C ! 1 !
! ! ! ! ! !
! !I ! 'Y15.1' sec before land/event A320! C ! 1 !
! ! ! A321! C ! 1 !
! ! ! A319! C ! 1 !
! ! ! A318! C ! 1 !
! ! ! ! ! !
! !J ! 'Y15.2' sec after land/event A320! C ! 3 !
! ! ! A321! C ! 3 !
! ! ! A319! C ! 3 !
! ! ! A318! C ! 3 !
! ! ! ! ! !
! !K ! 'Y15.3' sec before bounced A320! C ! 1 !
! ! ! A321! C ! 1 !
! ! ! A319! C ! 1 !
! ! ! A318! C ! 1 !
! ! ! ! ! !
! !L ! 'Y15.4' sec before bounced A320! C ! 1 !
! ! ! A321! C ! 1 !
! ! ! A319! C ! 1 !
! ! ! A318! C ! 1 !
! ! ! ! ! !
! !M ! 'Y15.5' sec after bounced A320! C ! 3 !
! ! ! A321! C ! 3 !
! ! ! A319! C ! 3 !
! ! ! A318! C ! 3 !
! ! ! ! ! !
! !N ! N dataset time (sample) at landing ! C ! 1 !
! ! ! to check for RALR trigger ! ! !
! ! ! Note: -N dataset time is programmable ! ! !
! ! ! from 0 to 5. ! ! !
! ! ! -1 sample is 1/16 second (16 Hz) ! ! !
!----!------!-----------------------------------------!------!---------!
!1000! ! Not applicable ! ! !
!----!------!-----------------------------------------!------!---------!
!2000! ! Not applicable ! ! !
!----!------!-----------------------------------------!------!---------!
!3000!3 ! Programmable Start Logic ! ! !
! !3.1 ! Logic algorithm ! C ! !
! !3.2 ! Logic criteria values ! C !not prog.!
!----!------!-----------------------------------------!------!---------!
! ! ! The parameters which are used for logic ! ! !
! ! ! items described as follows shall be ! ! !
! ! ! observed with a rate of 16 Hz. ! ! !
! ! ! Exceptions: ! ! !
! ! ! At landing (0.5 sec before and 0.5 sec ! ! !
! ! ! after landing or bounce), the non- ! ! !
! ! ! filtered acceleration VRTA and the non- ! ! !
! ! ! filtered landing gear status (see to ! ! !
! ! ! item no. 4.7) shall be observed with ! ! !
! ! ! a rate of 32 Hz. ! ! !
!----!------!-----------------------------------------!------!---------!
! !4 ! Report is generated if one of the ! ! !
! ! ! following logic items is present during ! ! !
! ! ! landing: ! ! !
!4100! ! RALR < RALRL ! ! !
! ! ! calculated between Start Sample Number ! ! !
! ! ! S1 and Stop Sample Number S2 ! ! !
! ! ! or ! ! !
!4400! ! VRTA > VRTAL1.1 ! ! !
! ! ! (during +/- 0.5 seconds before and after! ! !
! ! ! landing) calculated between Start ! ! !
! ! ! Sample Number S3 and Stop Sample ! ! !
! ! ! Number S4 ! ! !
! ! ! or ! ! !
!4800! ! GW > GWL (at landing) and RALR > RALRLG ! ! !
! ! ! (at dataset time at landing (see item ! ! !
! ! ! no. L)). ! ! !
! ! ! The appropriate GW (GWL1, GWL2, GWL3 or ! ! !
! ! ! GWL4) is taken depending on if an ! ! !
! ! ! aircraft is equipped with or without ACT! ! !
! ! ! (Additional Center Tanks). ! ! !
! ! ! ! ! !
! ! ! Logic for ACT detection ! ! !
! ! ! GW ! ! !
! ! ! FWC 26.1.276.01.26 26.1.276.01.27 Limit! ! !
! ! ! 26.1.276.10.26 26.1.276.10.27 ! ! !
! ! ! ! ! !
! ! ! 0 0 GWL1 ! ! !
! ! ! 1 0 GWL2 ! ! !
! ! ! 0 1 GWL3 ! ! !
! ! ! 1 1 GWL4 ! ! !
! ! ! ! ! !
! ! ! or ! ! !
! ! ! ! ! !
!4900! ! GW > GWL (at landing) and VRTA > VRTALG ! ! !
! ! ! (during +/- 0.5 sec before and after ! ! !
! ! ! landing). ! ! !
! ! ! The appropriate GW (GWL1, GWL2, GWL3 or ! ! !
! ! ! GWL4) is taken depending on if an ! ! !
! ! ! aircraft is equipped with or without ACT! ! !
! ! ! (Additional Center Tanks). Logic for ACT! ! !
! ! ! detection like Code No. 4800. ! ! !
! ! ! ! ! !
!4500! ! Report will be generated if one of the ! ! !
! ! ! following logic items is present during ! ! !
! ! ! the bouncing: ! ! !
! ! ! ! ! !
! ! ! VRTA > VRTAL1.2 during +/- 0.5 sec at ! ! !
! ! ! landing (1st touchdown) ! ! !
! ! ! ! ! !
! ! ! or ! ! !
! ! ! ! ! !
! ! ! VRTA > VRTAL1.3 during +/- 0.5 sec at ! ! !
! ! ! landing (2nd touchdown). ! ! !
!----!------!-----------------------------------------!------!---------!
! !4.1 ! RALRL limit (ft/sec) A320 ! C ! -9.0 !
! ! ! A321 ! C ! -9.0 !
! ! ! A319 ! C ! -9.0 !
! ! ! A318 ! C ! -9.0 !
! !4.2 ! RALT ! ! !
! !4.2.1 ! RALTL1 limit (ft) A320 ! C ! 150.0 !
! ! ! A321 ! C ! 150.0 !
! ! ! A319 ! C ! 150.0 !
! ! ! A318 ! C ! 150.0 !
! !4.3 ! RALR ! ! !
! !4.3.1 ! D geometrical correction factor for ! ! !
! ! ! ROLR (ft/deg) A320 ! C ! 0.0 !
! ! ! A321 ! C ! 0.0 !
! ! ! A319 ! C ! 0.0 !
! ! ! A318 ! C ! 0.0 !
! !4.3.2 ! DX lever arm correction (x-axis) ! ! !
! ! ! for R/A RALT (ft) A320 ! C ! 18.0 !
! ! ! A321 ! C ! 28.8 !
! ! ! A319 ! C ! 18.5 !
! ! ! A318 ! C ! 16.8 !
! !4.3.3 ! DZ lever arm correction (z-axis) ! ! !
! ! ! for R/A RALT (ft) A320 ! C ! 7.1 !
! ! ! A321 ! C ! 7.8 !
! ! ! A319 ! C ! 7.2 !
! ! ! A318 ! C ! 7.6 !
! !4.3.4 ! DXTPIR lever arm correction (x-axis) ! ! !
! ! ! for PTCH (ft) A320 ! C ! 39.0 !
! ! ! A321 ! C ! 53.1 !
! ! ! A319 ! C ! 33.8 !
! ! ! A318 ! C ! 29.5 !
! ! ! ! ! !
! !4.3.5 ! FC filter frequency (Hz) A320 ! C ! 0.3 !
! ! ! A321 ! C ! 0.3 !
! ! ! A319 ! C ! 0.3 !
! ! ! A318 ! C ! 0.3 !
! ! ! ! ! !
! !4.3.6 ! K1 filter constant A320 ! C ! 5.2 !
! ! ! A321 ! C ! 5.2 !
! ! ! A319 ! C ! 5.2 !
! ! ! A318 ! C ! 5.2 !
! ! ! ! ! !
! !4.3.7 ! K2 filter constant A320 ! C ! 25.0 !
! ! ! A321 ! C ! 25.0 !
! ! ! A319 ! C ! 25.0 !
! ! ! A318 ! C ! 25.0 !
! ! ! ! ! !
! !4.3.8 ! K3 filter constant A320 ! C ! 5.0 !
! ! ! A321 ! C ! 5.0 !
! ! ! A319 ! C ! 5.0 !
! ! ! A318 ! C ! 5.0 !
! ! ! ! ! !
! !4.3.9 ! THETA0 (deg) A320 ! C ! 6.0 !
! ! ! A321 ! C ! 4.5 !
! ! ! A319 ! C ! 2.0 !
! ! ! A318 ! C ! 6.0 !
! ! ! ! ! !
! !4.3.10! S1 (sample) A320 ! C ! -4.0 !
! ! ! A321 ! C ! -4.0 !
! ! ! A319 ! C ! -4.0 !
! ! ! A318 ! C ! -4.0 !
! ! ! ! ! !
! !4.3.11! S2 (sample) A320 ! C ! 4.0 !
! ! ! A321 ! C ! 4.0 !
! ! ! A319 ! C ! 4.0 !
! ! ! A318 ! C ! 4.0 !
! ! ! ! ! !
! !4.4 ! VRTAL1.1 limit at landing (g) A320 ! C ! 2.6 !
! ! ! A321 ! C ! 2.6 !
! ! ! A319 ! C ! 2.6 !
! ! ! A318 ! C ! 2.6 !
! ! ! ! ! !
! !4.4.1 ! S3 (sample) A320 ! C ! -16 !
! ! ! A321 ! C ! -16 !
! ! ! A319 ! C ! -16 !
! ! ! A318 ! C ! -16 !
! ! ! ! ! !
! !4.4.2 ! S4 (sample) A320 ! C ! 16 !
! ! ! A321 ! C ! 16 !
! ! ! A319 ! C ! 16 !
! ! ! A318 ! C ! 16 !
! ! ! ! ! !
! !4.5 ! VRTAL1.2 limit at landing (1st touchdown! ! !
! ! ! ) from bounced land/event (g) A320 ! C ! 2.6 !
! ! ! A321 ! C ! 2.6 !
! ! ! A319 ! C ! 2.6 !
! ! ! A318 ! C ! 2.6 !
! ! ! ! ! !
! !4.5.1 ! VRTAL1.3 limit at bounce (2nd touchdown)! ! !
! ! ! from bounced land/event (g) A320 ! C ! 2.6 !
! ! ! A321 ! C ! 2.6 !
! ! ! A319 ! C ! 2.6 !
! ! ! A318 ! C ! 2.6 !
! !4.6 ! GW Overweight landing ! ! !
! !4.6.1 ! GWL1, GWL2, GWL3, GWL4 limit (kg) A320 ! C ! 64500 !
! ! ! A321 ! C ! 75500 !
! ! ! A319 ! C ! 61000 !
! ! ! A318 ! C ! 56000 !
! ! ! ! ! !
! ! ! NOTE: The standard GWL value stored ! ! !
! ! ! in the DMU is not always in line with ! ! !
! ! ! the MLW. We recommend to set the GWL ! ! !
! ! ! value in line with the MLW (Ref: AMM ! ! !
! ! ! 31-36-00). ! ! !
! ! ! ! ! !
! !4.6.2 ! RALRLG limit (ft/sec) A320 ! C ! -6.0 !
! ! ! A321 ! C ! -6.0 !
! ! ! A319 ! C ! -6.0 !
! ! ! A318 ! C ! -6.0 !
! ! ! ! ! !
! !4.6.3 ! VRTALG limit (g) A320 ! C ! 1.7 !
! ! ! A321 ! C ! 1.7 !
! ! ! A319 ! C ! 1.7 !
! ! ! A318 ! C ! 1.7 !
! ! ! ! ! !
! !4.7 ! Landing detection ! ! !
! ! ! Landing is detected when in PH7 or PH8 ! ! !
! ! ! 6D.1.021.01.13 = 1 (LH gear) ! ! !
! ! ! or ! ! !
! ! ! 6D.1.021.01.14 = 1 (RH gear) ! ! !
! ! ! ! ! !
! !4.8 ! Bounced landing detection ! ! !
! ! ! A bounced landing is detected when in ! ! !
! ! ! PH7 or PH8 parameter 6D.1.021.01.11 is ! ! !
! ! ! set to 1 for longer than 'Y15.6'*(1/32) ! ! !
! ! ! seconds ! ! !
! ! ! and ! ! !
! ! ! then one or both of 6D.1.021.01.13 or ! ! !
! ! ! 6D.1.021.01.14 is set to 0 for longer ! ! !
! ! ! than 'Y15.7'*(1/32) seconds ! ! !
! ! ! and ! ! !
! ! ! then the one which was set to 0 or the ! ! !
! ! ! first one of 6D.1.021.01.13 or ! ! !
! ! ! 6D.1.021.01.14 is set to 1 again within ! ! !
! ! ! within 'Y15.8'*(1/32) seconds. ! ! !
! ! ! ! ! !
! !4.9 ! 'Y15.6' landing gear compress time ! ! !
! ! ! (1st touchdown) (sample) A320 ! ! 16 !
! ! ! A321 ! ! 16 !
! ! ! A319 ! ! 16 !
! ! ! A318 ! ! 16 !
! ! ! ! ! !
! !4.10 ! 'Y15.7' time between bounces (sample) ! ! !
! ! ! A320 ! ! 32 !
! ! ! A321 ! ! 32 !
! ! ! A319 ! ! 32 !
! ! ! A318 ! ! 32 !
! ! ! ! ! !
! !4.11 ! 'Y15.8' landing gear compress time ! ! !
! ! ! (2nd touchdown) (sample) A320 ! ! 320 !
! ! ! A321 ! ! 320 !
! ! ! A319 ! ! 320 !
! ! ! A318 ! ! 320 !
! ! ! NOTE: 1 sample is 1/32 second (32 Hz) ! ! !
!----!------!-----------------------------------------!------!---------!
! !5 ! Report is generated if one of the ! ! !
! ! ! following logic items is present during ! ! !
! ! ! flight (PH5, 5.1, 6, 7, 7.1). There is a! ! !
! ! ! spacing time TURBWAIT sec. to enable the! ! !
! ! ! trigger logic again after the previous ! ! !
! ! ! report generation. ! ! !
! ! ! ! ! !
!5100!5.1 ! VRTA > VRTAL2.1 if FLAPL < 0.5 deg ! ! !
! ! ! ! ! !
!5200!5.2 ! VRTA < VRTAL2.2 if FLAPL < 0.5 deg ! ! !
! ! ! ! ! !
!5300!5.3 ! VRTA > VRTAL2.3 if FLAPL >= 0.5 deg or ! ! !
! ! ! VRTA < VRTAL2.4 if FLAPL >= 0.5 deg ! ! !
! ! ! ! ! !
! ! ! Limitation for Code 5100, 5200, 5300: ! ! !
! ! ! W15 TURBWAIT spacing time for re- ! ! !
! ! ! activating the trigger logic after the ! ! !
! ! ! previous report generation within the ! ! !
! ! ! same flight leg. ! ! !
! ! ! ! ! !
!5400!5.4 ! If one of the 5 spoiler excursion ! ! !
! ! ! counters has an overflow (999 is ! ! !
! ! ! reached). ! ! !
! ! ! ! ! !
! !5.5 ! VRTAL2.1 limit (g) A320 ! C ! 2.5 !
! ! ! A321 ! C ! 2.5 !
! ! ! A319 ! C ! 2.5 !
! ! ! A318 ! C ! 2.5 !
! ! ! ! ! !
! !5.6 ! VRTAL2.2 limit (g) A320 ! C ! -1.0 !
! ! ! A321 ! C ! -1.0 !
! ! ! A319 ! C ! -1.0 !
! ! ! A318 ! C ! -1.0 !
! ! ! ! ! !
! !5.7 ! VRTAL2.3 limit (g) A320 ! C ! 2.0 !
! ! ! A321 ! C ! 2.0 !
! ! ! A319 ! C ! 2.0 !
! ! ! A318 ! C ! 2.0 !
! ! ! ! ! !
! !5.8 ! VRTAL2.4 limit (g) A320 ! C ! 0.0 !
! ! ! A321 ! C ! 0.0 !
! ! ! A319 ! C ! 0.0 !
! ! ! A318 ! C ! 0.0 !
! ! ! ! ! !
! !5.9 ! TURBWAIT (sec.) A320 ! C ! 10 !
! ! ! A321 ! C ! 10 !
! ! ! A319 ! C ! 10 !
! ! ! A318 ! C ! 10 !
! ! ! ! ! !
! !5.10 ! FLAPL (deg) A320 ! C ! 0.5 !
! ! ! A321 ! C ! 0.5 !
! ! ! A319 ! C ! 0.5 !
! ! ! A318 ! C ! 0.5 !
!----------------------------------------------------------------------!
! A = Programmable by Airbus !
! C = Programmable by Customer !
+----------------------------------------------------------------------+

(19) Load Report Logic
+-------------------------------------------------------------------------+
!Code!Item ! ! Progr. !Standard !
!No. !No. ! Description of Function Item !GSE !MCDU!Value or !
! ! ! ! ! !Table TXY!
!----!------!-----------------------------------------!----!----!---------!
! !A ! Report Format ! ! ! !
! ! ! ! ! ! !
! !A.1 ! 'R015RLID' Report Layout Identifier ! ! ! 01 !
! ! ! (for ACARS header) ! ! ! !
! ! ! ! ! ! !
! !A.2 ! 'R015RLIS' 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 !
! ! ! (PH9, PH10, Immediately, Manually) ! ! !separate !
! ! ! ! ! !list !
! !E ! Transfer to ACARS MU (yes/no)! C ! C !see !
! ! ! ! ! !separate !
! ! ! ! ! !list !
! !F ! Increment of the report counter (yes/no)! C ! C !Yes !
! ! ! ! ! ! !
! !G ! Inhibit report triggers (yes/no)! C ! C !No !
! ! ! ! ! ! !
! !H ! 'Y15.0' sec before land/event A320! C ! C ! 1 !
! ! ! A321! C ! C ! 1 !
! ! ! A319! C ! C ! 1 !
! ! ! A318! C ! C ! 1 !
! ! ! ! ! ! !
! !I ! 'Y15.1' sec before land/event A320! C ! C ! 1 !
! ! ! A321! C ! C ! 1 !
! ! ! A319! C ! C ! 1 !
! ! ! A318! C ! C ! 1 !
! ! ! ! ! ! !
! !J ! 'Y15.2' sec after land/event A320! C ! C ! 3 !
! ! ! A321! C ! C ! 3 !
! ! ! A319! C ! C ! 3 !
! ! ! A318! C ! C ! 3 !
! ! ! ! ! ! !
! !K ! 'Y15.3' sec before bounced A320! C ! C ! 1 !
! ! ! A321! C ! C ! 1 !
! ! ! A319! C ! C ! 1 !
! ! ! A318! C ! C ! 1 !
! ! ! ! ! ! !
! !L ! 'Y15.4' sec before bounced A320! C ! C ! 1 !
! ! ! A321! C ! C ! 1 !
! ! ! A319! C ! C ! 1 !
! ! ! A318! C ! C ! 1 !
! ! ! ! ! ! !
! !M ! 'Y15.5' sec after bounced A320! C ! C ! 3 !
! ! ! A321! C ! C ! 3 !
! ! ! A319! C ! C ! 3 !
! ! ! A318! C ! C ! 3 !
! ! ! ! ! ! !
! !N ! N dataset time (sample) at landing ! C ! C ! 1 !
! ! ! to check for RALR trigger (RALRCHK) ! ! ! !
! ! ! Note: -N dataset time is programmable ! ! ! !
! ! ! from 0 to 5 ! ! ! !
! ! ! -1 sample is 1/16 second (16 Hz). ! ! ! !
!----!------!-----------------------------------------!----!----!---------!
!1000! ! Not applicable ! ! ! !
!----!------!-----------------------------------------!----!----!---------!
!2000! ! Not applicable ! ! ! !
!----!------!-----------------------------------------!----!----!---------!
!3000!3 ! Programmable Start Logic ! ! ! !
! !3.1 ! Logic algorithm ! ! ! !
! !3.2 ! Logic criteria values ! ! ! not !
! ! ! ! ! ! prog. !
! ! ! The parameters which are used for logic ! ! ! !
! ! ! items described as follows is observed ! ! ! !
! ! ! with a rate of 16 Hz. ! ! ! !
! ! ! Exceptions: ! ! ! !
! ! ! At landing (0.5 sec before and 0.5 sec ! ! ! !
! ! ! after landing or bounce), the non- ! ! ! !
! ! ! filtered acceleration VRTA and the non- ! ! ! !
! ! ! filtered landing gear status (see to ! ! ! !
! ! ! item no. 4.7) is observed with a rate ! ! ! !
! ! ! of 32 Hz. ! ! ! !
!----!------!-----------------------------------------!----!----!---------!
! !4 ! Report is generated if one of the ! ! ! !
! ! ! following logic items is present during ! ! ! !
! ! ! landing: ! ! ! !
!4100! ! RALR < RALRL ! ! ! !
! ! ! calculated between Start Sample Number ! ! ! !
! ! ! S1 and Stop Sample Number S2 ! ! ! !
! ! ! or ! ! ! !
!4400! ! VRTA > VRTAL1.1 ! ! ! !
! ! ! (during +/- 0.5 seconds before and after! ! ! !
! ! ! landing) calculated between Start ! ! ! !
! ! ! Sample Number S3 and Stop Sample ! ! ! !
! ! ! Number S4 ! ! ! !
! ! ! or ! ! ! !
!4800! ! GW > GWL (at landing) and RALR > RALRLG ! ! ! !
! ! ! (at dataset time at landing) (see item ! ! ! !
! ! ! no. L). ! ! ! !
! ! ! The appropriate GW (GWL1, GWL2, GWL3 or ! ! ! !
! ! ! GWL4) is taken depending if an aircraft ! ! ! !
! ! ! is equipped with or without ACT ! ! ! !
! ! ! (Additional Center Tanks). ! ! ! !
! ! ! ! ! ! !
! ! ! Logic for ACT detection ! ! ! !
! ! ! ! ! ! !
! ! ! FWC 26.1.276.01.26 26.1.276.01.27 GW ! ! ! !
! ! ! 26.2.276.10.26 26.2.276.10.27 Limit! ! ! !
! ! ! 0 0 GWL1 ! ! ! !
! ! ! 1 0 GWL2 ! ! ! !
! ! ! 0 1 GWL3 ! ! ! !
! ! ! 1 1 GWL4 ! ! ! !
! ! ! or ! ! ! !
!4900! ! GW > GWL (at landing) and VRTA > VRTALG ! ! ! !
! ! ! (during +/- 0.5 sec before and after ! ! ! !
! ! ! landing). ! ! ! !
! ! ! The appropriate GW (GWL1, GWL2, GWL3 or ! ! ! !
! ! ! GWL4) is taken depending if an ! ! ! !
! ! ! aircraft is equipped with or without ACT! ! ! !
! ! ! (Additional Center Tanks). Logic for ACT! ! ! !
! ! ! detection like Code No. 4800. ! ! ! !
! ! ! ! ! ! !
!4500! ! Report is generated if one of the ! ! ! !
! ! ! following logic items is present during ! ! ! !
! ! ! the bouncing: ! ! ! !
! ! ! ! ! ! !
! ! ! VRTA > VRTAL1.2 during +/- 0.5 sec at ! ! ! !
! ! ! landing (1st touchdown) ! ! ! !
! ! ! or ! ! ! !
! ! ! VRTA > VRTAL1.3 during +/- 0.5 sec at ! ! ! !
! ! ! landing (2nd touchdown). ! ! ! !
!----!------!-----------------------------------------!----!----!---------!
! !4.1 ! RALRL limit [ft/sec] A320 ! C ! C ! -9.0 !
! ! ! A321 ! C ! C ! -9.0 !
! ! ! A319 ! C ! C ! -9.0 !
! ! ! A318 ! C ! C ! -9.0 !
! !4.2 ! RALT ! ! ! !
! !4.2.1 ! RALTL1 limit [ft] A320 ! C ! C ! 150.0 !
! ! ! A321 ! C ! C ! 150.0 !
! ! ! A319 ! C ! C ! 150.0 !
! ! ! A318 ! C ! C ! 150.0 !
! !4.3 ! RALR ! ! ! !
! !4.3.1 ! D geometrical correction factor for ! ! ! !
! ! ! ROLR [ft/deg] A320 ! C ! C ! 0.0 !
! ! ! A321 ! C ! C ! 0.0 !
! ! ! A319 ! C ! C ! 0.0 !
! ! ! A318 ! C ! C ! 0.0 !
! !4.3.2 ! DX lever arm correction (x-axis) ! ! ! !
! ! ! for R/A RALT [ft] A320 ! C ! C ! 18.0 !
! ! ! A321 ! C ! C ! 28.8 !
! ! ! A319 ! C ! C ! 18.5 !
! ! ! A318 ! C ! C ! 16.8 !
! !4.3.3 ! DZ lever arm correction (z-axis) ! ! ! !
! ! ! for R/A RALT [ft] A320 ! C ! C ! 7.1 !
! ! ! A321 ! C ! C ! 7.8 !
! ! ! A319 ! C ! C ! 7.2 !
! ! ! A318 ! C ! C ! 7.6 !
! !4.3.4 ! DXTPIR lever arm correction (x-axis) ! ! ! !
! ! ! for PTCH [ft] A320 ! C ! C ! 39.0 !
! ! ! A321 ! C ! C ! 53.1 !
! ! ! A319 ! C ! C ! 33.8 !
! ! ! A318 ! C ! C ! 29.5 !
! ! ! ! ! ! !
! !4.3.5 ! FC filter frequency [Hz] A320 ! C ! C ! 0.3 !
! ! ! A321 ! C ! C ! 0.3 !
! ! ! A319 ! C ! C ! 0.3 !
! ! ! A318 ! C ! C ! 0.3 !
! ! ! ! ! ! !
! !4.3.6 ! K1 filter constant A320 ! C ! C ! 5.2 !
! ! ! A321 ! C ! C ! 5.2 !
! ! ! A319 ! C ! C ! 5.2 !
! ! ! A318 ! C ! C ! 5.2 !
! ! ! ! ! ! !
! !4.3.7 ! K2 filter constant A320 ! C ! C ! 25.0 !
! ! ! A321 ! C ! C ! 25.0 !
! ! ! A319 ! C ! C ! 25.0 !
! ! ! A318 ! C ! C ! 25.0 !
! ! ! ! ! ! !
! !4.3.8 ! K3 filter constant A320 ! C ! C ! 5.0 !
! ! ! A321 ! C ! C ! 5.0 !
! ! ! A319 ! C ! C ! 5.0 !
! ! ! A318 ! C ! C ! 5.0 !
! ! ! ! ! ! !
! !4.3.9 ! THETA0 [deg] A320 ! C ! C ! 6.0 !
! ! ! A321 ! C ! C ! 4.5 !
! ! ! A319 ! C ! C ! 2.0 !
! ! ! A318 ! C ! C ! 6.0 !
! ! ! ! ! ! !
! !4.3.10! S1 [sample] A320 ! C ! C ! -4.0 !
! ! ! A321 ! C ! C ! -4.0 !
! ! ! A319 ! C ! C ! -4.0 !
! ! ! A318 ! C ! C ! -4.0 !
! ! ! ! ! ! !
! !4.3.11! S2 [sample] A320 ! C ! C ! 4.0 !
! ! ! A321 ! C ! C ! 4.0 !
! ! ! A319 ! C ! C ! 4.0 !
! ! ! A318 ! C ! C ! 4.0 !
! ! ! ! ! ! !
! !4.4 ! VRTAL1.1 limit at landing [g] A320 ! C ! C ! 2.6 !
! ! ! A321 ! C ! C ! 2.6 !
! ! ! A319 ! C ! C ! 2.6 !
! ! ! A318 ! C ! C ! 2.6 !
! ! ! ! ! ! !
! !4.4.1 ! S3 [sample] A320 ! C ! C ! -16 !
! ! ! A321 ! C ! C ! -16 !
! ! ! A319 ! C ! C ! -16 !
! ! ! A318 ! C ! C ! -16 !
! ! ! ! ! ! !
! !4.4.2 ! S4 [sample] A320 ! C ! C ! 16 !
! ! ! A321 ! C ! C ! 16 !
! ! ! A319 ! C ! C ! 16 !
! ! ! A318 ! C ! C ! 16 !
! ! ! ! ! ! !
! !4.5 ! VRTAL1.2 limit at landing ! ! ! !
! ! ! (1st touchdown) from bounced ! ! ! !
! ! ! land/event [g] A320 ! C ! C ! 2.6 !
! ! ! A321 ! C ! C ! 2.6 !
! ! ! A319 ! C ! C ! 2.6 !
! ! ! A318 ! C ! C ! 2.6 !
! ! ! ! ! ! !
! !4.5.1 ! VRTAL1.3 limit at bounce (2nd touchdown)! ! ! !
! ! ! from bounced land/event [g] A320 ! C ! C ! 2.6 !
! ! ! A321 ! C ! C ! 2.6 !
! ! ! A319 ! C ! C ! 2.6 !
! ! ! A318 ! C ! C ! 2.6 !
! ! ! ! ! ! !
! !4.6 ! GW Overweight landing ! ! ! !
! !4.6.1 ! GWL1, GWL2, GWL3, GWL4 limit [kg] A320 ! C ! C ! 64500 !
! ! ! A321 ! C ! C ! 75500 !
! ! ! A319 ! C ! C ! 61000 !
! ! ! A318 ! C ! C ! 56500 !
! ! ! ! ! ! !
! ! ! ! ! ! !
! !4.6.2 ! RALRLG limit [ft/sec] A320 ! C ! C ! -6.0 !
! ! ! A321 ! C ! C ! -6.0 !
! ! ! A319 ! C ! C ! -6.0 !
! ! ! A318 ! C ! C ! -6.0 !
! ! ! ! ! ! !
! !4.6.3 ! VRTALG limit [g] A320 ! C ! C ! 1.7 !
! ! ! A321 ! C ! C ! 1.7 !
! ! ! A319 ! C ! C ! 1.7 !
! ! ! A318 ! C ! C ! 1.7 !
! ! ! ! ! ! !
! !4.7 ! Landing detection ! ! ! !
! ! ! Landing is detected when in PH7 or PH8 ! ! ! !
! ! ! 6D.1.021.01.13 = 1 (LH gear) ! ! ! !
! ! ! or ! ! ! !
! ! ! 6D.1.021.01.14 = 1 (RH gear) ! ! ! !
! ! ! ! ! ! !
! !4.8 ! Bounced landing detection ! ! ! !
! ! ! A bounced landing is detected when in ! ! ! !
! ! ! PH7 or PH8 parameter 6D.1.021.01.11 ! ! ! !
! ! ! is set to 1 for longer than 'Y15.5' ! ! ! !
! ! ! seconds ! ! ! !
! ! ! and ! ! ! !
! ! ! then one or both of 6D.1.021.01.13 ! ! ! !
! ! ! or Bit 14 is set to 0 for longer than ! ! ! !
! ! ! 'Y15.6' seconds ! ! ! !
! ! ! and ! ! ! !
! ! ! then the one which was set to 0 or the ! ! ! !
! ! ! first one of 6D.1.021.01.13 or ! ! ! !
! ! ! 6D.1.021.01.14 is set to 1 again ! ! ! !
! ! ! within 'Y15.7' seconds. ! ! ! !
! ! ! ! ! ! !
! !4.9 ! 'Y15.5' landing gear compress time ! ! ! !
! ! ! (1st touchdown) [sample] A320 ! C ! C ! 16 !
! ! ! A321 ! C ! C ! 16 !
! ! ! A319 ! C ! C ! 16 !
! ! ! A318 ! C ! C ! 16 !
! ! ! ! ! ! !
! !4.10 ! 'Y15.6' time between bounces [sample] ! ! ! !
! ! ! A320 ! C ! C ! 32 !
! ! ! A321 ! C ! C ! 32 !
! ! ! A319 ! C ! C ! 32 !
! ! ! A318 ! C ! C ! 32 !
! ! ! ! ! ! !
! !4.11 ! 'Y15.7' landing gear compress time ! ! ! !
! ! ! (2nd touchdown) [sample] A320 ! C ! C ! 320 !
! ! ! A321 ! C ! C ! 320 !
! ! ! A319 ! C ! C ! 320 !
! ! ! A318 ! C ! C ! 320 !
! ! ! NOTE: - 1 sample is 1/32 second (32 Hz) ! ! ! !
!----!------!-----------------------------------------!----!----!---------!
! !5 ! Report is generated if one of the ! ! ! !
! ! ! following logic items is present during ! ! ! !
! ! ! (PH 5, 5.1, 6, 7, 7.1). There is a ! ! ! !
! ! ! spacing time TURBWAIT (sec) to enable ! ! ! !
! ! ! the trigger logic again after the ! ! ! !
! ! ! previous report generation. ! ! ! !
! ! ! ! ! ! !
!5100!5.1 ! VRTA > VRTAL2.1 if FLAPL < 0.5 deg ! ! ! !
! ! ! ! ! ! !
!5200!5.2 ! VRTA < VRTAL2.2 if FLAPL < 0.5 deg ! ! ! !
! ! ! ! ! ! !
!5300!5.3 ! VRTA > VRTAL2.3 if FLAPL >/= 0.5 deg ! ! ! !
! ! ! or ! ! ! !
! ! ! VRTA < VRTAL2.4 if FLAPL >/= 0.5 deg ! ! ! !
! ! ! ! ! ! !
! ! ! Limitation for Code 5100, 5200, 5300: ! ! ! !
! ! ! W15 TURBWAIT spacing time for ! ! ! !
! ! ! re-activating the trigger logic after ! ! ! !
! ! ! the previous report generation within ! ! ! !
! ! ! the same flight leg. ! ! ! !
! ! ! ! ! ! !
!5400!5.4 ! If one of the 5 spoiler excursion ! ! ! !
! ! ! counters has an overflow (999 is ! ! ! !
! ! ! reached). ! ! ! !
!----!------!-----------------------------------------!----!----!---------!
! !5.5 ! VRTAL2.1 limit [g] A320 ! C ! C ! 2.5 !
! ! ! A321 ! C ! C ! 2.5 !
! ! ! A319 ! C ! C ! 2.5 !
! ! ! A318 ! C ! C ! 2.5 !
! ! ! ! ! ! !
! !5.6 ! VRTAL2.2 limit [g] A320 ! C ! C ! -1.0 !
! ! ! A321 ! C ! C ! -1.0 !
! ! ! A319 ! C ! C ! -1.0 !
! ! ! A318 ! C ! C ! -1.0 !
! ! ! ! ! ! !
! !5.7 ! VRTAL2.3 limit [g] A320 ! C ! C ! 2.0 !
! ! ! A321 ! C ! C ! 2.0 !
! ! ! A319 ! C ! C ! 2.0 !
! ! ! A318 ! C ! c ! 2.0 !
! ! ! ! ! ! !
! !5.8 ! VRTAL2.4 limit [g] A320 ! C ! C ! 0.0 !
! ! ! A321 ! C ! C ! 0.0 !
! ! ! A319 ! C ! C ! 0.0 !
! ! ! A318 ! C ! C ! 0.0 !
! ! ! ! ! ! !
! !5.9 ! TURBWAIT [sec] A320 ! C ! C ! 10 !
! ! ! A321 ! C ! C ! 10 !
! ! ! A319 ! C ! C ! 10 !
! ! ! A318 ! C ! C ! 10 !
! ! ! ! ! ! !
! !5.10 ! FLAPL [deg] A320 ! C ! C ! 0.5 !
! ! ! A321 ! C ! C ! 0.5 !
! ! ! A319 ! C ! C ! 0.5 !
! ! ! A318 ! C ! C ! 0.5 !
!----!------!-----------------------------------------!----!----!---------!
!8100!8.1 ! ACARS MU uplink request with IMI 'REQ15'! ! ! !
! ! ! The report <15> is immediately ! ! ! !
! ! ! generated to the ACARS MU ! ! ! !
!-------------------------------------------------------------------------!
! A = Programmable by Airbus !
! C = Programmable by Customer !
+-------------------------------------------------------------------------+

(20) Load Report Logic <15>
+----------------------------------------------------------------------+
!Code!Item ! !Progr.!Standard !
! No.!No. ! Description of Function Item !MCDU !Value or !
! ! ! !/GSE !Table TXY!
!----!------!-----------------------------------------!------!---------!
! !A ! Report Format ! ! !
! ! ! ! ! !
! !B ! Parameter Table ! ! !
! ! ! ! ! !
! !C ! First three lines of Report ! ! Blank !
! ! ! ! ! !
! !D ! Print Out Rules : ! C ! PH10 see!
! ! ! PH9,PH10, Immediately, Manually ! ! separate!
! ! ! ! ! list !
! !E ! Transfer to ACARS MU: yes/no ! C ! see !
! ! ! ! ! separate!
! ! ! ! ! list !
! !F ! Increment of the report counter: yes/no ! C ! Yes !
! ! ! ! ! !
! !G ! Inhibit report triggers: yes/no ! C ! No !
! ! ! ! ! !
! !H ! 'Y15.0' sec before land/event A320! C ! 1 !
! ! ! A321! C ! 1 !
! ! ! A319! C ! 1 !
! ! ! A318! C ! 1 !
! ! ! ! ! !
! !I ! 'Y15.1' sec before land/event A320! C ! 1 !
! ! ! A321! C ! 1 !
! ! ! A319! C ! 1 !
! ! ! A318! C ! 1 !
! ! ! ! ! !
! !J ! 'Y15.2' sec after land/event A320! C ! 3 !
! ! ! A321! C ! 3 !
! ! ! A319! C ! 3 !
! ! ! A318! C ! 3 !
! ! ! ! ! !
! !K ! 'Y15.3' sec before bounced A320! C ! 1 !
! ! ! A321! C ! 1 !
! ! ! A319! C ! 1 !
! ! ! A318! C ! 1 !
! ! ! ! ! !
! !L ! 'Y15.4' sec before bounced A320! C ! 1 !
! ! ! A321! C ! 1 !
! ! ! A319! C ! 1 !
! ! ! A318! C ! 1 !
! ! ! ! ! !
! !M ! 'Y15.5' sec after bounced A320! C ! 3 !
! ! ! A321! C ! 3 !
! ! ! A319! C ! 3 !
! ! ! A318! C ! 3 !
! ! ! ! ! !
! !N ! N dataset time (sample) at landing ! C ! 1 !
! ! ! to check for RALR trigger ! ! !
! ! ! Note: -N dataset time is programmable ! ! !
! ! ! from 0 to 5. ! ! !
! ! ! -1 sample is 1/16 second (16 Hz). ! ! !
!----!------!-----------------------------------------!------!---------!
!1000! ! Not applicable ! ! !
!----!------!-----------------------------------------!------!---------!
!2000! ! Not applicable ! ! !
!----!------!-----------------------------------------!------!---------!
!3000!3 ! Programmable Start Logic ! ! !
! !3.1 ! Logic algorithm ! ! !
! !3.2 ! Logic criteria values ! !not prog.!
!----!------!-----------------------------------------!------!---------!
! ! ! The parameters which are used for logic ! ! !
! ! ! items described as follows shall be ! ! !
! ! ! observed with a rate of 16 Hz. ! ! !
! ! ! Exceptions: ! ! !
! ! ! At landing (0.5 sec before and 0.5 sec ! ! !
! ! ! after landing or bounce), the non- ! ! !
! ! ! filtered acceleration VRTA and the non- ! ! !
! ! ! filtered landing gear status (see to ! ! !
! ! ! item no. 4.7) shall be observed with ! ! !
! ! ! a rate of 32 Hz. ! ! !
!----!------!-----------------------------------------!------!---------!
! !4 ! Report is generated if one of the ! ! !
! ! ! following logic items is present during ! ! !
! ! ! landing: ! ! !
!4100! ! RALR < RALRL ! ! !
! ! ! calculated between Start Sample Number ! ! !
! ! ! S1 and Stop Sample Number S2 ! ! !
! ! ! or ! ! !
!4400! ! VRTA > VRTAL1.1 ! ! !
! ! ! (during +/- 0.5 seconds before and after! ! !
! ! ! landing) calculated between Start ! ! !
! ! ! Sample Number S3 and Stop Sample ! ! !
! ! ! Number S4 ! ! !
! ! ! or ! ! !
!4800! ! GW > GWL (at landing) and RALR < RALRLG ! ! !
! ! ! (at dataset time at landing (see item ! ! !
! ! ! no. L)). ! ! !
! ! ! The appropriate GW (GWL1, GWL2, GWL3 or ! ! !
! ! ! GWL4) shall be taken depending on if an ! ! !
! ! ! aircraft is equipped with or without ACT! ! !
! ! ! (Additional Center Tanks). ! ! !
! ! ! ! ! !
! ! ! Logic for ACT detection ! ! !
! ! ! ! ! !
! ! ! FWC 26.1.276.01.26 26.1.276.01.27 GW ! ! !
! ! ! 26.1.276.10.26 26.1.276.10.27 Limit! ! !
! ! !-----------------------------------------! ! !
! ! ! 0 0 GWL1 ! ! !
! ! ! 1 0 GWL2 ! ! !
! ! ! 0 1 GWL3 ! ! !
! ! ! 1 1 GWL4 ! ! !
! ! ! ! ! !
! ! ! or ! ! !
! ! ! ! ! !
!4900! ! GW > GWL (at landing) and VRTA > VRTALG ! ! !
! ! ! (during +/- 0.5 sec before and after ! ! !
! ! ! landing). ! ! !
! ! ! The appropriate GW (GWL1, GWL2, GWL3 or ! ! !
! ! ! GWL4) shall be taken depending on if an ! ! !
! ! ! aircraft is equipped with or without ACT! ! !
! ! ! (Additional Center Tanks). Logic for ACT! ! !
! ! ! detection like Code No. 4800. ! ! !
!----!------!-----------------------------------------!------!---------!
!4500! ! Report will be generated if one of the ! ! !
! ! ! following logic items is present during ! ! !
! ! ! the bouncing: ! ! !
! ! ! ! ! !
! ! ! VRTA > VRTAL1.2 during +/- 0.5 sec at ! ! !
! ! ! landing (1st touchdown) ! ! !
! ! ! ! ! !
! ! ! or ! ! !
! ! ! ! ! !
! ! ! VRTA > VRTAL1.3 during +/- 0.5 sec at ! ! !
! ! ! landing (2nd touchdown). ! ! !
! !4.1 ! RALRL limit (ft/sec) A320 ! C ! -9.0 !
! ! ! A321 ! C ! -9.0 !
! ! ! A319 ! C ! -9.0 !
! ! ! A318 ! C ! -9.0 !
! !4.2 ! RALT ! ! !
! !4.2.1 ! RALTL1 limit (ft) A320 ! C ! 150.0 !
! ! ! A321 ! C ! 150.0 !
! ! ! A319 ! C ! 150.0 !
! ! ! A318 ! C ! 150.0 !
! !4.3 ! RALR ! ! !
! !4.3.1 ! D geometrical correction factor for ! ! !
! ! ! ROLR (ft/deg) A320 ! C ! 0.0 !
! ! ! A321 ! C ! 0.0 !
! ! ! A319 ! C ! 0.0 !
! ! ! A318 ! C ! 0.0 !
! !4.3.2 ! DX lever arm correction (x-axis) ! ! !
! ! ! for R/A RALT (ft) A320 ! C ! 18.0 !
! ! ! A321 ! C ! 28.8 !
! ! ! A319 ! C ! 18.5 !
! ! ! A318 ! C ! 16.8 !
! !4.3.3 ! DZ lever arm correction (z-axis) ! ! !
! ! ! for R/A RALT (ft) A320 ! C ! 7.1 !
! ! ! A321 ! C ! 7.8 !
! ! ! A319 ! C ! 7.2 !
! ! ! A318 ! C ! 7.6 !
! !4.3.4 ! DXTPIR lever arm correction (x-axis) ! ! !
! ! ! for PTCH (ft) A320 ! C ! 39.0 !
! ! ! A321 ! C ! 53.1 !
! ! ! A319 ! C ! 33.8 !
! ! ! A318 ! C ! 29.5 !
! ! ! ! ! !
! !4.3.5 ! FC filter frequency (Hz) A320 ! C ! 0.3 !
! ! ! A321 ! C ! 0.3 !
! ! ! A319 ! C ! 0.3 !
! ! ! A318 ! C ! 0.3 !
! ! ! ! ! !
! !4.3.6 ! K1 filter constant A320 ! C ! 5.2 !
! ! ! A321 ! C ! 5.2 !
! ! ! A319 ! C ! 5.2 !
! ! ! A318 ! C ! 5.2 !
! ! ! ! ! !
! !4.3.7 ! K2 filter constant A320 ! C ! 25.0 !
! ! ! A321 ! C ! 25.0 !
! ! ! A319 ! C ! 25.0 !
! ! ! A318 ! C ! 25.0 !
! ! ! ! ! !
! !4.3.8 ! K3 filter constant A320 ! C ! 5.0 !
! ! ! A321 ! C ! 5.0 !
! ! ! A319 ! C ! 5.0 !
! ! ! A318 ! C ! 5.0 !
! ! ! ! ! !
! !4.3.9 ! THETA0 (deg) A320 ! C ! 6.0 !
! ! ! (averaged Pitch at touchdown) A321 ! C ! 4.5 !
! ! ! A319 ! C ! 2.0 !
! ! ! A318 ! C ! 6.0 !
! ! ! ! ! !
! !4.3.10! S1 (sample) A320 ! C ! -4.0 !
! ! ! A321 ! C ! -4.0 !
! ! ! A319 ! C ! -4.0 !
! ! ! A318 ! C ! -4.0 !
! ! ! ! ! !
! !4.3.11! S2 (sample) A320 ! C ! 4.0 !
! ! ! A321 ! C ! 4.0 !
! ! ! A319 ! C ! 4.0 !
! ! ! A318 ! C ! 4.0 !
! ! ! ! ! !
! !4.4 ! VRTAL1.1 limit at landing (g) A320 ! C ! 2.6 !
! ! ! A321 ! C ! 2.6 !
! ! ! A319 ! C ! 2.6 !
! ! ! A318 ! C ! 2.6 !
! ! ! ! ! !
! !4.4.1 ! S3 (sample) A320 ! C ! -16 !
! ! ! A321 ! C ! -16 !
! ! ! A319 ! C ! -16 !
! ! ! A318 ! C ! -16 !
! ! ! ! ! !
! !4.4.2 ! S4 (sample) A320 ! C ! 16 !
! ! ! A321 ! C ! 16 !
! ! ! A319 ! C ! 16 !
! ! ! A318 ! C ! 16 !
! ! ! ! ! !
! !4.5 ! VRTAL1.2 limit at landing (g) A320 ! C ! 2.6 !
! ! ! (1st touchdown) A321 ! C ! 2.6 !
! ! ! from bunced land/event A319 ! C ! 2.6 !
! ! ! A318 ! C ! 2.6 !
! ! ! ! ! !
! !4.5.1 ! VRTAL1.3 limit at bounce (g) A320 ! C ! 2.6 !
! ! ! (2nd touchdown) A321 ! C ! 2.6 !
! ! ! from bounced land/event A319 ! C ! 2.6 !
! ! ! A318 ! C ! 2.6 !
! !4.6 ! GW Overweight landing ! ! !
! !4.6.1 ! GWL1, GWL2, GWL3, GWL4 limit (kg) A320 ! C ! 64500 !
! ! ! A321 ! C ! 75500 !
! ! ! A319 ! C ! 61000 !
! ! ! A318 ! C ! 56000 !
! ! ! NOTE: The standard GWL value stored ! ! !
! ! ! in the DMU is not always in line with ! ! !
! ! ! the MLW. We recommend to set the GWL ! ! !
! ! ! value in line with the MLW (Ref: AMM ! ! !
! ! ! 31-36-00). ! ! !
! ! ! ! ! !
! !4.6.2 ! RALRLG limit (ft/sec) A320 ! C ! -6.0 !
! ! ! A321 ! C ! -6.0 !
! ! ! A319 ! C ! -6.0 !
! ! ! A318 ! C ! -6.0 !
! ! ! ! ! !
! !4.6.3 ! VRTALG limit (g) A320 ! C ! 1.7 !
! ! ! A321 ! C ! 1.7 !
! ! ! A319 ! C ! 1.7 !
! ! ! A318 ! C ! 1.7 !
! ! ! ! ! !
! !4.7 ! Landing detection ! ! !
! ! ! Landing is detected when in PH7 or PH8 ! ! !
! ! ! 6D.1.021.01.13 = 1 (LH gear) ! ! !
! ! ! or ! ! !
! ! ! 6D.1.021.01.14 = 1 (RH gear) ! ! !
! ! ! ! ! !
! !4.8 ! Bounced landing detection ! ! !
! ! ! A bounced landing is detected when in ! ! !
! ! ! PH7 or PH8 parameter 6D.1.021.01.11 is ! ! !
! ! ! set to 1 for longer than 'Y15.6'*(1/32) ! ! !
! ! ! seconds ! ! !
! ! ! and ! ! !
! ! ! then one or both of 6D.1.021.01.13 or ! ! !
! ! ! 6D.1.021.01.14 is set to 0 for longer ! ! !
! ! ! than 'Y15.7'*(1/32) seconds ! ! !
! ! ! and ! ! !
! ! ! then the one which was set to 0 or the ! ! !
! ! ! first one of 6D.1.021.01.13 or ! ! !
! ! ! 6D.1.021.01.14 is set to 1 again within ! ! !
! ! ! 'Y15.8'*(1/32) seconds. ! ! !
! ! ! ! ! !
! !4.9 ! 'Y15.6' landing gear compress time ! ! !
! ! ! (1st touchdown) (sample) A320 ! ! 16 !
! ! ! A321 ! ! 16 !
! ! ! A319 ! ! 16 !
! ! ! A318 ! ! 16 !
! ! ! ! ! !
! !4.10 ! 'Y15.7' time between bounces (sample) ! ! !
! ! ! A320 ! ! 32 !
! ! ! A321 ! ! 32 !
! ! ! A319 ! ! 32 !
! ! ! A318 ! ! 32 !
! ! ! ! ! !
! !4.11 ! 'Y15.8' landing gear compress time ! ! !
! ! ! (2nd touchdown) (sample) A320 ! ! 320 !
! ! ! A321 ! ! 320 !
! ! ! A319 ! ! 320 !
! ! ! A318 ! ! 320 !
! ! ! NOTE: 1 sample is 1/32 second (32 Hz) ! ! !
!----!------!-----------------------------------------!------!---------!
! !5 ! Report shall be generated if one of the ! ! !
! ! ! following logic items is present during ! ! !
! ! ! flight (PH5, 5.1, 6, 7, 7.1). There is a! ! !
! ! ! spacing time TURBWAIT sec. to enable the! ! !
! ! ! trigger logic again after the previous ! ! !
! ! ! report generation. ! ! !
! ! ! ! ! !
!5100!5.1 ! VRTA > VRTAL2.1 if FLAP < FLAPL ! ! !
! ! ! ! ! !
!5200!5.2 ! VRTA < VRTAL2.2 if FLAP < FLAPL ! ! !
! ! ! ! ! !
!5300!5.3 ! VRTA > VRTAL2.3 if FLAP >= FLAPL OR ! ! !
! ! ! VRTA < VRTAL2.4 if FLAP >= FLAPL ! ! !
! ! ! ! ! !
! ! ! Limitation for Code 5100, 5200, 5300: ! ! !
! ! ! W15 TURBWAIT spacing time for re- ! ! !
! ! ! activating the trigger logic after the ! ! !
! ! ! previous report generation within the ! ! !
! ! ! same flight leg. ! ! !
! ! ! ! ! !
!5400!5.4 ! If one of the 5 spoiler excursion ! ! !
! ! ! counters has an overflow (999 is ! ! !
! ! ! reached). ! ! !
!----!------!-----------------------------------------!------!---------!
! !5.5 ! VRTAL2.1 limit (g) A320 ! C ! 2.5 !
! ! ! A321 ! C ! 2.5 !
! ! ! A319 ! C ! 2.5 !
! ! ! A318 ! C ! 2.5 !
! ! ! ! ! !
! !5.6 ! VRTAL2.2 limit (g) A320 ! C ! -1.0 !
! ! ! A321 ! C ! -1.0 !
! ! ! A319 ! C ! -1.0 !
! ! ! A318 ! C ! -1.0 !
! ! ! ! ! !
! !5.7 ! VRTAL2.3 limit (g) A320 ! C ! 2.0 !
! ! ! A321 ! C ! 2.0 !
! ! ! A319 ! C ! 2.0 !
! ! ! A318 ! C ! 2.0 !
! ! ! ! ! !
! !5.8 ! VRTAL2.4 limit (g) A320 ! C ! 0.0 !
! ! ! A321 ! C ! 0.0 !
! ! ! A319 ! C ! 0.0 !
! ! ! A318 ! C ! 0.0 !
! ! ! ! ! !
! !5.9 ! TURBWAIT (sec.) A320 ! C ! 10 !
! ! ! A321 ! C ! 10 !
! ! ! A319 ! C ! 10 !
! ! ! A318 ! C ! 10 !
! ! ! ! ! !
! !5.10 ! FLAPL (deg) A320 ! C ! 0.5 !
! ! ! A321 ! C ! 0.5 !
! ! ! A319 ! C ! 0.5 !
! ! ! A318 ! C ! 0.5 !
!----!------!-----------------------------------------!------!---------!
!8100!8.1 !ACARS MU uplink request with IMI 'REQ15':! ! !
! ! !The report <15> shall be immediately ! ! !
! ! !generated and transmitted to the ACARS ! ! !
! ! !MU. ! ! !
!----------------------------------------------------------------------!
! A = Programmable by Airbus !
! C = Programmable by Customer !
+----------------------------------------------------------------------+

(21) Load Report Logic <15>
+----------------------------------------------------------------------+
!Code!Item ! !Progr.!Standard !
! No.!No. ! Description of Function Item !MCDU !Value !
!----!------!-----------------------------------------!------!---------!
! !A ! Report Format ! ! !
! ! ! ! ! !
! !B ! Parameter Table ! ! !
! ! ! ! ! !
! !C ! First three lines of Report ! ! Blank !
! ! ! ! ! !
! !D ! Print Out Rules ! C ! PH10 see!
! ! ! (PH9,PH10, Immediately, Manually) ! ! separate!
! ! ! ! ! list !
! !E ! Transfer to ACARS MU (yes/no) ! C ! see !
! ! ! ! ! separate!
! ! ! ! ! list !
! !F ! Increment of the report counter (yes/no)! C ! Yes !
! ! ! ! ! !
! !G ! Inhibit report triggers (yes/no) ! C ! No !
! ! ! ! ! !
! !H ! 'Y15.0' sec before land/event A320! C ! 1 !
! ! ! A321! C ! 1 !
! ! ! A319! C ! 1 !
! ! ! A318! C ! 1 !
! ! ! ! ! !
! !I ! 'Y15.1' sec before land/event A320! C ! 1 !
! ! ! A321! C ! 1 !
! ! ! A319! C ! 1 !
! ! ! A318! C ! 1 !
! ! ! ! ! !
! !J ! 'Y15.2' sec after land/event A320! C ! 3 !
! ! ! A321! C ! 3 !
! ! ! A319! C ! 3 !
! ! ! A318! C ! 3 !
! ! ! ! ! !
! !K ! 'Y15.3' sec before bounced A320! C ! 1 !
! ! ! A321! C ! 1 !
! ! ! A319! C ! 1 !
! ! ! A318! C ! 1 !
! ! ! ! ! !
! !L ! 'Y15.4' sec before bounced A320! C ! 1 !
! ! ! A321! C ! 1 !
! ! ! A319! C ! 1 !
! ! ! A318! C ! 1 !
! ! ! ! ! !
! !M ! 'Y15.5' sec after bounced A320! C ! 3 !
! ! ! A321! C ! 3 !
! ! ! A319! C ! 3 !
! ! ! A318! C ! 3 !
! ! ! ! ! !
! !N ! N dataset time (sample) at landing ! C ! 1 !
! ! ! to check for RALR trigger ! ! !
! ! ! Note: -N dataset time is programmable ! ! !
! ! ! from 0 to 5. ! ! !
! ! ! -1 sample is 1/16 second (16 Hz) ! ! !
!----!------!-----------------------------------------!------!---------!
!1000! ! Not applicable ! ! !
!----!------!-----------------------------------------!------!---------!
!2000! ! Not applicable ! ! !
!----!------!-----------------------------------------!------!---------!
!3000!3 ! Programmable Start Logic ! ! !
! !3.1 ! Logic algorithm ! ! !
! !3.2 ! Logic criteria values ! !not prog.!
!----!------!-----------------------------------------!------!---------!
! ! ! The parameters which are used for logic ! ! !
! ! ! items described as follows are observed ! ! !
! ! ! with a rate of 16 Hz. ! ! !
! ! ! Exceptions: ! ! !
! ! ! At landing (0.5 sec before and 0.5 sec ! ! !
! ! ! after landing or bounce), the non- ! ! !
! ! ! filtered acceleration VRTA and the non- ! ! !
! ! ! filtered landing gear status (see to ! ! !
! ! ! item no. 4.7) are observed with a rate ! ! !
! ! ! of 32 Hz. ! ! !
!----!------!-----------------------------------------!------!---------!
! !4 ! Report is generated if one of the ! ! !
! ! ! following logic items is present during ! ! !
! ! ! landing: ! ! !
!4100! ! RALR < RALRL ! ! !
! ! ! calculated between Start Sample Number ! ! !
! ! ! S1 and Stop Sample Number S2 ! ! !
! ! ! or ! ! !
!4400! ! VRTA > VRTAL1.1 ! ! !
! ! ! (during +/- 0.5 seconds before and after! ! !
! ! ! landing) calculated between Start ! ! !
! ! ! Sample Number S3 and Stop Sample ! ! !
! ! ! Number S4 ! ! !
! ! ! or ! ! !
!4800! ! GW > GWL (at landing) and RALR < RALRLG ! ! !
! ! ! (at dataset time at landing (see item ! ! !
! ! ! no. L)). ! ! !
! ! ! The appropriate GW (GWL1, GWL2, GWL3 or ! ! !
! ! ! GWL4) is taken depending on if an ! ! !
! ! ! aircraft is equipped with or without ACT! ! !
! ! ! (Additional Center Tanks). ! ! !
! ! ! ! ! !
! ! ! Logic for ACT detection ! ! !
! ! ! GW ! ! !
! ! ! FWC 26.1.276.01.26 26.1.276.01.27 Limit! ! !
! ! ! 26.1.276.10.26 26.1.276.10.27 ! ! !
! ! ! ! ! !
! ! ! 0 0 GWL1 ! ! !
! ! ! 1 0 GWL2 ! ! !
! ! ! 0 1 GWL3 ! ! !
! ! ! 1 1 GWL4 ! ! !
! ! ! ! ! !
! ! ! or ! ! !
! ! ! ! ! !
!4900! ! GW > GWL (at landing) and VRTA > VRTALG ! ! !
! ! ! (during +/- 0.5 sec before and after ! ! !
! ! ! landing). ! ! !
! ! ! The appropriate GW (GWL1, GWL2, GWL3 or ! ! !
! ! ! GWL4) is taken depending on if an ! ! !
! ! ! aircraft is equipped with or without ACT! ! !
! ! ! (Additional Center Tanks). Logic for ACT! ! !
! ! ! detection like Code No. 4800. ! ! !
! ! ! ! ! !
!4500! ! Report will be generated if one of the ! ! !
! ! ! following logic items is present during ! ! !
! ! ! the bouncing: ! ! !
! ! ! ! ! !
! ! ! VRTA > VRTAL1.2 during +/- 0.5 sec at ! ! !
! ! ! landing (1st touchdown) ! ! !
! ! ! ! ! !
! ! ! or ! ! !
! ! ! ! ! !
! ! ! VRTA > VRTAL1.3 during +/- 0.5 sec at ! ! !
! ! ! landing (2nd touchdown). ! ! !
! ! ! ! ! !
! !4.1 ! RALRL limit (ft/sec) A320 ! C ! -9.0 !
! ! ! A321 ! C ! -9.0 !
! ! ! A319 ! C ! -9.0 !
! ! ! A318 ! C ! -9.0 !
! !4.2 ! RALT ! ! !
! !4.2.1 ! RALTL1 limit (ft) A320 ! C ! 150.0 !
! ! ! A321 ! C ! 150.0 !
! ! ! A319 ! C ! 150.0 !
! ! ! A318 ! C ! 150.0 !
! !4.3 ! RALR ! ! !
! !4.3.1 ! D geometrical correction factor for ! ! !
! ! ! ROLR (ft/deg) A320 ! C ! 0.0 !
! ! ! A321 ! C ! 0.0 !
! ! ! A319 ! C ! 0.0 !
! ! ! A318 ! C ! 0.0 !
! !4.3.2 ! DX lever arm correction (x-axis) ! ! !
! ! ! for R/A RALT (ft) A320 ! C ! 18.0 !
! ! ! A321 ! C ! 28.8 !
! ! ! A319 ! C ! 18.5 !
! ! ! A318 ! C ! 16.8 !
! !4.3.3 ! DZ lever arm correction (z-axis) ! ! !
! ! ! for R/A RALT (ft) A320 ! C ! 7.1 !
! ! ! A321 ! C ! 7.8 !
! ! ! A319 ! C ! 7.2 !
! ! ! A318 ! C ! 7.6 !
! !4.3.4 ! DXTPIR lever arm correction (x-axis) ! ! !
! ! ! for PTCH (ft) A320 ! C ! 39.0 !
! ! ! A321 ! C ! 53.1 !
! ! ! A319 ! C ! 33.8 !
! ! ! A318 ! C ! 29.5 !
! ! ! ! ! !
! !4.3.5 ! FC filter frequency (Hz) A320 ! C ! 0.3 !
! ! ! A321 ! C ! 0.3 !
! ! ! A319 ! C ! 0.3 !
! ! ! A318 ! C ! 0.3 !
! ! ! ! ! !
! !4.3.6 ! K1 filter constant A320 ! C ! 5.2 !
! ! ! A321 ! C ! 5.2 !
! ! ! A319 ! C ! 5.2 !
! ! ! A318 ! C ! 5.2 !
! ! ! ! ! !
! !4.3.7 ! K2 filter constant A320 ! C ! 25.0 !
! ! ! A321 ! C ! 25.0 !
! ! ! A319 ! C ! 25.0 !
! ! ! A318 ! C ! 25.0 !
! ! ! ! ! !
! !4.3.8 ! K3 filter constant A320 ! C ! 5.0 !
! ! ! A321 ! C ! 5.0 !
! ! ! A319 ! C ! 5.0 !
! ! ! A318 ! C ! 5.0 !
! ! ! ! ! !
! !4.3.9 ! THETA0 (averaged pitch at A320 ! C ! 6.0 !
! ! ! touchdown) deg A321 ! C ! 4.5 !
! ! ! A319 ! C ! 2.0 !
! ! ! A318 ! C ! 6.0 !
! ! ! ! ! !
! !4.3.10! S1 (sample) A320 ! C ! -4.0 !
! ! ! A321 ! C ! -4.0 !
! ! ! A319 ! C ! -4.0 !
! ! ! A318 ! C ! -4.0 !
! ! ! ! ! !
! !4.3.11! S2 (sample) A320 ! C ! 4.0 !
! ! ! A321 ! C ! 4.0 !
! ! ! A319 ! C ! 4.0 !
! ! ! A318 ! C ! 4.0 !
! ! ! ! ! !
! !4.4 ! VRTAL1.1 limit at landing (g) A320 ! C ! 2.6 !
! ! ! A321 ! C ! 2.6 !
! ! ! A319 ! C ! 2.6 !
! ! ! A318 ! C ! 2.6 !
! ! ! ! ! !
! !4.4.1 ! S3 (sample) A320 ! C ! -16 !
! ! ! A321 ! C ! -16 !
! ! ! A319 ! C ! -16 !
! ! ! A318 ! C ! -16 !
! ! ! ! ! !
! !4.4.2 ! S4 (sample) A320 ! C ! 16 !
! ! ! A321 ! C ! 16 !
! ! ! A319 ! C ! 16 !
! ! ! A318 ! C ! 16 !
! ! ! ! ! !
! !4.5 ! VRTAL1.2 limit at landing-1st touchdown ! ! !
! ! ! from bounced land/event (g) A320 ! C ! 2.6 !
! ! ! A321 ! C ! 2.6 !
! ! ! A319 ! C ! 2.6 !
! ! ! A318 ! C ! 2.6 !
! ! ! ! ! !
! !4.5.1 ! VRTAL1.3 limit at bounce (2nd touchdown)! ! !
! ! ! from bounced land/event (g) A320 ! C ! 2.6 !
! ! ! A321 ! C ! 2.6 !
! ! ! A319 ! C ! 2.6 !
! ! ! A318 ! C ! 2.6 !
! !4.6 ! GW Overweight landing ! ! !
! !4.6.1 ! GWL1, GWL2, GWL3, GWL4 limit (kg) A320 ! C ! 64500 !
! ! ! A321 ! C ! 73500 !
! ! ! A319 ! C ! 61000 !
! ! ! A318 ! C ! 56000 !
! ! ! ! ! !
! !4.6.2 ! RALRLG limit (ft/sec) A320 ! C ! -6.0 !
! ! ! A321 ! C ! -6.0 !
! ! ! A319 ! C ! -6.0 !
! ! ! A318 ! C ! -6.0 !
! ! ! ! ! !
! !4.6.3 ! VRTALG limit (g) A320 ! C ! 1.7 !
! ! ! A321 ! C ! 1.7 !
! ! ! A319 ! C ! 1.7 !
! ! ! A318 ! C ! 1.7 !
! ! ! ! ! !
! !4.7 ! Landing detection ! ! !
! ! ! Landing is detected when in PH7 or PH8 ! ! !
! ! ! 6D.1.021.01.13 = 1 (LH gear) ! ! !
! ! ! or ! ! !
! ! ! 6D.1.021.01.14 = 1 (RH gear) ! ! !
! ! ! ! ! !
! !4.8 ! Bounced landing detection ! ! !
! ! ! A bounced landing is detected when in ! ! !
! ! ! PH7 or PH8 parameter 6D.1.021.01.11 is ! ! !
! ! ! set to 1 for longer than 'Y15.6'*(1/32) ! ! !
! ! ! seconds ! ! !
! ! ! and ! ! !
! ! ! then one or both of 6D.1.021.01.13 or ! ! !
! ! ! 6D.1.021.01.14 is set to 0 for longer ! ! !
! ! ! than 'Y15.7'*(1/32) seconds ! ! !
! ! ! and ! ! !
! ! ! then the one which was set to 0 or the ! ! !
! ! ! first one of 6D.1.021.01.13 or ! ! !
! ! ! 6D.1.021.01.14 is set to 1 again within ! ! !
! ! ! within 'Y15.8'*(1/32) seconds. ! ! !
! ! ! ! ! !
! !4.9 ! 'Y15.6' landing gear compress time ! ! !
! ! ! (1st touchdown) (sample) A320 ! ! 16 !
! ! ! A321 ! ! 16 !
! ! ! A319 ! ! 16 !
! ! ! A318 ! ! 16 !
! ! ! ! ! !
! !4.10 ! 'Y15.7' time between bounces (sample) ! ! !
! ! ! A320 ! ! 32 !
! ! ! A321 ! ! 32 !
! ! ! A319 ! ! 32 !
! ! ! A318 ! ! 32 !
! ! ! ! ! !
! !4.11 ! 'Y15.8' landing gear compress time ! ! !
! ! ! (2nd touchdown) (sample) A320 ! ! 320 !
! ! ! A321 ! ! 320 !
! ! ! A319 ! ! 320 !
! ! ! A318 ! ! 320 !
! ! ! NOTE: 1 sample is 1/32 second (32 Hz) ! ! !
!----!------!-----------------------------------------!------!---------!
! !5 ! Report is generated if one of the ! ! !
! ! ! following logic items is present during ! ! !
! ! ! flight (PH5, 5.1, 6, 7, 7.1). There is a! ! !
! ! ! spacing time TURBWAIT (sec.) to enable ! ! !
! ! ! the trigger logic again after the ! ! !
! ! ! previous report generation. ! ! !
! ! ! ! ! !
!5100!5.1 ! VRTA > VRTAL2.1 if FLAP < FLAPL ! ! !
! ! ! ! ! !
!5200!5.2 ! VRTA < VRTAL2.2 if FLAP < FLAPL ! ! !
! ! ! ! ! !
!5300!5.3 ! VRTA > VRTAL2.3 if FLAP >= FLAPL OR ! ! !
! ! ! VRTA < VRTAL2.4 if FLAP >= FLAPL ! ! !
! ! ! ! ! !
! ! ! Limitation for Code 5100, 5200, 5300: ! ! !
! ! ! W15 TURBWAIT spacing time for re- ! ! !
! ! ! activating the trigger logic after the ! ! !
! ! ! previous report generation within the ! ! !
! ! ! same flight leg. ! ! !
! ! ! ! ! !
!5400!5.4 ! If one of the 5 spoiler excursion ! ! !
! ! ! counters has an overflow (999 is ! ! !
! ! ! reached). ! ! !
! ! ! ! ! !
! !5.5 ! VRTAL2.1 limit (g) A320 ! C ! 2.5 !
! ! ! A321 ! C ! 2.5 !
! ! ! A319 ! C ! 2.5 !
! ! ! A318 ! C ! 2.5 !
! ! ! ! ! !
! !5.6 ! VRTAL2.2 limit (g) A320 ! C ! -1.0 !
! ! ! A321 ! C ! -1.0 !
! ! ! A319 ! C ! -1.0 !
! ! ! A318 ! C ! -1.0 !
! ! ! ! ! !
! !5.7 ! VRTAL2.3 limit (g) A320 ! C ! 2.0 !
! ! ! A321 ! C ! 2.0 !
! ! ! A319 ! C ! 2.0 !
! ! ! A318 ! C ! 2.0 !
! ! ! ! ! !
! !5.8 ! VRTAL2.4 limit (g) A320 ! C ! 0.0 !
! ! ! A321 ! C ! 0.0 !
! ! ! A319 ! C ! 0.0 !
! ! ! A318 ! C ! 0.0 !
! ! ! ! ! !
! !5.9 ! TURBWAIT (sec.) A320 ! C ! 10 !
! ! ! A321 ! C ! 10 !
! ! ! A319 ! C ! 10 !
! ! ! A318 ! C ! 10 !
! ! ! ! ! !
! !5.10 ! FLAPL (deg) A320 ! C ! 0.5 !
! ! ! A321 ! C ! 0.5 !
! ! ! A319 ! C ! 0.5 !
! ! ! A318 ! C ! 0.5 !
!----!------!-----------------------------------------!------!---------!
!8100!8.1 !ACARS MU uplink request with IMI 'REQ15':! ! !
! ! !The report <15> is immediately generated ! ! !
! ! !and transmitted to the ACARS MU ! ! !
!----------------------------------------------------------------------!
! A = Programmable by Airbus !
! C = Programmable by Customer !
+----------------------------------------------------------------------+

(22) Load Report Logic
+----------------------------------------------------------------------+
!Code!Item ! !Progr.!Standard !
! No.!No. ! Description of Function Item !MCDU !Value or !
! ! ! !GSE !Table !
!----!------!-----------------------------------------!------!---------!
! !A ! Report Format ! ! !
! ! ! ! ! !
! !B ! Parameter Table ! ! !
! ! ! ! ! !
! !C ! First three lines of Report ! !Blank !
! ! ! ! ! !
! !D ! Print Out Rules ! C ! PH10 !
! ! ! (PH9,PH10, Immediately, Manually) ! ! !
! !E ! Transfer to ACARS MU (yes/no) ! C ! No !
! ! ! ! ! !
! !F ! Increment of the report counter (yes/no)! ! Yes !
! ! ! ! ! !
! !G ! Inhibit report triggers (yes/no) ! C ! No !
! ! ! ! ! !
! !H ! 'Y15.0' sec before land/event A320! C ! 1 !
! ! ! A321! C ! 1 !
! ! ! A319! C ! 1 !
! ! ! ! ! !
! !I ! 'Y15.1' sec before land/event A320! C ! 1 !
! ! ! A321! C ! 1 !
! ! ! A319! C ! 1 !
! ! ! ! ! !
! !J ! 'Y15.2' sec after land/event A320! C ! 3 !
! ! ! A321! C ! 3 !
! ! ! A319! C ! 3 !
! ! ! ! ! !
! !K ! 'Y15.3' sec before bounced A320! C ! 1 !
! ! ! A321! C ! 1 !
! ! ! A319! C ! 1 !
! ! ! ! ! !
! !L ! 'Y15.4' sec before bounced A320! C ! 1 !
! ! ! A321! C ! 1 !
! ! ! A319! C ! 1 !
! ! ! ! ! !
! !M ! 'Y15.5' sec after bounced A320! C ! 3 !
! ! ! A321! C ! 3 !
! ! ! A319! C ! 3 !
! ! ! ! ! !
! !N ! N dataset time (sample) at landing ! C ! 1 !
! ! ! to check for RALR trigger ! ! !
! ! ! Note: -N dataset time is programmable ! ! !
! ! ! from 0 to 5. ! ! !
! ! ! -1 sample is 1/16 second (16 Hz) ! ! !
!----!------!-----------------------------------------!------!---------!
!1000! ! Manual selection via MCDU ! ! !
!----!------!-----------------------------------------!------!---------!
!2000! ! Flight phase dependent manual selection ! ! !
! ! ! via remote print button if programmed. ! ! !
! ! ! Remote print button assignment ! ! !
!----!------!-----------------------------------------!------!---------!
!3000!3 ! Programmable Start Logic ! ! !
! !3.1 ! Logic algorithm ! ! !
! !3.2 ! Logic criteria values ! !not progr!
! ! ! ! ! !
! ! ! The parameters which are used for logic ! ! !
! ! ! items described as follows will be ! ! !
! ! ! observed with a rate of 16 Hz. ! ! !
! ! ! Exceptions: ! ! !
! ! ! At landing (0.5 sec before and 0.5 sec ! ! !
! ! ! after landing or bounce), the non- ! ! !
! ! ! filtered acceleration VRTA and the non- ! ! !
! ! ! filtered landing gear status (see to ! ! !
! ! ! item no. 4.7) will be observed with ! ! !
! ! ! a rate of 32 Hz. ! ! !
!----!------!-----------------------------------------!------!---------!
! !4 ! Report will be generated if one of the ! ! !
! ! ! following logic items is present during ! ! !
! ! ! landing: ! ! !
!4100! ! RALR < RALRL ! ! !
! ! ! calculated between Start Sample Number ! ! !
! ! ! S1 and Stop Sample Number S2 ! ! !
! ! ! or ! ! !
!4400! ! VRTA > VRTAL1.1 ! ! !
! ! ! (during +/- 0.5 seconds before and after! ! !
! ! ! landing) calculated between Start ! ! !
! ! ! Sample Number S3 and Stop Sample ! ! !
! ! ! Number S4 ! ! !
! ! ! or ! ! !
!4800! ! GW > GWL (at landing) and RALR < RALRLG ! ! !
! ! ! (at dataset time at landing (see item ! ! !
! ! ! no. L)). ! ! !
! ! ! The appropriate GW (GWL1, GWL2, GWL3 or ! ! !
! ! ! GWL4) will be taken depending if an ! ! !
! ! ! aircraft is equipped with or without ACT! ! !
! ! ! (Additional Center Tanks). ! ! !
! ! ! ! ! !
! ! ! Logic for ACT detection ! ! !
! ! ! ! ! !
! ! ! FWC 26.1.276.01 Bit 26 Bit 27 GW Limit! ! !
! ! ! 26.2.276.10 26 27 ! ! !
! ! ! 0 0 GWL1 ! ! !
! ! ! 1 0 GWL2 ! ! !
! ! ! 0 1 GWL3 ! ! !
! ! ! 1 1 GWL4 ! ! !
! ! ! ! ! !
! ! ! or ! ! !
! ! ! ! ! !
!4900! ! GW > GWL (at landing) and VRTA > VRTALG ! ! !
! ! ! (during +/- 0.5 sec before and after ! ! !
! ! ! landing). ! ! !
! ! ! The appropriate GW (GWL1, GWL2, GWL3 or ! ! !
! ! ! GWL4) will be taken depending if an ! ! !
! ! ! aircraft is equipped with or without ACT! ! !
! ! ! (Additional Center Tanks). Logic for ACT! ! !
! ! ! detection like Code No. 4800. ! ! !
! ! ! ! ! !
!4500! ! Report will be generated if one of the ! ! !
! ! ! following logic items is present during ! ! !
! ! ! the bouncing: ! ! !
! ! ! ! ! !
! ! ! VRTA > VRTAL1.2 during +/- 0.5 sec at ! ! !
! ! ! landing (1st touchdown) ! ! !
! ! ! ! ! !
! ! ! or ! ! !
! ! ! ! ! !
! ! ! VRTA > VRTAL1.3 during +/- 0.5 sec at ! ! !
! ! ! bouncing (2nd touchdown). ! ! !
!----!------!-----------------------------------------!------!---------!
! !4.1 ! RALRL limit (ft/sec) A320 ! C ! -9.0 !
! ! ! A321 ! C ! -9.0 !
! ! ! A319 ! C ! -9.0 !
! !4.2 ! RALT ! ! !
! !4.2.1 ! RALTL1 limit (ft) A320 ! C ! 150.0 !
! ! ! A321 ! C ! 150.0 !
! ! ! A319 ! C ! 150.0 !
! !4.3 ! RALR ! ! !
! !4.3.1 ! D geometrical correction factor for ! ! !
! ! ! ROLR (ft/deg) A320 ! C ! 0.0 !
! ! ! A321 ! C ! 0.0 !
! ! ! A319 ! C ! 0.0 !
! !4.3.2 ! DX lever arm correction (x-axis) ! ! !
! ! ! for R/A RALT (ft) A320 ! C ! 18.0 !
! ! ! A321 ! C ! 28.8 !
! ! ! A319 ! C ! 18.5 !
! !4.3.3 ! DZ lever arm correction (z-axis) ! ! !
! ! ! for R/A RALT (ft) A320 ! C ! 7.1 !
! ! ! A321 ! C ! 7.8 !
! ! ! A319 ! C ! 7.2 !
! !4.3.4 ! DXTPIR lever arm correction (x-axis) ! ! !
! ! ! for PTCH (ft) A320 ! C ! 39.0 !
! ! ! A321 ! C ! 53.1 !
! ! ! A319 ! C ! 33.8 !
! ! ! ! ! !
! !4.3.5 ! FC filter frequency (Hz) A320 ! C ! 0.3 !
! ! ! A321 ! C ! 0.3 !
! ! ! A319 ! C ! 0.3 !
! ! ! ! ! !
! !4.3.6 ! K1 filter constant A320 ! C ! 5.2 !
! ! ! A321 ! C ! 5.2 !
! ! ! A319 ! C ! 5.2 !
! ! ! ! ! !
! !4.3.7 ! K2 filter constant A320 ! C ! 25.0 !
! ! ! A321 ! C ! 25.0 !
! ! ! A319 ! C ! 25.0 !
! ! ! ! ! !
! !4.3.8 ! K3 filter constant A320 ! C ! 5.0 !
! ! ! A321 ! C ! 5.0 !
! ! ! A319 ! C ! 5.0 !
! ! ! ! ! !
! !4.3.9 ! THETA0 (deg) A320 ! C ! 6.0 !
! ! ! A321 ! C ! 4.5 !
! ! ! A319 ! C ! 2.0 !
! ! ! ! ! !
! !4.3.10! S1 (sample) A320 ! C ! -4.0 !
! ! ! A321 ! C ! -4.0 !
! ! ! A319 ! C ! -4.0 !
! ! ! ! ! !
! !4.3.11! S2 (sample) A320 ! C ! 4.0 !
! ! ! A321 ! C ! 4.0 !
! ! ! A319 ! C ! 4.0 !
! ! ! ! ! !
! !4.4 ! VRTAL1.1 limit at landing (g) A320 ! C ! 2.6 !
! ! ! A321 ! C ! 2.6 !
! ! ! A319 ! C ! 2.6 !
! ! ! ! ! !
! !4.4.1 ! S3 (sample) A320 ! C ! -16 !
! ! ! A321 ! C ! -16 !
! ! ! A319 ! C ! -16 !
! ! ! ! ! !
! !4.4.2 ! S4 (sample) A320 ! C ! 16 !
! ! ! A321 ! C ! 16 !
! ! ! A319 ! C ! 16 !
! ! ! ! ! !
! !4.5 ! VRTAL1.2 limit at landing (1st touchdown! ! !
! ! ! ) from bounced land/event (g) A320 ! C ! 2.6 !
! ! ! A321 ! C ! 2.6 !
! ! ! A319 ! C ! 2.6 !
! ! ! ! ! !
! !4.5.1 ! VRTAL1.3 limit at bounce (2nd touchdown)! ! !
! ! ! from bounced land/event (g) A320 ! C ! 2.6 !
! ! ! A321 ! C ! 2.6 !
! ! ! A319 ! C ! 2.6 !
! !4.6 ! GW Overweight landing ! ! !
! !4.6.1 ! GWL1,GWL2,GWL3,GWL4 limit (kg) A320 ! C ! 64500 !
! ! ! A321 ! C ! 73500 !
! ! ! A319 ! C ! 61000 !
! ! ! ! ! !
! ! ! NOTE: The standard GWL value stored ! ! !
! ! ! in the DMU is not always in line with ! ! !
! ! ! the MLW. We recommend to set the GWL ! ! !
! ! ! value in line with the MLW (Ref: AMM ! ! !
! ! ! 31-36-00). ! ! !
! ! !
! !4.6.2 ! RALRLG limit (ft/sec) A320 ! C ! -6.0 !
! ! ! A321 ! C ! -6.0 !
! ! ! A319 ! C ! -6.0 !
! ! ! ! ! !
! !4.6.3 ! VRTALG limit (g) A320 ! C ! 1.7 !
! ! ! A321 ! C ! 1.7 !
! ! ! A319 ! C ! 1.7 !
! ! ! ! ! !
! !4.7 ! Landing detection ! ! !
! ! ! Landing is detected when in PH7 or PH8 ! ! !
! ! ! 6D.1.021.01 Bit 13 = 1 (LH gear) ! ! !
! ! ! or ! ! !
! ! ! 6D.1.021.01 Bit 14 = 1 (RH gear) ! ! !
! ! ! ! ! !
! !4.8 ! Bounced landing detection ! ! !
! ! ! A bounced landing is detected when in ! ! !
! ! ! PH7 or PH8 parameter 6D.1.021.01 Bit 11 ! ! !
! ! ! is set to 1 for longer than 'Y15.5' ! ! !
! ! ! seconds and ! ! !
! ! ! then one or both of 6D.1.021.01 Bit 13 ! ! !
! ! ! or Bit 14 is set to 0 for longer than ! ! !
! ! ! 'Y15.6' seconds and ! ! !
! ! ! then the one which was set to 0 or the ! ! !
! ! ! first one of 6D.1.021.01 Bit 13 or ! ! !
! ! ! Bit 14 is set to 1 again within 'Y15.7' ! ! !
! ! ! seconds. ! ! !
! ! ! ! ! !
! !4.9 ! 'Y15.5' landing gear compress time ! ! !
! ! ! (1st touchdown) (sample) A320 ! ! 16 !
! ! ! A321 ! ! 16 !
! ! ! A319 ! ! 16 !
! ! ! ! ! !
! !4.10 ! 'Y15.6' time between bounces (sample) ! ! !
! ! ! A320 ! ! 32 !
! ! ! A321 ! ! 32 !
! ! ! A319 ! ! 32 !
! ! ! ! ! !
! !4.11 ! 'Y15.7' landing gear compress time ! ! !
! ! ! (2nd touchdown) (sample) A320 ! ! 320 !
! ! ! A321 ! ! 320 !
! ! ! A319 ! ! 320 !
! ! ! Note: -1 sample is 1/32 second (32 Hz) ! ! !
!----!------!-----------------------------------------!------!---------!
! !5 ! Report will be generated if one of the ! ! !
! ! ! flight (PH5, 5.1, 6, 7, 7.1). There ! ! !
! ! ! will be a spacing time TURBWAIT (sec) ! ! !
! ! ! to enable the trigger logic again after ! ! !
! ! ! the previous report generation. ! ! !
! ! ! ! ! !
!5100!5.1 ! VRTA > VRTAL2.1 if FLAPL < 0.5 deg ! ! !
! ! ! ! ! !
!5200!5.2 ! VRTA < VRTAL2.2 if FLAPL < 0.5 deg ! ! !
! ! ! ! ! !
!5300!5.3 ! VRTA > VRTAL2.3 if FLAPL >/= 0.5 deg or ! ! !
! ! ! VRTA < VRTAL2.4 if FLAPL >/= 0.5 deg ! ! !
! ! ! ! ! !
! ! ! Limitation for Code 5100, 5200, 5300: ! ! !
! ! ! W15 TURBWAIT spacing time for re- ! ! !
! ! ! activating the trigger logic after the ! ! !
! ! ! previous report generation within the ! ! !
! ! ! same flight leg. ! ! !
! ! ! ! ! !
!5400!5.4 ! If one of the 5 spoiler excursion ! ! !
! ! ! counters has an overflow (999 is ! ! !
! ! ! reached). ! ! !
! ! ! ! ! !
! !5.5 ! VRTAL2.1 limit (g) A320 ! C ! 2.5 !
! ! ! A321 ! C ! 2.5 !
! ! ! A319 ! C ! 2.5 !
! ! ! ! ! !
! !5.6 ! VRTAL2.2 limit (g) A320 ! C ! -1.0 !
! ! ! A321 ! C ! -1.0 !
! ! ! A319 ! C ! -1.0 !
! ! ! ! ! !
! !5.7 ! VRTAL2.3 limit (g) A320 ! C ! 2.0 !
! ! ! A321 ! C ! 2.0 !
! ! ! A319 ! C ! 2.0 !
! ! ! ! ! !
! !5.8 ! VRTAL2.4 limit (g) A320 ! C ! 0.0 !
! ! ! A321 ! C ! 0.0 !
! ! ! A319 ! C ! 0.0 !
! ! ! ! ! !
! !5.9 ! TURBWAIT (sec.) A320 ! C ! 10 !
! ! ! A321 ! C ! 10 !
! ! ! A319 ! C ! 10 !
! ! ! ! ! !
! !5.10 ! FLAPL (deg) A320 ! C ! 0.5 !
! ! ! A321 ! C ! 0.5 !
! ! ! A319 ! C ! 0.5 !
!----------------------------------------------------------------------!
! A = Programmable by Airbus !
! C = Programmable by Customer !
+----------------------------------------------------------------------+

(23) Load Report Logic <15>
+----------------------------------------------------------------------+
!Code!Item ! !Progr.!Standard !
! No.!No. ! Description of Function Item !MCDU !Value or !
! ! ! !GSE !Table !
!----!------!-----------------------------------------!------!---------!
! !A ! Report Format ! ! !
! ! ! ! ! !
! !B ! Parameter Table ! ! !
! ! ! ! ! !
! !C ! First three lines of Report ! ! Blank !
! ! ! ! ! !
! !D ! Print Out Rules ! C ! PH10 see!
! ! ! (PH9,PH10, Immediately, Manually) ! ! separate!
! ! ! ! ! list !
! !E ! Transfer to ACARS MU (yes/no) ! C ! see !
! ! ! ! ! separate!
! ! ! ! ! list !
! !F ! Increment of the report counter (yes/no)! C ! Yes !
! ! ! ! ! !
! !G ! Inhibit report triggers (yes/no) ! C ! No !
! ! ! ! ! !
! !H ! 'Y15.0' sec before land/event A320! C ! 1 !
! ! ! A321! C ! 1 !
! ! ! A319! C ! 1 !
! ! ! A318! C ! 1 !
! ! ! ! ! !
! !I ! 'Y15.1' sec before land/event A320! C ! 1 !
! ! ! A321! C ! 1 !
! ! ! A319! C ! 1 !
! ! ! A318! C ! 1 !
! ! ! ! ! !
! !J ! 'Y15.2' sec after land/event A320! C ! 3 !
! ! ! A321! C ! 3 !
! ! ! A319! C ! 3 !
! ! ! A318! C ! 3 !
! ! ! ! ! !
! !K ! 'Y15.3' sec before bounced A320! C ! 1 !
! ! ! A321! C ! 1 !
! ! ! A319! C ! 1 !
! ! ! A318! C ! 1 !
! ! ! ! ! !
! !L ! 'Y15.4' sec before bounced A320! C ! 1 !
! ! ! A321! C ! 1 !
! ! ! A319! C ! 1 !
! ! ! A318! C ! 1 !
! ! ! ! ! !
! !M ! 'Y15.5' sec after bounced A320! C ! 3 !
! ! ! A321! C ! 3 !
! ! ! A319! C ! 3 !
! ! ! A318! C ! 3 !
! ! ! ! ! !
! !N ! N dataset time (sample) at landing ! C ! 1 !
! ! ! to check for RALR trigger ! ! !
! ! ! Note: -N dataset time is programmable ! ! !
! ! ! from 0 to 5. ! ! !
! ! ! -1 sample is 1/16 second (16 Hz) ! ! !
!----!------!-----------------------------------------!------!---------!
!1000! ! Not applicable ! ! !
!----!------!-----------------------------------------!------!---------!
!2000! ! Not applicable ! ! !
!----!------!-----------------------------------------!------!---------!
!3000!3 ! Programmable Start Logic ! ! !
! !3.1 ! Logic algorithm ! ! !
! !3.2 ! Logic criteria values ! !not prog.!
!----!------!-----------------------------------------!------!---------!
! ! ! The parameters which are used for logic ! ! !
! ! ! items described as follows shall be ! ! !
! ! ! observed with a rate of 16 Hz. ! ! !
! ! ! Exceptions: ! ! !
! ! ! At landing (0.5 sec before and 0.5 sec ! ! !
! ! ! after landing or bounce), the non- ! ! !
! ! ! filtered acceleration VRTA and the non- ! ! !
! ! ! filtered landing gear status (see to ! ! !
! ! ! item no. 4.7) shall be observed with ! ! !
! ! ! a rate of 32 Hz. ! ! !
!----!------!-----------------------------------------!------!---------!
! !4 ! Report is generated if one of the ! ! !
! ! ! following logic items is present during ! ! !
! ! ! landing: ! ! !
!4100! ! RALR < RALRL ! ! !
! ! ! calculated between Start Sample Number ! ! !
! ! ! S1 and Stop Sample Number S2 ! ! !
! ! ! or ! ! !
!4400! ! VRTA > VRTAL1.1 ! ! !
! ! ! (during +/- 0.5 seconds before and after! ! !
! ! ! landing) calculated between Start ! ! !
! ! ! Sample Number S3 and Stop Sample ! ! !
! ! ! Number S4 ! ! !
! ! ! or ! ! !
!4800! ! GW > GWL (at landing) and RALR < RALRLG ! ! !
! ! ! (at dataset time at landing (see item ! ! !
! ! ! no. L)). ! ! !
! ! ! The appropriate GW (GWL1, GWL2, GWL3 or ! ! !
! ! ! GWL4) is taken depending on if an ! ! !
! ! ! aircraft is equipped with or without ACT! ! !
! ! ! (Additional Center Tanks). ! ! !
! ! ! ! ! !
! ! ! Logic for ACT detection ! ! !
! ! ! GW ! ! !
! ! ! FWC 26.1.276.01.26 26.1.276.01.27 Limit! ! !
! ! ! 26.1.276.10.26 26.1.276.10.27 ! ! !
! ! ! ! ! !
! ! ! 0 0 GWL1 ! ! !
! ! ! 1 0 GWL2 ! ! !
! ! ! 0 1 GWL3 ! ! !
! ! ! 1 1 GWL4 ! ! !
! ! ! ! ! !
! ! ! or ! ! !
! ! ! ! ! !
!4900! ! GW > GWL (at landing) and VRTA > VRTALG ! ! !
! ! ! (during +/- 0.5 sec before and after ! ! !
! ! ! landing). ! ! !
! ! ! The appropriate GW (GWL1, GWL2, GWL3 or ! ! !
! ! ! GWL4) is taken depending on if an ! ! !
! ! ! aircraft is equipped with or without ACT! ! !
! ! ! (Additional Center Tanks). Logic for ACT! ! !
! ! ! detection like Code No. 4800. ! ! !
! ! ! ! ! !
!4500! ! Report will be generated if one of the ! ! !
! ! ! following logic items is present during ! ! !
! ! ! the bouncing: ! ! !
! ! ! ! ! !
! ! ! VRTA > VRTAL1.2 during +/- 0.5 sec at ! ! !
! ! ! landing (1st touchdown) ! ! !
! ! ! ! ! !
! ! ! or ! ! !
! ! ! ! ! !
! ! ! VRTA > VRTAL1.3 during +/- 0.5 sec at ! ! !
! ! ! landing (2nd touchdown). ! ! !
!----!------!-----------------------------------------!------!---------!
! !4.1 ! RALRL limit (ft/sec) A320 ! C ! -9.0 !
! ! ! A321 ! C ! -9.0 !
! ! ! A319 ! C ! -9.0 !
! ! ! A318 ! C ! -9.0 !
! !4.2 ! RALT ! ! !
! !4.2.1 ! RALTL1 limit ft| A320 ! C ! 150.0 !
! ! ! A321 ! C ! 150.0 !
! ! ! A319 ! C ! 150.0 !
! ! ! A318 ! C ! 150.0 !
! !4.3 ! RALR ! ! !
! !4.3.1 ! D geometrical correction factor for ! ! !
! ! ! ROLR (ft/deg) A320 ! C ! 0.0 !
! ! ! A321 ! C ! 0.0 !
! ! ! A319 ! C ! 0.0 !
! ! ! A318 ! C ! 0.0 !
! !4.3.2 ! DX lever arm correction (x-axis) ! ! !
! ! ! for R/A RALT (ft) A320 ! C ! 18.0 !
! ! ! A321 ! C ! 28.8 !
! ! ! A319 ! C ! 18.5 !
! ! ! A318 ! C ! 16.8 !
! !4.3.3 ! DZ lever arm correction (z-axis) ! ! !
! ! ! for R/A RALT (ft) A320 ! C ! 7.1 !
! ! ! A321 ! C ! 7.8 !
! ! ! A319 ! C ! 7.2 !
! ! ! A318 ! C ! 7.6 !
! !4.3.4 ! DXTPIR lever arm correction (x-axis) ! ! !
! ! ! for PTCH (ft) A320 ! C ! 39.0 !
! ! ! A321 ! C ! 53.1 !
! ! ! A319 ! C ! 33.8 !
! ! ! A318 ! C ! 29.5 !
! ! ! ! ! !
! !4.3.5 ! FC filter frequency (Hz) A320 ! C ! 0.3 !
! ! ! A321 ! C ! 0.3 !
! ! ! A319 ! C ! 0.3 !
! ! ! A318 ! C ! 0.3 !
! ! ! ! ! !
! !4.3.6 ! K1 filter constant A320 ! C ! 5.2 !
! ! ! A321 ! C ! 5.2 !
! ! ! A319 ! C ! 5.2 !
! ! ! A318 ! C ! 5.2 !
! ! ! ! ! !
! !4.3.7 ! K2 filter constant A320 ! C ! 25.0 !
! ! ! A321 ! C ! 25.0 !
! ! ! A319 ! C ! 25.0 !
! ! ! A318 ! C ! 25.0 !
! ! ! ! ! !
! !4.3.8 ! K3 filter constant A320 ! C ! 5.0 !
! ! ! A321 ! C ! 5.0 !
! ! ! A319 ! C ! 5.0 !
! ! ! A318 ! C ! 5.0 !
! ! ! ! ! !
! !4.3.9 ! THETA0 (averaged pitch at A320 ! C ! 6.0 !
! ! ! touchdown) deg A321 ! C ! 4.5 !
! ! ! A319 ! C ! 2.0 !
! ! ! A318 ! C ! 6.0 !
! ! ! ! ! !
! !4.3.10! S1 (sample) A320 ! C ! -4.0 !
! ! ! A321 ! C ! -4.0 !
! ! ! A319 ! C ! -4.0 !
! ! ! A318 ! C ! -4.0 !
! ! ! ! ! !
! !4.3.11! S2 (sample) A320 ! C ! 4.0 !
! ! ! A321 ! C ! 4.0 !
! ! ! A319 ! C ! 4.0 !
! ! ! A318 ! C ! 4.0 !
! ! ! ! ! !
! !4.4 ! VRTAL1.1 limit at landing (g) A320 ! C ! 2.6 !
! ! ! A321 ! C ! 2.6 !
! ! ! A319 ! C ! 2.6 !
! ! ! A318 ! C ! 2.6 !
! ! ! ! ! !
! !4.4.1 ! S3 (sample) A320 ! C ! -16 !
! ! ! A321 ! C ! -16 !
! ! ! A319 ! C ! -16 !
! ! ! A318 ! C ! -16 !
! ! ! ! ! !
! !4.4.2 ! S4 (sample) A320 ! C ! 16 !
! ! ! A321 ! C ! 16 !
! ! ! A319 ! C ! 16 !
! ! ! A318 ! C ! 16 !
! ! ! ! ! !
! !4.5 ! VRTAL1.2 limit at landing (1st touchdown! ! !
! ! ! ) from bounced land/event (g) A320 ! C ! 2.6 !
! ! ! A321 ! C ! 2.6 !
! ! ! A319 ! C ! 2.6 !
! ! ! A318 ! C ! 2.6 !
! ! ! ! ! !
! !4.5.1 ! VRTAL1.3 limit at bounce (2nd touchdown)! ! !
! ! ! from bounced land/event (g) A320 ! C ! 2.6 !
! ! ! A321 ! C ! 2.6 !
! ! ! A319 ! C ! 2.6 !
! ! ! A318 ! C ! 2.6 !
! !4.6 ! GW Overweight landing ! ! !
! !4.6.1 ! GWL1, GWL2, GWL3, GWL4 limit (kg) A320 ! C ! 64500 !
! ! ! A321 ! C ! 75500 !
! ! ! A319 ! C ! 61000 !
! ! ! A318 ! C ! 56000 !
! ! ! NOTE: The standard GWL value stored ! ! !
! ! ! in the DMU is not always in line with ! ! !
! ! ! the MLW. We recommend to set the GWL ! ! !
! ! ! value in line with the MLW (Ref: AMM ! ! !
! ! ! 31-36-00). ! ! !
! ! ! ! ! !
! !4.6.2 ! RALRLG limit (ft/sec) A320 ! C ! -6.0 !
! ! ! A321 ! C ! -6.0 !
! ! ! A319 ! C ! -6.0 !
! ! ! A318 ! C ! -6.0 !
! ! ! ! ! !
! !4.6.3 ! VRTALG limit (g) A320 ! C ! 1.7 !
! ! ! A321 ! C ! 1.7 !
! ! ! A319 ! C ! 1.7 !
! ! ! A318 ! C ! 1.7 !
! ! ! ! ! !
! !4.7 ! Landing detection ! ! !
! ! ! Landing is detected when in PH7 or PH8 ! ! !
! ! ! 6D.1.021.01.13 = 1 (LH gear) ! ! !
! ! ! or ! ! !
! ! ! 6D.1.021.01.14 = 1 (RH gear) ! ! !
! ! ! ! ! !
! !4.8 ! Bounced landing detection ! ! !
! ! ! A bounced landing is detected when in ! ! !
! ! ! PH7 or PH8 parameter 6D.1.021.01.11 is ! ! !
! ! ! set to 1 for longer than 'Y15.6'*(1/32) ! ! !
! ! ! seconds ! ! !
! ! ! and ! ! !
! ! ! then one or both of 6D.1.021.01.13 or ! ! !
! ! ! 6D.1.021.01.14 is set to 0 for longer ! ! !
! ! ! than 'Y15.7'*(1/32) seconds ! ! !
! ! ! and ! ! !
! ! ! then the one which was set to 0 or the ! ! !
! ! ! first one of 6D.1.021.01.13 or ! ! !
! ! ! 6D.1.021.01.14 is set to 1 again within ! ! !
! ! ! within 'Y15.8'*(1/32) seconds. ! ! !
! ! ! ! ! !
! !4.9 ! 'Y15.6' landing gear compress time ! ! !
! ! ! (1st touchdown) (sample) A320 ! ! 16 !
! ! ! A321 ! ! 16 !
! ! ! A319 ! ! 16 !
! ! ! A318 ! ! 16 !
! ! ! ! ! !
! !4.10 ! 'Y15.7' time between bounces (sample) ! ! !
! ! ! A320 ! ! 32 !
! ! ! A321 ! ! 32 !
! ! ! A319 ! ! 32 !
! ! ! A318 ! ! 32 !
! ! ! ! ! !
! !4.11 ! 'Y15.8' landing gear compress time ! ! !
! ! ! (2nd touchdown) (sample) A320 ! ! 320 !
! ! ! A321 ! ! 320 !
! ! ! A319 ! ! 320 !
! ! ! A318 ! ! 320 !
! ! ! NOTE: 1 sample is 1/32 second (32 Hz) ! ! !
!----!------!-----------------------------------------!------!---------!
! !5 ! Report is generated if one of the ! ! !
! ! ! following logic items is present during ! ! !
! ! ! flight (PH5, 5.1, 6, 7, 7.1). There is a! ! !
! ! ! spacing time TURBWAIT sec. to enable the! ! !
! ! ! trigger logic again after the previous ! ! !
! ! ! report generation. ! ! !
! ! ! ! ! !
!5100!5.1 ! VRTA > VRTAL2.1 if FLAP < FLAPL ! ! !
! ! ! ! ! !
!5200!5.2 ! VRTA < VRTAL2.2 if FLAP < FLAPL ! ! !
! ! ! ! ! !
!5300!5.3 ! VRTA > VRTAL2.3 if FLAP >= FLAPL OR ! ! !
! ! ! VRTA < VRTAL2.4 if FLAP >= FLAPL ! ! !
! ! ! ! ! !
! ! ! Limitation for Code 5100, 5200, 5300: ! ! !
! ! ! W15 TURBWAIT spacing time for re- ! ! !
! ! ! activating the trigger logic after the ! ! !
! ! ! previous report generation within the ! ! !
! ! ! same flight leg. ! ! !
! ! ! ! ! !
!5400!5.4 ! If one of the 5 spoiler excursion ! ! !
! ! ! counters has an overflow (999 is ! ! !
! ! ! reached). ! ! !
! ! ! ! ! !
! !5.5 ! VRTAL2.1 limit (g) A320 ! C ! 2.5 !
! ! ! A321 ! C ! 2.5 !
! ! ! A319 ! C ! 2.5 !
! ! ! A318 ! C ! 2.5 !
! ! ! ! ! !
! !5.6 ! VRTAL2.2 limit (g) A320 ! C ! -1.0 !
! ! ! A321 ! C ! -1.0 !
! ! ! A319 ! C ! -1.0 !
! ! ! A318 ! C ! -1.0 !
! ! ! ! ! !
! !5.7 ! VRTAL2.3 limit (g) A320 ! C ! 2.0 !
! ! ! A321 ! C ! 2.0 !
! ! ! A319 ! C ! 2.0 !
! ! ! A318 ! C ! 2.0 !
! ! ! ! ! !
! !5.8 ! VRTAL2.4 limit (g) A320 ! C ! 0.0 !
! ! ! A321 ! C ! 0.0 !
! ! ! A319 ! C ! 0.0 !
! ! ! A318 ! C ! 0.0 !
! ! ! ! ! !
! !5.9 ! TURBWAIT (sec.) A320 ! C ! 10 !
! ! ! A321 ! C ! 10 !
! ! ! A319 ! C ! 10 !
! ! ! A318 ! C ! 10 !
! ! ! ! ! !
! !5.10 ! FLAPL (deg) A320 ! C ! 0.5 !
! ! ! A321 ! C ! 0.5 !
! ! ! A319 ! C ! 0.5 !
! ! ! A318 ! C ! 0.5 !
!----------------------------------------------------------------------!
! A = Programmable by Airbus !
! C = Programmable by Customer !
+----------------------------------------------------------------------+

(24) Load Report Logic
+-------------------------------------------------------------------------+
!Code!Item ! ! Progr. !Standard !
!No. !No. ! Description of Function Item !GSE !MCDU!Value or !
! ! ! ! ! !Table TXY!
!----!------!-----------------------------------------!----!----!---------!
! !A ! Report Format ! ! ! !
! ! ! ! ! ! !
! !A.1 ! 'R015RLID' Report Layout Identifier ! ! ! DT37 !
! ! ! (for ACARS header) ! ! ! !
! ! ! ! ! ! !
! !A.2 ! 'R015RLIS' Report Layout Issue ! ! ! DT37 !
! ! ! (for ACARS header) ! ! ! !
! ! ! ! ! ! !
! !B ! Parameter Table ! ! ! !
! ! ! ! ! ! !
! !C ! First three lines of Report ! C ! ! Blank !
! ! ! ! ! ! !
! !D ! Print Out Rules ! C ! C !PH10 see !
! ! ! (PH9, PH10, Immediately, Manually) ! ! !separate !
! ! ! ! ! !list !
! !E ! Transfer to ACARS MU (yes/no)! C ! C !see !
! ! ! ! ! !separate !
! ! ! ! ! !list !
! !F ! Increment of the report counter (yes/no)! C ! C !Yes !
! ! ! ! ! ! !
! !G ! Inhibit report triggers (yes/no)! C ! C !No !
! ! ! ! ! ! !
! !H ! 'Y15.0' sec before land/event A320! C ! C ! 1 !
! ! ! A321! C ! C ! 1 !
! ! ! A319! C ! C ! 1 !
! ! ! A318! C ! C ! 1 !
! ! ! ! ! ! !
! !I ! 'Y15.1' sec before land/event A320! C ! C ! 1 !
! ! ! A321! C ! C ! 1 !
! ! ! A319! C ! C ! 1 !
! ! ! A318! C ! C ! 1 !
! ! ! ! ! ! !
! !J ! 'Y15.2' sec after land/event A320! C ! C ! 3 !
! ! ! A321! C ! C ! 3 !
! ! ! A319! C ! C ! 3 !
! ! ! A318! C ! C ! 3 !
! ! ! ! ! ! !
! !K ! 'Y15.3' sec before bounced A320! C ! C ! 1 !
! ! ! A321! C ! C ! 1 !
! ! ! A319! C ! C ! 1 !
! ! ! A318! C ! C ! 1 !
! ! ! ! ! ! !
! !L ! 'Y15.4' sec before bounced A320! C ! C ! 1 !
! ! ! A321! C ! C ! 1 !
! ! ! A319! C ! C ! 1 !
! ! ! A318! C ! C ! 1 !
! ! ! ! ! ! !
! !M ! 'Y15.5' sec after bounced A320! C ! C ! 3 !
! ! ! A321! C ! C ! 3 !
! ! ! A319! C ! C ! 3 !
! ! ! A318! C ! C ! 3 !
! ! ! ! ! ! !
! !N ! N dataset time (sample) at landing ! C ! C ! 1 !
! ! ! to check for RALR trigger (RALRCHK) ! ! ! !
! ! ! Note: -N dataset time is programmable ! ! ! !
! ! ! from 0 to 5 ! ! ! !
! ! ! -1 sample is 1/16 second (16 Hz). ! ! ! !
!----!------!-----------------------------------------!----!----!---------!
!1000! ! Not applicable ! ! ! !
!----!------!-----------------------------------------!----!----!---------!
!2000! ! Not applicable ! ! ! !
!----!------!-----------------------------------------!----!----!---------!
!3000!3 ! Programmable Start Logic ! ! ! !
! !3.1 ! Logic algorithm ! ! ! !
! !3.2 ! Logic criteria values ! ! ! not !
! ! ! ! ! ! prog. !
!----!------!-----------------------------------------!----!----!---------!
! ! ! The parameters which are used for the ! ! ! !
! ! ! logic items described as follows are ! ! ! !
! ! ! observed at a rate of 16 Hz. ! ! ! !
! ! ! Exceptions: ! ! ! !
! ! ! At landing (0.5 sec before and 0.5 sec ! ! ! !
! ! ! after landing or bounce), the non- ! ! ! !
! ! ! filtered acceleration VRTA and the non- ! ! ! !
! ! ! filtered landing gear status (see to ! ! ! !
! ! ! item no. 4.7) are observed at a rate of ! ! ! !
! ! ! 32 Hz. ! ! ! !
!----!------!-----------------------------------------!----!----!---------!
! !4 ! Report is generated if one of the ! ! ! !
! ! ! following logic items is present during ! ! ! !
! ! ! landing: ! ! ! !
!4100! ! RALR < RALRL ! ! ! !
! ! ! calculated between Start Sample Number ! ! ! !
! ! ! S1 and Stop Sample Number S2 ! ! ! !
! ! ! or ! ! ! !
!4400! ! VRTA > VRTAL1.1 ! ! ! !
! ! ! (during +/- 0.5 seconds before and after! ! ! !
! ! ! landing) calculated between Start ! ! ! !
! ! ! Sample Number S3 and Stop Sample ! ! ! !
! ! ! Number S4 ! ! ! !
! ! ! or ! ! ! !
!4800! ! GW > GWL (at landing) and RALR > RALRLG ! ! ! !
! ! ! (at dataset time at landing) (see item ! ! ! !
! ! ! no. L). ! ! ! !
! ! ! The appropriate GW (GWL1, GWL2, GWL3 or ! ! ! !
! ! ! GWL4) is processed if an aircraft ! ! ! !
! ! ! is equipped with or without ACT ! ! ! !
! ! ! (Additional Center Tanks). ! ! ! !
! ! ! ! ! ! !
! ! ! Logic for ACT detection ! ! ! !
! ! ! ! ! ! !
! ! ! FWC 26.1.276.01.26 26.1.276.01.27 GW ! ! ! !
! ! ! 26.2.276.10.26 26.2.276.10.27 Limit! ! ! !
! ! ! 0 0 GWL1 ! ! ! !
! ! ! 1 0 GWL2 ! ! ! !
! ! ! 0 1 GWL3 ! ! ! !
! ! ! 1 1 GWL4 ! ! ! !
! ! ! or ! ! ! !
!4900! ! GW > GWL (at landing) and VRTA > VRTALG ! ! ! !
! ! ! (during +/- 0.5 sec before and after ! ! ! !
! ! ! landing). ! ! ! !
! ! ! The appropriate GW (GWL1, GWL2, GWL3 or ! ! ! !
! ! ! GWL4) is processed if an ! ! ! !
! ! ! aircraft is equipped with or without ACT! ! ! !
! ! ! (Additional Center Tanks). Logic for ACT! ! ! !
! ! ! detection like Code No. 4800. ! ! ! !
! ! ! ! ! ! !
!4500! ! Report is generated if one of the ! ! ! !
! ! ! subsequent logic items is present ! ! ! !
! ! ! during the bouncing: ! ! ! !
! ! ! ! ! ! !
! ! ! VRTA > VRTAL1.2 during +/- 0.5 sec at ! ! ! !
! ! ! landing (1st touchdown) ! ! ! !
! ! ! or ! ! ! !
! ! ! VRTA > VRTAL1.3 during +/- 0.5 sec at ! ! ! !
! ! ! landing (2nd touchdown). ! ! ! !
!----!------!-----------------------------------------!----!----!---------!
! !4.1 ! RALRL limit [ft/sec] A320 ! C ! C ! -9.0 !
! ! ! A321 ! C ! C ! -9.0 !
! ! ! A319 ! C ! C ! -9.0 !
! ! ! A318 ! C ! C ! -9.0 !
! !4.2 ! RALT ! ! ! !
! !4.2.1 ! RALTL1 limit [ft] A320 ! C ! C ! 150.0 !
! ! ! A321 ! C ! C ! 150.0 !
! ! ! A319 ! C ! C ! 150.0 !
! ! ! A318 ! C ! C ! 150.0 !
! !4.3 ! RALR ! ! ! !
! !4.3.1 ! D geometrical correction factor for ! ! ! !
! ! ! ROLR [ft/deg] A320 ! C ! C ! 0.0 !
! ! ! A321 ! C ! C ! 0.0 !
! ! ! A319 ! C ! C ! 0.0 !
! ! ! A318 ! C ! C ! 0.0 !
! !4.3.2 ! DX lever arm correction (x-axis) ! ! ! !
! ! ! for R/A RALT [ft] A320 ! C ! C ! 18.0 !
! ! ! A321 ! C ! C ! 28.8 !
! ! ! A319 ! C ! C ! 18.5 !
! ! ! A318 ! C ! C ! 16.8 !
! !4.3.3 ! DZ lever arm correction (z-axis) ! ! ! !
! ! ! for R/A RALT [ft] A320 ! C ! C ! 7.1 !
! ! ! A321 ! C ! C ! 7.8 !
! ! ! A319 ! C ! C ! 7.2 !
! ! ! A318 ! C ! C ! 7.6 !
! !4.3.4 ! DXTPIR lever arm correction (x-axis) ! ! ! !
! ! ! for PTCH [ft] A320 ! C ! C ! 39.0 !
! ! ! A321 ! C ! C ! 53.1 !
! ! ! A319 ! C ! C ! 33.8 !
! ! ! A318 ! C ! C ! 29.5 !
! ! ! ! ! ! !
! !4.3.5 ! FC filter frequency [Hz] A320 ! C ! C ! 0.3 !
! ! ! A321 ! C ! C ! 0.3 !
! ! ! A319 ! C ! C ! 0.3 !
! ! ! A318 ! C ! C ! 0.3 !
! ! ! ! ! ! !
! !4.3.6 ! K1 filter constant A320 ! C ! C ! 5.2 !
! ! ! A321 ! C ! C ! 5.2 !
! ! ! A319 ! C ! C ! 5.2 !
! ! ! A318 ! C ! C ! 5.2 !
! ! ! ! ! ! !
! !4.3.7 ! K2 filter constant A320 ! C ! C ! 25.0 !
! ! ! A321 ! C ! C ! 25.0 !
! ! ! A319 ! C ! C ! 25.0 !
! ! ! A318 ! C ! C ! 25.0 !
! ! ! ! ! ! !
! !4.3.8 ! K3 filter constant A320 ! C ! C ! 5.0 !
! ! ! A321 ! C ! C ! 5.0 !
! ! ! A319 ! C ! C ! 5.0 !
! ! ! A318 ! C ! C ! 5.0 !
! ! ! ! ! ! !
! !4.3.9 ! THETA0 (averaged Pitch A320 ! C ! C ! 6.0 !
! ! ! at touchdown) [deg] A321 ! C ! C ! 4.5 !
! ! ! A319 ! C ! C ! 2.0 !
! ! ! A318 ! C ! C ! 6.0 !
! ! ! ! ! ! !
! !4.3.10! S1 [sample] A320 ! C ! C ! -4.0 !
! ! ! A321 ! C ! C ! -4.0 !
! ! ! A319 ! C ! C ! -4.0 !
! ! ! A318 ! C ! C ! -4.0 !
! ! ! ! ! ! !
! !4.3.11! S2 [sample] A320 ! C ! C ! 4.0 !
! ! ! A321 ! C ! C ! 4.0 !
! ! ! A319 ! C ! C ! 4.0 !
! ! ! A318 ! C ! C ! 4.0 !
! ! ! ! ! ! !
! !4.4 ! VRTAL1.1 limit at landing [g] A320 ! C ! C ! 2.6 !
! ! ! A321 ! C ! C ! 2.6 !
! ! ! A319 ! C ! C ! 2.6 !
! ! ! A318 ! C ! C ! 2.6 !
! ! ! ! ! ! !
! !4.4.1 ! S3 [sample] A320 ! C ! C ! -16 !
! ! ! A321 ! C ! C ! -16 !
! ! ! A319 ! C ! C ! -16 !
! ! ! A318 ! C ! C ! -16 !
! ! ! ! ! ! !
! !4.4.2 ! S4 [sample] A320 ! C ! C ! 16 !
! ! ! A321 ! C ! C ! 16 !
! ! ! A319 ! C ! C ! 16 !
! ! ! A318 ! C ! C ! 16 !
! ! ! ! ! ! !
! !4.5 ! VRTAL1.2 limit at landing ! ! ! !
! ! ! (1st touchdown) from bounced ! ! ! !
! ! ! land/event [g] A320 ! C ! C ! 2.6 !
! ! ! A321 ! C ! C ! 2.6 !
! ! ! A319 ! C ! C ! 2.6 !
! ! ! A318 ! C ! C ! 2.6 !
! ! ! ! ! ! !
! !4.5.1 ! VRTAL1.3 limit at bounce (2nd touchdown)! ! ! !
! ! ! from bounced land/event [g] A320 ! C ! C ! 2.6 !
! ! ! A321 ! C ! C ! 2.6 !
! ! ! A319 ! C ! C ! 2.6 !
! ! ! A318 ! C ! C ! 2.6 !
! ! ! ! ! ! !
! !4.6 ! GW Overweight landing ! ! ! !
! !4.6.1 ! GWL1, GWL2, GWL3, GWL4 limit [kg] A320 ! C ! C ! 64500 !
! ! ! A321 ! C ! C ! 73500 !
! ! ! A319 ! C ! C ! 61000 !
! ! ! A318 ! C ! C ! 56500 !
! ! ! ! ! ! !
! ! ! ! ! ! !
! !4.6.2 ! RALRLG limit [ft/sec] A320 ! C ! C ! -6.0 !
! ! ! A321 ! C ! C ! -6.0 !
! ! ! A319 ! C ! C ! -6.0 !
! ! ! A318 ! C ! C ! -6.0 !
! ! ! ! ! ! !
! !4.6.3 ! VRTALG limit [g] A320 ! C ! C ! 1.7 !
! ! ! A321 ! C ! C ! 1.7 !
! ! ! A319 ! C ! C ! 1.7 !
! ! ! A318 ! C ! C ! 1.7 !
! ! ! ! ! ! !
! !4.7 ! Landing detection ! ! ! !
! ! ! Landing is detected when in PH7 or PH8 ! ! ! !
! ! ! 6D.1.021.01.13 = 1 (LH gear) ! ! ! !
! ! ! or ! ! ! !
! ! ! 6D.1.021.01.14 = 1 (RH gear) ! ! ! !
! ! ! ! ! ! !
! !4.8 ! Bounced landing detection ! ! ! !
! ! ! A bounced landing is detected when: ! ! ! !
! ! ! - In PH7 or PH8 parameter 6D.1.021.01.11! ! ! !
! ! ! is set to 1 for more than 'Y15.6'* ! ! ! !
! ! ! (1/32) seconds ! ! ! !
! ! ! - After detection, parameter ! ! ! !
! ! ! 6D.1.021.01.13 or/and 6D.1.021.01.14 ! ! ! !
! ! ! is/are set to 0 for more than 'Y15.7'* ! ! ! !
! ! ! (1/32) seconds ! ! ! !
! ! ! - Depending which parameter was set to ! ! ! !
! ! ! 0 or the first one of 6D.1.021.01.13 or! ! ! !
! ! ! 6D.1.021.01.14 is set to 1 again in ! ! ! !
! ! ! 'Y15.8'* (1/32) seconds. ! ! ! !
! ! ! ! ! ! !
! !4.9 ! 'Y15.6' landing gear compress time ! ! ! !
! ! ! (1st touchdown) [sample] A320 ! C ! C ! 16 !
! ! ! A321 ! C ! C ! 16 !
! ! ! A319 ! C ! C ! 16 !
! ! ! A318 ! C ! C ! 16 !
! ! ! ! ! ! !
! !4.10 ! 'Y15.7' time between bounces [sample] ! ! ! !
! ! ! A320 ! C ! C ! 32 !
! ! ! A321 ! C ! C ! 32 !
! ! ! A319 ! C ! C ! 32 !
! ! ! A318 ! C ! C ! 32 !
! ! ! ! ! ! !
! !4.11 ! 'Y15.8' landing gear compress time ! ! ! !
! ! ! (2nd touchdown) [sample] A320 ! C ! C ! 320 !
! ! ! A321 ! C ! C ! 320 !
! ! ! A319 ! C ! C ! 320 !
! ! ! A318 ! C ! C ! 320 !
! ! ! NOTE: - 1 sample is 1/32 second (32 Hz) ! ! ! !
!----!------!-----------------------------------------!----!----!---------!
! !5 ! Report is generated if one of the ! ! ! !
! ! ! subsequent logic items is present during! ! ! !
! ! ! flight (PH 5, 5.1, 6, 7, 7.1). There is ! ! ! !
! ! ! a spacing time TURBWAIT (sec) to enable ! ! ! !
! ! ! the trigger logic again after the ! ! ! !
! ! ! previous report generation. ! ! ! !
! ! ! ! ! ! !
!5100!5.1 ! VRTA > VRTAL2.1 if FLAP < FLAPL ! ! ! !
! ! ! ! ! ! !
!5200!5.2 ! VRTA < VRTAL2.2 if FLAP < FLAPL ! ! ! !
! ! ! ! ! ! !
!5300!5.3 ! VRTA > VRTAL2.3 if FLAP >/= FLAPL ! ! ! !
! ! ! or ! ! ! !
! ! ! VRTA < VRTAL2.4 if FLAP >/= FLAPL ! ! ! !
! ! ! ! ! ! !
! ! ! Limitation for Code 5100, 5200, 5300: ! ! ! !
! ! ! W15 TURBWAIT spacing time for ! ! ! !
! ! ! re-activating the trigger logic after ! ! ! !
! ! ! the previous report generation within ! ! ! !
! ! ! the same flight leg. ! ! ! !
! ! ! ! ! ! !
!5400!5.4 ! If one of the 5 spoiler excursion ! ! ! !
! ! ! counters has an overflow (999 is ! ! ! !
! ! ! reached). ! ! ! !
!----!------!-----------------------------------------!----!----!---------!
! !5.5 ! VRTAL2.1 limit [g] A320 ! C ! C ! 2.5 !
! ! ! A321 ! C ! C ! 2.5 !
! ! ! A319 ! C ! C ! 2.5 !
! ! ! A318 ! C ! C ! 2.5 !
! ! ! ! ! ! !
! !5.6 ! VRTAL2.2 limit [g] A320 ! C ! C ! -1.0 !
! ! ! A321 ! C ! C ! -1.0 !
! ! ! A319 ! C ! C ! -1.0 !
! ! ! A318 ! C ! C ! -1.0 !
! ! ! ! ! ! !
! !5.7 ! VRTAL2.3 limit [g] A320 ! C ! C ! 2.0 !
! ! ! A321 ! C ! C ! 2.0 !
! ! ! A319 ! C ! C ! 2.0 !
! ! ! A318 ! C ! c ! 2.0 !
! ! ! ! ! ! !
! !5.8 ! VRTAL2.4 limit [g] A320 ! C ! C ! 0.0 !
! ! ! A321 ! C ! C ! 0.0 !
! ! ! A319 ! C ! C ! 0.0 !
! ! ! A318 ! C ! C ! 0.0 !
! ! ! ! ! ! !
! !5.9 ! TURBWAIT [sec] A320 ! C ! C ! 10 !
! ! ! A321 ! C ! C ! 10 !
! ! ! A319 ! C ! C ! 10 !
! ! ! A318 ! C ! C ! 10 !
! ! ! ! ! ! !
! !5.10 ! FLAPL [deg] A320 ! C ! C ! 0.5 !
! ! ! A321 ! C ! C ! 0.5 !
! ! ! A319 ! C ! C ! 0.5 !
! ! ! A318 ! C ! C ! 0.5 !
!----!------!-----------------------------------------!----!----!---------!
!8100!8.1 ! ACARS MU uplink request with IMI 'REQ15'! ! ! !
! ! ! The report <15> is immediately generated! ! ! !
! ! ! and transmitted to the ACARS MU ! ! ! !
!-------------------------------------------------------------------------!
! A = Programmable by Airbus !
! C = Programmable by Customer !
+-------------------------------------------------------------------------+

(25) Load Report Logic
+--------------------------------------------------------------- ----------+
!Code!Item ! Description of Item ! Progr. !Standard !
!No. !No. ! Load Report <15> !GSE !MCDU!Value or !
! ! ! ! ! !Table TXY!
!----!-------!-----------------------------------------!----!----!---------!
! !A ! Report Format ! ! ! !
! ! ! ! ! ! !
! !A.1 ! 'R015RLID' Report Layout Identifier ! ! ! 01 !
! ! ! (for ACARS header) ! ! ! !
! ! ! ! ! ! !
! !A.2 ! 'R015RLIS' Report Layout Issue ! ! ! 02 !
! ! ! (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 !Yes !
! ! ! report was triggered by a code number ! ! ! !
! ! ! >1000: 1 = yes, 0 = no! C ! C ! 1 !
! ! ! ! ! ! !
! !G ! Inhibit report triggers: 1 = yes, 0 = no! C ! C ! 0 !
! ! ! ! ! ! !
! !H ! 'Y15.01' sec before land/event A320! C ! C ! 1 !
! ! ! A321! C ! C ! 1 !
! ! ! A319! C ! C ! 1 !
! ! ! A318! C ! C ! 1 !
! ! ! ! ! ! !
! !I ! 'Y15.02' sec after land/event A320! C ! C ! 3 !
! ! ! A321! C ! C ! 3 !
! ! ! A319! C ! C ! 3 !
! ! ! A318! C ! C ! 3 !
! ! ! ! ! ! !
! !J ! 'Y15.04' sec before bounced A320! C ! C ! 1 !
! ! ! A321! C ! C ! 1 !
! ! ! A319! C ! C ! 1 !
! ! ! A318! C ! C ! 1 !
! ! ! ! ! ! !
! !K ! 'Y15.05' sec after bounced A320! C ! C ! 3 !
! ! ! A321! C ! C ! 3 !
! ! ! A319! C ! C ! 3 !
! ! ! A318! C ! C ! 3 !
! ! ! ! ! ! !
! !L ! Inhibit report trigger code 5400: ! ! ! !
! ! ! 1 = yes, 0 = no! C ! C ! 1 !
! ! ! ! ! ! !
! !M.1 ! 'Y15.11' sec before first land/event ! ! ! !
! ! ! (IMPACT1) ! C ! C ! 1.7 !
! ! ! (used to calculate VRTAMA1) ! ! ! !
! ! ! ! ! ! !
! !M.2 ! 'Y15.12' sec after first land/event ! ! ! !
! ! ! (IMPACT1) ! C ! C ! 1.7 !
! ! ! (used to calculate VRTAMA1) ! ! ! !
! ! ! ! ! ! !
! !M.3 ! 'Y15.21' sec before second land/event ! ! ! !
! ! ! (IMPACT2) ! C ! C ! 1.7 !
! ! ! (used to calculate VRTAMA2) ! ! ! !
! ! ! ! ! ! !
! !M.4 ! 'Y15.22' sec after second land/event ! ! ! !
! ! ! (IMPACT2) ! C ! C ! 1.7 !
! ! ! (used to calculate VRTAMA2) ! ! ! !
! ! ! ! ! ! !
! !M.5 ! 'Y15.31' sec before detection of VTRAMA1! ! ! !
! ! ! during first land/event(IMPACT1) ! C ! C ! 0.7 !
! ! ! (used to calculate LATAMA1) ! ! ! !
! ! ! ! ! ! !
! !M.6 ! 'Y15.32' sec after detection of VTRAMA1 ! ! ! !
! ! ! during first land/event(IMPACT1) ! C ! C ! 0.8 !
! ! ! (used to calculate LATAMA1) ! ! ! !
! ! ! ! ! ! !
! !M.7 ! 'Y15.41' sec before detection of VTRAMA2! ! ! !
! ! ! during second land/event(IMPACT2) ! C ! C ! 0.7 !
! ! ! (used to calculate LATAMA2) ! ! ! !
! ! ! ! ! ! !
! !M.8 ! 'Y15.42' sec after detection of VTRAMA2 ! ! ! !
! ! ! during second land/event(IMPACT2) ! C ! C ! 0.8 !
! ! ! (used to calculate LATAMA2) ! ! ! !
! ! ! ! ! ! !
! !M.9 ! 'Y15.51' sec before detection of VRTAMA1! ! ! !
! ! ! during first land/event(IMPACT1) ! C ! C ! 0.7 !
! ! ! (used to calculate VRTAMI1) ! ! ! !
! ! ! ! ! ! !
! !M.10 ! 'Y15.52' sec after detection of VRTAMA1 ! ! ! !
! ! ! during first land/event(IMPACT1) ! C ! C ! 0.2 !
! ! ! (used to calculate VRTAMI1) ! ! ! !
! ! ! ! ! ! !
! !M.11 ! 'Y15.61' sec before detection of VRTAMA2! ! ! !
! ! ! during second land/event(IMPACT2) ! C ! C ! 0.7 !
! ! ! (used to calculate VRTAMI2) ! ! ! !
! ! ! ! ! ! !
! !M.12 ! 'Y15.62' sec after detection of VRTAMA2 ! ! ! !
! ! ! during second land/event(IMPACT2) ! C ! C ! 0.2 !
! ! ! (used to calculate VRTAMI2) ! ! ! !
!----!-------!-----------------------------------------!----!----!---------!
!1000! ! Manual Trigger ! ! ! !
!----!-------!-----------------------------------------!----!----!---------!
!2000! ! Not applicable ! ! ! !
!----!-------!-----------------------------------------!----!----!---------!
!3000!3 ! Programmable Start Logic ! ! ! !
! !3.1 ! Logic algorithm ! ! ! !
! !3.2 ! Logic criteria values ! ! ! not !
! ! ! ! ! ! progr. !
!----!-------!-----------------------------------------!----!----!---------!
! !4 ! Use applicable GW (GWL1, GWL2, GWL3 or ! ! ! !
! ! ! GWL4) if ACT (Additional Center Tanks) ! ! ! !
! ! ! is installed or not. ! ! ! !
!----!-------!-----------------------------------------!----!----!---------!
! ! ! Logic for ACT detection ! ! ! !
! ! ! ! ! ! !
! ! !FWC! 26.1.276.01.26 26.1.276.01.27 GW ! ! ! !
! ! ! ! 26.1.276.10.26 26.1.276.10.27 Limit! ! ! !
! ! !-----------------------------------------! ! ! !
! ! ! ! 0 0 GWL1 ! ! ! !
! ! ! ! 1 0 GWL2 ! ! ! !
! ! ! ! 0 1 GWL3 ! ! ! !
! ! ! ! 1 1 GWL4 ! ! ! !
! ! ! ! ! ! !
! ! ! Report will be made if one of the items ! ! ! !
! ! ! that follow is given during landing: ! ! ! !
!----!-------!-----------------------------------------!----!----!---------!
!7000!4.1 ! The report must be done during each ! ! ! !
! ! ! landing. ! ! ! !
! ! ! ! ! ! !
! ! ! For landing detection refer to item 4.9.! ! ! !
! ! ! ! ! ! !
! ! ! Report code 7000 must be erased and ! ! ! !
! ! ! replaced by report code 4xxx when given ! ! ! !
! ! ! during the same landing. ! ! ! !
!----!-------!-----------------------------------------!----!----!---------!
! ! 4.2 ! Trigger Code assignment: ! ! ! !
! ! ! -Red Zone: 4310, 4410, 4510, 4610 ! ! ! !
! ! ! -Amber Zone: 4320, 4420, 4520, 4620 ! ! ! !
! ! ! -Green Zone: 7000. ! ! ! !
!----!-------!-----------------------------------------!----!----!---------!
! !4.3 ! Importance of trigger codes: ! ! ! !
! !4.3.1 ! Group 43xx is the most important, then ! ! ! !
! ! ! group 44xx, then group 45xx and last is ! ! ! !
! ! ! group 46xx. ! ! ! !
! ! ! ! ! ! !
! !4.3.2 ! In trigger group 43xx code 4310 is the ! ! ! !
! ! ! most important, then code 4320. ! ! ! !
! ! ! ! ! ! !
! !4.3.3 ! In trigger group 44xx code 4410 is the ! ! ! !
! ! ! most important, then code 4420. ! ! ! !
! ! ! ! ! ! !
! !4.3.4 ! In trigger group 45xx code 4510 is the ! ! ! !
! ! ! most important, then code 4520. ! ! ! !
! ! ! ! ! ! !
! !4.3.5 ! In trigger group 46xx code 4610 is the ! ! ! !
! ! ! most important, then code 4620. ! ! ! !
!----!-------!-----------------------------------------!----!----!---------!
!43xx!4.4 ! The trigger must be calculated one time,! ! ! !
! ! ! when DNZKPI1, DNZKPI2, NYKPI1 and NYKPI2! ! ! !
! ! ! are calculated. ! ! ! !
! ! ! ! ! ! !
! ! ! Report will be made if one of the logic ! ! ! !
! ! ! items that follow is given during ! ! ! !
! ! ! landing: ! ! ! !
!----!-------!-----------------------------------------!----!----!---------!
! !4.4.1 ! Condition A (red): (during first ! ! ! !
! ! ! touchdown) ! ! ! !
! ! ! ! ! ! !
! ! ! (GWKG > GWL) ! ! ! !
! ! ! ! ! ! !
! ! ! and ! ! ! !
! ! ! ! ! ! !
! ! ! ( (NYKPI1 >= NyL.C2) ! ! ! !
! ! ! or ! ! ! !
! ! !DNZKPI1 > (NzL.C2-NzL.C4)*NYKPI1/NyL.C2+ ! ! ! !
! ! ! +NzL.C4 ) ! ! ! !
!----!-------!-----------------------------------------!----!----!---------!
! !4.4.2 ! Condition B (amber): (during first ! ! ! !
! ! ! touchdown) ! ! ! !
! ! ! ! ! ! !
! ! ! (GWKG > GWL) ! ! ! !
! ! ! ! ! ! !
! ! ! and ! ! ! !
! ! ! ! ! ! !
! ! ! ( (NYKPI1 >= NyL.C1) ! ! ! !
! ! ! or ! ! ! !
! ! !DNZKPI1 > (NzL.C1-NzL.C3)*NYKPI1/NyL.C1+ ! ! ! !
! ! ! +NzL.C3 ) ! ! ! !
!----!-------!-----------------------------------------!----!----!---------!
! !4.4.3 ! Condition C (red): (during second ! ! ! !
! ! ! touchdown) ! ! ! !
! ! ! ! ! ! !
! ! ! (GWKG > GWL) ! ! ! !
! ! ! ! ! ! !
! ! ! and ! ! ! !
! ! ! ! ! ! !
! ! ! ( (NYKPI2 >= NyL.D2) ! ! ! !
! ! ! or ! ! ! !
! ! !DNZKPI2 > (NzL.D2-NzL.D4)*NYKPI2/NyL.D2+ ! ! ! !
! ! ! +NzL.D4 ) ! ! ! !
!----!-------!-----------------------------------------!----!----!---------!
! !4.4.4 ! Condition D (amber): (during second ! ! ! !
! ! ! touchdown) ! ! ! !
! ! ! ! ! ! !
! ! ! (GWKG > GWL) ! ! ! !
! ! ! ! ! ! !
! ! ! and ! ! ! !
! ! ! ! ! ! !
! ! ! ( (NYKPI2 >= NyL.D1) ! ! ! !
! ! ! or ! ! ! !
! ! !DNZKPI2 > (NzL.D1-NzL.D3)*NYKPI2/NyL.D1+ ! ! ! !
! ! ! +NzL.D3 ) ! ! ! !
!----!-------!-----------------------------------------!----!----!---------!
!4310!4.4.5 ! Overweight red bounce hard landing if ! ! ! !
! ! !conditions "A" and/or "C" are applicable.! ! ! !
!----!-------!-----------------------------------------!----!----!---------!
!4320!4.4.6 ! Overweight amber bounce hard landing if ! ! ! !
! ! !conditions "A" and "C" are not applicable! ! ! !
! ! !and "B" and/or "D" are applicable. ! ! ! !
!----!-------!-----------------------------------------!----!----!---------!
!44xx!4.5 ! The trigger must be calculated one time,! ! ! !
! ! ! when DNZKPI1 and NYKPI1 are calculated. ! ! ! !
! ! ! ! ! ! !
! ! ! Report will be made if one of the logic ! ! ! !
! ! ! items that follow is given during ! ! ! !
! ! ! landing: ! ! ! !
!----!-------!-----------------------------------------!----!----!---------!
!4410!4.5.1 ! Overweight red hard landing if: ! ! ! !
! ! ! ! ! ! !
! ! ! (GWKG > GWL) ! ! ! !
! ! ! ! ! ! !
! ! ! and ! ! ! !
! ! ! ! ! ! !
! ! ! ( (NYKPI1 >= NyL.G2) ! ! ! !
! ! ! or ! ! ! !
! ! !DNZKPI1 > (NzL.G2-NzL.G4)*NYKPI1/NyL.G2+ ! ! ! !
! ! ! +NzL.G4 ) ! ! ! !
!----!-------!-----------------------------------------!----!----!---------!
!4420!4.5.2 ! Overweight amber hard landing if: ! ! ! !
! ! ! ! ! ! !
! ! ! (GWKG > GWL) ! ! ! !
! ! ! ! ! ! !
! ! ! and ! ! ! !
! ! ! ! ! ! !
! ! ! ( (NYKPI1 >= NyL.G1) ! ! ! !
! ! ! or ! ! ! !
! ! !DNZKPI1 > (NzL.G1-NzL.G3)*NYKPI1/NyL.G1+ ! ! ! !
! ! ! +NzL.G3 ) ! ! ! !
!----!-------!-----------------------------------------!----!----!---------!
!45xx!4.6 ! The trigger must be calculated one time,! ! ! !
! ! ! when DNZKPI1, DNZKPI2, NYKPI1 and NYKPI2! ! ! !
! ! ! are calculated. ! ! ! !
! ! ! ! ! ! !
! ! ! Report will be made if one of the logic ! ! ! !
! ! ! items that follow is given during ! ! ! !
! ! ! landing: ! ! ! !
!----!-------!-----------------------------------------!----!----!---------!
! !4.6.1 ! Condition E (red): (during first ! ! ! !
! ! ! touchdown) ! ! ! !
! ! ! ! ! ! !
! ! ! (NYKPI1 >= NyL.A2) ! ! ! !
! ! ! ! ! ! !
! ! ! or ! ! ! !
! ! ! ! ! ! !
! ! !DNZKPI1 > (NzL.A2-NzL.A4)*NYKPI1/NyL.A2+ ! ! ! !
! ! ! +NzL.A4 ! ! ! !
!----!-------!-----------------------------------------!----!----!---------!
! !4.6.2 ! Condition F (amber): (during first ! ! ! !
! ! ! touchdown) ! ! ! !
! ! ! ! ! ! !
! ! ! (NYKPI1 >= NyL.A1) ! ! ! !
! ! ! ! ! ! !
! ! ! or ! ! ! !
! ! ! ! ! ! !
! ! !DNZKPI1 > (NzL.A1-NzL.A3)*NYKPI1/NyL.A1+ ! ! ! !
! ! ! +NzL.A3 ! ! ! !
!----!-------!-----------------------------------------!----!----!---------!
! !4.6.3 ! Condition G (red): (during second ! ! ! !
! ! ! touchdown) ! ! ! !
! ! ! ! ! ! !
! ! ! (NYKPI2 >= NyL.B2) ! ! ! !
! ! ! ! ! ! !
! ! ! or ! ! ! !
! ! ! ! ! ! !
! ! !DNZKPI2 > (NzL.B2-NzL.B4)*NYKPI2/NyL.B2+ ! ! ! !
! ! ! +NzL.B4 ! ! ! !
!----!-------!-----------------------------------------!----!----!---------!
! !4.6.4 ! Condition H (amber): (during second ! ! ! !
! ! ! touchdown) ! ! ! !
! ! ! ! ! ! !
! ! ! (NYKPI2 >= NyL.B1) ! ! ! !
! ! ! ! ! ! !
! ! ! or ! ! ! !
! ! ! ! ! ! !
! ! !DNZKPI2 > (NzL.B1-NzL.B3)*NYKPI2/NyL.B1+ ! ! ! !
! ! ! +NzL.B3 ! ! ! !
!----!-------!-----------------------------------------!----!----!---------!
!4510!4.6.5 ! Red bounce hard landing if conditions ! ! ! !
! ! ! "E" and/or "G" are applicable. ! ! ! !
!----!-------!-----------------------------------------!----!----!---------!
!4520!4.6.6 ! Amber bounce hard landing if condition ! ! ! !
! ! ! "E" and "G" are not applicable and "F" ! ! ! !
! ! ! and/or "H" are applicable. ! ! ! !
!----!-------!-----------------------------------------!----!----!---------!
!46xx!4.7 ! The trigger must be calculated one time,! ! ! !
! ! ! when DNZKPI1 and NYKPI1 are calculated. ! ! ! !
! ! ! ! ! ! !
! ! ! Report will be made if one of the logic ! ! ! !
! ! ! items that follow is given during ! ! ! !
! ! ! landing: ! ! ! !
!----!-------!-----------------------------------------!----!----!---------!
!4610!4.7.1 ! Red hard landing if: ! ! ! !
! ! ! ! ! ! !
! ! ! (NYKPI1 >= NyL.L2) ! ! ! !
! ! ! ! ! ! !
! ! ! or ! ! ! !
! ! ! ! ! ! !
! ! !DNZKPI1 > (NzL.L2-NzL.L4)*NYKPI1/NyL.L2+ ! ! ! !
! ! ! +NzL.L4 ! ! ! !
!----!-------!-----------------------------------------!----!----!---------!
!4620!4.7.2 ! Amber hard landing if: ! ! ! !
! ! ! ! ! ! !
! ! ! (NYKPI1 >= NyL.L1) ! ! ! !
! ! ! ! ! ! !
! ! ! or ! ! ! !
! ! ! ! ! ! !
! ! !DNZKPI1 > (NzL.L1-NzL.L3)*NYKPI1/NyL.L1+ ! ! ! !
! ! ! +NzL.L3 ! ! ! !
!----!-------!-----------------------------------------!----!----!---------!
! !4.8 ! GW Overweight landing ! ! ! !
! ! ! ! ! ! !
! !4.8.1 ! GWL1, GWL2, GWL3, GWL4 limit (kg) ! ! ! !
! ! ! A320 CEO ! C ! C ! 64500 !
! ! ! A321 CEO ! C ! C ! 73500 !
! ! ! A319 CEO ! C ! C ! 61000 !
! ! ! A318 CEO ! C ! C ! 56000 !
! ! ! ! ! ! !
! !4.8.2 ! GWL1, GWL2, GWL3, GWL4 limit (kg) ! ! ! !
! ! ! A320 NEO ! C ! C ! 67400 !
! ! ! A321 NEO ! C ! C ! 79200 !
! ! ! A319 NEO ! C ! C ! 63900 !
!----!-------!-----------------------------------------!----!----!---------!
! !4.9 ! The non-filtered landing gear parameters! ! ! !
! ! !which are used for the landing and bounce! ! ! !
! ! !detection below (refer to item 4.9.1 and ! ! ! !
! ! !4.9.2) must be monitored with a rate of ! ! ! !
! ! !32 Hz during the interval of 0.5 sec ! ! ! !
! ! !before and 0.5 sec after IMPACT1 and ! ! ! !
! ! !IMPACT2. ! ! ! !
!----!-------!-----------------------------------------!----!----!---------!
! !4.9.1 ! Landing detection (IMPACT1) ! ! ! !
! ! ! ! ! ! !
! ! ! Landing is detected when in PH 7 or PH 8! ! ! !
! ! ! LHLG=1 (LH gear) ! ! ! !
! ! ! ! ! ! !
! ! ! or ! ! ! !
! ! ! ! ! ! !
! ! ! RHLG=1 (RH gear) ! ! ! !
!----!-------!-----------------------------------------!----!----!---------!
! !4.9.2 ! Bounced landing detection (IMPACT2) ! ! ! !
! ! ! ! ! ! !
! ! ! A bounced landing is detected when in ! ! ! !
! ! ! PH 7 or PH 8 any landing gear parameter ! ! ! !
! ! ! [LH gear (LHLG) or RH gear (RHLG) or ! ! ! !
! ! ! both (MLG)] is set to 1 for longer than ! ! ! !
! ! ! 'Y15.06' *(1/32) seconds. ! ! ! !
! ! ! ! ! ! !
! ! ! and ! ! ! !
! ! ! ! ! ! !
! ! ! Then any landing gear parameter (LHLG, ! ! ! !
! ! ! RHLG, MLG) which was set to 1 returns ! ! ! !
! ! ! to 0 for longer than 'Y15.07' *(1/32) ! ! ! !
! ! ! seconds. ! ! ! !
! ! ! ! ! ! !
! ! ! and ! ! ! !
! ! ! ! ! ! !
! ! ! Then the one which was set to 0 or the ! ! ! !
! ! ! first one of LHLG or RHLG is set to 1 ! ! ! !
! ! ! again within 'Y15.08' *(1/32) seconds. ! ! ! !
!----!-------!-----------------------------------------!----!----!---------!
! !4.10.1 ! 'Y15.06' landing gear compress time ! ! ! !
! ! ! (first touchdown) ! ! ! !
! ! ! (sample) A320 ! C ! C ! 8 !
! ! ! A321 ! C ! C ! 8 !
! ! ! A319 ! C ! C ! 8 !
! ! ! A318 ! C ! C ! 8 !
!----!-------!-----------------------------------------!----!----!---------!
! !4.10.2 ! 'Y15.07' time between bounces ! ! ! !
! ! ! (sample) A320 ! C ! C ! 16 !
! ! ! A321 ! C ! C ! 16 !
! ! ! A319 ! C ! C ! 16 !
! ! ! A318 ! C ! C ! 16 !
!----!-------!-----------------------------------------!----!----!---------!
! !4.10.3 ! 'Y15.08' landing gear compress time ! ! ! !
! ! ! (second touchdown) ! ! ! !
! ! ! (sample) A320 ! C ! C ! 320 !
! ! ! A321 ! C ! C ! 320 !
! ! ! A319 ! C ! C ! 320 !
! ! ! A318 ! C ! C ! 320 !
!----!-------!-----------------------------------------!----!----!---------!
! !4.10.4 ! 'Y15.09' bounce searching time ! ! ! !
! ! ! (max time between IMPACT1 and IMPACT2) ! ! ! !
! ! ! (sample) A320 ! C ! C ! 320 !
! ! ! A321 ! C ! C ! 320 !
! ! ! A319 ! C ! C ! 320 !
! ! ! A318 ! C ! C ! 320 !
! ! ! NOTE: 1 sample is 1/32 second (32 Hz) ! ! ! !
!----!-------!-----------------------------------------!----!----!---------!
! !4.11 ! N/A ! ! ! !
!----!-------!-----------------------------------------!----!----!---------!
! !4.12 ! N/A ! ! ! !
!----!-------!-----------------------------------------!----!----!---------!
! !4.13 ! Limits for Trigger Codes 43xx ! ! ! !
! !4.13.1 ! 'NzL.C1' limit at GW landing (IMPACT1) ! ! ! !
! ! ! from bounce land event (g) A320 ! C ! C ! 1.80 !
! ! ! A321 ! C ! C ! 1.80 !
! ! ! A319 ! C ! C ! 1.80 !
! ! ! A318 ! C ! C ! 1.80 !
! ! ! ! ! ! !
! !4.13.2 ! 'NzL.C2' limit at GW landing (IMPACT1) ! ! ! !
! ! ! from bounce land event (g) A320 ! C ! C ! 2.06 !
! ! ! A321 ! C ! C ! 2.06 !
! ! ! A319 ! C ! C ! 2.06 !
! ! ! A318 ! C ! C ! 2.06 !
! ! ! ! ! ! !
! !4.13.3 ! 'NzL.C3' limit at GW landing (IMPACT1) ! ! ! !
! ! ! from bounce land event (g) A320 ! C ! C ! 1.80 !
! ! ! A321 ! C ! C ! 1.80 !
! ! ! A319 ! C ! C ! 1.80 !
! ! ! A318 ! C ! C ! 1.80 !
! ! ! ! ! ! !
! !4.13.4 ! 'NzL.C4' limit at GW landing (IMPACT1) ! ! ! !
! ! ! from bounce land event (g) A320 ! C ! C ! 2.06 !
! ! ! A321 ! C ! C ! 2.06 !
! ! ! A319 ! C ! C ! 2.06 !
! ! ! A318 ! C ! C ! 2.06 !
! ! ! ! ! ! !
! !4.13.5 ! 'NyL.C1' limit at GW landing (IMPACT1) ! ! ! !
! ! ! from bounce land event (g) A320 ! C ! C ! 0.45 !
! ! ! A321 ! C ! C ! 0.45 !
! ! ! A319 ! C ! C ! 0.45 !
! ! ! A318 ! C ! C ! 0.45 !
! ! ! ! ! ! !
! !4.13.6 ! 'NyL.C2' limit at GW landing (IMPACT1) ! ! ! !
! ! ! from bounce land event (g) A320 ! C ! C ! 0.50 !
! ! ! A321 ! C ! C ! 0.50 !
! ! ! A319 ! C ! C ! 0.50 !
! ! ! A318 ! C ! C ! 0.50 !
! ! ! ! ! ! !
! !4.13.7 ! 'NzL.D1' limit at GW landing (IMPACT2) ! ! ! !
! ! ! from bounce land event (g) A320 ! C ! C ! 1.80 !
! ! ! A321 ! C ! C ! 1.80 !
! ! ! A319 ! C ! C ! 1.80 !
! ! ! A318 ! C ! C ! 1.80 !
! ! ! ! ! ! !
! !4.13.8 ! 'NzL.D2' limit at GW landing (IMPACT2) ! ! ! !
! ! ! from bounce land event (g) A320 ! C ! C ! 2.06 !
! ! ! A321 ! C ! C ! 2.06 !
! ! ! A319 ! C ! C ! 2.06 !
! ! ! A318 ! C ! C ! 2.06 !
! ! ! ! ! ! !
! !4.13.9 ! 'NzL.D3' limit at GW landing (IMPACT2) ! ! ! !
! ! ! from bounce land event (g) A320 ! C ! C ! 1.80 !
! ! ! A321 ! C ! C ! 1.80 !
! ! ! A319 ! C ! C ! 1.80 !
! ! ! A318 ! C ! C ! 1.80 !
! ! ! ! ! ! !
! !4.13.10! 'NzL.D4' limit at GW landing (IMPACT2) ! ! ! !
! ! ! from bounce land event (g) A320 ! C ! C ! 2.06 !
! ! ! A321 ! C ! C ! 2.06 !
! ! ! A319 ! C ! C ! 2.06 !
! ! ! A318 ! C ! C ! 2.06 !
! ! ! ! ! ! !
! !4.13.11! 'NyL.D1' limit at GW landing (IMPACT2) ! ! ! !
! ! ! from bounce land event (g) A320 ! C ! C ! 0.45 !
! ! ! A321 ! C ! C ! 0.45 !
! ! ! A319 ! C ! C ! 0.45 !
! ! ! A318 ! C ! C ! 0.45 !
! ! ! ! ! ! !
! !4.13.12! 'NyL.D2' limit at GW landing (IMPACT2) ! ! ! !
! ! ! from bounce land event (g) A320 ! C ! C ! 0.50 !
! ! ! A321 ! C ! C ! 0.50 !
! ! ! A319 ! C ! C ! 0.50 !
! ! ! A318 ! C ! C ! 0.50 !
!----!-------!-----------------------------------------!----!----!---------!
! !4.14 ! Limits for Trigger Codes 44xx ! ! ! !
! !4.14.1 ! 'NzL.G1' limit at GW landing (g) A320 ! C ! C ! 1.80 !
! ! ! A321 ! C ! C ! 1.80 !
! ! ! A319 ! C ! C ! 1.80 !
! ! ! A318 ! C ! C ! 1.80 !
! ! ! ! ! ! !
! !4.14.2 ! 'NzL.G2' limit at GW landing (g) A320 ! C ! C ! 2.06 !
! ! ! A321 ! C ! C ! 2.06 !
! ! ! A319 ! C ! C ! 2.06 !
! ! ! A318 ! C ! C ! 2.06 !
! ! ! ! ! ! !
! !4.14.3 ! 'NzL.G3' limit at GW landing (g) A320 ! C ! C ! 1.80 !
! ! ! A321 ! C ! C ! 1.80 !
! ! ! A319 ! C ! C ! 1.80 !
! ! ! A318 ! C ! C ! 1.80 !
! ! ! ! ! ! !
! !4.14.4 ! 'NzL.G4' limit at GW landing (g) A320 ! C ! C ! 2.06 !
! ! ! A321 ! C ! C ! 2.06 !
! ! ! A319 ! C ! C ! 2.06 !
! ! ! A318 ! C ! C ! 2.06 !
! ! ! ! ! ! !
! !4.14.5 ! 'NyL.G1' limit at GW landing (g) A320 ! C ! C ! 0.45 !
! ! ! A321 ! C ! C ! 0.45 !
! ! ! A319 ! C ! C ! 0.45 !
! ! ! A318 ! C ! C ! 0.45 !
! ! ! ! ! ! !
! !4.14.6 ! 'NyL.G2' limit at GW landing (g) A320 ! C ! C ! 0.50 !
! ! ! A321 ! C ! C ! 0.50 !
! ! ! A319 ! C ! C ! 0.50 !
! ! ! A318 ! C ! C ! 0.50 !
!----!-------!-----------------------------------------!----!----!---------!
! !4.15 ! Limits for Trigger Codes 45xx ! ! ! !
! !4.15.1 ! 'NzL.A1' limit at landing (IMPACT1) ! ! ! !
! ! ! from bounce land event (g) A320 ! C ! C ! 1.80 !
! ! ! A321 ! C ! C ! 1.80 !
! ! ! A319 ! C ! C ! 1.80 !
! ! ! A318 ! C ! C ! 1.80 !
! ! ! ! ! ! !
! !4.15.2 ! 'NzL.A2' limit at landing (IMPACT1) ! ! ! !
! ! ! from bounce land event (g) A320 ! C ! C ! 2.06 !
! ! ! A321 ! C ! C ! 2.06 !
! ! ! A319 ! C ! C ! 2.06 !
! ! ! A318 ! C ! C ! 2.06 !
! ! ! ! ! ! !
! !4.15.3 ! 'NzL.A3' limit at landing (IMPACT1) ! ! ! !
! ! ! from bounce land event (g) A320 ! C ! C ! 1.80 !
! ! ! A321 ! C ! C ! 1.80 !
! ! ! A319 ! C ! C ! 1.80 !
! ! ! A318 ! C ! C ! 1.80 !
! ! ! ! ! ! !
! !4.15.4 ! 'NzL.A4' limit at landing (IMPACT1) ! ! ! !
! ! ! from bounce land event (g) A320 ! C ! C ! 2.06 !
! ! ! A321 ! C ! C ! 2.06 !
! ! ! A319 ! C ! C ! 2.06 !
! ! ! A318 ! C ! C ! 2.06 !
! ! ! ! ! ! !
! !4.15.5 ! 'NyL.A1' limit at landing (IMPACT1) ! ! ! !
! ! ! from bounce land event (g) A320 ! C ! C ! 0.45 !
! ! ! A321 ! C ! C ! 0.45 !
! ! ! A319 ! C ! C ! 0.45 !
! ! ! A318 ! C ! C ! 0.45 !
! ! ! ! ! ! !
! !4.15.6 ! 'NyL.A2' limit at landing (IMPACT1) ! ! ! !
! ! ! from bounce land event (g) A320 ! C ! C ! 0.50 !
! ! ! A321 ! C ! C ! 0.50 !
! ! ! A319 ! C ! C ! 0.50 !
! ! ! A318 ! C ! C ! 0.50 !
! ! ! ! ! ! !
! !4.15.7 ! 'NzL.B1' limit at landing (IMPACT2) ! ! ! !
! ! ! from bounce land event (g) A320 ! C ! C ! 1.80 !
! ! ! A321 ! C ! C ! 1.80 !
! ! ! A319 ! C ! C ! 1.80 !
! ! ! A318 ! C ! C ! 1.80 !
! ! ! ! ! ! !
! !4.15.8 ! 'NzL.B2' limit at landing (IMPACT2) ! ! ! !
! ! ! from bounce land event (g) A320 ! C ! C ! 2.06 !
! ! ! A321 ! C ! C ! 2.06 !
! ! ! A319 ! C ! C ! 2.06 !
! ! ! A318 ! C ! C ! 2.06 !
! ! ! ! ! ! !
! !4.15.9 ! 'NzL.B3' limit at landing (IMPACT2) ! ! ! !
! ! ! from bounce land event (g) A320 ! C ! C ! 1.80 !
! ! ! A321 ! C ! C ! 1.80 !
! ! ! A319 ! C ! C ! 1.80 !
! ! ! A318 ! C ! C ! 1.80 !
! ! ! ! ! ! !
! !4.15.10! 'NzL.B4' limit at landing (IMPACT2) ! ! ! !
! ! ! from bounce land event (g) A320 ! C ! C ! 2.06 !
! ! ! A321 ! C ! C ! 2.06 !
! ! ! A319 ! C ! C ! 2.06 !
! ! ! A318 ! C ! C ! 2.06 !
! ! ! ! ! ! !
! !4.15.11! 'NyL.B1' limit at landing (IMPACT2) ! ! ! !
! ! ! from bounce land event (g) A320 ! C ! C ! 0.45 !
! ! ! A321 ! C ! C ! 0.45 !
! ! ! A319 ! C ! C ! 0.45 !
! ! ! A318 ! C ! C ! 0.45 !
! ! ! ! ! ! !
! !4.15.12! 'NyL.B2' limit at landing (IMPACT2) ! ! ! !
! ! ! from bounce land event (g) A320 ! C ! C ! 0.50 !
! ! ! A321 ! C ! C ! 0.50 !
! ! ! A319 ! C ! C ! 0.50 !
! ! ! A318 ! C ! C ! 0.50 !
!----!-------!-----------------------------------------!----!----!---------!
! !4.16 ! Limits for Trigger Codes 46xx ! ! ! !
! !4.16.1 ! NzL.L1 limit at landing (g) A320 ! C ! C ! 1.80 !
! ! ! A321 ! C ! C ! 1.80 !
! ! ! A319 ! C ! C ! 1.80 !
! ! ! A318 ! C ! C ! 1.80 !
! ! ! ! ! ! !
! !4.16.2 ! 'NzL.L2' limit at landing (g) A320 ! C ! C ! 2.06 !
! ! ! A321 ! C ! C ! 2.06 !
! ! ! A319 ! C ! C ! 2.06 !
! ! ! A318 ! C ! C ! 2.06 !
! ! ! ! ! ! !
! !4.16.3 ! 'NzL.L3' limit at landing (g) A320 ! C ! C ! 1.80 !
! ! ! A321 ! C ! C ! 1.80 !
! ! ! A319 ! C ! C ! 1.80 !
! ! ! A318 ! C ! C ! 1.80 !
! ! ! ! ! ! !
! !4.16.4 ! 'NzL.L4' limit at landing (g) A320 ! C ! C ! 2.06 !
! ! ! A321 ! C ! C ! 2.06 !
! ! ! A319 ! C ! C ! 2.06 !
! ! ! A318 ! C ! C ! 2.06 !
! ! ! ! ! ! !
! !4.16.5 ! 'NyL.L1' limit at landing (g) A320 ! C ! C ! 0.45 !
! ! ! A321 ! C ! C ! 0.45 !
! ! ! A319 ! C ! C ! 0.45 !
! ! ! A318 ! C ! C ! 0.45 !
! ! ! ! ! ! !
! !4.16.6 ! 'NyL.L2' limit at landing (g) A320 ! C ! C ! 0.50 !
! ! ! A321 ! C ! C ! 0.50 !
! ! ! A319 ! C ! C ! 0.50 !
! ! ! A318 ! C ! C ! 0.50 !
!----!-------!-----------------------------------------!----!----!---------!
! !4.17 ! ACCONSTI1 (IMPACT1) A320 ! C ! C ! 1.79 !
! ! ! A321 ! C ! C ! 1.86 !
! ! ! A319 ! C ! C ! 1.72 !
! ! ! A318 ! C ! C ! 1.72 !
!----!-------!-----------------------------------------!----!----!---------!
! !4.18 ! ACCONSTI2 (IMPACT2) A320 ! C ! C ! 1.79 !
! ! ! A321 ! C ! C ! 1.86 !
! ! ! A319 ! C ! C ! 1.72 !
! ! ! A318 ! C ! C ! 1.72 !
!----!-------!-----------------------------------------!----!----!---------!
! !4.19 ! LATACONST1 (IMPACT1) A320 ! C ! C ! 1.2 !
! ! ! A321 ! C ! C ! 1.2 !
! ! ! A319 ! C ! C ! 1.2 !
! ! ! A318 ! C ! C ! 1.2 !
!----!-------!-----------------------------------------!----!----!---------!
! !4.20 ! LATACONST2 (IMPACT2) A320 ! C ! C ! 1.2 !
! ! ! A321 ! C ! C ! 1.2 !
! ! ! A319 ! C ! C ! 1.2 !
! ! ! A318 ! C ! C ! 1.2 !
!----!-------!-----------------------------------------!----!----!---------!
! !4.21 ! DNZCONST1 A320 ! C ! C ! 1 !
! ! ! (Gamma constant for IMPACT1) A321 ! C ! C ! 1 !
! ! ! A319 ! C ! C ! 1 !
! ! ! A318 ! C ! C ! 1 !
!----!-------!-----------------------------------------!----!----!---------!
! !4.22 ! DNZCONST2 A320 ! C ! C ! 1 !
! ! ! (Gamma constant for IMPACT2) A320 ! C ! C ! 1 !
! ! ! A320 ! C ! C ! 1 !
! ! ! A320 ! C ! C ! 1 !
!----!-------!-----------------------------------------!----!----!---------!
! !5 ! Report must be generated if one of the ! ! ! !
! ! ! logic items that follow is given during ! ! ! !
! ! ! flight (PH 5, 5.1, 6, 7, 7.1). There ! ! ! !
! ! ! must be a time TURBWAIT (sec) to enable ! ! ! !
! ! ! the trigger logic again after the ! ! ! !
! ! ! previous report generation. ! ! ! !
! ! ! ! ! ! !
!5100!5.1 ! VRTA > VRTAL2.1 if FLAP < FLAPL ! ! ! !
! ! ! ! ! ! !
!5200!5.2 ! VRTA < VRTAL2.2 if FLAP < FLAPL ! ! ! !
! ! ! ! ! ! !
!5300!5.3 ! VRTA > VRTAL2.3 if FLAP >= FLAPL ! ! ! !
! ! ! or ! ! ! !
! ! ! VRTA < VRTAL2.4 if FLAP >= FLAPL ! ! ! !
! ! ! ! ! ! !
! ! ! Limitation for Code 5100, 5200, 5300, ! ! ! !
! ! ! 5600, 5700: ! ! ! !
! ! ! Wait TURBWAIT time for re-activating ! ! ! !
! ! ! the trigger logic after the previous ! ! ! !
! ! ! report generation in the same flight ! ! ! !
! ! ! leg. ! ! ! !
! ! ! ! ! ! !
!5400!5.4 ! If one of the 5 spoiler excursion ! ! ! !
! ! ! counters has an overflow (then is 999) ! ! ! !
! ! ! ! ! ! !
! !5.5 ! n/a ! ! ! !
! ! ! ! ! ! !
!5600!5.6 ! LATAL1 <= |LATA| <= LATAL2 ! ! ! !
! ! ! ! ! ! !
!5700!5.7 ! |LATA| > LATAL2 ! ! ! !
! ! ! ! ! ! !
! !5.8 ! Importance of trigger codes: ! ! ! !
! ! ! ! ! ! !
! !5.8.1 ! Trigger codes 4xxx are more important ! ! ! !
! ! ! than trigger codes 5xxx ! ! ! !
! ! ! ! ! ! !
! !5.8.2 ! Trigger codes 5xxx are more important ! ! ! !
! ! ! than trigger code 7000 ! ! ! !
!----!-------!-----------------------------------------!----!----!---------!
! !5.9.1 ! VRTAL2.1 limit (g) A320 ! C ! C ! 2.5 !
! ! ! A321 ! C ! C ! 2.5 !
! ! ! A319 ! C ! C ! 2.5 !
! ! ! A318 ! C ! C ! 2.5 !
! ! ! ! ! ! !
! !5.9.2 ! VRTAL2.2 limit (g) A320 ! C ! C ! -1.0 !
! ! ! A321 ! C ! C ! -1.0 !
! ! ! A319 ! C ! C ! -1.0 !
! ! ! A318 ! C ! C ! -1.0 !
! ! ! ! ! ! !
! !5.9.3 ! VRTAL2.3 limit (g) A320 ! C ! C ! 2.0 !
! ! ! A321 ! C ! C ! 2.0 !
! ! ! A319 ! C ! C ! 2.0 !
! ! ! A318 ! C ! c ! 2.0 !
! ! ! ! ! ! !
! !5.9.4 ! VRTAL2.4 limit (g) A320 ! C ! C ! 0.0 !
! ! ! A321 ! C ! C ! 0.0 !
! ! ! A319 ! C ! C ! 0.0 !
! ! ! A318 ! C ! C ! 0.0 !
! ! ! ! ! ! !
! !5.9.5 ! TURBWAIT (sec) A320 ! C ! C ! 3 !
! ! ! A321 ! C ! C ! 3 !
! ! ! A319 ! C ! C ! 3 !
! ! ! A318 ! C ! C ! 3 !
! ! ! ! ! ! !
! !5.9.6 ! FLAPL (deg) A320 ! C ! C ! 0.5 !
! ! ! A321 ! C ! C ! 0.5 !
! ! ! A319 ! C ! C ! 0.5 !
! ! ! A318 ! C ! C ! 0.5 !
! ! ! ! ! ! !
! !5.9.7 ! LATAL1 (g) A320 ! C ! C ! 0.35 !
! ! ! A321 ! C ! C ! 0.35 !
! ! ! A319 ! C ! C ! 0.35 !
! ! ! A318 ! C ! C ! 0.35 !
! ! ! ! ! ! !
! !5.9.8 ! LATAL2 (g) A320 ! C ! C ! 0.41 !
! ! ! A321 ! C ! C ! 0.41 !
! ! ! A319 ! C ! C ! 0.41 !
! ! ! A318 ! C ! C ! 0.41 !
! ! ! ! ! ! !
!----!-------!-----------------------------------------!----!----!---------!
!8100!8.1 ! ACARS MU uplink request with IMI 'REQ15'! ! ! !
! ! ! The report <15> is immediately generated! ! ! !
! ! ! and transmitted to the ACARS MU ! ! ! !
+--------------------------------------------------------------------------+

B. Report Limits for Load Report <15>.
(1) CFMI Engines A318, A319, A320, A321
+-----------------------------------------------------------------------------+
!Limit ! Description of Report Item ! A318 ! A319 ! A320 !A321 ! Unit !
!No ! ! CFM ! CFM ! CFM !CFM ! !
!------!--------------------------------!-------!-------!-------!------!------!
! 321 ! increment report counter if ! 1 ! 1 ! 1 ! 1 ! !
! ! logic trig.>1000 (YES:1,NO:1) ! ! ! ! ! !
!------!--------------------------------!-------!-------!-------!------!------!
! ! RALR computing ! ! ! ! ! !
!------!--------------------------------!-------!-------!-------!------!------!
! 322 ! FC: filter frequency ! 0.3 ! 0.3 ! 0.3 ! 0.3 ! Hz !
!------!--------------------------------!-------!-------!-------!------!------!
! 323 ! DXTPIR: lever arm correction ! 29.5 ! 33.8 ! 39.0 ! 53.1 !ft/deg!
! ! (x-axis) for PTCH ! ! ! ! ! !
!------!--------------------------------!-------!-------!-------!------!------!
! 324 ! THETA0: average pitch at ! 6.0 ! 2.0 ! 6.0 ! 4.5 ! deg !
! ! touchdown ! ! ! ! ! !
!------!--------------------------------!-------!-------!-------!------!------!
! 325 ! DX: lever arm correction ! 16.8 ! 18.5 ! 18.0 ! 28.8 ! ft !
! ! (x-axis) for RALT ! ! ! ! ! !
!------!--------------------------------!-------!-------!-------!------!------!
! 326 ! DZ: lever arm correction ! 7.6 ! 7.2 ! 7.1 ! 7.8 ! ft !
! ! (z-axis) for RALT ! ! ! ! ! !
!------!--------------------------------!-------!-------!-------!------!------!
! 327 ! K1: kalman filter cte ! 5.2 ! 5.2 ! 5.2 ! 5.2 ! !
!------!--------------------------------!-------!-------!-------!------!------!
! 328 ! K2: kalman filter cte ! 25.0 ! 25.0 ! 25.0 ! 25.0 ! !
!------!--------------------------------!-------!-------!-------!------!------!
! 329 ! K3: kalman filter cte ! 5.0 ! 5.0 ! 5.0 ! 5.0 ! !
!------!--------------------------------!-------!-------!-------!------!------!
! 330 ! D: correction factor for ROLR ! 0.0 ! 0.0 ! 0.0 ! 0.0 !ft/deg!
!------!--------------------------------!-------!-------!-------!------!------!
! 331 ! RALT1 ! 150 ! 150 ! 150 ! 150 ! ft !
!------!--------------------------------!-------!-------!-------!------!------!
! 332 ! Reserved ! ! ! ! ! !
!------!--------------------------------!-------!-------!-------!------!------!
! 333 ! Reserved ! ! ! ! ! !
!------!--------------------------------!-------!-------!-------!------!------!
! 334 ! RALRL ! -9.0 ! -9.0 ! -9.0 ! -9.0 !ft/sec!
!------!--------------------------------!-------!-------!-------!------!------!
! ! RALR time intervals at ! ! ! ! ! !
! ! landing ! ! ! ! ! !
!------!--------------------------------!-------!-------!-------!------!------!
! 335 ! S1: start sample number (16Hz) ! -4 ! -4 ! -4 ! -4 ! !
!------!--------------------------------!-------!-------!-------!------!------!
! 336 ! S2: stop sample number (16Hz) ! 4 ! 4 ! 4 ! 4 ! !
!------!--------------------------------!-------!-------!-------!------!------!
! 337 ! VRTAL1.1 (at landing) ! 2.6 ! 2.6 ! 2.6 ! 2.6 ! g !
!------!--------------------------------!-------!-------!-------!------!------!
! 338 ! VRTAL1.2 (at landing) ! 2.6 ! 2.6 ! 2.6 ! 2.6 ! g !
!------!--------------------------------!-------!-------!-------!------!------!
! 339 ! VRTAL1.3 (at bounce) ! 2.6 ! 2.6 ! 2.6 ! 2.6 ! g !
!------!--------------------------------!-------!-------!-------!------!------!
! ! VTAR time intervals at ! ! ! ! ! !
! ! landing ! ! ! ! ! !
!------!--------------------------------!-------!-------!-------!------!------!
! 340 ! S3: start sample number (32Hz) ! -16 ! -16 ! -16 ! -16 ! !
!------!--------------------------------!-------!-------!-------!------!------!
! 341 ! S4: stop sample number (32Hz) ! 16 ! 16 ! 16 ! 16 ! !
!------!--------------------------------!-------!-------!-------!------!------!
! ! VTAR time intervals at ! ! ! ! ! !
! ! bounce ! ! ! ! ! !
!------!--------------------------------!-------!-------!-------!------!------!
! 342 ! S5: start sample number (32Hz) ! -16 ! -16 ! -16 ! -16 ! !
!------!--------------------------------!-------!-------!-------!------!------!
! 343 ! S6: stop sample number (32Hz) ! 16 ! 16 ! 16 ! -16 ! !
!------!--------------------------------!-------!-------!-------!------!------!
! 344 ! GWL1 ! 56000 ! 61000 ! 64500 ! 75500! Kg !
!------!--------------------------------!-------!-------!-------!------!------!
! 345 ! GWL2 ! 56000 ! 61000 ! 64500 ! 75500! Kg !
!------!--------------------------------!-------!-------!-------!------!------!
! 346 ! GWL3 ! 56000 ! 61000 ! 64500 ! 75500! Kg !
!------!--------------------------------!-------!-------!-------!------!------!
! 347 ! GWL4 ! 56000 ! 61000 ! 64500 ! 75500! Kg !
!------!--------------------------------!-------!-------!-------!------!------!
! 348 ! RALRLG ! -6.0 ! -6.0 ! -6.0 ! -6.0 !ft/sec!
!------!--------------------------------!-------!-------!-------!------!------!
! 349 ! VRTALG ! 1.7 ! 1.7 ! 1.7 ! 1.7 ! g !
!------!--------------------------------!-------!-------!-------!------!------!
! ! report data display, time ! ! ! ! ! !
! ! interval ! ! ! ! ! !
!------!--------------------------------!-------!-------!-------!------!------!
! 350 ! Y15.0: time before landing ! 1 ! 1 ! 1 ! 1 ! sec. !
! ! event ! ! ! ! ! !
!------!--------------------------------!-------!-------!-------!------!------!
! 351 ! Y15.1: time before landing ! 1 ! 1 ! 1 ! 1 ! sec. !
! ! event ! ! ! ! ! !
!------!--------------------------------!-------!-------!-------!------!------!
! 352 ! Y15.2: time after landing ! 3 ! 3 ! 3 ! 3 ! sec. !
! ! event ! ! ! ! ! !
!------!--------------------------------!-------!-------!-------!------!------!
! 353 ! Y15.3: time before bounce ! 1 ! 1 ! 1 ! 1 ! sec. !
! ! event ! ! ! ! ! !
!------!--------------------------------!-------!-------!-------!------!------!
! 354 ! Y15.4: time before bounce ! 1 ! 1 ! 1 ! 1 ! sec. !
! ! event ! ! ! ! ! !
!------!--------------------------------!-------!-------!-------!------!------!
! 355 ! Y15.5: time after bounce ! 3 ! 3 ! 3 ! 3 ! sec. !
! ! event ! ! ! ! ! !
!------!--------------------------------!-------!-------!-------!------!------!
! ! bounce landing detection ! ! ! ! ! !
!------!--------------------------------!-------!-------!-------!------!------!
! 356 ! Y15.6: ldg compress time ! 0.5 ! 0.5 ! 0.5 ! 0.5 ! sec. !
!------!--------------------------------!-------!-------!-------!------!------!
! 357 ! Y15.7: bounce minimum time ! 1.0 ! 1.0 ! 1.0 ! 1.0 ! sec. !
!------!--------------------------------!-------!-------!-------!------!------!
! 358 ! Y15.8: bounce maximum time ! 10.0 ! 10.0 ! 10.0 ! 10.0 ! sec. !
!------!--------------------------------!-------!-------!-------!------!------!
! ! In flight VRTA exeedances ! ! ! ! ! !
!------!--------------------------------!-------!-------!-------!------!------!
! 359 ! VRTAL2.1 ! 2.5 ! 2.5 ! 2.5 ! 2.5 ! g !
!------!--------------------------------!-------!-------!-------!------!------!
! 360 ! VRTAL2.2 ! -1.0 ! - 1.0 ! -1.0 ! 2.5 ! g !
!------!--------------------------------!-------!-------!-------!------!------!
! 361 ! VRTAL2.3 ! 2.0 ! 2.0 ! 2.0 ! 2.0 ! g !
!------!--------------------------------!-------!-------!-------!------!------!
! 362 ! VRTAL2.4 ! 0.0 ! 0.0 ! 0.0 ! 0.0 ! g !
!------!--------------------------------!-------!-------!-------!------!------!
! 363 ! FLAPL ! 0.5 ! 0.5 ! 0.5 ! 0.5 ! g !
!------!--------------------------------!-------!-------!-------!------!------!
! ! report limitation ! ! ! ! ! !
! ! (0 disable report) ! ! ! ! ! !
!------!--------------------------------!-------!-------!-------!------!------!
! 364 ! enable report code 4100 (m15) ! 1 ! 1 ! 1 ! 1 ! !
!------!--------------------------------!-------!-------!-------!------!------!
! 365 ! enable report code 4400 (n15) ! 1 ! 1 ! 1 ! 1 ! !
!------!--------------------------------!-------!-------!-------!------!------!
! 366 ! enable report code 4500 (p15) ! 1 ! 1 ! 1 ! 1 ! !
!------!--------------------------------!-------!-------!-------!------!------!
! 367 ! enable report code 4800 (q15) ! 1 ! 1 ! 1 ! 1 ! !
!------!--------------------------------!-------!-------!-------!------!------!
! 368 ! enable report code 4900 (q15) ! 1 ! 1 ! 1 ! 1 ! !
!------!--------------------------------!-------!-------!-------!------!------!
! 369 ! number of report code 5100 ! 10 ! 10 ! 10 ! 10 ! !
! ! per leg (s15) ! ! ! ! ! !
!------!--------------------------------!-------!-------!-------!------!------!
! 370 ! number of report code 5200 ! 10 ! 10 ! 10 ! 10 ! !
! ! per leg (t15) ! ! ! ! ! !
!------!--------------------------------!-------!-------!-------!------!------!
! 371 ! number of report code 5300 ! 10 ! 10 ! 10 ! 10 ! !
! ! per leg (u15) ! ! ! ! ! !
!------!--------------------------------!-------!-------!-------!------!------!
! 372 ! number of report code 5400 ! 10 ! 10 ! 10 ! 10 ! !
! ! per leg (v15) ! ! ! ! ! !
!------!--------------------------------!-------!-------!-------!------!------!
! 373 ! time intervals before two ! ! ! ! ! !
! ! 5xxx generation (w15) ! ! ! ! ! !
!------!--------------------------------!-------!-------!-------!------!------!
! ! counter for spoiler extensions ! ! ! ! ! !
!------!--------------------------------!-------!-------!-------!------!------!
! 374 ! SPL1 ! 0 ! 0 ! 0 ! 0 ! deg !
!------!--------------------------------!-------!-------!-------!------!------!
! 375 ! SPL2 ! -5 ! -5 ! -5 ! -5 ! deg !
!------!--------------------------------!-------!-------!-------!------!------!
! 376 ! SPL3 ! -10 ! -10 ! -10 ! -10 ! deg !
!------!--------------------------------!-------!-------!-------!------!------!
! 377 ! SPL4 ! -15 ! -15 ! -15 ! -15 ! deg !
!------!--------------------------------!-------!-------!-------!------!------!
! 378 ! SPL5 ! -20 ! -20 ! -20 ! -20 ! deg !
!------!--------------------------------!-------!-------!-------!------!------!
! 379 ! Reserved ! ! ! ! ! !
!------!--------------------------------!-------!-------!-------!------!------!
! 380 ! Reserved ! ! ! ! ! !
+-----------------------------------------------------------------------------+

C. AIDS Reports Print Rules - Default Values for Report <15>
+------------------------------------------------+
! ! ! !
! Code ! Printer Output ! ACARS-output !
! ! ! !
!-------!-----------------------!----------------!
! ! ! !
! 1000 ! Print immediatly ! No ACARS !
! ! ! !
!-------!-----------------------!----------------!
! ! ! !
! 2000 ! Print immediatly ! No ACARS !
! ! ! !
!-------!-----------------------!----------------!
! ! ! !
! 4100 ! Print at landing ! ACARS VHF !
! ! ! !
!-------!-----------------------!----------------!
! ! ! !
! 4400 ! Print at landing ! ACARS VHF !
! ! ! !
!-------!-----------------------!----------------!
! ! ! !
! 4500 ! Print at landing ! ACARS VHF !
! ! ! !
!-------!-----------------------!----------------!
! ! ! !
! 4800 ! Print at landing ! ACARS VHF !
! ! ! !
!-------!-----------------------!----------------!
! ! ! !
! 4900 ! Print at landing ! ACARS VHF !
! ! ! !
!-------!-----------------------!----------------!
! ! ! !
! 5100 ! Print at landing ! ACARS VHF !
! ! ! !
!-------!-----------------------!----------------!
! ! ! !
! 5200 ! Print at landing ! ACARS VHF !
! ! ! !
!-------!-----------------------!----------------!
! ! ! !
! 5300 ! Print at landing ! ACARS VHF !
! ! ! !
!-------!-----------------------!----------------!
! ! ! !
! 5400 ! Print at landing ! ACARS VHF !
! ! ! !
!-------!-----------------------!----------------!
! ! ! !
! 8100 ! No print ! ACARS VHF !
! ! ! !
+------------------------------------------------+

+-------------------------------------------------------------------------+
!Trigger! to ACARS ! to printer ! store !
! Code !--------------------------------+-----------------+--------------!
! No !Ground ! VHF ! SAT- ! HF ! at ! imme- ! internal& !
! ! ! ! COM ! !landing ! diate ! external !
! ! ! ! ! ! ! !(build in RAM&!
! ! ! ! ! ! ! ! PCMCIA) !
!-------+-------+--------+-------+-------+--------+--------+--------------!
! ! ! If ! ! ! ! If !PCMCIA only if!
! 1000 ! NO ! SEND ! NO ! NO ! NO ! PRINT ! STORE !
! ! !selected! ! ! !selected! selected on !
! ! !on MCDU ! ! ! !on MCDU ! MCDU !
!-------!-------!--------!-------!-------!--------!--------!--------------!
! 2000 ! NO ! NO ! NO ! NO ! ! YES ! YES !
!-------!-------!--------!-------!-------! !--------!--------------!
! 3000 ! NO ! NO ! NO ! NO ! ! NO ! YES !
!-------!-------!--------!------ !-------! !--------!--------------!
! 4100 ! NO ! YES ! NO ! NO ! ! NO ! YES !
!-------!-------!--------!-------!-------! !--------!--------------!
! 4400 ! NO ! YES ! NO ! NO ! ! NO ! YES !
!-------!-------!--------!-------!-------! !--------!--------------!
! 4500 ! NO ! YES ! NO ! NO ! ! NO ! YES !
!-------!-------!--------!-------!-------! !--------!--------------!
! 4800 ! NO ! YES ! NO ! NO ! Y ! NO ! YES !
!-------!-------!--------!-------!-------! E !--------!--------------!
! 4900 ! NO ! YES ! NO ! NO ! S ! NO ! YES !
!-------!-------!--------!-------!-------! !--------!--------------!
! 5100 ! NO ! YES ! NO ! NO ! ! NO ! YES !
!-------!-------!--------!-------!-------! !--------!--------------!
! 5200 ! NO ! YES ! NO ! NO ! ! NO ! YES !
!-------!-------!--------!-------!-------! !--------!--------------!
! 5300 ! NO ! YES ! NO ! NO ! ! NO ! YES !
!-------!-------!--------!-------!-------! !--------!--------------!
! 5400 ! NO ! YES ! NO ! NO ! ! NO ! YES !
!-------!-------!--------!-------!-------! !--------!--------------!
! 8100 ! NO ! YES ! NO ! NO ! ! NO ! YES !
+-------------------------------------------------------------------------+

+-------------------------------------------------------------------------+
!Trigger! to ACARS ! to printer ! store !
! Code !------------------------------ -!-----------------!--------------!
! No !Ground ! VHF ! SAT- ! HF ! at ! imme- ! internal& !
! ! ! ! COM ! !landing ! diate ! external !
! ! ! ! ! ! ! !(build in RAM&!
! ! ! ! ! ! ! ! PCMCIA) !
!-------!-------!--------!-------!-------!--------!--------!--------------!
! 1000 ! NO ! NO ! NO ! NO ! NO ! YES ! YES !
!-------!-------!--------!-------!-------!--------!--------!--------------!
! 2000 ! NO ! NO ! NO ! NO ! NO ! YES ! YES !
!-------!-------!--------!-------!-------!--------!--------!--------------!
! 3000 ! NO ! NO ! NO ! NO ! NO ! NO ! YES !
!-------!-------!--------!------ !-------!--------!--------!--------------!
! 4100 ! NO ! YES ! NO ! NO ! YES ! NO ! YES !
!-------!-------!--------!-------!-------!--------!--------!--------------!
! 4400 ! NO ! YES ! NO ! NO ! YES ! NO ! YES !
!-------!-------!--------!-------!-------!--------!--------!--------------!
! 4500 ! NO ! YES ! NO ! NO ! YES ! NO ! YES !
!-------!-------!--------!-------!-------!--------!--------!--------------!
! 4800 ! NO ! YES ! NO ! NO ! YES ! NO ! YES !
!-------!-------!--------!-------!-------!--------!--------!--------------!
! 4900 ! NO ! YES ! NO ! NO ! YES ! NO ! YES !
!-------!-------!--------!-------!-------!--------!--------!--------------!
! 5100 ! NO ! YES ! NO ! NO ! YES ! NO ! YES !
!-------!-------!--------!-------!-------!--------!--------!--------------!
! 5200 ! NO ! YES ! NO ! NO ! YES ! NO ! YES !
!-------!-------!--------!-------!-------!--------!--------!--------------!
! 5300 ! NO ! YES ! NO ! NO ! YES ! NO ! YES !
!-------!-------!--------!-------!-------!--------!--------!--------------!
! 5400 ! NO ! YES ! NO ! NO ! YES ! NO ! YES !
!-------!-------!--------!-------!-------!--------!--------!--------------!
! 8100 ! NO ! YES ! NO ! NO ! NO ! NO ! YES !
+-------------------------------------------------------------------------+

+-------------------------------------------------------------------------+
!Trigger! to ACARS ! to printer ! store !
! Code !--------------------------------!-----------------!--------------!
! No !Ground ! VHF ! SAT- ! HF ! at ! imme- ! internal& !
! ! ! ! COM ! !landing ! diate ! external !
! ! ! ! ! ! ! !(build in RAM&!
! ! ! ! ! ! ! ! PCMCIA) !
!-------!-------!--------!-------!-------!--------!--------!--------------!
! 1000 ! NO ! NO ! NO ! NO ! NO ! YES ! YES !
!-------!-------!--------!-------!-------!--------!--------!--------------!
! 2000 ! NO ! NO ! NO ! NO ! NO ! YES ! YES !
!-------!-------!--------!-------!-------!--------!--------!--------------!
! 3000 ! NO ! NO ! NO ! NO ! NO ! NO ! YES !
!-------!-------!--------!------ !-------!--------!--------!--------------!
! 4100 ! NO ! YES ! NO ! NO ! YES ! NO ! YES !
!-------!-------!--------!-------!-------!--------!--------!--------------!
! 4400 ! NO ! YES ! NO ! NO ! YES ! NO ! YES !
!-------!-------!--------!-------!-------!--------!--------!--------------!
! 4500 ! NO ! YES ! NO ! NO ! YES ! NO ! YES !
!-------!-------!--------!-------!-------!--------!--------!--------------!
! 4800 ! NO ! YES ! NO ! NO ! YES ! NO ! YES !
!-------!-------!--------!-------!-------!--------!--------!--------------!
! 4900 ! NO ! YES ! NO ! NO ! YES ! NO ! YES !
!-------!-------!--------!-------!-------!--------!--------!--------------!
! 5100 ! NO ! YES ! NO ! NO ! YES ! NO ! YES !
!-------!-------!--------!-------!-------!--------!--------!--------------!
! 5200 ! NO ! YES ! NO ! NO ! YES ! NO ! YES !
!-------!-------!--------!-------!-------!--------!--------!--------------!
! 5300 ! NO ! YES ! NO ! NO ! YES ! NO ! YES !
!-------!-------!--------!-------!-------!--------!--------!--------------!
! 5400 ! NO ! YES ! NO ! NO ! YES ! NO ! YES !
!-------!-------!--------!-------!-------!--------!--------!--------------!
! 8100 ! NO ! YES ! NO ! NO ! NO ! NO ! YES !
+-------------------------------------------------------------------------+

NOTE: For detailed description of the trigger codes, refer to Para. (3) Load Report Logic.
+-------------------------------------------------------------------------+
!Trigger! to ACARS ! to printer ! store !
! Code !--------------------------------!-----------------!--------------!
! No !Ground ! VHF ! SAT- ! HF ! at ! imme- ! internal& !
! ! ! ! COM ! !landing ! diate ! external !
! ! ! ! ! ! ! !(build in RAM&!
! ! ! ! ! ! ! ! PCMCIA) !
!-------!-------!--------!-------!-------!--------!--------!--------------!
! 1000 ! NO ! NO ! NO ! NO ! NO ! YES ! YES !
!-------!-------!--------!-------!-------!--------!--------!--------------!
! 2000 ! NO ! NO ! NO ! NO ! NO ! YES ! YES !
!-------!-------!--------!-------!-------!--------!--------!--------------!
! 3000 ! NO ! NO ! NO ! NO ! NO ! NO ! YES !
!-------!-------!--------!------ !-------!--------!--------!--------------!
! 4310 ! NO ! YES ! NO ! NO ! YES ! NO ! YES !
!-------!-------!--------!-------!-------!--------!--------!--------------!
! 4320 ! NO ! YES ! NO ! NO ! YES ! NO ! YES !
!-------!-------!--------!-------!-------!--------!--------!--------------!
! 4410 ! NO ! YES ! NO ! NO ! YES ! NO ! YES !
!-------!-------!--------!-------!-------!--------!--------!--------------!
! 4420 ! NO ! YES ! NO ! NO ! YES ! NO ! YES !
!-------!-------!--------!-------!-------!--------!--------!--------------!
! 4510 ! NO ! YES ! NO ! NO ! YES ! NO ! YES !
!-------!-------!--------!-------!-------!--------!--------!--------------!
! 4520 ! NO ! YES ! NO ! NO ! YES ! NO ! YES !
!-------!-------!--------!-------!-------!--------!--------!--------------!
! 4610 ! NO ! YES ! NO ! NO ! YES ! NO ! YES !
!-------!-------!--------!-------!-------!--------!--------!--------------!
! 4620 ! NO ! YES ! NO ! NO ! YES ! NO ! YES !
!-------!-------!--------!-------!-------!--------!--------!--------------!
! 5100 ! NO ! YES ! NO ! NO ! YES ! NO ! YES !
!-------!-------!--------!-------!-------!--------!--------!--------------!
! 5200 ! NO ! YES ! NO ! NO ! YES ! NO ! YES !
!-------!-------!--------!-------!-------!--------!--------!--------------!
! 5300 ! NO ! YES ! NO ! NO ! YES ! NO ! YES !
!-------!-------!--------!-------!-------!--------!--------!--------------!
! 5400 ! NO ! YES ! NO ! NO ! YES ! NO ! YES !
!-------!-------!--------!-------!-------!--------!--------!--------------!
! 5600 ! NO ! YES ! NO ! NO ! YES ! NO ! YES !
!-------!-------!--------!-------!-------!--------!--------!--------------!
! 5700 ! NO ! YES ! NO ! NO ! YES ! NO ! YES !
!-------!-------!--------!-------!-------!--------!--------!--------------!
! 7000 ! NO ! NO ! NO ! NO ! NO ! NO ! YES !
!-------!-------!--------!-------!-------!--------!--------!--------------!
! 8100 ! NO ! YES ! NO ! NO ! NO ! NO ! YES !
+-------------------------------------------------------------------------+

NOTE: For detailed description of the trigger codes, refer to Para. (3) Load Report Logic.
[Rev.10 from 2021] 2026.04.01 03:58:18 UTC
"Aviabrain" 2025