** ON A/C 010-017, 103-104
POST SB 31-1319 for A/C 025-025, 027-028, 108-109, 452-452
POST SB 31-1391 for A/C 025-025, 027-028, 108-109, 452-452
EMB SB 31-1168 for A/C 108-109
EMB SB 31-1179 for A/C 108-109
EMB SB 31-1341 for A/C 010-017, 103-104
(1)
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. Otherwise these lines are omitted (inclusive header lines 41, 42, 45, 48 and 49).
Customer : AEE
Type : A318/A319/A320/A321
Rev. Date : Aug 01, 2017
Manual : AMM
Selected applicability : ALL
31-37-51 PB 001 CONF 00 - AIDS - STRUCTURE
REPORTS - DESCRIPTION AND OPERATION
Print Date: September 27, 2018
Page 24 of 83
© AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.
+---------------------------------------------------------------------+
! 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 !
! ! !
! ! 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 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 ! (00 to 24) !
! ! FMGC 1 and 2 (FGC part) for Auto Pilot 1 and 2 !
!!-------------!--------------------!-------------------!------------!!
!!Auto Pilot ! Parameter for AP1 ! Parameter for 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 !!
Customer : AEE
Type : A318/A319/A320/A321
Rev. Date : Aug 01, 2017
Manual : AMM
Selected applicability : ALL
31-37-51 PB 001 CONF 00 - AIDS - STRUCTURE
REPORTS - DESCRIPTION AND OPERATION
Print Date: September 27, 2018
Page 25 of 83
© AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.
!! ! ! !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 !!
Customer : AEE
Type : A318/A319/A320/A321
Rev. Date : Aug 01, 2017
Manual : AMM
Selected applicability : ALL
31-37-51 PB 001 CONF 00 - AIDS - STRUCTURE
REPORTS - DESCRIPTION AND OPERATION
Print Date: September 27, 2018
Page 26 of 83
© AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.
!! ! 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 !
! ! !
! ! 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 on the parameter !
! ! !
! ! Source: Depends on the parameter !
! ! !
! ! Remark: If code = 4500 the limit which was exceeded !
! ! is displayed in reference to MAX either at landing !
! ! or at bounce landing. !
Customer : AEE
Type : A318/A319/A320/A321
Rev. Date : Aug 01, 2017
Manual : AMM
Selected applicability : ALL
31-37-51 PB 001 CONF 00 - AIDS - STRUCTURE
REPORTS - DESCRIPTION AND OPERATION
Print Date: September 27, 2018
Page 27 of 83
© AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.
!--------------!------------------------------------------------------!
! 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 __________________________! !
! ! !
! ! 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 XXXXXXXXXX !
! XXXXXXXXXX ! Format: 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 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 !
Customer : AEE
Type : A318/A319/A320/A321
Rev. Date : Aug 01, 2017
Manual : AMM
Selected applicability : ALL
31-37-51 PB 001 CONF 00 - AIDS - STRUCTURE
REPORTS - DESCRIPTION AND OPERATION
Print Date: September 27, 2018
Page 28 of 83
© AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.
! ! 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 !
! ! Remark: The calculation of Radio Altitude Rate is !
! ! started when: RALT
! ! - 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 !
Customer : AEE
Type : A318/A319/A320/A321
Rev. Date : Aug 01, 2017
Manual : AMM
Selected applicability : ALL
31-37-51 PB 001 CONF 00 - AIDS - STRUCTURE
REPORTS - DESCRIPTION AND OPERATION
Print Date: September 27, 2018
Page 29 of 83
© AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.
! ! *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 !
! ! param. 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 !
! ! param. 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 !
! ! param. 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 !
! ! param. 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. !
! ! -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 shown with 'N' on the !
! ! first position. Otherwise the first position is !
! ! used for the value. !
! ! -3.00 to 6.00 g !
Customer : AEE
Type : A318/A319/A320/A321
Rev. Date : Aug 01, 2017
Manual : AMM
Selected applicability : ALL
31-37-51 PB 001 CONF 00 - AIDS - STRUCTURE
REPORTS - DESCRIPTION AND OPERATION
Print Date: September 27, 2018
Page 30 of 83
© AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.
! ! param. 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) !
! ! param. 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) !
! ! param. SDAC 29.1.332.01 !
! ! 29.2.332.01 !
+---------------------------------------------------------------------+
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