Reports description and operation
** ON A/C 010-017, 103-104
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- EMB SB 31-1341 for A/C 010-017, 103-104
| ** 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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