7/22/2019 A320 Sil 00-028 CFDS Anomalies http://slidepdf.com/reader/full/a320-sil-00-028-cfds-anomalies 1/203 CUSTOMER SERVICES DIRECTORATE AIRBUS1 ROND POINT MAURICE BELLONTE 31707 BLAGNAC CEDEX FRANCE TELEPHONE + 33 (0)5 61 93 33 33 TELEX AIRBU 530526F SERVICE INFORMATION LETTER SUBJECT:ATA CHAPTER:AIRCRAFT TYPE:APPLICABILITY:Centralized Fault Display System (CFDS) Anomalies A318, A319, A320, A321 All Aircraft 00
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1. The ATA chapter of the message or warning to be filtered if applicable.
2. The first line of the message or warning to be filtered if applicable.
3. The second line of the message or warning to be filtered if applicable.
4. The Flight phase criteria if applicable.
5. The source criteria if applicable.
6. The P/N which is concerned by the anomaly.
7. The name of the part which is concerned by the anomaly.
Nota 5: A character “_” means that a space has to be entered by the operator when creating a filter itemmanually through MFT.
Nota 6: CFDIU specificity:
To prevent duplication of messages in the filter content, a character “$” is used instead of theposition number where the computer is installed i e VHF $ instead of VHF 1 VHF 2 VHF 3
For short term, Airbus recommend all operators, having activated both the filtering function and the real timewarning transmission, to remove the ECAM warnings from the filter list (only the warning, not the BITEmessage faults).
Consequence:
All spurious warnings will be received at each flight but none will be missing. Maintenance should refer to the appendix part E of the present SIL to isolate the spurious
warning via the Airbus SIL/Airline comments if it is a known spurious. Maintenance should use the filtering function of ground software tools.
3. MATERIAL INFORMATION
Part E of this SIL - Filter Content - is available on floppy disk - called “Filenv31.320” (31: Revisionnumber).For customization, refer to Maintenance Filter Tool (MFT) - SIL 00-088.
- select the SIL 00-028 folder to access the package content.
Note that Filter Envelop used for A320, A330 and A340 require the Maintenance Filter Tool(MFT). Please refer to SIL 00-088 which explains how to install MFT.
Aircraft Communication Addressing & Reporting SystemAir Conditionning System ControlerAudio Control PanelAir Data Inertial Reference UnitAutomatic Direction FinderAir Data ReferenceAvionic Equipment Ventilation ControllerAuto Flight SystemAircraft Integrated Data System
Aircraft Maintenance ManualAudio Management UnitAngle-Of-AttackAuxiliary Power UnitAssemblyAir Transport Association
Environmental Control SystemEngine Control UnitEngine Fire Detection UnitEngine Interface UnitElevator Aileron ComputerEngine Vibration Monitoring UnitFull Authority Digital Engine ControlFlight Augmentation ComputerFlight Control DisplayFlight Control Data ConcentratorFuel Control and Management ComputerFlight Control UnitFlow control Valve
Flight Data Interface Management UnitFlight Data Interface UnitFlight GuidanceFunctional Item NumberFlight LevelFlight ManagementFli h M & G id C
Maintenance Planning DocumentMaintenance Review BoardManufacturer Serial NumberMean Time Between FailuresMean Time Between RemovalMean Time Between Unscheduled RemovalManagement Unit
Navigation Display
Nose Landing Gear Nautic MilesOn Board Replaceable ModuleOverheatPublic AddressPack ControllerP l U i
2 163 34 S DA Ci : N O DA TA FR OM E CS j ( I= 1 o r 2 ) ( J=1 o r2)
NO MAINT. ACTION if occurs in phase 6 TFU 216334051 N
Part Affected P/N Corrective P/NZONE CONTROLLER 775A0000-06 775A0000-07
2 163 34 E IUi : NO ZO NE CO NT j DA TA ( i=1 o r 2 ) ( j=P o rS) Associated with ECAM warning : ENG1(2) BLEED STATUS FAULT.NO MAINT. ACTION on A/C equipped with CFM engines TFU 732900029TFU 216334051 N
Part Affected P/N Corrective P/NZONE CONTROLLER 775A0000-06 775A0000-07
2 163 34 E IUi N O ZO NE CO NT j DA TA (i =1 or 2) (j =P orS)
NO MAINT. ACTION If not associated to Maintenance Status : ENG1(2)EIU TFU 732534005TFU 732534042
228112 FCU(2CA)CP-L BUS/ WXRi(1SQi) (i = 1 or 2) No maintenance action required if no logbook complaint. N
Part Affected P/N Corrective P/NRADAR 822-1710-201 822-1710-202
228112 FCU(2CA)CP-R BUS/ WXRi(1SQi) (i = 1 or 2) No maintenance action required if no logbook complaint. N
Part Affected P/N Corrective P/NRADAR 822-1710-201 822-1710-202
228112 FCU(3CA)CP-L BUS/ WXRi 1SQi (I=1 or 2) NO MAINT. ACTION if recorded during Engine Start (flight phase 02) or duringswitching from WXR1 to WXR2 and no associated cockpit effect.
N
Part Affected P/N Corrective P/N
RADAR 822-1710-201 822-1710-202
228112 FCU(3CA)CP-R BUS/ WXRi 1SQi (I=1 or 2) NO MAINT. ACTION if recorded during Engine Start (flight phase 02) or duringswitching from WXR1 to WXR2 and no associated cockpit effect.
N
Part Affected P/N Corrective P/N
RADAR 822-1710-201 822-1710-202
2 281 12 RA DA Ri :NO DA TA FRO M EF IS j P ANE L ( i=1 o r2) (j =1 or 2)
228334 FMGCi(1CAi)/ RMPi(1RGi)/ ILSi(1RTi) ( i = 1 or 2) No maintenance act ion i f no FM auto reset reported in the logbook. Airbus_SIL 22-038Airbus_SIL 22-037
228334 FMGCi(1CAi) BUS MMR/ MMRi (40RTi) Reset FMGC1 when i equal 1. Reset FMGC2 when i equal 2. If in the MMR1 (2)Ground Scanning , fault message "FMGC BUS ILS/MMR" or in the TSD "PORT B RXFAIL" are recorded, carry out associated TSM task.
TSM_Task 343600810870TSM_Task 343600810871
N
Part Affected P/N Corrective P/NMMR 822-1152-121 VSB COLLINS GLU_920-34-19
2 283 34 A FS : F MGC i ( i= 1 o r 2 ) M es sa ge tr ig ge re d f ol lo wi ng r ese t of FM GC 1 ( or 2) fo ll ow ing vo lun tar y d isco nn ec ti onof one FD during Taxi or Roll-outNo Maint. Action.
228334 FMGCi(1CAi)/ RMPi(1RGi)/ ILSi(1RTi) ( i = 1 or 2) No maintenance act ion i f no FM auto reset reported in the logbook. Airbus_SIL 22-038Airbus_SIL 22-037
N
Part Affected P/N Corrective P/NFMGC ALL P/N NONE
228334 FMGCi(1CAi) BUS MMR/ MMRi (40RTi) Reset FMGC1 when i equal 1. Reset FMGC2 when i equal 2. If in the MMR1 (2)Ground Scanning , fault message "FMGC BUS ILS/MMR" or in the TSD "PORT B RXFAIL" are recorded, carry out associated TSM task.
TSM_Task 343600810870TSM_Task 343600810871
N
Part Affected P/N Corrective P/NMMR 822-1152-121 VSB COLLINS GLU_920-34-19
2 283 34 A FS : F MGC i ( i= 1 o r 2 ) M es sa ge tr ig ge re d f ol lo wi ng r ese t of FM GC 1 ( or 2) fo ll ow ing vo lun tar y d isco nn ec ti onof one FD during Taxi or Roll-outNo Maint. Action.
228334 FMGCi (1CAi)/ RMPi(1RGi)/ILSi(2RTi) (i=1 or 2) No maintenance action if not logbook complaint N
Part Affected P/N Corrective P/NRECEIVER ILS 066-50006-X202 TBDRECEIVER ILS 622-9738-041 822-0298-020
228334 FMGECi(1CAi)/ RMPi(1RGi)/ILSi(1RTi) No maintenance action if no logbook entry N
Part Affected P/N Corrective P/NRECEIVER ILS 622-9738-041 N/A
231100 ICAO ADDRESS/HFi(3REi) (i=0, 1, 2) This message is triggered if Datalink not activated (MOD 31286)and CFDIU Label157 not received within 30s after HFDR power-up. This message is associated withCLASS3 Fault message "462134 ATSU(1TX1)/ HFi(3Ri)"NO MAINT. ACTION.
Y
Part Affected P/N Corrective P/NHFDR 822-0990-003 TBD
231111 CHECK HFi ANTENNA CIRCUIT (i=1 or 2 or 3) NO MAINT ACTION if no log book entry TFU 231100002 N
231133 HFDRi(3REi)/ATSU1(1TX1) (i=1 or 2) spurious message if HFDR not activated and CFDIU PRE STD 9B (Source name"ACARS MU" in the PFR)NO MAINT. ACTION
231133 HFDRi(3REi)/ATSU1(1TX1) (i=1 or 2) spurious message if HFDR not activated and CFDIU PRE STD 9B (Source name"ACARS MU" in the PFR)NO MAINT. ACTION
232834 SDU1(5RV1)/ATSU1(1TX1) Generated by ATSU when SATCOM not installed.Disregard when SATCOM not installed. This message may be displayed on PFR,System Test and Ground scanning.
TFU 460000002 Y
Part Affected P/N Corrective P/NATSU PLAT SW LA2T0S162C0C0F1 LA2T0S111C1B0F1
237300 DIR1 (101RH)/ OBRM Spurious message due to software anomaly.A CIDS interface and power-up test must be performed to confirm validity of thefailure and to clear the failure message from the ground report.
Airbus_SIL 23-039 N
Part Affected P/N Corrective P/NOBRM CIDS DIR Z064H000030F Z064H000032AOBRM CIDS DIR Z064H000031B Z064H000032AOBRM CIDS DIR Z064H000031C Z064H000032AOBRM CIDS DIR Z064H000031D Z064H000032AOBRM CIDS DIR Z064H000031A Z064H000032A
2 373 00 FA P 1 (12 0RH) / DI Ri /CA M ( i= 1 o r 2 ) S pu rio us fa ul t m es sa ge d ue to p owe r tr an sf er .Check the validity of the FAP failure message, please select the FAP status page.Should any anomaly be visible on subject page, please refer to the correspondingtrouble shooting task.
Airbus_SIL 23-039 N
Part Affected P/N Corrective P/NOBRM CIDS DIR Z064H000031B Z064H000032AOBRM CIDS DIR Z064H000031A Z064H000032AOBRM CIDS DIR Z064H000031D Z064H000032AOBRM CIDS DIR Z064H000031C Z064H000032A
237300 DIR1 (101RH)/ OBRM Spurious message due to software anomaly.A CIDS interface and power-up test must be performed to confirm validity of thefailure and to clear the failure message from the ground report.
Airbus_SIL 23-039 N
Part Affected P/N Corrective P/N
OBRM CIDS DIR Z064H000030F Z064H000032AOBRM CIDS DIR Z064H000031B Z064H000032AOBRM CIDS DIR Z064H000031C Z064H000032A
OBRM CIDS DIR Z064H000031D Z064H000032AOBRM CIDS DIR Z064H000031A Z064H000032A
2 373 00 FA P 1 (12 0RH) / DI Ri /CA M ( i= 1 o r 2 ) S pu rio us fa ul t m es sa ge d ue to p owe r tr an sf er .Check the validity of the FAP failure message, please select the FAP status page.Should any anomaly be visible on subject page, please refer to the correspondingtrouble shooting task.
Airbus_SIL 23-039 N
Part Affected P/N Corrective P/N
OBRM CIDS DIR Z064H000031B Z064H000032AOBRM CIDS DIR Z064H000031A Z064H000032AOBRM CIDS DIR Z064H000031D Z064H000032AOBRM CIDS DIR Z064H000031C Z064H000032A
237313 AAP(126RH)ATT 4L/ DEU B (300RH7) Software anomaly.Maintenance advice: If an AAP failure message is recorded into the PFR, perform avisual check of the AAP¨operation to determine the validity of the fault message.
Airbus_SIL 23-039 N
Part Affected P/N Corrective P/NOBRM CIDS DIR Z064H000030F Z064H000031BOBRM CIDS DIR Z064H000030F Z064H000031A
237313 AAP(126RH)ATT 4L Software anomaly.Maintenance advice: If an AAP failure message is recorded into the PFR, perform avisual check of the AAP¨operation to determine the validity of the fault message.
Airbus_SIL 23-039 N
Part Affected P/N Corrective P/NOBRM CIDS DIR Z064H000030F Z064H000031BOBRM CIDS DIR Z064H000030F Z064H000031A
237313 AAP(126RH)ATT 4L/ DEU B (300RH7) Software anomaly.Maintenance advice: If an AAP failure message is recorded into the PFR, perform avisual check of the AAP¨operation to determine the validity of the fault message.
Airbus_SIL 23-039 N
Part Affected P/N Corrective P/NOBRM CIDS DIR Z064H000030F Z064H000031BOBRM CIDS DIR Z064H000030F Z064H000031A
237313 AAP(126RH)ATT 4L Software anomaly.Maintenance advice: If an AAP failure message is recorded into the PFR, perform avisual check of the AAP¨operation to determine the validity of the fault message.
Airbus_SIL 23-039 N
Part Affected P/N Corrective P/NOBRM CIDS DIR Z064H000030F Z064H000031BOBRM CIDS DIR Z064H000030F Z064H000031A
237322 AIP(320RH1)ATT 1L Due to a Software anomaly, subject class III fault may be triggered onto the PFR.Maintenance advice: A CIDS interface and power-up test should be performed toconfirm validity of the failure message. The associated time may be completelyerroneous.
Airbus_SIL 23-039 N
Part Affected P/N Corrective P/NOBRM CIDS DIR Z064H000030F Z064H000031A
237322 AIP(320RH9)ATT 4L Due to a Software anomaly, subject class III fault may be triggered onto the PFR.Maintenance advice: A CIDS interface and power-up test should be performed toconfirm validity of the failure message. The associated time may be completelyerroneous.
Airbus_SIL 23-039 N
Part Affected P/N Corrective P/N
OBRM CIDS DIR Z064H000030F Z064H000031A
237322 AIP(320RH1)ATT 1L Due to a Software anomaly, subject class III fault may be triggered onto the PFR.Maintenance advice: A CIDS interface and power-up test should be performed toconfirm validity of the failure message. The associated time may be completelyerroneous.
Airbus_SIL 23-039 N
Part Affected P/N Corrective P/NOBRM CIDS DIR Z064H000030F Z064H000031A
237322 AIP(320RH9)ATT 4L Due to a Software anomaly, subject class III fault may be triggered onto the PFR.Maintenance advice: A CIDS interface and power-up test should be performed toconfirm validity of the failure message. The associated time may be completelyerroneous.
237334 CIDS2(102RH) Problem of a discrete label status computed by the CIDS2 and used by ACSC 1 and2.If Associated with MAINT STATUS TEMP CTL 1 and TEMP CTL 2 then NO MAINT.ACTION is required.
Airbus_SIL 23-039 N
Part Affected P/N Corrective P/N
ACSC 1803A0000-03 1803A0000-04
240000 POWER SUPPLY INTERRUPT NO MAINT. ACTION Airbus_SIL 23-039 Y
240000 POWER SUPPLY INTERRUPT No Maintenance act ion i f occurs during PWR transfer: Phase 01 and 02 (Enginestart-up), Phase 09 and 10 (Engine Shut Down).
Y
Part Affected P/N Corrective P/NEIS II SOFTWARE SXT3FE2SA0410 SXT4EE2SA050A
EIS II SOFTWARE SXT3CE2SA0420 SXT4EE2SA050A
240000 POWER SUPPLY INTERRUPT NO MAINTENANCE ACTION N
Part Affected P/N Corrective P/NRECEIVER ILS 066-50008-0301 066-50008-0405
240000 POWER SUPPLY INTERRUPT NO MAINT. ACTION Airbus_SIL 23-039 Y
240000 POWER SUPPLY INTERRUPT No Maintenance act ion i f occurs during PWR transfer: Phase 01 and 02 (Enginestart-up), Phase 09 and 10 (Engine Shut Down).
Y
Part Affected P/N Corrective P/NEIS II SOFTWARE SXT3FE2SA0410 SXT4EE2SA050AEIS II SOFTWARE SXT3CE2SA0420 SXT4EE2SA050A
240000 POWER SUPPLY INTERRUPT NO MAINTENANCE ACTION N
Part Affected P/N Corrective P/NRECEIVER ILS 066-50008-0301 066-50008-0405
242151 IDGI DISCONNECTED (i=1 or 2) nullCheck Class 3 Fault messages
Airbus_SB 24-1077TFU 244100002
N
Part Affected P/N Corrective P/NGPCU 740121A 740121B
242151 IDGi(Ei-4000XU)OIL LEVELSENSOR/GCUi(1XUi) (i=1 or 2)
Quality issue affecting component inside the GCU. Ony GCUs manufactured beforeNov 2002 are affected.When message is triggered, the GCU should be removed and sent to vendorHamilton Sundstrand for repair.
TFU 242100039 N
Part Affected P/N Corrective P/N
GCU 767584J
242151 IDGI DISCONNECTED (i=1 or 2) nullCheck Class 3 Fault messages
242151 IDGi(Ei-4000XU)OIL LEVELSENSOR/GCUi(1XUi) (i=1 or 2)
Quality issue affecting component inside the GCU. Ony GCUs manufactured beforeNov 2002 are affected.When message is triggered, the GCU should be removed and sent to vendorHamilton Sundstrand for repair.
TFU 242100039 N
Part Affected P/N Corrective P/N
GCU 767584J
242151 IDGI DISCONNECTED (i=1 or 2) null
Check Class 3 Fault messages
Airbus_SB 24-1077
TFU 244100002
N
Part Affected P/N Corrective P/N
GPCU 740121A 740121B
242255 AFS:28V PWR 11XU1 No MAINT. ACTION if occurs during PWR transfer: Phase 02 (Engine start-up),Phase 09 and 10 (Engine Shut Down)
Y
Part Affected P/N Corrective P/N
FMGC ALL P/N
242300 CHECK GCU APU PIN C1,C5 GEN APU PINA9,A10
null1.If associated with a generator trip : remove the APU generator, otherwise, NOMAINT.ACTION. 2.If APU GEN FAULT immediately after APU start,reset APU GENP/B SW. on OVHD panel.
Airbus_SB 24-1074TFU 244100008
N
Part Affected P/N Corrective P/NGCU 740120B 740120CGCU 740120A 740120C
243251 SDACi:NO TR1 CURRENT 1PU1 (i=1 or 2) At APU start NO MAINT. ACTION TFU 315500003 Y
Part Affected P/N Corrective P/NSDAC 350E5161122 350E5151331SDAC 350E5151022 350E5151331
261715 SMK DET LAV X Associated to PFR ECAM WARNING "260000 SMOKE LAV DET FAULT".Perform a CIDS reset to recover lavatory smoke detection function as described inSIL 23-039 Rev6
261715 SMK DET LAV X CONTAMINATION Associated to PFR ECAM WARNING "260000 SMOKE LAV DET FAULT".Perform a CIDS reset to recover lavatory smoke detection function as described inSIL 23-039 Rev6
261715 SMK DET LAV X Associated to PFR ECAM WARNING "260000 SMOKE LAV DET FAULT".Perform a CIDS reset to recover lavatory smoke detection function as described in
261715 SMK DET LAV X CONTAMINATION Associated to PFR ECAM WARNING "260000 SMOKE LAV DET FAULT".Perform a CIDS reset to recover lavatory smoke detection function as described inSIL 23-039 Rev6
Airbus_SIL 23-039 N
Part Affected P/N Corrective P/NDIRECTOR-CIDS Z014H000131A Z014H000131A_AMDT_B
261734 SDCU CHANNEL 2(10WQ) NO MAINT. ACTION if reset of the SDCU clears the message TFU 261734012Airbus_SB 92-1021
N
Part Affected P/N Corrective P/NSDCU RAI2800M0706 POST SB 92_1021
275100 SFCCi OR FLP PPU POWER (I=1 or 2) If recorded in PFR without associated warning, NO MAINTENANCE ACTION
required. If recorded in the PFR with the associated Ecam Warning: "F/CTL FLAPSYSi FAULT" or "F/CTL FLAP LOCKED" perform a manual reset of the SFCCthrough the SFCC MCDU BITE menu: SFCC/WTB RESET.Only a batch of SFCC is affected: SFCC PN 49-170-10 , [SN 1732 --> SN 1934]SFCC PN 49-170-07 , [SN 1743 --> SN 1904]
TFU 275134025 N
Part Affected P/N Corrective P/NSFCC 49-117-10 49-170-11SFCC 49-170-07 49-170-11
275100 SLT/FLT CSU 51CV OR WIRING TOSLT1(2)/FLP1(2)
If recorded in PFR without warning No MAINT. ACTION required. If Warning refer toTFU 27 51 00 004
TFU 275100004 N
Part Affected P/N Corrective P/N
SFCC 49-170-11 49-170-11 AMDT_A
275100 SFCCi OR FLP PPU POWER (i=1 or 2) If associated with failure message FLP1(2) PCU VALVEBLOCK 23(24) CV.Corrective action: replace SFCC at the origin of the fault.Please also refer to OIT 999.0047/05 Only a batch of SFCC is affected: SFCC PN49-170-11 , [SN 5813 --> SN 5956]
N
Part Affected P/N Corrective P/N
SFCC 49-170-11
275100 SFCCi OR FLP PPU POWER (I=1 or 2) If recorded in PFR without associated warning, NO MAINTENANCE ACTIONrequired. If recorded in the PFR with the associated Ecam Warning: "F/CTL FLAPSYSi FAULT" or "F/CTL FLAP LOCKED" perform a manual reset of the SFCCthrough the SFCC MCDU BITE menu: SFCC/WTB RESET.
Only a batch of SFCC is affected: SFCC PN 49-170-10 , [SN 1732 --> SN 1934]SFCC PN 49-170-07 , [SN 1743 --> SN 1904]
275100 SLT/FLT CSU 51CV OR WIRING TOSLT1(2)/FLP1(2)
If recorded in PFR without warning No MAINT. ACTION required. If Warning refer toTFU 27 51 00 004
TFU 275100004 N
Part Affected P/N Corrective P/NSFCC 49-170-11 49-170-11 AMDT_A
275100 SFCCi OR FLP PPU POWER (i=1 or 2) If associated with failure message FLP1(2) PCU VALVEBLOCK 23(24) CV.
Corrective action: replace SFCC at the origin of the fault.Please also refer to OIT 999.0047/05 Only a batch of SFCC is affected: SFCC PN49-170-11 , [SN 5813 --> SN 5956]
N
Part Affected P/N Corrective P/N
SFCC 49-170-11
2 751 34 S DA Ci :NO D AT A FRO M S FC Cj ( i=1 o r 2 , j =1 o r2)
275453 FLP1(2) PCU VALVEBLOCK 23(24) CV If associated with failure message SFCC1(2) or FLP PPU POWER. Corrective action:replace SFCC at the origin of the fault.Only a batch of SFCC is affected: SFCC PN 49-170-11 , [SN 5813 --> SN 5956]
N
Part Affected P/N Corrective P/N
SFCC 49-170-11
278100 SFCCi OR SLT PPU POWER (i=1 or 2) If recorded in PFR without warning: NO MAINTENANCE ACTION required. Ifassociated with Ecam Warning: "F/CTL SLAT SYSi FAULT" or "F/CTL SLATLOCKED" performed a SFCC/WTB reset through the MCDU.
If this ECAM message is reported, perform functional BITE test of the ICTVs - FLSSStatus (AMM 28-15-00-740-002) and a functional BITE test of the low-level sensors -FLSS BITE (AMM 28-46-00-740-001). No further action is required if both test of theFLSS status and FLSS BITE show NO FAULT.
284248 FUEL QUANTITY R ULTRACOMP 52QT On A321 a/c only, the failure message FUEL QUANTITY R ULTRACOMP 52QT isspurious if triggered during flight phase 6. This is due to Ultracomp 52QTmeasurement being out of range. There are no associated flightdeck effects.No maintenance actions. Message can be filtered from the PFR.
284634 FUEL LEVEL SENSING L (or R) UNFULLSENSOR 25QJ1 (or 25QJ2 or 26QJ1 or 26QJ2)
NO MAINT. ACTION if triggered in flight phase 02 N
Part Affected P/N Corrective P/N
COMPUTER-FQI ALL P/N
284634 FUEL LEVEL SENSING FLSCU1(2) 7QJ (9QJ) If this fault is reported in the PFR, perform the FLSCU BITE test (AMM28-46-00-740-001). If the test shows NO FAULT then no further action is required.
N
Part Affected P/N Corrective P/NLEVEL SENSING ALL P/N
3 071 51 DRA IN MAS T HE ATE R MI D V al id o nly i f Mo d. 2 15 98 e mb od ie d a nd DRA IN MA ST A SS Y PN DRA IN MA ST AS SY4-60000H800-00 or DRAIN MAST ASSY 4-60000H840-00 is installed.NO MAINT. ACTION if no blockage or system malfunction reported.
3 071 51 DRA IN MAS T HE ATE R MI D V al id o nly i f Mo d 2 159 8 e mb od ied . Re pl ace th e d ra in ma st ev en i f t he fa ul t is n otconfirmed on ground.
Airbus_SB 30-1030TFU 307100003
N
Part Affected P/N Corrective P/NDRAIN MAST ASSY 4-60000H880-00 4-60000H882-00
307151 DRAINMAST HEATER AFT (FWD) NO MAINT. ACTION if no blockage or system malfunction reported. Airbus_SB 30-1030TFU 307100002
3 071 51 DRA IN MAS T HE ATE R MI D V al id o nly i f Mo d. 2 15 98 e mb od ie d a nd DRA IN MA ST A SS Y PN DRA IN MA ST AS SY4-60000H800-00 or DRAIN MAST ASSY 4-60000H840-00 is installed.NO MAINT. ACTION if no blockage or system malfunction reported.
3 071 51 DRA IN MAS T HE ATE R MI D V al id o nly i f Mo d 2 159 8 e mb od ied . Re pl ace th e d ra in ma st ev en i f t he fa ul t is n otconfirmed on ground. Airbus_SB 30-1030TFU 307100003 N
Part Affected P/N Corrective P/NDRAIN MAST ASSY 4-60000H880-00 4-60000H882-00
307151 DRAINMAST HEATER AFT (FWD) NO MAINT. ACTION if no blockage or system malfunction reported. Airbus_SB 30-1030TFU 307100002
3 071 51 DRA IN MAS T HE ATE R MI D V al id o nly i f Mo d. 2 15 98 e mb od ie d a nd DRA IN MA ST A SS Y PN DRA IN MA ST AS SY4-60000H800-00 or DRAIN MAST ASSY 4-60000H840-00 is installed.NO MAINT. ACTION if no blockage or system malfunction reported.
3 071 51 DRA IN MAS T HE ATE R MI D V al id o nly i f Mo d. 2 15 98 e mb od ie d a nd DRA IN MA ST A SS Y PN DRA IN MA ST AS SY4-60000H800-00 or DRAIN MAST ASSY 4-60000H840-00 is installed.NO MAINT. ACTION if no blockage or system malfunction reported.
3 071 51 DRA IN MAS T HE ATE R MI D V al id o nly i f Mo d 2 159 8 e mb od ied . Re pl ace th e d ra in ma st ev en i f t he fa ul t is n otconfirmed on ground. Airbus_SB 30-1030TFU 307100003 N
Part Affected P/N Corrective P/NDRAIN MAST ASSY 4-60000H880-00 4-60000H882-00
307151 DRAINMAST HEATER AFT (FWD) NO MAINT. ACTION if no blockage or system malfunction reported. Airbus_SB 30-1030TFU 307100002
307151 DRAINMAST HEATER AFT (FWD) Replace the drainmast even if the fault is not confirmed on ground. Airbus_SB 30-1030TFU 307100003
N
Part Affected P/N Corrective P/NDRAIN MAST ASSY 4-60000H880-00 4-60000H882-00
3 071 51 DRA IN MAS T HE ATE R MI D V al id o nly i f Mo d. 2 15 98 e mb od ie d a nd DRA IN MA ST A SS Y PN DRA IN MA ST AS SY4-60000H800-00 or DRAIN MAST ASSY 4-60000H840-00 is installed.NO MAINT. ACTION if no blockage or system malfunction reported.
3 071 51 DRA IN MAS T HE ATE R MI D V al id o nly i f Mo d 2 159 8 e mb od ied . Re pl ace th e d ra in ma st ev en i f t he fa ul t is n otconfirmed on ground.
Airbus_SB 30-1030TFU 307100003
N
Part Affected P/N Corrective P/NDRAIN MAST ASSY 4-60000H880-00 4-60000H882-00
311234 FLPi NO CFDIU DATA (i=1 or 2) Wrong ATA chapter. Should be 313434 instead. N
313522 AFS:PRINTER Printer failure seen by the AFS. May also be triggered in flight in case of PRINTERdoor opening.No Maint. Action if no logbook entry regarding AFS report printing failure. Operatormay decide to filter this message if flight crew confirmed that they open the printerdoor.
Y
Part Affected P/N Corrective P/NPRINTER ALL P/N N/A
313634 NO DMU DATA (INTM) No Maintenance Action required N
Part Affected P/N Corrective P/NDMU 795040-30-001
313652 DAR No Maintenance Action required N
Part Affected P/N Corrective P/N
DMU 795040-30-001 795040-31-002
313652 DAR TAPE LOW No Maintenance Action required N
323171 LGCIU i 05GAi (i=1 or 2) NO MAINT. ACTION TFU 323134043 N
Part Affected P/N Corrective P/NLGCIU 664700500A4A 664700500A4B
323171 CHECK LGCIU-PHC3 INTERFACE NO MAINT. ACTION if t riggered in FWC f light phase 06 or 07 and i f not associatedwith fault message "L/G EXT PROX SNSR 24GA(25GA) TGT POS"
N
Part Affected P/N Corrective P/NBSCU E21327001 TBDBSCU E21327003 TBD
324224 SDACi:NO DATA FROM BSCU1+2 (i=1 or 2) Wrong ATA REF. Should be 324234 instead.All FWC in BASIC configuration (Pre Mod 24159) are affected (E2, E3, E4, F2).
324224 SDACi:NO DATA FROM BSCU1 (i=1 or 2) Wrong ATA REF. Should be 324234 instead.All FWC in BASIC configuration (Pre Mod 24159) are affected (E2, E3, E4, F2)
324224 SDACI:NO DATA FROM BSCU1 (i=1 or 2) NO MAINT. ACTION if no Log Book complaint N
Part Affected P/N Corrective P/NSDAC 350E5161122 350E5151331SDAC 350E5151022 350E5151331
324224 SDACi:NO DATA FROM BSCU1+2 (i=1 or 2) Wrong ATA REF. Should be 324234 instead.All FWC in BASIC configuration (Pre Mod 24159) are affected (E2, E3, E4, F2).
324224 SDACi:NO DATA FROM BSCU1 (i=1 or 2) Wrong ATA REF. Should be 324234 instead.All FWC in BASIC configuration (Pre Mod 24159) are affected (E2, E3, E4, F2)
324234 SDACi:NO DATA FROM BSCU2 (i=1 or 2) NO MAINT. ACTION if no Log Book complaint N
Part Affected P/N Corrective P/NSDAC 350E5161122 350E5151331SDAC 350E5151022 350E5151331
3 242 34 NO B SCU i DA TA ( i= 1 or 2) R ep la ce t he B SCU a s pe r I SB A3 20 -3 2- 13 -18 . B rak ing an d s te rr ing fu ncti on s a re n otaffected by the anomaly described in TFU 32.42.34.049
324234 BSCU (10GG) NO MAINT. ACTION if the associated TSD shows fault code 530 AND if triggered onground during Engine start or Engine shut-down AND A/C equipped with BSCS EMM(mod 26925).
N
Part Affected P/N Corrective P/NBSCU E21327003 E21327004
3 242 34 NO B SCU i DA TA ( i= 1 or 2) R ep la ce t he B SCU a s pe r I SB A3 20 -3 2- 13 -18 . B rak ing an d s te rr ing fu ncti on s a re n otaffected by the anomaly described in TFU 32.42.34.049
324234 BSCU (10GG) NO MAINT. ACTION if the associated TSD shows fault code 530 AND if triggered onground during Engine start or Engine shut-down AND A/C equipped with BSCS EMM(mod 26925).
324327 BRK ALTN SERVOVLV (43GG) Wrong servo valve FIN number. Should be 40GG instead. TSM_Task 324300810802TSM_Task 324300810803
N
Part Affected P/N Corrective P/NBSCU E213270B1 TBD
324327 BRK ALTN SERVOVLV (40GG) Wrong servo valve FIN number. Should be 43GG instead. TSM_Task 324300810802TSM_Task 324300810803
N
Part Affected P/N Corrective P/NBSCU E213270B1 TBD
324327 BRK ALTN SERVOVLV (43GG) Wrong servo valve FIN number. Should be 40GG instead. TSM_Task 324300810802TSM_Task 324300810803
N
Part Affected P/N Corrective P/N
BSCU E213270B1 TBD
324334 ABCU(95GG)/ BRK SELECTOR VALVE(23GG) NO MAINT. ACTION if triggered in flight phase 01 or 02 on A/C equipped with BSCSEMM (mod 26925)
N
Part Affected P/N Corrective P/N
BSCU E21327003 E21327004
3 244 18 S DA Ci : L H Y B RK P RE SS XD CR 6 3G G. ( i=1 O R2)
A)NO MAINT ACTION if not associated with the fault message "BRK ALTN PRESSTRANSDUCER 101GG" Source BSCU. B)Wrong FIN number coded in FWC BITEmessage. Should be 101GG instead.Message to be filtered if BSCU POST MOD 26925 and FWC PN 350E053020606are embodied.
Y
Part Affected P/N Corrective P/N
FWC 350E053020606 350E053020707
3 244 18 S DA Ci : R H Y B RK PRE SS X DCR 6 2G G. ( i=1 OR2)
A) NO MAINT ACTION if not associated with fault message "BRK ALTN PRESSTRANSDUCER 100GG" Source BSCU. B) Wrong FIN number coded in FWC BITEmessage. Should be 100GG instead.Message to be filtered if BSCU POST MOD 26925 and FWC PN 350E053020606
Part Affected P/N Corrective P/NFWC 350E053020606 350E053020707
3 244 18 S DA Ci : L H Y B RK P RE SS XD CR 6 3G G. ( i=1 O R2)
A)NO MAINT ACTION if not associated with the fault message "BRK ALTN PRESSTRANSDUCER 101GG" Source BSCU. B)Wrong FIN number coded in FWC BITEmessage. Should be 101GG instead.Message to be filtered if BSCU POST MOD 26925 and FWC PN 350E053020606are embodied.
Y
Part Affected P/N Corrective P/NFWC 350E053020606 350E053020707
3 244 18 S DA Ci : R H Y B RK PRE SS X DCR 6 2G G. ( i=1 OR2)
A) NO MAINT ACTION if not associated with fault message "BRK ALTN PRESSTRANSDUCER 100GG" Source BSCU. B) Wrong FIN number coded in FWC BITEmessage. Should be 100GG instead.Message to be filtered if BSCU POST MOD 26925 and FWC PN 350E053020606are embodied.
Y
Part Affected P/N Corrective P/NFWC 350E053020606 350E053020707
324553 PARK BRAKE SELECTOR
VALVE(102GG)/BSCU(10GG)
This message may be triggered when the park brake is applied with the park
accumulator depressurized.No Maint. Action if triggered in phase 02.
3 251 51 S TE ER ING E LE CTRO H YDR AU LI C M ODU LE6GC
No MAINT. ACTION if fault message triggered after Landing Gear free fall extensionand code 58 (code 6A on A320 with BOGIE) has been recorded in BSCU BITE.
N
Part Affected P/N Corrective P/NBSCU C202163 SERIES N/ABSCU PRE MOD 26925BSCU C202452 SERIES N/A
325151 STEERING ELECTRO-HYD MODULE(6GC) No MAINT. ACTION if fault message triggered after Landing Gear free fall extensionand code 654 has been recorded in BSCU BITE.
N
Part Affected P/N Corrective P/NBSCU E21327 SERIES N/ABSCU PRE MOD 26925
3 251 51 S TE ER ING E LE CTRO H YDR AU LI C M ODU LE6GC
No MAINT. ACTION if fault message triggered after Landing Gear free fall extensionand code 58 (code 6A on A320 with BOGIE) has been recorded in BSCU BITE.
N
Part Affected P/N Corrective P/NBSCU C202163 SERIES N/A
BSCU PRE MOD 26925BSCU C202452 SERIES N/A
325151 STEERING ELECTRO-HYD MODULE(6GC) No MAINT. ACTION if fault message triggered after Landing Gear free fall extensionand code 654 has been recorded in BSCU BITE.
N
Part Affected P/N Corrective P/N
BSCU E21327 SERIES N/ABSCU PRE MOD 26925
341119 AOA SENSOR 3FPi (i=1 , 2 or 3) Associated with the ECAM warning ANTI ICE CAPT (F/O,STBY) AOA. TFU 303100016Other TSM-ATA30
TFU 303134006
N
Part Affected P/N Corrective P/N
PHC 1663214200 1663214301
Revision 31 PART A
ATA Failure Messages Remark Doc X Ref F
341119 AOA SNSRi (3FPi)/ ADIRUi(1FPi) (i 1 2 or 3) NO MAINTENANCE ACTION if appears after an AOA test TFU 341000017 N
341234 AFS:ADIRU1/2/3 DISAGREE NO MAINT. ACTION if not associated to any message in the ADIRU Bite TFU 229100009 Y
Part Affected P/N Corrective P/N
FAC B397CAM0101 B397BAM0509FAC B397BAM0407 B397BAM0509FAC B397BAM0406 B397BAM0509FAC B397CAM0102 B397BAM0509
341234 NO ADIRUi DATA CHECK WIRING TOSLT(FLP)i (i=1 or 2)
When this message is followed by 27-51-34 SFCC1(2), 21(22)CV ignore this secondmessage.
TFU 275144003 N
Part Affected P/N Corrective P/N
SFCC 49-117-06 49-117-07
341234 AFS:ADIRU1/2/3 DISAGREE No maintenance action if no logbook complaint TFU 220000012 Y
Part Affected P/N Corrective P/N
FAC B397AAM0507 B397BAM0513FAC B397AAM0508 B397BAM0513FAC B397BAM0406 B397BAM0513FAC B397BAM0407 B397BAM0513
Revision 31 PART A
ATA Failure Messages Remark Doc X Ref F
341234 RADARi: NO DATA FROM ADIRU (i=1 or 2) The fault appears during ground test Repeat test If result OK no further MAINT V en dor S IL 9 5- 29 Re v1 N
341234 ADIRU2+3(1FP2+3)BUS IR/ WXR2(1SQ2) May be triggered if PWS function is set to auto when ADIRU alignement is not
completed or during an engine start.If no logbook complaint, do not remove the RTA-4B from the aircraft. Power cyclingthe RTA-4B or executing the Radar Test on the MCDU will clear the nuisance fault ifit continues to be displayed in Ground Scanning.
341234 ADIRU1+3(1FP1+3)BUS IR/ WXR1(1SQ1) May be triggered by the Honeywell RTA-4B family Transceiver if PWS function is set
to auto when ADIRU alignement is not completed or during an engine start.If no logbook complaint, do not remove the Transceiver from the aircraft. Powercycling the Transceiver or executing the Radar Test on the MCDU will clear thenuisance fault if it continues to be displayed in Ground Scanning.
341234 ADIRU2+3(1FP2+3)BUS IR/ WXR2(1SQ2) May be triggered if PWS function is set to auto when ADIRU alignement is notcompleted or during an engine start.If no logbook complaint, do not remove the RTA-4B from the aircraft. Power cyclingthe RTA-4B or executing the Radar Test on the MCDU will clear the nuisance fault ifit continues to be displayed in Ground Scanning.
341234 ADIRU1+3(1FP1+3)BUS IR/ WXR1(1SQ1) May be triggered by the Honeywell RTA-4B family Transceiver if PWS function is setto auto when ADIRU alignement is not completed or during an engine start.If no logbook complaint, do not remove the Transceiver from the aircraft. Powercycling the Transceiver or executing the Radar Test on the MCDU will clear thenuisance fault if it continues to be displayed in Ground Scanning.
343631 ILSi RECEIVER (i=1 or 2) NO MAINT. ACTION if no Log book complaint TFU 343600004 Y
Part Affected P/N Corrective P/NRECEIVER ILS 204-1230-3518 204-1230-3521RECEIVER ILS 204-1230-3518 204-1230-3532
343631 AFS:ILSi (i= 1 or 2) NO MAINT. ACTION if occurs at the end of the flight Y
Part Affected P/N Corrective P/NFMGC ALL P/N TBD
343631 FWCi :NO DATA FROM ILSj (i=1 or 2)(j=1 or 2) NO MAINT ACTION if occurs in flight phases 02 and 07. Y
Part Affected P/N Corrective P/NRECEIVER ILS 622-9738-020 622-9738-041
343631 ILSi(2RTi) (i=1 or 2) This message is triggered when receiver not tuned to any station and a self test isperformed.NO MAINT. ACTION required if no logbook complaint.
N
Part Affected P/N Corrective P/N
RECEIVER ILS 622-9738-041 VSB COLLINS ILS-720-34-11
RECEIVER ILS 622-9738-020 VSB COLLINS ILS-720-34-6
Revision 31 PART A
ATA Failure Messages Remark Doc X Ref F
343631 MMR1 (40RT1)/GPWC (1WZ) NO MAINT. ACTION required Y
344112 WXR CTL PNL(3SQ)/ WXRi(1SQi) (i = 1 or 2) NO MAINT. ACTION if recorded during Engine Start (flight phase 02) or duringswitching from WXR1 to WXR2 and no associated cockpit effect.
N
Part Affected P/N Corrective P/NRADAR 822-1710-201 822-1710-202
344112 RADAR1 CONTROL UNIT NO MAINT. ACTION if no log book complaint N
Part Affected P/N Corrective P/N
RADAR 622-5132-120 VSB WRT-701X_34-77
RADAR 622-5132-020 VSB WRT-701X_34-68
Revision 31 PART A
ATA Failure Messages Remark Doc X Ref F
344112 WXR CTL PNL(3SQ)/ WXRi(1SQi) (i = 1 or 2) NO MAINT. ACTION if recorded during Engine Start (flight phase 02) or duringswitching from WXR1 to WXR2 and no associated cockpit effect.
344133 DMCi: NO WXRj CHj DATA (i=1, 2 or 3; j=1 or 2) Associated to ECAM warning "NAV PRED W/S DET FAULT". Perform AMM Task31-60-00-740-002 "EIS Input TEST". If test ok, the WXR/DMC interface worksproperly and the WXR transceiver units should not be removed. If the test fails, applycorresponding TSM 34-41-00-810-8x "Loss of Weather Radar Channel j busidentified by the EIS i".
N
Part Affected P/N Corrective P/NRADAR 622-5132-622 TBDRADAR 622-5132-623 TBD
344133 RADAR1 TRANSCEIVER NO MAINT. ACTION if no log book complaint N
344133 RADARi TRANSCEIVER (i=1 or 2) NO MAINT ACTION if message recorded immediately after engine start (this i temconcerns only 2 airlines).
Y
Part Affected P/N Corrective P/NRADAR MI585306402 TBD
Revision 31 PART A
ATA Failure Messages Remark Doc X Ref F
3 441 33 WX Ri (1S Qi ) ( i=1 o r 2 ) T hi s fa ul t msg m ay b e tr ig ge re d i f r ad ar se lec te d O FF a nd Pr ed Wi nd sh ear sca nn ingautomatically activated during take-off or approach.N M i A i if f l d d i h PFR i h k i ff d i
344133 DMCi: NO WXRj CHj DATA (i=1, 2 or 3; j=1 or 2) Associated to ECAM warning "NAV PRED W/S DET FAULT". Perform AMM Task31-60-00-740-002 "EIS Input TEST". If test ok, the WXR/DMC interface worksproperly and the WXR transceiver units should not be removed. If the test fails, applycorresponding TSM 34-41-00-810-8x "Loss of Weather Radar Channel j busidentified by the EIS i".
N
Part Affected P/N Corrective P/NRADAR 622-5132-622 TBDRADAR 622-5132-623 TBD
344133 RADAR1 TRANSCEIVER NO MAINT. ACTION if no log book complaint N
Part Affected P/N Corrective P/NRADAR MI585306402 TBD
3 441 33 WX Ri (1S Qi ) ( i=1 o r 2 ) T hi s fa ul t msg m ay b e tr ig ge re d i f r ad ar se lec te d O FF a nd Pr ed Wi nd sh ear sca nn ingautomatically activated during take-off or approach.
No Maint. Action if fault msg recorded in the PFR without cockpit effect and isassociated with specific TSD (final 4 digits "0000").
344133 WXRi(1SQi) (i= 1 or 2) No maintenance action if no logbook complaint. N
Part Affected P/N Corrective P/NRADAR 822-1710-201 822-1710-202
3 441 37 WX R MO UN TING TRA Y( 5S Q)/ WX Ri (1 SQi ) ( i =1 or 2)
No maintenance action required if no logbook complaint. N
Part Affected P/N Corrective P/N
RADAR 822-1710-201 822-1710-202
344233 RA1 (2SA1)+RA2 (2SA2)/ WXR1 (1SQ1) If no logbook complaint, do not remove the radar RTA-4B from the aircraft. Powercycling the RTA-4B or executing the Radar Test on the MCDU will clear the nuisancefault if it continues to be displayed in Ground Scanning.
N
Part Affected P/N Corrective P/N
RADAR 066-50008-407 TBD
RADAR 066-50008-409 TBDRADAR 066-50008-405 TBD
Revision 31 PART A
ATA Failure Messages Remark Doc X Ref F
344233 RA1 (2SA1)+RA2 (2SA2)/ WXR2 (1SQ2) If no logbook complaint, do not remove the radar RTA-4B from the aircraft. Powercycling the RTA-4B or executing the Radar Test on the MCDU will clear the nuisancefault if it continues to be displayed in Ground Scanning
344233 RA1(2SA1)+RA2((2SA2)/ WXRi (1SQi) (I=1 or 2) NO MAINT. ACTION if recorded during Engine Start (flight phase 02) or duringswitching from WXR1 to WXR2 and no associated cockpit effect. N
Part Affected P/N Corrective P/NRADAR 822-1710-201 822-1710-202
344233 RA1 (2SA1)+RA2 (2SA2)/ WXR1 (1SQ1) If no logbook complaint, do not remove the radar RTA-4B from the aircraft. Powercycling the RTA-4B or executing the Radar Test on the MCDU will clear the nuisancefault if it continues to be displayed in Ground Scanning.
N
Part Affected P/N Corrective P/NRADAR 066-50008-407 TBDRADAR 066-50008-409 TBD
RADAR 066-50008-405 TBD
344233 RA1 (2SA1)+RA2 (2SA2)/ WXR2 (1SQ2) If no logbook complaint, do not remove the radar RTA-4B from the aircraft. Powercycling the RTA-4B or executing the Radar Test on the MCDU will clear the nuisancefault if it continues to be displayed in Ground Scanning.
344233 RA1(2SA1)+RA2((2SA2)/ WXRi (1SQi) (I=1 or 2) NO MAINT. ACTION if recorded during Engine Start (flight phase 02) or duringswitching from WXR1 to WXR2 and no associated cockpit effect.
N
Part Affected P/N Corrective P/N
RADAR 822-1710-201 822-1710-202
Revision 31 PART A
ATA Failure Messages Remark Doc X Ref F
3 443 00 DMC( i) : NO TC AS D AT A ( i = 1 or 2 o r 3 ) N o ma int ena nce ac ti on r equ ir ed i f no l og bo ok c om pl ai nt an d i f TCA S B ITE i s OK . T FU 3 44 30 001 1 N
Part Affected P/N Corrective P/NTCAS 7517900-10002TCAS 822-1293-322TCAS 7517900-10003TCAS 622-8971-320TCAS 622-8971-322
3 443 00 DMC( i) : NO TC AS D AT A ( i = 1 or 2 o r 3 ) N o ma int ena nce ac ti on r equ ir ed i f no l og bo ok c om pl ai nt an d i f TCA S B ITE i s OK . T FU 3 44 30 001 1 N
3 443 00 DMC( i) : NO TC AS D AT A ( i = 1 or 2 o r 3 ) N o ma int ena nce ac ti on r equ ir ed i f no l og bo ok c om pl ai nt an d i f TCA S B ITE i s OK . T FU 3 44 30 001 1 N
3 443 00 DMC( i) : NO TC AS D AT A ( i = 1 or 2 o r 3 ) N o ma int ena nce ac ti on r equ ir ed i f no l og bo ok c om pl ai nt an d i f TCA S B ITE i s OK . T FU 3 44 30 001 1 N
3 443 33 FWC i :N O DA TA FR OM TCA S ( i = 1 o r 2 ) N o ma int ena nce ac ti on r equ ir ed i f no l og bo ok c om pl ai nt an d i f TCA S B ITE i s OK . T FU 344 30 001 1 N
3 443 33 FWC i :N O DA TA FR OM TCA S ( i = 1 o r 2 ) N o ma int ena nce ac ti on r equ ir ed i f no l og bo ok c om pl ai nt an d i f TCA S B ITE i s OK . T FU 344 30 001 1 N
3 443 33 FWC i :N O DA TA FR OM TCA S ( i = 1 o r 2 ) N o ma int ena nce ac ti on r equ ir ed i f no l og bo ok c om pl ai nt an d i f TCA S B ITE i s OK . T FU 344 30 001 1 N
Part Affected P/N Corrective P/NTCAS 7517900-10002 N/ATCAS 7517900-10003 N/A
3 443 33 FWC i :N O DA TA FR OM TCA S ( i = 1 o r 2 ) N o ma int ena nce ac ti on r equ ir ed i f no l og bo ok c om pl ai nt an d i f TCA S B ITE i s OK . T FU 344 30 001 1 N
3 443 33 FWC i :N O DA TA FR OM TCA S ( i = 1 o r 2 ) N o ma int ena nce ac ti on r equ ir ed i f no l og bo ok c om pl ai nt an d i f TCA S B ITE i s OK . T FU 344 30 001 1 N
344333 NO TCAS DATA No maintenance action required if no logbook complaint and if TCAS BITE is OK. TFU 344300011 N
Part Affected P/N Corrective P/N
TCAS 822-1293-322 N/ATCAS 622-8971-320 N/A
TCAS 622-8971-322 N/A
Revision 31 PART A
ATA Failure Messages Remark Doc X Ref F
3 443 33 FWC i :N O DA TA FR OM TCA S ( i = 1 o r 2 ) N o ma int ena nce ac ti on r equ ir ed i f no l og bo ok c om pl ai nt an d i f TCA S B ITE i s OK . T FU 344 30 001 1 N
344334 ATC- i :NO DATA FROM TCAS (i = 1 or 2) No maintenance action required if associated to the TCAS fault message "344334TCAS (1SG)" and if TCAS BITE is OK.
344334 TCAS (1SG) No maintenance action required if no logbook complaint and if TCAS BITE is OK. TFU 344300011 N
Part Affected P/N Corrective P/N
TCAS 7517900-10003 N/ATCAS 7517900-10002 N/A
3 443 34 A TC- i :NO DA TA FRO M T CA S ( i = 1 or 2) N o ma int ena nce ac ti on r equ ir ed i f no l og bo ok c om pl ai nt an d i f TCA S B ITE i s OK . T FU 344 30 001 1 N
3 443 34 A TC- i :NO DA TA FRO M T CA S ( i = 1 or 2) N o ma int ena nce ac ti on r equ ir es i f n o l og bo ok co mp la in t a nd i f TCA S B ITE i s O K. T FU 344 30 001 1 N
3 443 34 A TC- i :NO DA TA FRO M T CA S ( i = 1 or 2) N o ma int ena nce ac ti on r equ ir ed i f no l og bo ok c om pl ai nt an d i f TCA S B ITE i s OK . T FU 344 30 001 1 N
344334 ATC- i :NO DATA FROM TCAS (i = 1 or 2) No maintenance action required if associated to the TCAS fault message "344334TCAS (1SG)" and if TCAS BITE is OK.
TFU 344300004 N
Part Affected P/N Corrective P/NTCAS 066-50000-0102TCAS 066-50000-0208 TPA-81A-34-75REV1
344334 TCAS (1SG) No maintenance action required if no logbook complaint and if TCAS BITE is OK. TFU 344300011 N
Part Affected P/N Corrective P/N
TCAS 7517900-10003 N/ATCAS 7517900-10002 N/A
Revision 31 PART A
ATA Failure Messages Remark Doc X Ref F
3 443 34 A TC- i :NO DA TA FRO M T CA S ( i = 1 or 2) N o ma int ena nce ac ti on r equ ir ed i f no l og bo ok c om pl ai nt an d i f TCA S B ITE i s OK . T FU 344 30 001 1 N
3 443 34 A TC- i :NO DA TA FRO M T CA S ( i = 1 or 2) N o ma int ena nce ac ti on r equ ir es i f n o l og bo ok co mp la in t a nd i f TCA S B ITE i s O K. T FU 344 30 001 1 N
3 443 34 A TC- i :NO DA TA FRO M T CA S ( i = 1 or 2) N o ma int ena nce ac ti on r equ ir ed i f no l og bo ok c om pl ai nt an d i f TCA S B ITE i s OK . T FU 344 30 001 1 N
Part Affected P/N Corrective P/NTCAS 7517900-10003 N/ATCAS 7517900-10002 N/A
344334 TCAS (1SG) No maintenance action required if no logbook complaint and if TCAS BITE is OK. TFU 344300011 N
345133 AFS:DMEi (i=1 or 2) Due to A/C out of emitter range. No Maint. Action if no Log Book complaint.Message to be filtered on A/C equipped with FMGC LEGACY and INTERROGATORDME P/N 622-4540-023
345133 AFS:DMEi (i=1 or 2) Due to A/C out of emitter range. No Maint. Action if no Log Book complaint.Message to be filtered on A/C equipped with FMGC LEGACY and INTERROGATORDME P/N 622-4540-023
345133 AFS:DMEi (i=1 or 2) NO MAINT ACTION if no log book complaint Y
Part Affected P/N Corrective P/NFMGC C13043AA01 TBD
345212 ATC CTL PNL (2SH) / ATCi (1SHi) (i = 1 or 2) Wrong FIN number (2SH). Correct one is (3SH) for SA. No maintenance actionrequired.
N
Part Affected P/N Corrective P/N
TRANSPONDER-ATC 7517800-10005 TBD
Revision 31 PART A
ATA Failure Messages Remark Doc X Ref F
345233 ATCi (1SHi)/TCAS (1SG) (i = 1 or 2) No maintenance action required if not associated to ECAM WARNING "NAV TCASFAULT". CLASS 1 fault message when ATC transponder is the active one. CLASS 3fault message if the ATC transponder is in standby (See PART C).
Part Affected P/N Corrective P/NTCAS 7517900-10002 N/ATCAS 7517900-10003 N/A
345233 ATCi(1SHi)/TCAS(100SG) (i = 1 or 2) No maintenance action required if not associated to ECAM WARNING "NAV TCASFAULT". CLASS 1 fault message when ATC transponder is the active one. CLASS 3
fault message if the ATC transponder is in standby (See PART C).
N
Part Affected P/N Corrective P/NT2CAS 9000000-10110 TBD
3 452 33 NO A TCi DA TA ( i = 1 o r 2 ) N o ma int ena nce ac ti on r equ ir ed i s re qu ir ed if n o l og boo k co mp la int a nd i f AT C B IT Eis OK.
N
Part Affected P/N Corrective P/NTRANSPONDER-ATC 7517800-10002 TBDTRANSPONDER-ATC 7517800-10005 TBD
3 452 33 Q UAL IFIE R Ci /WX Rj (1 SQ j) ( i = 1 or 2 a nd j = 1or 2)
No maintenance action if no logbook complaint. N
Part Affected P/N Corrective P/NRADAR 822-1710-201 822-1710-202
345233 ATCi (1SHi)/TCAS (1SG) (i = 1 or 2) No maintenance action required if not associated to ECAM WARNING "NAV TCASFAULT". CLASS 1 fault message when ATC transponder is the active one. CLASS 3fault message if the ATC transponder is in standby (See PART C).
TFU 344300011 N
Part Affected P/N Corrective P/N
TCAS 7517900-10002 N/ATCAS 7517900-10003 N/A
Revision 31 PART A
ATA Failure Messages Remark Doc X Ref F
345233 ATCi(1SHi)/TCAS(100SG) (i = 1 or 2) No maintenance action required if not associated to ECAM WARNING "NAV TCASFAULT". CLASS 1 fault message when ATC transponder is the active one. CLASS 3fault message if the ATC transponder is in standby (See PART C).
Part Affected P/N Corrective P/NT2CAS 9000000-10110 TBD
3 452 33 NO A TCi DA TA ( i = 1 o r 2 ) N o ma int ena nce ac ti on r equ ir ed i s re qu ir ed if n o l og boo k co mp la int a nd i f AT C B IT Eis OK.
N
Part Affected P/N Corrective P/NTRANSPONDER-ATC 7517800-10002 TBDTRANSPONDER-ATC 7517800-10005 TBD
3 452 33 Q UAL IFIE R Ci /WX Rj (1 SQ j) ( i = 1 or 2 a nd j = 1or 2)
No maintenance action if no logbook complaint. N
Part Affected P/N Corrective P/NRADAR 822-1710-201 822-1710-202
345331 ADFi(1RPI) (i=1, 2 or 3) Wrong FIN number. Should be 2RP1 for ADF1 and 2RP2 for ADF2. Issue due to
wrong FIN number coded by ADF BITE when installed on A320 fam. A/C.Update ADF receiver with VSB COLLINS SB 2
N
Part Affected P/N Corrective P/N
RECEIVER ADF 822-0299-020 POST_VSB_COLLINS_SB2
345331 NO ADF(i) DATA (i=1 or 2) No maintenance action when ADF 1 or/and 2 not installed on the aircraft. Y
Part Affected P/N Corrective P/N
CFDIU ALL P/N
Revision 31 PART A
ATA Failure Messages Remark Doc X Ref F
345331 ADFi(1RPI) (i=1, 2 or 3) Wrong FIN number. Should be 2RP1 for ADF1 and 2RP2 for ADF2. Issue due towrong FIN number coded by ADF BITE when installed on A320 fam. A/C.Update ADF receiver with VSB COLLINS SB 2
Part Affected P/N Corrective P/NVSC 14404-011A 14404-011B
3 831 41 TO IL ET A SS Y L AV i ( wi th i = A , D, E, o r F ) S oft wa re a no ma lyThe system operation can be checked on ground by using the MCDU toilet groundreport or by selecting the FAP Water/Waste page.
Airbus_SIL 23-039TFU 383100026
Y
Part Affected P/N Corrective P/NOBRM CIDS DIR Z064H000030D Z064H000031AOBRM CIDS DIR Z064H000030D Z064H000030FOBRM CIDS DIR Z064H000030E Z064H000031B
383163 LIQD LVL XMTR (40MG) Software anomalyThe system operation can be checked on ground by using the MCDU toilet groundreport or by referring the FAP Water/Waste page.
Airbus_SIL 23-039TFU 383100026
Y
Part Affected P/N Corrective P/NOBRM CIDS DIR Z064H000030D Z064H000031AOBRM CIDS DIR Z064H000030E Z064H000031BOBRM CIDS DIR Z064H000030F Z064H000031A
383168 DIFF PRESS XDCR NO MAINT. ACTION if 42MG XDCR has been disconnected. Airbus_SB 38-1027TFU 383100003TSM_Task ATA38
N
Part Affected P/N Corrective P/NVSC 14404-001-1 14404-011A
Revision 31 PART A
ATA Failure Messages Remark Doc X Ref F
492316 LCDT SENSOR P29 No MAINT. ACTION Airbus_SB 49-1061 Y
493211 FUEL CTL UNIT P19 NO MAINT. ACTION if no logbook complaint Airbus_SB 49-1053 N
Part Affected P/N Corrective P/N
ECB 304817-1 304817-2
496134 SDACi:NO DATA FROM ECB (i=1 or 2) NO MAINT. ACTION if no Log Book complaint (GTCP36.300) N
Part Affected P/N Corrective P/N
SDAC 350E5151022 350E5151331
SDAC 350E5161122 350E5151331
499414 OIL PRESS SW P14 NO MAINT. ACTION if no logbook complaint N
Part Affected P/N Corrective P/N
ECB 304817-1 304817-2
Revision 31 PART A
ATA Failure Messages Remark Doc X Ref F
4 996 51 A PU O IL HE ATE R (8 09 3KM ) N O MA INT. A CTI ON r eq ui re d o n A /C p ost SB 49 -1 026 an d A PU 3 6- 30 0 p reHoneywell VSB 49-6702 and ECB P/N 3888394-230300 or ECB P/N 304817-1 orECB P/N 304817-2
5 200 00 DO OR B TL X Y/ DEU B ( 30 0RHZ) ( X=1 , 3 o r 4 )
(Y=R or L )(Z=1, 6 or 8)
No maintenance action required. N
Part Affected P/N Corrective P/NOBRM CIDS DIR Z064H000030F Z064H000031AOBRM CIDS DIR Z064H000030F Z064H000031B
7 311 50 FRV (CL OSE D) ,J7 (J8 ), ECU N O MA INTE NA NC E AC TIO N i f t rig ge re d d ur in g FA DE C mo to ri ng te st a nd i f E CU5.BE or 5.DE not fitted on A/C.
TFU 732900033 N
Part Affected P/N Corrective P/NECU 1820M89P02 SB_73-1034ECU 1820M88P02
ECU 1820M36P02 SB_73-1037ECU 1820M87P02
7 321 60 DMCi :NO E CUi A (B ) DA TA N o Ma int . Ac ti on i f i t o cc urs i n p ha se 0 1 o r 0 2 a t th e e nd o f an en gi ne r un ( 80 KTS n otreached) or after any FADEC reset.Message to be filtered on CFM eng A/C
Y
Part Affected P/N Corrective P/N
DMC - EIS 1 ALL P/N
Revision 31 PART A
ATA Failure Messages Remark Doc X Ref F
7 321 60 E CU( Ei- 40 00 KS ) ( i=1 o r 2 ) N o Ma int . Ac ti on i f i t o cc urs i n p ha se 0 1 o r 0 2 a t th e e nd o f an en gi ne r un ( 80 KTS n otreached) or after any FADEC reset.Message to be filtered on CFM eng A/C and equipped with EIS II STANDARD
EIS II SOFTWARE SXT3FE2SA0410EIS II SOFTWARE SXT3DE2SA0700EIS II SOFTWARE SXT3CE2SA0420EIS II SOFTWARE SXT4EE2SA050A
7 321 60 DMCi :NO E CUi A (B ) DA TA N o Ma int . Ac ti on i f i t o cc urs i n p ha se 0 1 o r 0 2 a t th e e nd o f an en gi ne r un ( 80 KTS n otreached) or after any FADEC reset.Message to be filtered on CFM eng A/C
Y
Part Affected P/N Corrective P/N
DMC - EIS 1 ALL P/N
7 321 60 E CU( Ei- 40 00 KS ) ( i=1 o r 2 ) N o Ma int . Ac ti on i f i t o cc urs i n p ha se 0 1 o r 0 2 a t th e e nd o f an en gi ne r un ( 80 KTS n otreached) or after any FADEC reset.Message to be filtered on CFM eng A/C and equipped with EIS II STANDARD
Y
Part Affected P/N Corrective P/NEIS II SOFTWARE SXT3FE2SA0410EIS II SOFTWARE SXT3DE2SA0700
EIS II SOFTWARE SXT3CE2SA0420EIS II SOFTWARE SXT4EE2SA050A
7 322 34 DMCi : NO E ECi A (B ) DA TA N o Ma int . Ac ti on i f i t o cc urs i n p ha se 0 1 o r 0 2 a t th e e nd o f an en gi ne r un ( 80 KTS n otreached) or after any FADEC reset.Message to be filtered on IAE eng A/C
Y
Part Affected P/N Corrective P/N
DMC - EIS 1 ALL P/N
7 322 34 E EC ( Ei- 40 00K S) ( i=1 o r 2 ) N o Ma int . Ac ti on i f i t o cc urs i n p ha se 0 1 o r 0 2 a t th e e nd o f an en gi ne r un ( 80 KTS n otreached) or after any FADEC reset.Message to be filtered on IAE eng A/C and EIS 2 SOFT P/N SXT3CE2SA0420
Y
Part Affected P/N Corrective P/N
EIS II SOFTWARE SXT3CE2SA0420 SXT3DE2SA0700
Revision 31 PART A
ATA Failure Messages Remark Doc X Ref F
7 322 34 DMCi : NO E ECi A (B ) DA TA N o Ma int . Ac ti on i f i t o cc urs i n p ha se 0 1 o r 0 2 a t th e e nd o f an en gi ne r un ( 80 KTS n otreached) or after any FADEC reset.Message to be filtered on IAE eng A/C
7 322 34 E EC ( Ei- 40 00K S) ( i=1 o r 2 ) N o Ma int . Ac ti on i f i t o cc urs i n p ha se 0 1 o r 0 2 a t th e e nd o f an en gi ne r un ( 80 KTS n otreached) or after any FADEC reset.Message to be filtered on IAE eng A/C and EIS 2 SOFT P/N SXT3CE2SA0420
Y
Part Affected P/N Corrective P/NEIS II SOFTWARE SXT3CE2SA0420 SXT3DE2SA0700
752210 LPTC VLV, HMU ENG1A (1B, 2A or 2B) No maintenance action if triggered during FADEC motoring test and ECU 5.BE or5.DE not fitted on A/C.
783142 HC/PROX SW/T/R UP ACT1 Associated with Maint. Status Eng i FADEC. No Maint. Act ion i f recorded duringphase 07 or 08 and if there is no crew report.
TFU 783100080 N
Part Affected P/N Corrective P/N
EEC SCN12C SCN12D
Revision 31 PART A
ATA Failure Messages Remark Doc X Ref F
7 933 11 Q UAL IFIE R Bi /WX Rj ( 1S Qj ) ( i=1 o r 2 an d j = 1 o r2)
NO MAINT. ACTION if recorded during Engine Start (flight phase 02) or duringswitching from WXR1 to WXR2 and no associated cockpit effect.
2 131 CA B P R S YS i FA UL T ( i=1 o r 2 ) I f th is w ar ni ng o ccu rs on gr ou nd wi th AD IRS " OFF" , S ele ct A DI RS " ON" . I f th ewarning still present, ref TSM
TFU 213134005 N
Part Affected P/N Corrective P/NCPC 902215702-7 902215702-8
2131 CAB PR LO DIFF PR NO MAINT. ACTION if it occurs after a rapid flight profile change TFU 213100005 Y
Part Affected P/N Corrective P/NCPC 902215702-8CPC 902215702-7 902215702-10
2 131 CA B P R S YS i FA UL T ( i=1 o r 2 ) I f th is w ar ni ng o ccu rs on gr ou nd wi th AD IRS " OFF" , S ele ct A DI RS " ON" . I f th ewarning still present, ref TSM TFU 213134005 N
Part Affected P/N Corrective P/NCPC 902215702-7 902215702-8
2161 PACK i (i=1 or 2) (MAINT STS= Associated to P1(2) FLOW CTL VALVENO MAINT. ACTION if Bite test OK
TFU 215151004 N
Part Affected P/N Corrective P/N
FLOW CTL VALVE 751A0000-06 751A0000-07
Revision 31 PART
ATA Cockpit Effect Remark Doc X Ref F
2161 AIR:PACK i REGUL FAULT (i=1 or 2) When not associated with any maintenance message, check all sensors peripheral tothe pack controler.
Airbus_SIL 21-049TFU 216134003
N
Part Affected P/N Corrective P/NPACK TEMP CTLR ALL P/N
2161 TEMP CTL 1 (or 2) (MAINT STS) NO MAINT. ACTION if associated with fault message "237334 CIDS2(102RH)Source TEMP CTL". Status problem of a discrete label computed by the CIDS2 andused by ACSC 1 and 2.
Airbus_SB 21-1149Vendor_SB 1803A-21-02
N
Part Affected P/N Corrective P/NACSC 1803A000003 1803B000001
2161 AIR PACK 1+2 FAULT NO MAINT ACTION if it occurs at the flight beginning (PHASE 03 or 04). Y
Part Affected P/N Corrective P/N
ACSC ALL P/NPACK TEMP CTLR ALL P/N
2161 PACK i (i=1 or 2) (MAINT STS= Associated to P1(2) FLOW CTL VALVE
NO MAINT. ACTION if Bite test OK
TFU 215151004 N
Part Affected P/N Corrective P/N
FLOW CTL VALVE 751A0000-06 751A0000-07
2161 AIR:PACK i REGUL FAULT (i=1 or 2) When not associated with any maintenance message, check all sensors peripheral tothe pack controler.
Airbus_SIL 21-049TFU 216134003
N
Part Affected P/N Corrective P/N
PACK TEMP CTLR ALL P/N
Revision 31 PART
ATA Cockpit Effect Remark Doc X Ref F
2161 TEMP CTL 1 (or 2) (MAINT STS) NO MAINT. ACTION if associated with fault message "237334 CIDS2(102RH)Source TEMP CTL". Status problem of a discrete label computed by the CIDS2 andused by ACSC 1 and 2.
Airbus_SB 21-1149Vendor_SB 1803A-21-02
N
Part Affected P/N Corrective P/NACSC 1803A000003 1803B000001
2 200 A UTO FL T Y AW DA MP ER S YS N O MA INT. A CTI ON i f o ccu rs at E ng in e s ta rt du ri ng st ron g w in d c ond iti on s.Recentering the Yaw damper before Engine start with Electric Pump will avoid themessage.
TFU 226300005 N
Part Affected P/N Corrective P/NFAC B397BAM0406 B397BAM0510FAC B397AAM0509 B397BAM0510
FAC B397CAM0101 B397BAM0510FAC B397AAM0510 B397BAM0510FAC B397AAM0508 B397BAM0510
2200 WINDSHEAR DET FAULT Appears at Slat extension if an ADR test has been performed on ground.Pull the FAC C/B during the ADR test to avoid the message
TFU 226600004AMM_Task 341300pb501
N
Part Affected P/N Corrective P/N
FAC B397BAM0406 B397BAM0509FAC B397BAM0407 B397BAM0509FAC B397AAM0508 B397BAM0509FAC B397AAM0507 B397BAM0509
2200 AUTO FLT AP OFF Configuration Warning Y
Part Affected P/N Corrective P/NFMGC ALL P/N NONE
2200 AUTO FLT A/THR OFF Configuration Warning Y
Part Affected P/N Corrective P/N
FMGC ALL P/N NONE
Revision 31 PART
ATA Cockpit Effect Remark Doc X Ref F
2 200 A UTO FL T Y AW DA MP ER S YS N O MA INT. A CTI ON i f o ccu rs at E ng in e s ta rt du ri ng st ron g w in d c ond iti on s.Recentering the Yaw damper before Engine start with Electric Pump will avoid themessage.
TFU 226300005 N
Part Affected P/N Corrective P/NFAC B397BAM0406 B397BAM0510FAC B397AAM0509 B397BAM0510
FAC B397CAM0101 B397BAM0510FAC B397AAM0510 B397BAM0510FAC B397AAM0508 B397BAM0510
2200 WINDSHEAR DET FAULT Appears at Slat extension if an ADR test has been performed on ground.Pull the FAC C/B during the ADR test to avoid the message
TFU 226600004AMM_Task 341300pb501
N
Part Affected P/N Corrective P/N
FAC B397BAM0406 B397BAM0509FAC B397BAM0407 B397BAM0509FAC B397AAM0508 B397BAM0509FAC B397AAM0507 B397BAM0509
2200 AUTO FLT AP OFF Configuration Warning Y
Part Affected P/N Corrective P/NFMGC ALL P/N NONE
2200 AUTO FLT A/THR OFF Configuration Warning Y
Part Affected P/N Corrective P/N
FMGC ALL P/N NONE
Revision 31 PART
ATA Cockpit Effect Remark Doc X Ref F
2 300 CID S1 (o r 2 ) (M AI NT ST S) N o Ma int A ct ion if n o f au lt me ss ag e t ri gg er ed fo ll owi ng a CID S i nte rfa ce & p owe r- uptest. This spurious MAINT STS may be triggered due to short power interrupts.
N
Part Affected P/N Corrective P/NDIRECTOR-CIDS Z014H000131A TBDDIRECTOR-CIDS Z014H000031A TBD
Part Affected P/N Corrective P/NBCL 35-0L5-1004-07 PN BCL TESTBCL 35-0L5-1003-06
2600 SMOKE LAVATORY DET SMOKE I f associated with the SDCU fault message "SMOKE DET LAV x" (x is the lavatoryaffected), ref the maintenance advice field of the TFU 261715003
TFU 261715003 N
Part Affected P/N Corrective P/NSMOKE DET LAV GAI2800-02 TBDSMOKE DET LAV PAI2830-00 TBD
2600 AVIONICS SMOKE If triggered on ground, associated with amber memo LAND ASAP no evidence ofsmoke, then FWC1 & FWC2 should be reset in order to clear the latch condition ofthe warning. This allows to prevent spurious LAND ASAP memo to be triggered attake-off.
TFU 261515001 N
Part Affected P/N Corrective P/N
SMOKE DET AVNCS CG7GO CGDU2000-00
Revision 31 PART
ATA Cockpit Effect Remark Doc X Ref F
2600 SMOKE LAVATORY DET FAULT Associated to PFR fault messages "261715 SMK DET LAV" and/or "261715 SMKDET LAV X CONTAMINATION". Perform a CIDS reset to recover lavatory smokedetection function as described in SIL 23-039 Rev6
Airbus_SIL 23-039 N
Part Affected P/N Corrective P/NDIRECTOR-CIDS Z014H000031A Z014H000231BDIRECTOR-CIDS Z014H000131A
2 600 S MOK E A FT CRG BT L1 FA UL T M ai nte na nce a dvi se : Ma ke s ur e t hat wh en A MM Ta sk 2 6- 16 -00 -7 10 -0 01"Operational test of the cargo-compartment Smoke-detection system by PTT" isperformed, the PTT button is hold 20 seconds as recommended and activated onlyone time.
N
Part Affected P/N Corrective P/NDIRECTOR-CIDS Z014H000030C Z014H000131ADIRECTOR-CIDS Z014H000030C Z014H000031A
2600 SMOKE AFT CRG BTL2 FAULT (if installed) Maintenance advise: Make sure that when AMM Task 26-16-00-710-001"Operational test of the cargo-compartment Smoke-detection system by PTT" isperformed, the PTT button is hold 20 seconds as recommended and activated onlyone time.
2600 SMOKE FWD CRG BTL2 FAULT (if installed) Maintenance advise: Make sure that when AMM Task 26-16-00-710-001"Operational test of the cargo-compartment Smoke-detection system by PTT" isperformed, the PTT button is hold 20 seconds as recommended and activated onlyone time.
2600 SMOKE LAVATORY DET SMOKE I f associated with the SDCU fault message "SMOKE DET LAV x" (x is the lavatoryaffected), ref the maintenance advice field of the TFU 261715003
TFU 261715003 N
Part Affected P/N Corrective P/N
SMOKE DET LAV GAI2800-02 TBDSMOKE DET LAV PAI2830-00 TBD
Revision 31 PART
ATA Cockpit Effect Remark Doc X Ref F
2600 AVIONICS SMOKE If triggered on ground, associated with amber memo LAND ASAP no evidence ofsmoke, then FWC1 & FWC2 should be reset in order to clear the latch condition ofthe warning. This allows to prevent spurious LAND ASAP memo to be triggered attake-off.
2600 SMOKE LAVATORY DET FAULT Associated to PFR fault messages "261715 SMK DET LAV" and/or "261715 SMKDET LAV X CONTAMINATION". Perform a CIDS reset to recover lavatory smokedetection function as described in SIL 23-039 Rev6
2 600 S MOK E A FT CRG BT L1 FA UL T M ai nte na nce a dvi se : Ma ke s ur e t hat wh en A MM Ta sk 2 6- 16 -00 -7 10 -0 01"Operational test of the cargo-compartment Smoke-detection system by PTT" isperformed, the PTT button is hold 20 seconds as recommended and activated onlyone time.
2600 SMOKE AFT CRG BTL2 FAULT (if installed) Maintenance advise: Make sure that when AMM Task 26-16-00-710-001"Operational test of the cargo-compartment Smoke-detection system by PTT" isperformed, the PTT button is hold 20 seconds as recommended and activated onlyone time.
2600 SMOKE FWD CRG BTL2 FAULT (if installed) Maintenance advise: Make sure that when AMM Task 26-16-00-710-001"Operational test of the cargo-compartment Smoke-detection system by PTT" isperformed, the PTT button is hold 20 seconds as recommended and activated onlyone time.
N
Part Affected P/N Corrective P/NDIRECTOR-CIDS Z014H000030C Z014H000031A
DIRECTOR-CIDS Z014H000030C Z014H000131A
Revision 31 PART
ATA Cockpit Effect Remark Doc X Ref F
2 616 S MOK E F WD C RG B TL 1 FA UL T M ai nte na nce a dvi se : Ma ke s ur e t hat wh en A MM Ta sk 2 6- 16 -00 -7 10 -0 01"Operational test of the cargo-compartment Smoke-detection system by PTT" isperformed, the PTT button is hold 20 seconds as recommended and activated onlyone time.
2 700 F/C TL E LAC 1 ( 2) P IT CH F AU LT I F N O MA INTE NA NC E ME SS AG E a sso ci ate d : CH EC K th e P ITC H C HAN GE OV ERDISCRETES LANE.
TFU 279300028 N
Part Affected P/N Corrective P/NFCDC 115370-0105 115370-1016FCDC 115370-0105 115370-0106
2 700 F/C TL E LAC 1( 2) F AU LT E ve n i f a ss oc iat ed wi th " EL AC1 (2 )" ma in te na nce me ss ag e, fa il ure of o pp os ite E LA Cmay be suspected. Apply TSM procedure.
TFU 279500039 N
Part Affected P/N Corrective P/NFCDC 115370-1016 N/AFCDC 115370-0105 N/A
2700 F/CTL ALTN LAW IF OCCURS AT ENGINE START,PERFORM ELACs RESET WITH ALLHYDRAULIC SYSTEMS DEPRESSURIZED.
Other FCOM_3.02.27TFU 279300040
N
Part Affected P/N Corrective P/NELAC 3945122502 3945122505
2 700 F/C TL FL AP S L OC KE D I f ex pe ri en ce d a t fi rst A /C po we r- up wh en e lec tr ica l p owe r i s po we re d f ro m b at te ri esref TFU 275134026 MAINTENANCE ADVICE field.
TFU 275134026 N
Part Affected P/N Corrective P/N
SFCC 49-170-07 49-170-07 AMDT_ASFCC ALL P/N 49-170-11SFCC 49-117-10 49-117-10 AMDT_A
Revision 31 PART
ATA Cockpit Effect Remark Doc X Ref F
2 700 F/C TL S LAT S L OC KE D I f ex pe ri en ce d a t fi rst A /C po we r- up, wh en e le ctr ic al po we r i s su pp li ed fr om b att er ie sref TFU 27134026 MAINTENANCE ADVICE field
TFU 275134026 N
Part Affected P/N Corrective P/NSFCC 49-170-07 49-170-07 AMDT_ASFCC 49-117-10 49-117-10 AMDT_ASFCC ALL P/N 49 170 11
2 700 F/C TL E LAC 2 P IT CH F AU LT A t e ngi ne s ta rt, i f a sso ci ate d wi th " THS A CTR S ERV O MOT 1 9 CE " ma in te na ncemessage refer to TFU 27 90 00 028. NO MAINTENANCE ACTION required if
warning "F/CTL ELAC 2 PITCH FAULT" can be cleared through ELAC 2 push buttonreset.
2 700 F/C TL E LAC 1( 2) F AU LT E ve n i f a ss oc iat ed wi th " EL AC1 (2 )" ma in te na nce me ss ag e, fa il ure of o pp os ite E LA Cmay be suspected. Apply TSM procedure.
TFU 279500039 N
Part Affected P/N Corrective P/NFCDC 115370-1016 N/AFCDC 115370-0105 N/A
2700 F/CTL ALTN LAW IF OCCURS AT ENGINE START,PERFORM ELACs RESET WITH ALLHYDRAULIC SYSTEMS DEPRESSURIZED.
Other FCOM_3.02.27TFU 279300040
N
Part Affected P/N Corrective P/NELAC 3945122502 3945122505
2 700 F/C TL FL AP S L OC KE D I f ex pe ri en ce d a t fi rst A /C po we r- up wh en e lec tr ica l p owe r i s po we re d f ro m b at te ri es
ref TFU 275134026 MAINTENANCE ADVICE field.
TFU 275134026 N
Part Affected P/N Corrective P/NSFCC 49-170-07 49-170-07 AMDT_ASFCC ALL P/N 49-170-11SFCC 49-117-10 49-117-10 AMDT_A
2 700 F/C TL S LAT S L OC KE D I f ex pe ri en ce d a t fi rst A /C po we r- up, wh en e le ctr ic al po we r i s su pp li ed fr om b att er ie sref TFU 27134026 MAINTENANCE ADVICE field
TFU 275134026 N
Part Affected P/N Corrective P/NSFCC 49-170-07 49-170-07 AMDT_A
SFCC 49-117-10 49-117-10 AMDT_ASFCC ALL P/N 49-170-11
Revision 31 PART
ATA Cockpit Effect Remark Doc X Ref F
2 700 F/C TL E LAC 2 P IT CH F AU LT A t e ngi ne s ta rt, i f a sso ci ate d wi th " THS A CTR S ERV O MOT 1 9 CE " ma in te na ncemessage refer to TFU 27 90 00 028. NO MAINTENANCE ACTION required ifwarning "F/CTL ELAC 2 PITCH FAULT" can be cleared through ELAC 2 push buttonreset.
2700 F/CTL (MAINT. STS) If associated with the PFR message "SFCC1(2) FLAP(SLAT)", reset the SFCC. TFU 275134027 N
Part Affected P/N Corrective P/NSFCC 49-170-07 49-170-11SFCC 49-170-07 49-170-07 AMDT_C
2700 F/CTL ALTN LAW IF OCCURS AT ENGINE START,PERFORM ELACs RESET WITH ALLHYDRAULIC SYSTEMS DEPRESSURIZED.
Other FCOM_3.02.27TFU 279300040
N
Part Affected P/N Corrective P/NELAC 3945122502 3945122505
2700 F/CTL SPD BRK DISAGREE Configuration warning Y
Part Affected P/N Corrective P/NFCDC ALL_P/N
2800 FUEL L (R) WING TK LO LVL NO MAINT. ACTION if occurs at beginning of descent. TFU 284615003 N
Part Affected P/N Corrective P/N
LEVEL SENSING N/A
Revision 31 PART
ATA Cockpit Effect Remark Doc X Ref F
2 800 FUE L L (R) X FR V AL VE O PEN I f th is E CA M me ssa ge i s re po rte d, pe rfo rm fu ncti on al B ITE t est o f t he ICT Vs - F LS SStatus (AMM 28-15-00-740-002) and a functional BITE test of the low-level sensors -FLSS BITE (AMM 28-46-00-740-001). No further action is required, if both test of theFLSS status and FLSS BITE show NO FAULT.
2800 FUEL L (R) WING TK LO LVL NO MAINT. ACTION if occurs at beginning of descent. TFU 284615003 N
Part Affected P/N Corrective P/NLEVEL SENSING N/A
2 800 FUE L L (R) X FR V AL VE O PEN I f th is E CA M me ssa ge i s re po rte d, pe rfo rm fu ncti on al B ITE t est o f t he ICT Vs - F LS SStatus (AMM 28-15-00-740-002) and a functional BITE test of the low-level sensors -FLSS BITE (AMM 28-46-00-740-001). No further action is required, if both test of theFLSS status and FLSS BITE show NO FAULT.
TFU 281500003 N
Part Affected P/N Corrective P/N
COMPUTER-FQI ALL P/N
3 031 A NTI ICE CA PT ( F/O ) T AT N O MA INT. A CTI ON i f o ccu rs on gr ou nd d ur in g we t / sn owy / i cy w ea the r, o r a fte rde-icing/high-press cleaning
TFU 326100003TFU 303100017TFU 344200003
N
Part Affected P/N Corrective P/NTRANSCEIVER-RADIOALTIMETER
9599-607-14932 9599-607-14942
TRANSCEIVER-RADIOALTIMETER
9599-607-12333 9599-607-12352
PHC 1663214200
3 031 A NTI ICE CA PT ( F/O ) P ITO T D IS RE GA RD th e me ssa ge i f o ccu rs a ft er g ea r n on -r et rac ti on . T hi s d evi ati on h asbeen identified and will be cured at the next opportunaty of a new PHC std.
TFU 323173001TFU 323171043
N
Part Affected P/N Corrective P/N
LGCIU 664700500A4B 664700500A4D
Revision 31 PART
ATA Cockpit Effect Remark Doc X Ref F
3 031 A NTI ICE CA PT ( F/O ) T AT N O MA INT. A CTI ON i f o ccu rs on gr ou nd d ur in g we t / sn owy / i cy w ea the r, o r a fte rde-icing/high-press cleaning
TFU 326100003TFU 303100017TFU 344200003
N
Part Affected P/N Corrective P/NTRANSCEIVER-RADIOALTIMETER
3 031 A NTI ICE CA PT ( F/O ) P ITO T D IS RE GA RD th e me ssa ge i f o ccu rs a ft er g ea r n on -r et rac ti on . T hi s d evi ati on h asbeen identified and will be cured at the next opportunaty of a new PHC std.
TFU 323173001TFU 323171043
N
Part Affected P/N Corrective P/N
LGCIU 664700500A4B 664700500A4D
3 044 A NTI ICE L ( R) WI NDO W O cc ur s wh en wi nd ows W in dsh ie ld a re e xp ose d to t he su n i n h ot an d d ry a tmo sp he refor more than one hour
TFU 304200004 N
Part Affected P/N Corrective P/N
WHC 66642024WHC 6664287-0
WHC 66642022 41600318001WHC 6664202-3 41600318003
3100 CFDIU (MAINT STS) NO MAINT. ACTION if CFDIU power up test result is : CFDIU BITE MEMORY TSM_Task ATA31TFU 313234031
N
Part Affected P/N Corrective P/NCFDIU B401ACM0404 CFDIU WITH AMDT A
Revision 31 PART
ATA Cockpit Effect Remark Doc X Ref F
3100 DMU (MAINT STS) Associated with the message : CAGA MEMORY FAIL. TSM_Task TSM_ATA31TFU 313600013
3200 BRAKES BSCU CH1 (2) FAULT If occurs at engine shutdown, reset the BSCU (FCOM 3.04.32) Other FCOM_3.04.32
TFU 324234041
N
Part Affected P/N Corrective P/N
BSCU ALL P/N N/A
3200 BRAKES HOT This is a configuration warning that does not reflect a malfunction of the system.Instead, it is triggered to remind the flight crew that take-off is not permitted withbrakes hot.
Y
Part Affected P/N Corrective P/NBSCU ALL P/N N/A
3200 L/G LGCIU 1 (2) FAULT If not LGCIU faut message available in the PFR, refer to the Last Leg Report of theLGCIU
N
Part Affected P/N Corrective P/NLGCIU 664700500A4C 664700500A4D
3200 L/G LGCIU 1 (2) FAULT NO MAINT. ACTION if BITE test OK TFU 323134043 N
Part Affected P/N Corrective P/NLGCIU 664700500A4A 664700500A4B
Revision 31 PART
ATA Cockpit Effect Remark Doc X Ref F
3200 L/G SHOCK ABSORBER FAULT NO MAINT. ACTION if occurs on ground during wet / snowy / icy weather, or afterde-icing/high-press cleaning
TFU 344200005TFU 326100003TFU 344200003
Y
Part Affected P/N Corrective P/NTRANSCEIVER-RADIOALTIMETER
3200 BRAKES BSCU CH1 (2) FAULT If occurs at engine shutdown, reset the BSCU (FCOM 3.04.32) Other FCOM_3.04.32
TFU 324234041
N
Part Affected P/N Corrective P/N
BSCU ALL P/N N/A
3200 BRAKES HOT This is a configuration warning that does not reflect a malfunction of the system.Instead, it is triggered to remind the flight crew that take-off is not permitted withbrakes hot.
Y
Part Affected P/N Corrective P/NBSCU ALL P/N N/A
3200 L/G LGCIU 1 (2) FAULT If not LGCIU faut message available in the PFR, refer to the Last Leg Report of theLGCIU
N
Part Affected P/N Corrective P/NLGCIU 664700500A4C 664700500A4D
3400 NAV GPWS FAULT No maintenance action is required if occurs on ground during Taxiing or Lining-up. TFU 344800002 Y
Part Affected P/N Corrective P/NRECEIVER ILS 204-1230-3518 204-1230-3521
Revision 31 PART
ATA Cockpit Effect Remark Doc X Ref F
3400 NAV TCAS FAULT No maintenance action is required if TCAS BITE test is OK. If not OK ref to TSM. TFU 344300006 N
Part Affected P/N Corrective P/NTCAS 4066010-903 4066010-905
3400 NAV TCAS FAULT No maintenance action is required if TCAS BITE test is OK If not OK ref to TSM TFU 344300004 N
3400 NAV RAi FAULT (=1 or 2) NO MAINT ACTION if event happens at high altitude (above 8192 ft). TFU 344200007 N
Part Affected P/N Corrective P/NTRANSCEIVER-RADIOALTIMETER
9599-607-14942 VSB ERT-530-34-35
TRANSCEIVER-RADIO
ALTIMETER
9599-607-14942 VSB ERT-530-34-34
3 400 NA V RA i FA UL T ( i=1 o r 2 ) A pp ly Ma in te na nce a ct io n d esc rib ed i n T FU 3 44 200 00 8 i f co rr el ate d w ith b oth P FRfault messages "LRAi TRANSCEIVER" and "LRAi ANTENNA"Issue corrected with ANTENNA S/N > 2014
Vendor_SB 95-01Other AOT_34-03TFU 344200008
N
Part Affected P/N Corrective P/N
RA ANTENNA 622-8701-002
3 400 NA V A DRi F AU LT ( i=1 , 2 or 3 ) I f no as so ci ate d ma in te na nc e me ssa ge s ou rce AD R, fo ll ow a dvi ce g ive n i n T FU341000012.
Airbus_SB 34-1084TFU 341000012
N
Part Affected P/N Corrective P/NADIRU HG1150AC05 HG1150AC06
Revision 31 PART
ATA Cockpit Effect Remark Doc X Ref F
3 400 A DR 1 (2 )( 3) ( MA INT S TS ) T he MA INTE NA NCE ST AT US ma y ap pe ar a ft er pe rfo rmi ng t he AO A S ENS OR te st .See maintenance advice given in TFU 34 10 00 017
TFU 341000017 N
Part Affected P/N Corrective P/NADIRU 465020-0303-0308 465020-0303-0309
3 400 NA V A DRi F AU LT ( i=1 2 or 3 ) A ss oci ate d to ADM fa ul t me ssa ge s NO MA IN TE NA NCE A CTI ON i f A IR DAT A TFU 341000016 N
3 400 NA V A DRi F AU LT ( i=1 , 2 or 3 ) A ss oci ate d to ADM fa ul t me ssa ge s. NO MA IN TE NA NCE A CTI ON i f A IR DAT Aparameters are valid on ground
TFU 341000016 N
Part Affected P/N Corrective P/NADIRU HG1150AC05 POST MOD 25882
3400 NAV ADR 1 (2)(3) FAULT If associated to ADM fault message "34 11 17 ADIRUx : NO DATA FROM ADM19FPx" ref MAINTENANCE ADVICE field of the TFU 341000021
TFU 341000021 N
Part Affected P/N Corrective P/N
ADM PG1152AC03 PG1152AC05
3 400 NA V A DRi F AU LT ( i=1 , 2 or 3 ) I f no as so ci ate d ma in te na nc e me ssa ge s ou rce AD R, fo ll ow a dvi ce g ive n i n T FU341000012.
Airbus_SB 34-1084TFU 341000012
N
Part Affected P/N Corrective P/N
ADIRU HG1150AC05 HG1150AC06
3 400 NA V RA i FA UL T ( i=1 o r 2 ) A pp ly Ma in te na nce a ct io n d esc rib ed i n T FU 3 44 200 00 8 i f co rr el ate d w ith b oth P FRfault messages "LRAi TRANSCEIVER" and "LRAi ANTENNA"Issue corrected with ANTENNA S/N > 2014
Vendor_SB 95-01Other AOT_34-03TFU 344200008
N
Part Affected P/N Corrective P/N
RA ANTENNA 622-8701-002
Revision 31 PART
ATA Cockpit Effect Remark Doc X Ref F
3400 NAV GPWS FAULT No maintenance action is required if occurs on ground during Taxiing or Lining-up. TFU 344800002 Y
Part Affected P/N Corrective P/NRECEIVER ILS 204-1230-3518 204-1230-3521
3400 NAV TCAS FAULT No maintenance action is required if TCAS BITE test is OK If not OK ref to TSM TFU 344300006 N
3400 NAV RAi FAULT (=1 or 2) NO MAINT ACTION if event happens at high altitude (above 8192 ft). TFU 344200007 N
Part Affected P/N Corrective P/NTRANSCEIVER-RADIOALTIMETER
9599-607-14942 VSB ERT-530-34-35
TRANSCEIVER-RADIOALTIMETER
9599-607-14942 VSB ERT-530-34-34
3 400 NA V RA i FA UL T ( i=1 o r 2 ) A pp ly Ma in te na nce a ct io n d esc rib ed i n T FU 3 44 200 00 8 i f co rr el ate d w ith b oth P FRfault messages "LRAi TRANSCEIVER" and "LRAi ANTENNA"Issue corrected with ANTENNA S/N > 2014
Vendor_SB 95-01Other AOT_34-03TFU 344200008
N
Part Affected P/N Corrective P/NRA ANTENNA 622-8701-002
Revision 31 PART
ATA Cockpit Effect Remark Doc X Ref F
3 400 NA V A DRi F AU LT ( i=1 , 2 or 3 ) I f no as so ci ate d ma in te na nc e me ssa ge s ou rce AD R, fo ll ow a dvi ce g ive n i n T FU341000012.
Airbus_SB 34-1084TFU 341000012
N
Part Affected P/N Corrective P/NADIRU HG1150AC05 HG1150AC06
3 400 A DR 1 (2 )( 3) ( MA INT S TS ) T he MA INTE NA NCE ST AT US ma y ap pe ar a ft er pe rfo rmi ng t he AO A S ENS OR te st . TFU 341000017 N
( )( ) ( ) y p p p gSee maintenance advice given in TFU 34 10 00 017
Part Affected P/N Corrective P/NADIRU 465020-0303-0308 465020-0303-0309
3 400 NA V A DRi F AU LT ( i=1 , 2 or 3 ) A ss oci ate d to ADM fa ul t me ssa ge s. NO MA IN TE NA NCE A CTI ON i f A IR DAT Aparameters are valid on ground
TFU 341000016 N
Part Affected P/N Corrective P/N
ADIRU HG1150AC05 POST MOD 25882
3400 NAV ADR 1 (2)(3) FAULT If associated to ADM fault message "34 11 17 ADIRUx : NO DATA FROM ADM19FPx" ref MAINTENANCE ADVICE field of the TFU 341000021
TFU 341000021 N
Part Affected P/N Corrective P/N
ADM PG1152AC03 PG1152AC05
3 400 NA V A DRi F AU LT ( i=1 , 2 or 3 ) I f no as so ci ate d ma in te na nc e me ssa ge s ou rce AD R, fo ll ow a dvi ce g ive n i n T FU341000012.
Airbus_SB 34-1084TFU 341000012
N
Part Affected P/N Corrective P/N
ADIRU HG1150AC05 HG1150AC06
Revision 31 PART
ATA Cockpit Effect Remark Doc X Ref F
3 400 NA V RA i FA UL T ( i=1 o r 2 ) A pp ly Ma in te na nce a ct io n d esc rib ed i n T FU 3 44 200 00 8 i f co rr el ate d w ith b oth P FRfault messages "LRAi TRANSCEIVER" and "LRAi ANTENNA"Issue corrected with ANTENNA S/N > 2014
Vendor_SB 95-01Other AOT_34-03TFU 344200008
N
Part Affected P/N Corrective P/NRA ANTENNA 622-8701-002
3441 RED WXR FLAG ON PFD DURING ON/OFF NO Maint. Action if WXR RADAR works correctly after power on. TFU 344100014 N
Part Affected P/N Corrective P/NRADAR 204-1217-0418RADAR 204-1218-0421
3 441 NA V P RE D W/ S DE T FA UL T I f as so ci ate d wi th fa ul t me ssa ge " DMCi : NO WX Rj Ch y D AT A" (i =1 , 2 o r 3 ; j =1 o r 2 ),perform SYSTEM TEST of both WXR units. If test ok, do not remove the WXRtransceiver units. If the test fails, apply corresponding TSM procedure.
N
Part Affected P/N Corrective P/NRADAR 622-5132-623 TBDRADAR 622-5132-622 TBD
3441 RED WXR FLAG ON PFD DURING ON/OFF
SEQUENCE
NO Maint. Action if WXR RADAR works correctly after power on. TFU 344100014 N
Part Affected P/N Corrective P/NRADAR 204-1217-0418RADAR 204-1218-0421
3 441 NA V P RE D W/ S DE T FA UL T I f as so ci ate d wi th fa ul t me ssa ge " DMCi : NO WX Rj Ch y D AT A" (i =1 , 2 o r 3 ; j =1 o r 2 ),perform SYSTEM TEST of both WXR units. If test ok, do not remove the WXRtransceiver units. If the test fails, apply corresponding TSM procedure.
N
Part Affected P/N Corrective P/NRADAR 622-5132-623 TBDRADAR 622-5132-622 TBD
Revision 31 PART
ATA Cockpit Effect Remark Doc X Ref F
3600 AIR BLEED (Maintenance Status) NO MAINT. ACTION if the AIR BLEED MAINTENANCE STATUS is recorded in thePFR in phase 2, without any associated Fault Message.
N
Part Affected P/N Corrective P/NBMC 785-002-7 N/ABMC 785-002-61 N/A
ENG DUAL FAILURE NO MAINT ACTION if d d i / / i h f TFU Y
7 700 E NG i FA DE C A( B) F AU LT Wi th ou t a sso ci at ed fa ult me ssa ge FA DE C. Cl ear ed i n s om e ca se s by t he DMUand/or SDCU replacement.
TFU 315300048TFU 313600041
N
Part Affected P/N Corrective P/NSDCU ALL P/N VSB RAI 2800-26-005DMU ALL P/N VSB 795020-31-019
7700 ENG OVSPD PROT FAULT Ref to FCOM 3.02.70. Other FCOM_3.02.70TFU 732000004
N
Part Affected P/N Corrective P/NEEC ALL P/N SCN10AEEC ALL P/N SCN12C
Revision 31 PART
ATA Cockpit Effect Remark Doc X Ref F
7700 ENGi OVSPD PROT FAULT Refer to FCOM 3.02.70 if it occurs at Engine start-up. Other FCOM_3.02.70TFU 732110004
7700 ENG i IGN A+B FAULT If appears when selecting Master Lever for Engine start, cycle EIU C/B and attempt anew Engine start.
TFU 743000082TFU 743000083
N
Part Affected P/N Corrective P/NEIU 3957905003 POST AMDT CEIU 3957900612 POST AMDT CEIU 3957900611 POST AMDT C
7 700 E NG X RE SER VE R FA UL T i f a sso cia ted to t he fo ll ow ing fa ult me ssa ge "H CU ( TRDV ), J 5 ( J6 ), ECU " a t en gi nestart, refer to FCOM TR 477-3 and AMM 71-00-00 page block 500 for alternate startprocedure.
7 700 E NG i RE VE RS ER FA UL T N o ma int ena nce ac ti on i s re qu ir ed wh en oc cu rs d ur ing en gi ne sh ut of f ph ase (E ng inemaster switch off)
Other 999.0111-99TFU 783100098
N
Part Affected P/N Corrective P/N
ECU 1820M89P07 N/AECU 1820M36P07 N/A
Revision 31 PART
ATA Cockpit Effect Remark Doc X Ref F
7 700 E NG1 RE VE RS ER F AU LT I f th is w ar ni ng o ccu rs du ri ng th e t hru st r eve rse r t est ( th rou gh t he EC U me nu mo de )and if associated to failure messages "HCU (TRPU), HYD" or "HCU(TRSOU),HYD"do an operational test of the thrust reverser with engine running or using an hydraulicground card to confirm the fault.
7700 ENG 2 FADEC FAULT No Maint action if no associated EEC fault message recorded in the PFR. This is aFADEC discrepency that occurs on V2500 A5 Engines only
Part Affected P/N Corrective P/NTRANSCEIVER-RADIOALTIMETER
9599-607-14942 9599-607-12352
TRANSCEIVER-RADIOALTIMETER
9599-607-12333 9599-607-12352
TRANSCEIVER-RADIOALTIMETER
9599-607-14932 9599-607-12352
TRANSCEIVER-RADIOALTIMETER
9599-607-12552 9599-607-12352
7 700 E NG i FA DE C A( B) F AU LT Wi th ou t a sso ci at ed fa ult me ssa ge FA DE C. Cl ear ed i n s om e ca se s by t he DMUand/or SDCU replacement.
TFU 315300048TFU 313600041
N
Part Affected P/N Corrective P/NSDCU ALL P/N VSB RAI 2800-26-005DMU ALL P/N VSB 795020-31-019
7700 ENG OVSPD PROT FAULT Ref to FCOM 3.02.70. Other FCOM_3.02.70TFU 732000004
N
Part Affected P/N Corrective P/NEEC ALL P/N SCN10AEEC ALL P/N SCN12C
Revision 31 PART
ATA Cockpit Effect Remark Doc X Ref F
7700 ENGi OVSPD PROT FAULT Refer to FCOM 3.02.70 if it occurs at Engine start-up. Other FCOM_3.02.70TFU 732110004
7700 ENG i IGN A+B FAULT If appears when selecting Master Lever for Engine start, cycle EIU C/B and attempt anew Engine start.
TFU 743000082TFU 743000083
N
Part Affected P/N Corrective P/NEIU 3957905003 POST AMDT CEIU 3957900612 POST AMDT CEIU 3957900611 POST AMDT C
7 700 E NG X RE SER VE R FA UL T i f a sso cia ted to t he fo ll ow ing fa ult me ssa ge "H CU ( TRDV ), J 5 ( J6 ), ECU " a t en gi nestart, refer to FCOM TR 477-3 and AMM 71-00-00 page block 500 for alternate startprocedure.
7 700 E NG i RE VE RS ER FA UL T N o ma int ena nce ac ti on i s re qu ir ed wh en oc cu rs d ur ing en gi ne sh ut of f ph ase (E ng inemaster switch off)
Other 999.0111-99TFU 783100098
N
Part Affected P/N Corrective P/N
ECU 1820M89P07 N/AECU 1820M36P07 N/A
Revision 31 PART
ATA Cockpit Effect Remark Doc X Ref F
7 700 E NG1 RE VE RS ER F AU LT I f th is w ar ni ng o ccu rs du ri ng th e t hru st r eve rse r t est ( th rou gh t he EC U me nu mo de )and if associated to failure messages "HCU (TRPU), HYD" or "HCU(TRSOU),HYD"do an operational test of the thrust reverser with engine running or using an hydraulicground card to confirm the fault.
7700 ENG 2 FADEC FAULT No Maint action if no associated EEC fault message recorded in the PFR. This is aFADEC discrepency that occurs on V2500 A5 Engines only
7711 ENG 1 FADEC FAULT No Maint action if no associated EEC fault message recorded in the PFR. This is aFADEC discrepency that occurs on V2500 A5 Engines only
231233 VDR3(1RC3)/ATSU1(1TX1) Interface issue between ATSU and VDR if VDR is mode 2 capable and ATSU not Mode 2 capableNO MAINT. ACTION if ATSU PN LA2T0J13000C0F1 and either one of the listed VDR PN areinstalled.
233346 SEB 41LFT, 41RGT REF SIL HUGHES 1142000-130-03 NO MAINT. ACTION TFU 233300009
Part Affected P/N Corrective P/N
PES-MULTIPLEXER 1142300-131-XX VSB AVI-9332
233346 SEB 42LFT, 42RGT REF SIL HUGHES 1142000-130-03 NO MAINT. ACTION TFU 233300009
Part Affected P/N Corrective P/N
PES-MULTIPLEXER 1142300-131-XX VSB AVI-9332
233346 SEB 41LFT, 41RGT REF SIL HUGHES 1142000-130-03 NO MAINT. ACTION TFU 233300009
Part Affected P/N Corrective P/N
PES-MULTIPLEXER 1142300-131-XX VSB AVI-9332
Revision 31 PART
ATA Class 3 message Remark Doc X Ref
233346 SEB 42LFT, 42RGT REF SIL HUGHES 1142000-130-03 NO MAINT. ACTION TFU 233300009
Part Affected P/N Corrective P/NPES-MULTIPLEXER 1142300-131-XX VSB AVI-9332
233600 NO SCU DATA No maintenance action if no cabin crew complaint. This message is recorded when the SCU pinprog is activated with the SCU not installed, and with the following SCU P/N: 743-0215-030,743-03xx-xxx, RD-AV3001-33, 610860-xxxx.
2 421 00 CHE CK G CUi P IN A8 A,A 9B ID G i P IN B7 ,B8WIRING (i=1 or 2)
No Maint Action TFU 244100002
Part Affected P/N Corrective P/N
GPCU 740121A 740121B
242200 CHECK FIRE HANDLE i RESET GENi (i=1 or 2) NO MAINT. ACTION if Fire handle switches actuation not mentionned in the Log Book. TFU 244100004
Part Affected P/N Corrective P/NGPCU 740121A 740121B
242218 TDC AC SENSOR 50XUi (i=1 or 2) After a GPCU test, Generator 1& 2 P/B switches in the cockpit must be reset. Otherwise, thismessage will appear after the 2nd GPCU test
TFU 244100003
Part Affected P/N Corrective P/N
GPCU 740121B VENDOR SIL 229GPCU 740121A VENDOR SIL 229
Revision 31 PART
ATA Class 3 message Remark Doc X Ref
244134 GPCU NO MAINT. ACTION
Part Affected P/N Corrective P/NGPCU 740121A 740121B
284216 L(R) CADENSICON 19QTi NO MAINT. ACTION TFU 284234029TFU 284234016
462134 ATSU (1TX1)/HFi (3REi) (i=1 or 2) NO MAINT. ACTION. This message is triggered if there is no ATSU link with HFDR, i.e. (MOD30625/30331 not installed).
Part Affected P/N Corrective P/NHFDR VSB COLLINS HFS-900DHFDR 822-0990-003 TBD
462134 ATSU (1TX1)/HFi (3REi) (i=1 or 2) NO MAINT. ACTION. This message is triggered if there is no ATSU link with HFDR, i.e. (MOD30625/30331 not installed).
2163 THE CAB TEMP SYSTEM INITIATED TESTRESULTS,WHEN FAILED,ARE IN CODEDFORM
THE CAB TEMP SYSTEM INITIATED TEST RESULTS,WHEN FAILED,ARE IN CODED FORM TFU 216134002TFU 216334004Other TSM-ATA21
Part Affected P/N Corrective P/N
ZONE CONTROLLER 775A0000-06 775A0000-07ZONE CONTROLLER 775A0000-05 775A0000-07
2 163 S pu ri ou s me ss age re cor de d i n t he PRE VIO USLEG REPORT: "NO ACCEPTABLE FAILURE ON212".Spurious message recorded in the LASTLEG REPORT: "NO ACCEPTABLE FAILURE IN26"
Spurious message recorded in the PREVIOUS LEG REPORT: "NO ACCEPTABLE FAILURE ON212". Spurious message recorded in the LAST LEG REPORT: "NO ACCEPTABLE FAILURE IN26"NO MAINT. ACTION if no log book complaint.
TFU 216334047
Part Affected P/N Corrective P/N
ZONE CONTROLLER 775A0000-05 775A0000-06
2163 THE CAB TEMP SYSTEM INITIATED TESTRESULTS,WHEN FAILED,ARE IN CODEDFORM
THE CAB TEMP SYSTEM INITIATED TEST RESULTS,WHEN FAILED,ARE IN CODED FORM TFU 216134002TFU 216334004Other TSM-ATA21
Part Affected P/N Corrective P/N
ZONE CONTROLLER 775A0000-06 775A0000-07ZONE CONTROLLER 775A0000-05 775A0000-07
Revision 31 PART
ATA CFDS anomalies Remark Doc X Ref
2 163 G ND f ail ur es r ep or t i n la st l eg r ep or t. G ND fa il ur es r epo rt i n l ast l eg r ep or t.
2 163 S pu ri ou s me ss age re cor de d i n t he PRE VIO USLEG REPORT: "NO ACCEPTABLE FAILURE ON212".Spurious message recorded in the LASTLEG REPORT: "NO ACCEPTABLE FAILURE IN26"
Spurious message recorded in the PREVIOUS LEG REPORT: "NO ACCEPTABLE FAILURE ON212". Spurious message recorded in the LAST LEG REPORT: "NO ACCEPTABLE FAILURE IN26"NO MAINT. ACTION if no log book complaint.
2163 Leg counting deviation at leg 99 Leg counting deviation at leg 99
Part Affected P/N Corrective P/N
ZONE CONTROLLER 775A0000-05 775A0000-07
2 200 Wr ong (A lte rn ate ) Ci ty P ai r o n t he PF R. Wr on g ( Al te rna te) Ci ty P ai r on th e P FR.If Lateral revision at destination is used for inserting/changing Altn destination, inserting/Modifyingvia init A page in pre-flight or via secondary flight plan will avoid this anomaly.
2200 The message THR LK no more displayed on thePFD at the step 7 of the land test.
The message THR LK no more displayed on the PFD at the step 7 of the land test.If DMC Mark II is installed, Ignore the land test step7 question, and answer YES even if nothing isdisplayed on the PFD.
TFU 229700004
Part Affected P/N Corrective P/N
FAC ALL P/N B397AAM0509FAC ALL P/N B397AAM0508DMC - EIS 1 ALL P/N
Revision 31 PART
ATA CFDS anomalies Remark Doc X Ref
2200 ELAC 1 & ELAC 2 messages displayed in theground scan if no hydraulic pressure
ELAC 1 & ELAC 2 messages displayed in the ground scan if no hydraulic pressure Other TSM-ATA22
Part Affected P/N Corrective P/NFAC ALL P/N N/A
2 200 Di sr eg ar d th e i ndi cat io n RTO K i n t he AF S Bi tereport
Disregard the indication RTOK in the AFS Bite report
2 200 Wr ong (A lte rn ate ) Ci ty P ai r o n t he PF R. Wr on g ( Al te rna te) Ci ty P ai r on th e P FR.If Lateral revision at destination is used for inserting/changing Altn destination, inserting/Modifyingvia init A page in pre-flight or via secondary flight plan will avoid this anomaly.
2200 The message THR LK no more displayed on thePFD at the step 7 of the land test.
The message THR LK no more displayed on the PFD at the step 7 of the land test.If DMC Mark II is installed, Ignore the land test step7 question, and answer YES even if nothing isdisplayed on the PFD.
TFU 229700004
Part Affected P/N Corrective P/NFAC ALL P/N B397AAM0509FAC ALL P/N B397AAM0508DMC - EIS 1 ALL P/N
2200 ELAC 1 & ELAC 2 messages displayed in theground scan if no hydraulic pressure
ELAC 1 & ELAC 2 messages displayed in the ground scan if no hydraulic pressure Other TSM-ATA22
Part Affected P/N Corrective P/NFAC ALL P/N N/A
Revision 31 PART
ATA CFDS anomalies Remark Doc X Ref
2 200 Di sr eg ar d th e i ndi cat io n RTO K i n t he AF S Bi tereport
Disregard the indication RTOK in the AFS Bite report
Part Affected P/N Corrective P/NFAC ALL P/N N/A
228334 FMGCi FMGCi Class 2 Fault message without associated Maintenance status.Apply TSM procedure
228334 RMP1(2,3) : NO DATA FROM FMGCi Wrong classification for fault message RMP1(2,3) : NO DATA FROM FMGCiClass 2 Fault message to be considered as a Class 3 message.
228334 FMGCi FMGCi Class 2 Fault message without associated Maintenance status.Apply TSM procedure
MPD_Task 279000-07
Part Affected P/N Corrective P/NFCDC 115370-0105 115370-0106FCDC 115370-0105 115370-1016
228334 RMP1(2,3) : NO DATA FROM FMGCi Wrong classification for fault message RMP1(2,3) : NO DATA FROM FMGCiClass 2 Fault message to be considered as a Class 3 message.
230000 To determine the status of the PES video system, it is recommended to check, after aircraft isenergized, the ground report of CIDS1/CIDS2 menu through the MCDU
Airbus_SB 23-1278
Part Affected P/N Corrective P/NOBRM CIDS DIR Z064H000030F Z064H000031AOBRM CIDS DIR Z064H000030F Z064H000031B
230000 No date indicat ion in the ground report of theCIDS or toilet system further to software loading.
No date indication in the ground report of the CIDS or toilet system further to software loading.It may happen that further to a software loading a failure message is displayed without any dateindication in the ground report of the CIDS1 or CIDS2 or the CIDS1 or 2 Toilet system.
Part Affected P/N Corrective P/NOBRM CIDS DIR Z064H000030F Z064H000031C
OBRM CIDS DIR Z064H000030F Z064H000031COBRM CIDS DIR Z064H000031A Z064H000031DOBRM CIDS DIR Z064H000031B
230000 No date indicat ion in the Last Leg Report of theCIDS Toilet system.
No date indication in the Last Leg Report of the CIDS Toilet system.It may happen that a failure message is displayed without any date indication in the Last LegReport of the CIDS1 or 2 Toilet system.
Part Affected P/N Corrective P/NOBRM CIDS DIR Z064H000030F Z064H000031COBRM CIDS DIR Z064H000031A Z064H000031DOBRM CIDS DIR Z064H000031B
230000 Video BITE Test The test of the Video System through MCDU provides unreliable result. Onlysimultaneous CIDS and PES power-up initiate the PES BITE to be correctly reported (normalmode)To determine the status of the PES video system, it is recommended to check, after aircraft isenergized, the ground report of CIDS1/CIDS2 menu through the MCDU
Part Affected P/N Corrective P/N
OBRM CIDS DIR Z064H000031B Z064H000031DOBRM CIDS DIR Z064H000031A Z064H000031C
Revision 31 PART
ATA CFDS anomalies Remark Doc X Ref
230000 The Lavatory Smoke detection test can not be performed if the CIDS is in a "cross-configuration"(AMM Task 26-17-00-710-001)Maintenance advise: Perform a CIDS reset as described in Appendix 1 to recover the usual CIDSconfiguration (CIDS part and CIDS-SDF part from the same unit active at the same time).
Part Affected P/N Corrective P/N
OBRM CIDS DIR Z064H000030F Z064H000031ADIRECTOR-CIDS Z014H000030C Z014H000131AOBRM CIDS DIR Z064H000030F Z064H000031BDIRECTOR-CIDS Z014H000030C Z014H000031A
230000 To determine the status of the PES video system, it is recommended to check, after aircraft isenergized, the ground report of CIDS1/CIDS2 menu through the MCDU
Part Affected P/N Corrective P/NOBRM CIDS DIR Z064H000030F Z064H000031AOBRM CIDS DIR Z064H000030F Z064H000031B
230000 No date indicat ion in the ground report of theCIDS or toilet system further to software loading.
No date indication in the ground report of the CIDS or toilet system further to software loading.It may happen that further to a software loading a failure message is displayed without any dateindication in the ground report of the CIDS1 or CIDS2 or the CIDS1 or 2 Toilet system.
Part Affected P/N Corrective P/NOBRM CIDS DIR Z064H000030F Z064H000031COBRM CIDS DIR Z064H000031A Z064H000031DOBRM CIDS DIR Z064H000031B
230000 No date indicat ion in the Last Leg Report of theCIDS Toilet system.
No date indication in the Last Leg Report of the CIDS Toilet system.It may happen that a failure message is displayed without any date indication in the Last LegReport of the CIDS1 or 2 Toilet system.
Part Affected P/N Corrective P/N
OBRM CIDS DIR Z064H000030F Z064H000031COBRM CIDS DIR Z064H000031A Z064H000031DOBRM CIDS DIR Z064H000031B
Revision 31 PART
ATA CFDS anomalies Remark Doc X Ref
230000 Video BITE Test The test of the Video System through MCDU provides unreliable result. Onlysimultaneous CIDS and PES power-up initiate the PES BITE to be correctly reported (normalmode)To determine the status of the PES video system, it is recommended to check, after aircraft isenergized, the ground report of CIDS1/CIDS2 menu through the MCDU
Part Affected P/N Corrective P/NOBRM CIDS DIR Z064H000031B Z064H000031DOBRM CIDS DIR Z064H000031A Z064H000031C
230000 The Lavatory Smoke detection test can not be performed if the CIDS is in a "cross-configuration"(AMM Task 26-17-00-710-001)Maintenance advise: Perform a CIDS reset as described in Appendix 1 to recover the usual CIDSconfiguration (CIDS part and CIDS-SDF part from the same unit active at the same time).
AMU AMU2790DA03 AMU2790DB06AMU AMU2790CA03 AMU2790CB06AMU PRE VSB 2790-23-007 VSB 2790-23-007AMU AMU2790EA03 AMU2790EB06AMU PRE VSB 2790-23-006 VSB 2790-23-006
2351 Wrong P/N of AMU and ACP in the audio LRUidentification
Wrong P/N of AMU and ACP in the audio LRU identificationNO MAINT. ACTION
TFU 235100013TFU 235100009
Part Affected P/N Corrective P/N
AMU PRE VSB 2790-23-007 VSB 2790-23-007AMU PRE VSB 2790-23-006 VSB 2790-23-006AMU AMU2790EA03 AMU2790EB06AMU AMU2790DA03 AMU2790DB06AMU AMU2790CA03 AMU2790CB06
Revision 31 PART D
ATA CFDS anomalies Remark Doc X Ref
2 373 E rr on eou s fa ul ts i n CI DS o r CI DS -SDF g ro udreport during software loading. Time indication forthese fault messages may be erroneous as well.
Erroneous faults in CIDS or CIDS-SDF groud report during software loading. Time indication forthese fault messages may be erroneous as well.Carry out a CIDS interface and power-up test to confirm validity of the following fault msg: 237334DIR1(101RH)BUS/DIR2(102RH) - 237300 FAP1(120RH)/DIR2/CAM - 237322 AIP(320RH1) ATT1L - 237322 AIP(320RH9) ATT 4L - 237334 AIR1(101RH)-SDF
Part Affected P/N Corrective P/NOBRM CIDS DIR Z064H000030F Z064H000031COBRM CIDS DIR Z064H000031BOBRM CIDS DIR Z064H000031A Z064H000031D
2373 Incorrect CFDS1(1TM)/ CIDS(10yRH)-SDFy (with(y=1 or 2)
Incorrect message CFDS1(1TM)/ CIDS(10yRH)-SDFy (with (y=1 or 2)The correct FIN of the CFDIU is 1TW instead of 1TM. Additionally, the ATA chapter and wordingshall be 313234 CFDIU(1TW)/CIDS(10yRH)-SDFy (with y=1 or 2) instead of 451334
Part Affected P/N Corrective P/NDIRECTOR-CIDS Z014H000030C Z014H000131ADIRECTOR-CIDS Z014H000030C Z014H000031A
2 373 E rr on eou s fa ul ts i n CI DS o r CI DS -SDF g ro udreport during software loading. Time indication forthese fault messages may be erroneous as well.
Erroneous faults in CIDS or CIDS-SDF groud report during software loading. Time indication forthese fault messages may be erroneous as well.Carry out a CIDS interface and power-up test to confirm validity of the following fault msg: 237334DIR1(101RH)BUS/DIR2(102RH) - 237300 FAP1(120RH)/DIR2/CAM - 237322 AIP(320RH1) ATT1L - 237322 AIP(320RH9) ATT 4L - 237334 AIR1(101RH)-SDF
Part Affected P/N Corrective P/NOBRM CIDS DIR Z064H000030F Z064H000031COBRM CIDS DIR Z064H000031BOBRM CIDS DIR Z064H000031A Z064H000031D
2373 Incorrect CFDS1(1TM)/ CIDS(10yRH)-SDFy (with(y=1 or 2)
Incorrect message CFDS1(1TM)/ CIDS(10yRH)-SDFy (with (y=1 or 2)The correct FIN of the CFDIU is 1TW instead of 1TM. Additionally, the ATA chapter and wordingshall be 313234 CFDIU(1TW)/CIDS(10yRH)-SDFy (with y=1 or 2) instead of 451334CFDS1(1TM)/CIDS(10yRH)-SDFy.
Part Affected P/N Corrective P/NDIRECTOR-CIDS Z014H000030C Z014H000131ADIRECTOR-CIDS Z014H000030C Z014H000031A
Revision 31 PART D
ATA CFDS anomalies Remark Doc X Ref
237334 Message "DIR2 (102RH) -SDF" is spuriously triggered during a system test of the smoke systemthrough the MCDU with the following configuration: both CIDS directors are powered (DIR1 active)and CIDS-SDF2 board is active (CIDS-SDF1 not energized).Subject configuration may be reproduced for trouble shooting purpose. Therefore, the validity ofthe failure message must be checked through a CIDS-SDF ground scanning.
Part Affected P/N Corrective P/NOBRM CIDS DIR Z064H000030F Z064H000031BOBRM CIDS DIR Z064H000030F Z064H000031ADIRECTOR-CIDS Z014H000030C Z014H000131ADIRECTOR-CIDS Z014H000030C Z014H000031A
2 400 B CL me ss ag es i n th e P FR, wi tho ut a ny th in g i nthe BCL Bite. (Bite memory erased after a reset)
BCL messages in the PFR, without anything in the BCL Bite. (Bite memory erased after a reset)Perform the Maint. actions corresponding to the PFR messages
2400 After a GPCU test, NO RESPONSE. After a GPCU test, NO RESPONSE.Reinitialize GPCU test
TFU 244100006
Part Affected P/N Corrective P/NGPCU 740121A VSB 740121-24-7GPCU 740121B VENDOR SIL 229
2400 Spurious fault message GCUi TEST NOT DONEor IDGi RUNNING
Spurious fault message GCUi TEST NOT DONE or IDGi RUNNINGNO MAINT. ACTION if appears after a GPCU test. Reinitialize the GPCU test.
TFU 244100005
Part Affected P/N Corrective P/NGPCU 740121B VENDOR SIL 229GPCU 740121A
2 400 B CL me ss ag es i n th e P FR, wi tho ut a ny th in g i nthe BCL Bite. (Bite memory erased after a reset)
BCL messages in the PFR, without anything in the BCL Bite. (Bite memory erased after a reset)Perform the Maint. actions corresponding to the PFR messages
TFU 243800009TFU 243800007
Part Affected P/N Corrective P/N
BCL 35-0L5-1005-08
Revision 31 PART D
ATA CFDS anomalies Remark Doc X Ref
2400 After a GPCU test, NO RESPONSE. After a GPCU test, NO RESPONSE.Reinitialize GPCU test
TFU 244100006
Part Affected P/N Corrective P/NGPCU 740121A VSB 740121-24-7GPCU 740121B VENDOR SIL 229
2400 Spurious fault message GCUi TEST NOT DONEor IDGi RUNNING
Spurious fault message GCUi TEST NOT DONE or IDGi RUNNINGNO MAINT. ACTION if appears after a GPCU test. Reinitialize the GPCU test.
2 423 34 S Pu ri ous f au lt G CU E ME RG I N A VIO NI CSTATUS
SPurious fault GCU EMERG IN AVIONIC STATUSIf test result is OK, no maintenance action. Could be corrected in a next CFDIU std
TFU 313234035
Part Affected P/N Corrective P/NGCU 520915 AMDT 4 TBD
2 617 00 O pe ra ti on al ch eck of t he La vat ory S mo kedetection function as per AMM task26-17-00-710-001 not possible in case DIR1 and
DIR-SDF2 or DIR2 and DIR-SDF1 are activesimultaneously (CIDS cross configuration).
Operational check of the Lavatory Smoke detection function as per AMM task 26-17-00-710-001not possible in case DIR1 and DIR-SDF2 or DIR2 and DIR-SDF1 are active simultaneously (CIDScross configuration).
Part Affected P/N Corrective P/NOBRM CIDS DIR Z064H000030F TBDOBRM CIDS DIR Z064H000030E TBDOBRM CIDS DIR Z064H000030D TBD
2 700 In te rr up ti on o f S FC C- CF DS co mmu ni ca ti onwhen selecting the print option
Interruption of SFCC- CFDS communication when selecting the print optionRe-enter the SFCC MENU (MCDU MENU key / CFDS prompt / SYSTEM REPORT/TEST / SFCC)
TFU 275151047
Part Affected P/N Corrective P/NSFCC 49-117-06 N/ASFCC 49-117-07 N/A
Revision 31 PART D
ATA CFDS anomalies Remark Doc X Ref
2700 During Ground Scanning, ECAM WARNING F/CTL AILERON SERVO FAULT may be triggeredwithout associated fault message if the failure affects the servovalve or the POS XDCR or theSOLENOID valve signal.TSM procedure should be followed using the ECAM WARNING as entry point.
2700 During a Ground Scanning, MAINT STATUSF/CTL may be triggered without associated faultmessage if the failure affects the servovalve orthe POS XDCR or the SOLENOID valve signal.
During a Ground Scanning, MAINT STATUS F/CTL may be triggered without associated faultmessage if the failure affects the servovalve or the POS XDCR or the SOLENOID valve signal.TSM procedure should be followed using the MAINT STATUS as entry point.
TFU 279500033
Part Affected P/N Corrective P/NFCDC 115370-0105 115370-1118
2 700 In te rr up ti on o f S FC C- CF DS co mmu ni ca ti onwhen selecting the print option
Interruption of SFCC- CFDS communication when selecting the print optionRe-enter the SFCC MENU (MCDU MENU key / CFDS prompt / SYSTEM REPORT/TEST / SFCC)
TFU 275151047
Part Affected P/N Corrective P/NSFCC 49-117-06 N/ASFCC 49-117-07 N/A
2700 During Ground Scanning, ECAM WARNING F/CTL AILERON SERVO FAULT may be triggeredwithout associated fault message if the failure affects the servovalve or the POS XDCR or theSOLENOID valve signal.TSM procedure should be followed using the ECAM WARNING as entry point.
2700 During a Ground Scanning, MAINT STATUSF/CTL may be triggered without associated faultmessage if the failure affects the servovalve orthe POS XDCR or the SOLENOID valve signal.
During a Ground Scanning, MAINT STATUS F/CTL may be triggered without associated faultmessage if the failure affects the servovalve or the POS XDCR or the SOLENOID valve signal.TSM procedure should be followed using the MAINT STATUS as entry point.
279334 ELACi COM (MON) OR BUS FROM FMGCi Class 2 fault message ELACi COM (MON) OR BUS FROM FMGCi without associatedMaintenance status.Apply TSM procedure
MPD_Task 279000-07
Part Affected P/N Corrective P/NFCDC 115370-0105 115370-1016
279334 SEC3 OR BUS2 FROM ADR2 (ADR3 / IR2 / IR3) Class 2 fault message SEC3 OR BUS2 FROM ADR2 (ADR3 / IR2 / IR3) without associatedMaintenance status.
Apply TSM procedure
MPD_Task 279000-07
Part Affected P/N Corrective P/NFCDC 115370-0105 115370-1016FCDC 115370-0105 115370-0106
279334 AFS:ELACi AFS:ELACiNO MAINT. ACTION if associated to B SYS LO PRESS (respectively Y SYS LO PRESS).
Part Affected P/N Corrective P/NFAC ALL P/N N/A
Revision 31 PART D
ATA CFDS anomalies Remark Doc X Ref
279334 ELACi COM (MON) OR BUS FROM FMGCi Class 2 fault message ELACi COM (MON) OR BUS FROM FMGCi without associatedMaintenance status.Apply TSM procedure
MPD_Task 279000-07
Part Affected P/N Corrective P/NFCDC 115370-0105 115370-1016
279334 SEC3 OR BUS2 FROM ADR2 (ADR3 / IR2 / IR3) Class 2 fault message SEC3 OR BUS2 FROM ADR2 (ADR3 / IR2 / IR3) without associatedMaintenance status.Apply TSM procedure
MPD_Task 279000-07
Part Affected P/N Corrective P/NFCDC 115370-0105 115370-1016
2 795 34 O P FCDC FA IL DIS CR C la ss 2 F aul t me ss ag e " OP FC DC F AI L DI SC R" wi th ou t as so ci ate d Ma in te na nce st atu s.Apply TSM procedure
MPD_Task 279000-07
Part Affected P/N Corrective P/NFCDC 115370-0105 115370-0106FCDC 115370-0105 115370-1016
3 011 51 L (R ) WA I FIL TE R OR V AL VE 9(1 0) A ss oc iat edwith E/Ws 30.00 WING ANTI ICE SYS FAULT
In case of message "L(R) WAI FILTER OR VALVE9(10)" associated with ECAM Warning 30.00WING ANTI ICE SYS FAULT, use CLASS 3 REPORT.
TFU 216334046Other TSM-ATA30
Part Affected P/N Corrective P/NZONE CONTROLLER 775A0000-05 775A0000-07
3132 Untimely print out of real time failure and warning. Untimely print out of real time failure (RTF) and warning (RTW)In flight pull, PRINTER C/B.
TFU 313234026
Part Affected P/N Corrective P/NCFDIU B401ACM0404 CFDIU WITH AMDT A
Revision 31 PART D
ATA CFDS anomalies Remark Doc X Ref
3132 NO DMC1 DATA recorded in CFDIU groundscanning
NO DMC1 DATA recorded in CFDIU ground scanningNO MAINT. ACTION.
TFU 313234030
Part Affected P/N Corrective P/NCFDIU B401ACM0404 B401ACM0506
3132 NO FWC DATA recorded in CFDIU last legreport.
NO FWC DATA recorded in CFDIU last leg report.NO MAINT. ACTION if no log book complaint.
TFU 313234030
Part Affected P/N Corrective P/NCFDIU B401ACM0404 B401ACM0506
3132 D li ti f F lt i PFR D li ti f F lt i PFR TFU 313234029
3 132 S yst em so ur ce wi tho ut Fa ul t m es sa ge. S ys te m s our ce wi th ou t F au lt me ss ag e.NO MAINT ACTION
TFU 313234029
Part Affected P/N Corrective P/N
CFDIU B401ACM0404 B401ACM0506
3132 PFR with NO FAULT / NO WARNING. PFR with NO FAULT / NO WARNING due to Flight phases transit ions anomalies.NO MAINT. ACTION.
TFU 313234029
Part Affected P/N Corrective P/N
CFDIU B401ACM0404 B401ACM0506
3132 DO NOT CHOOSE ECAM1/2,FDIU,SFCC1WHEN DOING STEP 6 OF AMM TASK 31 32 00710 002
DO NOT CHOOSE ECAM1/2,FDIU,SFCC1 WHEN DOING STEP 6 OF AMM TASK 31 32 00 710002
TFU 313234035
Part Affected P/N Corrective P/N
CFDIU B401ACM0506 TBD
Revision 31 PART D
ATA CFDS anomalies Remark Doc X Ref
3132 DIFFICULTIES FOR FILTER LOADING SOME DIFFICULTIES MAY BE ENCOUNTERED WHEN USING ANY OF THE PDL IN SERVICEBUT THE SFIM.
TFU 313234038
Part Affected P/N Corrective P/NCFDIU B401ACM0505 N/ACFDIU B401ACM0506 N/A
3132 NO "SYST" DATA (INTM) NO "SYST" DATA (INTM) Source CFDSIf no logbook complaint, NO MAINT ACTION. This message is generated by the CFDIU (Source :CFDS).
3 132 A ll IL S f ai lu re s a re co de d a s MMR f ai lu re s i n th efollowing case:
All ILS failures are coded as MMR failures in the following case: When the CFDIU is swapped froman aircraft fitted with the MMR to an aircraft fitted with an ILS.To recover proper ILS messages recording, a CFDIU Return To Service test must be carried out.
Part Affected P/N Corrective P/NCFDIU B401ACM0507 C12860AA02
3132 Untimely print out of real time failure and warning. Untimely print out of real time failure (RTF) and warning (RTW)In flight pull, PRINTER C/B.
TFU 313234026
Part Affected P/N Corrective P/NCFDIU B401ACM0404 CFDIU WITH AMDT A
3132 NO DMC1 DATA recorded in CFDIU groundscanning
NO DMC1 DATA recorded in CFDIU ground scanningNO MAINT. ACTION.
TFU 313234030
Part Affected P/N Corrective P/N
CFDIU B401ACM0404 B401ACM0506
Revision 31 PART D
ATA CFDS anomalies Remark Doc X Ref
3132 NO FWC DATA recorded in CFDIU last legreport.
NO FWC DATA recorded in CFDIU last leg report.NO MAINT. ACTION if no log book complaint.
TFU 313234030
Part Affected P/N Corrective P/NCFDIU B401ACM0404 B401ACM0506
3132 Duplication of Fault message in PFR. Duplication of Fault message in PFR. TFU 313234029
Part Affected P/N Corrective P/NCFDIU B401ACM0404 B401ACM0606
3132 Incoherent PFR Fault messages sent by the EIU. Incoherent PFR Fault messages sent by the EIU. TFU 313234029
3132 DO NOT CHOOSE ECAM1/2,FDIU,SFCC1WHEN DOING STEP 6 OF AMM TASK 31 32 00710 002
DO NOT CHOOSE ECAM1/2,FDIU,SFCC1 WHEN DOING STEP 6 OF AMM TASK 31 32 00 710002
TFU 313234035
Part Affected P/N Corrective P/N
CFDIU B401ACM0506 TBD
3132 DIFFICULTIES FOR FILTER LOADING SOME DIFFICULTIES MAY BE ENCOUNTERED WHEN USING ANY OF THE PDL IN SERVICEBUT THE SFIM.
TFU 313234038
Part Affected P/N Corrective P/N
CFDIU B401ACM0505 N/ACFDIU B401ACM0506 N/A
Revision 31 PART D
ATA CFDS anomalies Remark Doc X Ref
3132 NO "SYST" DATA (INTM) NO "SYST" DATA (INTM) Source CFDSIf no logbook complaint, NO MAINT ACTION. This message is generated by the CFDIU (Source :CFDS).
Part Affected P/N Corrective P/NCFDIU B401ACM0506 TBD
3 132 A ll IL S f ai lu re s a re co de d a s MMR f ai lu re s i n th efollowing case:
All ILS failures are coded as MMR failures in the following case: When the CFDIU is swapped froman aircraft fitted with the MMR to an aircraft fitted with an ILS.To recover proper ILS messages recording, a CFDIU Return To Service test must be carried out.
Part Affected P/N Corrective P/NCFDIU B401ACM0507 C12860AA02
3 132 34 CFDS pr omp t n ot a va il ab le on MCDU a t C FDIU CFDS prompt not available on MCDU at CFDIU power up.
power up. Wait 1 minute after CFDIU power up to get the CFDS prompt on the MCDU.
Part Affected P/N Corrective P/N
CFDIU C12860AA02 N/ACFDIU B401ACM0507 N/A
313234 ADFi : NO DATA FROM CFDIU Fault message ADFi : NO DATA FROM CFDIU souce ADFClass 2 Fault message to be considered as a Class 3 message.
Part Affected P/N Corrective P/NRECEIVER ADF 204-1168-7513RECEIVER ADF 622-5222-020
3 132 34 A UDIO N O DA TA FR OM CFD IU F au lt me ssa ge " AUDI O NO DA TA F RO M CF DIU" so urc e A MUClass 2 Fault message to be considered as a Class 3 message.
Part Affected P/N Corrective P/N
AMU AMU2790CA03
Revision 31 PART D
ATA CFDS anomalies Remark Doc X Ref
3 132 34 DME 1( 2, 3) : NO DA TA F ROM CFD IU F au lt me ssa ge DM E1 (2 ,3 ) : NO D AT A FRO M C FDI UClass 2 Fault message to be considered as a Class 3 message.
Part Affected P/N Corrective P/NDME 9599-614-03105DME 622-4540-023
313234 HFi : NO DATA FROM CFDIU HFi : NO DATA FROM CFDIUClass 2 Fault message to be considered as a Class 3 message.
Part Affected P/N Corrective P/N
TRANSCEIVER-HF 622-5272-020
313234 F l "NO DATA FROM CFDIU" F l "NO DATA FROM CFDIU"
313234 Fault message "NO DATA FROM CFDIU" Fault message "NO DATA FROM CFDIU"Class 2 Fault message to be considered as a Class 3 message.
Part Affected P/N Corrective P/NRECEIVER ILS 204-1230-3518 204-1230-3521
3 132 34 RMP 1( 2, 3) : NO DA TA F ROM CFD IU F au lt me ssa ge RM P1 (2 ,3 ) : NO D AT A FRO M C FDI UClass 2 Fault message to be considered as a Class 3 message.
Part Affected P/N Corrective P/NRMP 899-0850-003RMP 899-0850-004RMP 899-0850-002
3 132 34 V HF1 (2, 3) : NO DA TA F RO M CF DIU F au lt me ssa ge V HF1 (2 ,3 ) : NO DAT A FRO M CFDI UClass 2 Fault message to be considered as a Class 3 message.
Part Affected P/N Corrective P/NTRA NS CE IV ER- VHF 2 04 -12 37 -44 17
Revision 31 PART D
ATA CFDS anomalies Remark Doc X Ref
3 132 34 V OR 1 (2, 3) :NO D AT A FRO M CFDI U F au lt me ssa ge V OR 1 (2 ,3 ) : NO DA TA F ROM CFD IUClass 2 Fault message to be considered as a Class 3 message.
Part Affected P/N Corrective P/NRECEIVER-VOR 622-5220-020RECEIVER-VOR 2041231-3610RECEIVER-VOR 2041231-3622RECEIVER-VOR 2041231-3613RECEIVER-VOR 2041231-3623
313234 WRX i : NO DATA FROM CFDIU Fault message WRX i : NO DATA FROM CFDIUClass 2 Fault message to be considered as a Class 3 message.
3 132 34 A UDIO N O DA TA FR OM CFD IU F au lt me ssa ge " AUDI O NO DA TA F RO M CF DIU" so urc e A MUClass 2 Fault message to be considered as a Class 3 message.
Part Affected P/N Corrective P/NAMU AMU2790CA03
3 132 34 DME 1( 2, 3) : NO DA TA F ROM CFD IU F au lt me ssa ge DM E1 (2 ,3 ) : NO D AT A FRO M C FDI UClass 2 Fault message to be considered as a Class 3 message.
Part Affected P/N Corrective P/NDME 9599-614-03105
DME 622-4540-023
313234 HFi : NO DATA FROM CFDIU HFi : NO DATA FROM CFDIU
313234 HFi : NO DATA FROM CFDIU HFi : NO DATA FROM CFDIUClass 2 Fault message to be considered as a Class 3 message.
Part Affected P/N Corrective P/NTRANSCEIVER-HF 622-5272-020
313234 Fault message "NO DATA FROM CFDIU" Fault message "NO DATA FROM CFDIU"Class 2 Fault message to be considered as a Class 3 message.
Part Affected P/N Corrective P/NRECEIVER ILS 204-1230-3518 204-1230-3521
3 132 34 RMP 1( 2, 3) : NO DA TA F ROM CFD IU F au lt me ssa ge RM P1 (2 ,3 ) : NO D AT A FRO M C FDI UClass 2 Fault message to be considered as a Class 3 message.
Part Affected P/N Corrective P/N
RMP 899-0850-003RMP 899-0850-004RMP 899-0850-002
Revision 31 PART D
ATA CFDS anomalies Remark Doc X Ref
3 132 34 V HF1 (2, 3) : NO DA TA F RO M CF DIU F au lt me ssa ge V HF1 (2 ,3 ) : NO DAT A FRO M CFDI UClass 2 Fault message to be considered as a Class 3 message.
Part Affected P/N Corrective P/NTRA NS CE IV ER- VHF 2 04 -12 37 -44 17
3 132 34 V OR 1 (2, 3) :NO D AT A FRO M CFDI U F au lt me ssa ge V OR 1 (2 ,3 ) : NO DA TA F ROM CFD IUClass 2 Fault message to be considered as a Class 3 message.
Part Affected P/N Corrective P/NRECEIVER-VOR 622-5220-020
3 133 A CMS - L RU ID EN T p ag e Wr on g p ar t n umb er " F3 20- 00 1- 88 01 " i s di spl aye d i n pa ge L RU IDE NT , i nst ead of P N"F320-001-8802", when the aircraft is configured in 128 wd/s recording speed. PN is correctlydisplayed when MOD 32339 for 256 wd/s configuration is embodied (POST SB 31-1212).Following embodiement of SB 31-1255, incorrect reading of PN in LRU IDENT page should bedisregarded on A/C in conf 128W/S to close the SB. REF OIT 999.0033/07.
Part Affected P/N Corrective P/N
SOFTWARE-FDIMU F320-001-8802
3135 Bad PRINT OUT FORMAT. Bad PRINT OUT FORMAT.NO MAINT ACTION
TFU 313522001
Part Affected P/N Corrective P/N
PRINTER 8055154501 POST VSB M3367
Revision 31 PART D
ATA CFDS anomalies Remark Doc X Ref
3 136 B ad co un ti ng of t he fl ig ht l eg s i n t he Cl ass 3 Fa ul tmemory.
Bad counting of the flight legs in the Class 3 Fault memory. TFU 313600017
Part Affected P/N Corrective P/NDMU 903116243B0D0J1 AND SUBSEQUENT STDDMU 903116243B0D0J0 903116243B3B2G3DMU 903116243B0B0G0 903116243B3B3G4DMU 903116243B0B0G1 903116243B3D2J3
3160 Message NO RESPONSE, PRESS RETURNafter the start of DMC test.
Message NO RESPONSE, PRESS RETURN after the start of DMC test.To get the results, reenter DMC menu and access the "Test Result" item
Part Affected P/N Corrective P/NDMC - EIS 1 ALL P/N
3 162 De te ct ion th res hol d u sed fo r b ri gh tne ss t es t ar etoo restritive and lead to test fail.
Detection threshold used for brightness test is too restrictive and leads to test fail.Disregard TEST NOT OK result if no crew complaint. Temporary correction available throughreferenced VSBs.
Part Affected P/N Corrective P/NDU-DISPLAY UNIT C19366AF05DU-DISPLAY UNIT C19298AF05
3242 No access to BSCU BITE from CFDS No access to BSCU BITE from CFDSReplace the BSCU as per ISB A320-32-1318. Braking and Steering functions are not affected bythe anomaly described in TFU 32.42.34.049
3242 Wrong DATE, TIME and FLIGHT PHASE due tolack of communciation with CFDIU at the timefault msg is recorded.
Wrong DATE, TIME and FLIGHT PHASE due to lack of communciation with CFDIU at the timefault msg is recorded.TIME and DATE displayed correspond to TIME and DATE at time of consultation and not time / date of event. CLASS 3 fault msg "CFDIU(1TW)/BSCU(10GG)" should be memorized in BSCUCLASS 3 REPORT when this anomaly occurs
Part Affected P/N Corrective P/NBSCU E21327003 E21327004BSCU E21327001 E21327004
3242 No access to BSCU BITE from CFDS No access to BSCU BITE from CFDSReplace the BSCU as per ISB A320-32-1318. Braking and Steering functions are not affected bythe anomaly described in TFU 32.42.34.049
3242 Wrong DATE, TIME and FLIGHT PHASE due tolack of communciation with CFDIU at the timefault msg is recorded.
Wrong DATE, TIME and FLIGHT PHASE due to lack of communciation with CFDIU at the timefault msg is recorded.TIME and DATE displayed correspond to TIME and DATE at time of consultation and not time / date of event. CLASS 3 fault msg "CFDIU(1TW)/BSCU(10GG)" should be memorized in BSCUCLASS 3 REPORT when this anomaly occurs
Part Affected P/N Corrective P/NBSCU E21327003 E21327004BSCU E21327001 E21327004
3249 During TPIU Bite test "NO RESPONSE"message may appears on the MCDU
During TPIU Bite test "NO RESPONSE" message may appears on the MCDURestart the TPIU Bite test
Part Affected P/N Corrective P/NTPIS 1058-34 TBD
3269 L/G Menu Mode access possible during flight Menu Mode access possible during flight TFU 323134043
Part Affected P/N Corrective P/NLGCIU 664700500A4A 664700500A4B
Revision 31 PART D
ATA CFDS anomalies Remark Doc X Ref
3 269 No th in g i n th e L GCI U L ast L eg r ep or t in ste ad o f"NO FAILURE"
Nothing in the LGCIU Last Leg report instead of "NO FAILURE" TFU 323134043
Part Affected P/N Corrective P/NLGCIU 664700500A4A 664700500A4B
3269 Spurious NO DATA FROM CFDS in the LGCIUGround scanning, with date ???31
Spurious NO DATA FROM CFDS in the LGCIU Ground scanning, with date ???31NO MAINT. ACTION
TFU 323134041
Part Affected P/N Corrective P/NLGCIU 664700500A4A 664700500A4B
3269 No LGCIU fault message in the PFR. No LGCIU fault message in the PFR. The first failure logged in an empty LGCIU memory is nottransmitted to the CFDIU for PFR recording.
3269 Faults on the LGCIU ARINC OUTPUT BUS arereported "LGCIU i 05GAi". With the LGCIU std4D, the following messagewill be triggered: "LGCIU/WRG: BUS i FEEDBACK".
Faults on the LGCIU ARINC OUTPUT BUS are reported "LGCIU i 05GAi". With the LGCIU std 4D,the following message will be triggered: " LGCIU/WRG: BUS i FEEDBACK".
Part Affected P/N Corrective P/N
LGCIU 664700500A4CLGCIU 664700500A4B 664700500A4D
3 269 S el . va lve an d L GCIU fa ul ts a re co ve re d b y th efault message: "LGCIU i 05GAi".With the LGCIUstd 4D, the following message "LGCIU i 05GAi / L/G SEL VALVE 40G0A" will be triggered in caseof valve or LGCIU failure.
Sel. valve and LGCIU faults are covered by the fault message: "LGCIU i 05GAi". With the LGCIUstd 4D, the following message "LGCIU i 05GAi / L/G SEL VALVE 40G0A" will be triggered in caseof valve or LGCIU failure.
Part Affected P/N Corrective P/N
LGCIU 664700500A4CLGCIU 664700500A4B 664700500A4D
Revision 31 PART D
ATA CFDS anomalies Remark Doc X Ref
3 269 If a p owe r i nte rr up t o f 10 ms or gr ea te r o cc ursafter the transition from flight phase 1 to 2 withshock absorbers compressed any subsequentfaults detected by the LGCIU will be logged inground memory and not flight memory.
If a power interrupt of 10 ms or greater occurs after the transition from flight phase 1 to 2 withshock absorbers compressed any subsequent faults detected by the LGCIU will be logged inground memory and not flight memory.
Part Affected P/N Corrective P/NLGCIU 664700500A4B 664700500A4DLGCIU 664700500A4C 664700500A4D
3269 For all fault messages " PROX SNSR xxGA TGTPOS" related to the nose L/G doors sensor(mechanical failure) the "S"of POS is missing.
For all fault messages " PROX SNSR xxGA TGT POS" related to the nose L/G doors sensor(mechanical failure) the "S" of POS is missing.
Part Affected P/N Corrective P/NLGCIU 664700500A4C 664700500A4DLGCIU 664700500A4B 664700500A4D
3269 L/G Menu Mode access possible during flight Menu Mode access possible during flight TFU 323134043
Part Affected P/N Corrective P/NLGCIU 664700500A4A 664700500A4B
3 269 No th in g i n th e L GCI U L ast L eg r ep or t in ste ad o f"NO FAILURE"
Nothing in the LGCIU Last Leg report instead of "NO FAILURE" TFU 323134043
Part Affected P/N Corrective P/NLGCIU 664700500A4A 664700500A4B
3269 Spurious NO DATA FROM CFDS in the LGCIUGround scanning, with date ???31
Spurious NO DATA FROM CFDS in the LGCIU Ground scanning, with date ???31NO MAINT. ACTION
TFU 323134041
Part Affected P/N Corrective P/N
LGCIU 664700500A4A 664700500A4B
Revision 31 PART D
ATA CFDS anomalies Remark Doc X Ref
3269 No LGCIU fault message in the PFR. No LGCIU fault message in the PFR. The first failure logged in an empty LGCIU memory is nottransmitted to the CFDIU for PFR recording.
Part Affected P/N Corrective P/NLGCIU 664700500A4C 664700500A4D
3269 Faults on the LGCIU ARINC OUTPUT BUS arereported "LGCIU i 05GAi". With the LGCIU std4D, the following messagewill be triggered: "LGCIU/WRG: BUS i FEEDBACK".
Faults on the LGCIU ARINC OUTPUT BUS are reported "LGCIU i 05GAi". With the LGCIU std 4D,the following message will be triggered: " LGCIU/WRG: BUS i FEEDBACK".
Part Affected P/N Corrective P/N
LGCIU 664700500A4CLGCIU 664700500A4B 664700500A4D
3 269 S el . va lve an d L GCIU fa ul ts a re co ve re d b y th ef lt "LGCIU i 05GAi" With th LGCIU
Sel. valve and LGCIU faults are covered by the fault message: "LGCIU i 05GAi". With the LGCIUtd 4D th f ll i "LGCIU i 05GAi / L/G SEL VALVE 40G0A" ill b t i d i
fault message: "LGCIU i 05GAi".With the LGCIUstd 4D, the following message "LGCIU i 05GAi / L/G SEL VALVE 40G0A" will be triggered in caseof valve or LGCIU failure.
std 4D, the following message "LGCIU i 05GAi / L/G SEL VALVE 40G0A" will be triggered in caseof valve or LGCIU failure.
Part Affected P/N Corrective P/N
LGCIU 664700500A4CLGCIU 664700500A4B 664700500A4D
3 269 If a p owe r i nte rr up t o f 10 ms or gr ea te r o cc ursafter the transition from flight phase 1 to 2 withshock absorbers compressed any subsequentfaults detected by the LGCIU will be logged inground memory and not flight memory.
If a power interrupt of 10 ms or greater occurs after the transition from flight phase 1 to 2 withshock absorbers compressed any subsequent faults detected by the LGCIU will be logged inground memory and not flight memory.
335100 EPSUs Battery Capacity test not possible throughthe MCDU
EPSUs Battery Capacity test not possible through the MCDUPending availability of the MCDU test, the alternate AMM Task 33-51-00-710-011-01 "RemoveBatteries for capacity check" should be applied.
Part Affected P/N Corrective P/NOBRM CIDS DIR Z064H000030D Z064H000031AOBRM CIDS DIR Z064H000030FOBRM CIDS DIR Z064H000030E Z064H000031B
3 435 No t ra nsm is si on o f ex te rn al fa il ur e a t d ete ct io nbut after power cut
No transmission of external failure at detection but after power cutNO MAINT. ACTION.
Part Affected P/N Corrective P/N
HUDC 9615433401 9615433402
3441 Bad LRU identification Bad LRU identification TFU 344100007
361100 In case of message "WAI NO BLEED AIR ENG i" associated with ECAM Warning 30.00 WINGANTI ICE L(R) VALVE OPEN, use CLASS 3 REPORT.
TFU 301100014
Part Affected P/N Corrective P/N
ZONE CONTROLLER ALL P/N 775A0000-08
4 621 A /C in ter fa ce P /N d is pla yed on LR U i de nt p ag e i ssoftware P/N (LA2T0S162C0C000 orLA2T0S111C1B0000) and not disk P/N(LA2T0S162C0C0F1 or LA2T0S111C1B0F1)
A/C interface P/N displayed on LRU ident page is software P/N (LA2T0S162C0C000 orLA2T0S111C1B0000) and not disk P/N (LA2T0S162C0C0F1 or LA2T0S111C1B0F1)The correct P/N for A/C interface S/W ends with F1
4 621 L RU i de nti fi cat io n AO C d at aba se n ot d isp la ye don LRU ident MCDU page.
LRU identification AOC database not displayed on LRU ident MCDU page.For Honeywell AOC, all P/N are displayed on AOC CONFIGURATION page(ATSU>AOC>MISC>PART NUMBERS CONFIGURATION) For Rockwell-Collins AOC, all P/N aredisplayed on AOC SYSTEM CONFIG page (ATSU>AOC>MISC MENU>SYSTEM CONFIG)
AMM_Task 462100610TFU 460000002AMM_Task 462100610
Part Affected P/N Corrective P/N
ATSU PLAT SW LA2T0S162C0C0F1 LA2T0S111C1B0F1
4 621 A /C in ter fa ce P /N d is pla yed on LR U i de nt p ag e i ssoftware P/N (LA2T0S162C0C000 orLA2T0S111C1B0000) and not disk P/N(LA2T0S162C0C0F1 or LA2T0S111C1B0F1)
A/C interface P/N displayed on LRU ident page is software P/N (LA2T0S162C0C000 orLA2T0S111C1B0000) and not disk P/N (LA2T0S162C0C0F1 or LA2T0S111C1B0F1)The correct P/N for A/C interface S/W ends with F1
(ATSU>AOC>MISC>PART NUMBERS CONFIGURATION) For Rockwell-Collins AOC, all P/N aredisplayed on AOC SYSTEM CONFIG page (ATSU>AOC>MISC MENU>SYSTEM CONFIG)
AMM_Task 462100610
Part Affected P/N Corrective P/N
ATSU PLAT SW LA2T0S162C0C0F1 LA2T0S111C1B0F1
4 621 Wh en th e A TS U s yst em t es t f unc ti on i s ac ti va ted ,the prompt "<" associated to the "RETURN" key,and the remaining time of the test are not alwaysdisplayed.
When the ATSU system test function is activated, the prompt "<" associated to the "RETURN" key,and the remaining time of the test are not always displayed.The operator must wait the end of the system test (around 3minutes)
AMM_Task 462100740
Part Affected P/N Corrective P/NATSU PLAT SW LA2T0S162C0C0F1 LA2T0J13000C0F1
4621 ATSU failures may be missing in groundscanning report.
ATSU failures may be missing in ground scanning report.Always reset ATSU before performing the ground scanning function
Part Affected P/N Corrective P/NATSU PLAT SW LA2T0S162C0C0F1 LA2T0S111C1B0F1
Revision 31 PART D
ATA CFDS anomalies Remark Doc X Ref
4621 After the DUMP TSD prompt 2 consecutivesmessages are displayed : "Waiting for response"& "No response" even if the function is properlyperformed.
After the DUMP TSD prompt 2 consecutives messages are displayed : "Waiting for response" &"No response" even if the function is properly performed.Disregard fault messages
Part Affected P/N Corrective P/N
ATSU PLAT SW LA2T0S111C1B0F1 LA2T0J13000C0F1
4 621 Th e " *" i nd ica ti ng t he p os si bi li ty t o p ri nt i s n otalways displayed. The "*" is systematicalydisplayed after activatingthe PRINT function.A"PRINT FAILED" message can be displayed onMCDU, even if the print is successful.
The "*" indicating the possibility to print is not always displayed. The "*" is systematicaly displayedafter activating the PRINT function. A "PRINT FAILED" message can be displayed on MCDU, evenif the print is successful.Use the print function even if the "*" is not displayed. Disregard a "PRINT FAILED" message.
Part Affected P/N Corrective P/N
ATSU PLAT SW LA2T0S162C0C0F1 LA2T0S111C1B0F1
4 621 A /C in ter fa ce P /N d is pla yed on LR U i de nt p ag e i ssoftware P/N (LA2T0S162C0C000 orLA2T0S111C1B0000) d di k P/N
A/C interface P/N displayed on LRU ident page is software P/N (LA2T0S162C0C000 orLA2T0S111C1B0000) and not disk P/N (LA2T0S162C0C0F1 or LA2T0S111C1B0F1)Th P/N f A/C i f S/W d i h F1
4 621 L RU i de nti fi cat io n AO C d at aba se n ot d isp la ye don LRU ident MCDU page.
LRU identification AOC database not displayed on LRU ident MCDU page.For Honeywell AOC, all P/N are displayed on AOC CONFIGURATION page(ATSU>AOC>MISC>PART NUMBERS CONFIGURATION) For Rockwell-Collins AOC, all P/N aredisplayed on AOC SYSTEM CONFIG page (ATSU>AOC>MISC MENU>SYSTEM CONFIG)
AMM_Task 462100610TFU 460000002AMM_Task 462100610
Part Affected P/N Corrective P/NATSU PLAT SW LA2T0S162C0C0F1 LA2T0S111C1B0F1
4 621 A /C in ter fa ce P /N d is pla yed on LR U i de nt p ag e i ssoftware P/N (LA2T0S162C0C000 orLA2T0S111C1B0000) and not disk P/N(LA2T0S162C0C0F1 or LA2T0S111C1B0F1)
A/C interface P/N displayed on LRU ident page is software P/N (LA2T0S162C0C000 orLA2T0S111C1B0000) and not disk P/N (LA2T0S162C0C0F1 or LA2T0S111C1B0F1)The correct P/N for A/C interface S/W ends with F1
4 621 L RU i de nti fi cat io n AO C d at aba se n ot d isp la ye don LRU ident MCDU page.
LRU identification AOC database not displayed on LRU ident MCDU page.For Honeywell AOC, all P/N are displayed on AOC CONFIGURATION page(ATSU>AOC>MISC>PART NUMBERS CONFIGURATION) For Rockwell-Collins AOC, all P/N aredisplayed on AOC SYSTEM CONFIG page (ATSU>AOC>MISC MENU>SYSTEM CONFIG)
AMM_Task 462100610TFU 460000002AMM_Task 462100610
Part Affected P/N Corrective P/N
ATSU PLAT SW LA2T0S162C0C0F1 LA2T0S111C1B0F1
4 621 Wh en th e A TS U s yst em t es t f unc ti on i s ac ti va ted ,the prompt "<" associated to the "RETURN" key,and the remaining time of the test are not alwaysdisplayed.
When the ATSU system test function is activated, the prompt "<" associated to the "RETURN" key,and the remaining time of the test are not always displayed.The operator must wait the end of the system test (around 3minutes)
AMM_Task 462100740
Part Affected P/N Corrective P/N
ATSU PLAT SW LA2T0S162C0C0F1 LA2T0J13000C0F1
4621 ATSU failures may be missing in groundscanning report.
ATSU failures may be missing in ground scanning report.Always reset ATSU before performing the ground scanning function
4621 After the DUMP TSD prompt 2 consecutivesmessages are displayed : "Waiting for response"& "No response" even if the function is properlyperformed.
After the DUMP TSD prompt 2 consecutives messages are displayed : "Waiting for response" &"No response" even if the function is properly performed.Disregard fault messages
Part Affected P/N Corrective P/NATSU PLAT SW LA2T0S111C1B0F1 LA2T0J13000C0F1
4 621 Th e " *" i nd ica ti ng t he p os si bi li ty t o p ri nt i s n otalways displayed. The "*" is systematicalydisplayed after activatingthe PRINT function.A"PRINT FAILED" message can be displayed onMCDU, even if the print is successful.
The "*" indicating the possibility to print is not always displayed. The "*" is systematicaly displayedafter activating the PRINT function. A "PRINT FAILED" message can be displayed on MCDU, evenif the print is successful.Use the print function even if the "*" is not displayed. Disregard a "PRINT FAILED" message.
Part Affected P/N Corrective P/NATSU PLAT SW LA2T0S162C0C0F1 LA2T0S111C1B0F1
Revision 31 PART D
ATA CFDS anomalies Remark Doc X Ref
4961 Some messages are sent with more than 48characters
Some messages are sent with more than 48 characters
Part Affected P/N Corrective P/NECB 304640-3 304817-1
4 961 Me ssa ge s m ay b e d up li cat ed i n th e P FR . M es sa ges ma y be du pl ica te d i n t he P FR.
Part Affected P/N Corrective P/NECB 304817-1 304817-2
4961 Some messages are sent with more than 48characters
Some messages are sent with more than 48 characters
4 961 Me ssa ge s m ay b e d up li cat ed i n th e P FR . M es sa ges ma y be du pl ica te d i n t he P FR.
Part Affected P/N Corrective P/N
ECB 304817-1 304817-2
7322 FADEC Ground Scanning There is a specificsequence of events when running FADECGROUND SCANNING which can lead to timeoutin the software loop, causing "spurious"Watchdog Timer faults (WDTPOR).
There is a specific sequence of events when running FADEC GROUND SCANNING which canlead to timeout in the software loop, causing "spurious" Watchdog Timer faults (WDTPOR).To check if WDTPOR fault is spurious or not: Completely exit Menu Mode and run the EECself-test and then exit Menu Mode without selecting Ground Scanning."
Part Affected P/N Corrective P/N
EEC 808050-4-056 SCN18EEC 824972-2-010 SCN18
Revision 31 PART D
ATA CFDS anomalies Remark Doc X Ref
7325 OIL TEMP SENSOR 4004 EN RT OK in EIUground scanning.
Fault message "OIL TEMP SENSOR 4004 EN RT OK" in EIU ground scanning.NO MAINT. ACTION when RT OK (Result Test OK) is mentioned.
732160 DMC$:NO_ECU$$_DATA 01 02 09 DMC - EIS 1 ALL P/N
732160 ECU(E$-4000KS) 01 02 09 EIS 2 EIS II SOFTWARE SXT3FE2SA0410EIS II SOFTWARE SXT3DE2SA0700EIS II SOFTWARE SXT3CE2SA0420EIS II SOFTWARE SXT4EE2SA050A
Revision 31 PART
ATA Failure Messages Phases Source Part Affected PN
732160 ECU(E$-4000KS) 01 02 09 EIS 1 EIS II SOFTWARE SXT3FE2SA0410EIS II SOFTWARE SXT3DE2SA0700EIS II SOFTWARE SXT3CE2SA0420EIS II SOFTWARE SXT4EE2SA050A
732160 ECU(E$-4000KS) 01 02 09 EIS 3 EIS II SOFTWARE SXT3FE2SA0410EIS II SOFTWARE SXT3DE2SA0700EIS II SOFTWARE SXT3CE2SA0420EIS II SOFTWARE SXT4EE2SA050A
732234 DMC$:NO_EEC$$_DATA 01 02 09 DMC - EIS 1 ALL P/N
732234 EEC(E$-4000KS) 01 02 09 EIS 3 EIS II SOFTWARE SXT3CE2SA0420