A320 Sil 00-028 CFDS Anomalies

7/22/2019 A320 Sil 00-028 CFDS Anomalies

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CUSTOMER SERVICES DIRECTORATE AIRBUS

1 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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2 RECOMMENDATIONS

The appendix is divided into five parts, which are:

A. The list of PFR failure messages (internal and external) which request specific maintenance action.

B. The list of ECAM WARNINGS and MAINTENANCE STATUS shown on the PFR, which request specificmaintenance action.

C. The list of CLASS 3 failure messages which request specific maintenance action.

D. The anomalies related to the general use of the CFDS.

E. The list of messages/warnings which AIRBUS recommend to filter.

Nota 1: The classification criteria of data recorded in A, B, C, D, E of this document is the ATA chapterassociated to the message/anomaly.

Each page of parts A, B, C, D indicates:






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Each page of part E indicates:

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






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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.






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- 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.






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LIST OF ABREVIATIONS

SIGLUM TITLE

ACARSACSCACPADIRUADFADRAEVCAFSAIDS

AMMAMUAOAAPUASSYATA

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






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SIGLUM TITLE

ECSECUEFDUEIUELACEVMUFADECFACFCDFCDCFCOMFCUFCV

FDIMUFDIUFGFINFLFMFMGC

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






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SIGLUM TITLE

MELMFTMLGMMMMEL

MPDMRBMSNMTBFMTBRMTBURMU

ND

NLG NMOBRMOVHTPAPCPCU

Master Equipment ListMaintenance Filter ToolMain Landing GearMaintenance ManualMaster Minimum Equipment List

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






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SIGLUM TITLE

TBDTEMTFUTHSTLT

TPIUTRUTSMULDUPPR CRG DETVHFVORWAI

WAIVWDBWHCWRXZC

To Be DefinedTool and Equipment ManualTechnical Follow-UpTrimmable Horizontal StabilizerTemperature Limitation Thermostat

Tyre Pressure Indicating ComputerTransformer Rectifier UnitTrouble Shooting ManualUnit Load DeviceUpper Cargo Smoke DetectorVery High FrequencyVHF Omnidirectional RangeWing Anti-Ice

Wing Anti-ice ValveWall Disconnect BoxWindow Heat ComputerWeather Radar TransceiverZone Controller



ATA Failure Messages Remark Doc X Ref F

------ - - Recording in the PFR of "empty" DMU messages in flight phase 2 or 5.No Maintenance Action required. Ref TFU 313600063

TFU 313600063 N

Part Affected P/N Corrective P/NDMU 795040-31-002 TBD

------ GR-OU-ND or GN-D - - messages in phase 8/9 GR-OU-ND or GN-D - - messages in phase 8/9Disregard Y

Part Affected P/N Corrective P/NCFDIU B401ACM0506 C12860AA02CFDIU B401ACM0507

------ - - Recording in the PFR of "empty" DMU messages in flight phase 2 or 5.No Maintenance Action required. Ref TFU 313600063

TFU 313600063 N

Part Affected P/N Corrective P/NDMU 795040-31-002 TBD

------ GR-OU-ND or GN-D - - messages in phase 8/9 GR-OU-ND or GN-D - - messages in phase 8/9Disregard

Y

Part Affected P/N Corrective P/N

CFDIU B401ACM0506 C12860AA02CFDIU B401ACM0507

000000 NO DATA NO MAINT. ACTION N

Part Affected P/N Corrective P/NCFDIU B401ACM0505 B401ACM0506

SIL 00-028 PART A : PFR Faults

Revision 31 PART




212853 FWD CARGO FAN OR SPLY (6HN) NO MAINT. ACTION if power supply between FAN and CVC is OK, 115 V 3 phases.(Minimum value : 110 V)

TFU 212854002 N

Part Affected P/N Corrective P/NCARGO VENT CTLR 600615-00-502 600615-00-503CARGO VENT CTLR 600615-01-500 600615-01-502

212854 AFT CARGO FANS OR SPLY nullNO MAINT. ACTION if power supply between FAN and CVC is OK, 115 V 3 phases.(Minimum value : 110 V)

TFU 212854002 N

Part Affected P/N Corrective P/NCARGO VENT CTLR 600615-01-500 600615-01-502CARGO VENT CTLR 600615-00-502 600615-00-503

2 151 51 P i FL OW CO NT V AL VE ( i= 1 or 2) A ss oci ate d to Mai nt en an ce S ta tus P ACK 1 (2)NO MAINT. ACTION if Bite test OK

TFU 215151004 N


FLOW CTL VALVE 751A0000-06 751A0000-07

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

216334 NO ZONE CTL DATA NO MAINT. ACTION, Could be intermittent (INTM). TFU 216334051 N

Part Affected P/N Corrective P/NZONE CONTROLLER 775A0000-06 775A0000-07CFDIU B401ACM0404


Revision 31 PART

S




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


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


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

N


EIU 3957900610 3957900612EIU 3957905003 3957905004

EIU 3957900609 3957900612EIU 3957900611 3957900612

226634 DMCi: NO FACj DATA (i=1 or 2 or 3) (j=1 or 2) No Maintenance action Y

Part Affected P/N Corrective P/NDMC - EIS 1 ALL P/N 9615325050

228112 FCU (2CA) BUS CP-L/ WXR1 (1SQ1) If no logbook associated logbook complaint, No maintenance action is required. N

Part Affected P/N Corrective P/NRADAR 066-50008-301 066-50008-405


Revision 31 PART

SIL 00 028 PART A PFR F lt




228112 FCU(2CA)CP-L BUS/ WXRi(1SQi) (i = 1 or 2) No maintenance action required if no logbook complaint. N


228112 FCU(2CA)CP-R BUS/ WXRi(1SQi) (i = 1 or 2) No maintenance action required if no logbook complaint. N


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


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


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)

NO MAINT. ACTION if no log book complaint N


RADAR 622-5132-120 VSB WRT-701X_34-77

RADAR 622-5132-020 VSB WRT-701X_34-68


Revision 31 PART

SIL 00 028 PART A PFR F lt




228212 AFS:MCDUi (i=1 or 2) NO MAINT. ACTION if no log book complaint TFU 229100011 Y

Part Affected P/N Corrective P/NFMGC ALL P/N

228212 MCDU3(3CA3)/ATSU1(1TX1) No maintenance act ion i f MCDU 3 not installed. Can be f il tered i f MCDU 3 notinstalled TFU 460000002 Y

Part Affected P/N Corrective P/NATSU PLAT SW LA2T0S111C1B0F1 LA2T0J13000C0F1

228334 AFS:FMGCi (i=1 or 2) NO MAINT ACTION IF MESSAGE NOT ASSOCIATED WITH ANY ECAMWARNING AND COCKPIT EFFECT

TFU 229100055 Y


FMGC B398AAM0410 B546BCM0205FMGC B546CCM0101 B546CAM0102

FMGC B398BAM0207 C13042AA01FMGC B546CAM0101 B546CCM0104FMGC B546BAM0203 B546BAM0206

228334 AFS:FMGCi (FMi) (i= 1 or 2) NO MAINT. ACTION if no log book complaint TFU 229100010 Y

Part Affected P/N Corrective P/NFMGC B398BAM0205 B398BAM0206FMGC B398BCM0104 B398BCM0106FMGC B398AAM0408 B398AAM0409

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


FMGC ALL P/N NONE


Revision 31 PART

SIL 00 028 PART A : PFR Faults




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.

N

Part Affected P/N Corrective P/NFMGC C13042BA02 TBDFMGC C13043AA03 TBDFMGC C13042BA03 TBDFMGC C13043BA02 TBDFMGC C13043BA04 TBDFMGC C13043BA03 TBDFMGC C13042AA03 TBD

228334 AFS:FMGCi(DO NOT REMOVE) (i=1 or 2) NO MAINT. ACTION Y


FMGC C13042AA01FMGC C13043AA01FAC PRE_STD_B397BAM0617 B397BAM0617

228334 AFS:FMGCi/ATHR ENGD FDBK NO MAINT. ACTION if not associated with ECAM WARNING : AUTO FLT A/THROFF.

Y

Part Affected P/N Corrective P/NFMGC B398AAM0XXX TBDFMGC B398BAM0XXX TBD

FMGC B398BCM0XXX TBD


Revision 31 PART





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

228334 AFS:FMGCi (i=1 or 2) NO MAINT ACTION IF MESSAGE NOT ASSOCIATED WITH ANY ECAMWARNING AND COCKPIT EFFECT

TFU 229100055 Y

Part Affected P/N Corrective P/NFMGC B398AAM0410 B546BCM0205FMGC B546CCM0101 B546CAM0102FMGC B398BAM0207 C13042AA01FMGC B546CAM0101 B546CCM0104FMGC B546BAM0203 B546BAM0206

228334 AFS:FMGCi (FMi) (i= 1 or 2) NO MAINT. ACTION if no log book complaint TFU 229100010 Y


FMGC B398BAM0205 B398BAM0206FMGC B398BCM0104 B398BCM0106FMGC B398AAM0408 B398AAM0409


Revision 31 PART





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.

N


FMGC C13042BA02 TBDFMGC C13043AA03 TBDFMGC C13042BA03 TBDFMGC C13043BA02 TBDFMGC C13043BA04 TBDFMGC C13043BA03 TBDFMGC C13042AA03 TBD

228334 AFS:FMGCi(DO NOT REMOVE) (i=1 or 2) NO MAINT. ACTION Y


FMGC C13042AA01FMGC C13043AA01FAC PRE_STD_B397BAM0617 B397BAM0617


Revision 31 PART





228334 AFS:FMGCi/ATHR ENGD FDBK NO MAINT. ACTION if not associated with ECAM WARNING : AUTO FLT A/THROFF.

Y

Part Affected P/N Corrective P/NFMGC B398AAM0XXX TBDFMGC B398BAM0XXX TBDFMGC B398BCM0XXX TBD

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


TRANSCEIVER-HF 622-5272-020 VSB HFS-700-36


Revision 31 PART





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

TFU 460000002 Y

Part Affected P/N Corrective P/NCFDIU B401ACM0505 C12860AA02CFDIU B401ACM0506 C12860AA02CFDIU B401ACM0507 C12860AA02CFDIU B401ACM0404 C12860AA02

231133 HF1COUPLER(4RE1)/FEEDER(6RE1)/ANTENNA(5RE)

No maintenance action if no logbook compaint. N


COUPLER HF ANT 792-6140-001

231133 NO HF1 DATA No Maint. Action if triggered in phase 02. Y


TRANSCEIVER-HF 964-0452-012 TBDTRANSCEIVER-HF 964-0452-001 TBD

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

TFU 460000002 Y

Part Affected P/N Corrective P/NCFDIU B401ACM0505 C12860AA02CFDIU B401ACM0506 C12860AA02CFDIU B401ACM0507 C12860AA02CFDIU B401ACM0404 C12860AA02


Revision 31 PART A





231133 HF1COUPLER(4RE1)/FEEDER(6RE1)/ANTENNA(5RE)

No maintenance action if no logbook compaint. N

Part Affected P/N Corrective P/NCOUPLER HF ANT 792-6140-001

231133 NO HF1 DATA No Maint. Action if triggered in phase 02. Y

Part Affected P/N Corrective P/NTRANSCEIVER-HF 964-0452-012 TBDTRANSCEIVER-HF 964-0452-001 TBD

231211 CHECK VHF-1 ANTENNA CIRCUIT NO MAINT. ACTION if VSB mentioned in Corrective P/N not incorporated. TFU 231200011 N

Part Affected P/N Corrective P/NTRANSCEIVER-VHF 622-5219-020 VSB VHF-700-23-36TRANSCEIVER-VHF 622-5219-020 VSB VHF-700-23-30

231233 VHF3 TRANCEIVER NO MAINT. ACTION if no log book complaint N

Part Affected P/N Corrective P/NTRANSCEIVER-VHF 622-5219-020 VSB VHF-700-23-38

231233 VHF0(1RC0) NO MAINT. ACTION if occurs in phase 02 Y


TRANSCEIVER-VHF 822-1047-030 N/ATRANSCEIVER-VHF 822-1047-020 N/A

S 00 0 8 au ts

Revision 31 PART A





231233 NO VHF3 DATA NO MAINT. ACTION when VHF3 not installedMessage to be filtered on A/C not equipped with VHF3.

Y

Part Affected P/N Corrective P/NCFDIU C12860AA02 CFDIU_STD10

231233 VHF3 TRANCEIVER NO MAINT. ACTION if no log book complaint N


231233 VHF0(1RC0) NO MAINT. ACTION if occurs in phase 02 Y


TRANSCEIVER-VHF 822-1047-030 N/ATRANSCEIVER-VHF 822-1047-020 N/A

231233 NO VHF3 DATA NO MAINT. ACTION when VHF3 not installedMessage to be filtered on A/C not equipped with VHF3.

Y


CFDIU C12860AA02 CFDIU_STD10

231313 RMPi(1RGi)/RMPj(1RGj) [i=1, 2 or 3 - j=1, 2 or 3] NO MAINT. ACTION required Y


RMP C12848AA01 TBDRMP C12848CA01 TBD

Revision 31 PART A





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


OBRM CIDS DIR Z064H000030F Z064H000032AOBRM CIDS DIR Z064H000031B Z064H000032AOBRM CIDS DIR Z064H000031C Z064H000032A

OBRM CIDS DIR Z064H000031D Z064H000032AOBRM CIDS DIR Z064H000031A Z064H000032A

Revision 31 PART A





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


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 AAPöperation 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 AAPöperation to determine the validity of the fault message.

Airbus_SIL 23-039 N


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 AAPöperation to determine the validity of the fault message.

Airbus_SIL 23-039 N


Revision 31 PART A





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


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


Airbus_SIL 23-039 N


OBRM CIDS DIR Z064H000030F Z064H000031A


Airbus_SIL 23-039 N

Part Affected P/N Corrective P/NOBRM CIDS DIR Z064H000030F Z064H000031A


Airbus_SIL 23-039 N


OBRM CIDS DIR Z064H000030F Z064H000031A

Revision 31 PART A





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


ACSC 1803A0000-03 1803A0000-04

240000 POWER SUPPLY INTERRUPT NO MAINT. ACTION Airbus_SIL 23-039 Y


DIRECTOR-CIDS Z014H000131A TBDDIRECTOR-CIDS Z014H000231B TBDDIRECTOR-CIDS Z014H000031A TBD

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

Part Affected P/N Corrective P/NDIRECTOR-CIDS Z014H000131A TBDDIRECTOR-CIDS Z014H000231B TBDDIRECTOR-CIDS Z014H000031A TBD

Revision 31 PART A





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


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


GCU 767584J

242151 IDGI DISCONNECTED (i=1 or 2) nullCheck Class 3 Fault messages

Airbus_SB 24-1077TFU 244100002

N


GPCU 740121A 740121B

Revision 31 PART A





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


GCU 767584J

242151 IDGI DISCONNECTED (i=1 or 2) null

Check Class 3 Fault messages

Airbus_SB 24-1077

TFU 244100002

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


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

Revision 31 PART A





243834 SDACi:NO DATA FROM BCLj (i=1 or 2, j=1 or 2) NO MAINT. ACTION if no Log Book complaint. Y


2 562 00 S LI DE B TL X Y/ DE U B ( 30 0RHZ) wi th X =1 , 3 o r4 and Y=R or L and Z=1, 6 or 8.

Software anomaly.Fault validity must be checked on the FAP door page.

Airbus_SIL 23-039 N


261000 WRG: CAN BUS A (or B) NO MAINT. ACTION if fault message displayed after a reset of CIDS or CIDS-SDF Airbus_SIL 23-039 N

Part Affected P/N Corrective P/NOBRM CIDS DIR Z064H000030E TBD

OBRM CIDS DIR Z064H000030F TBDOBRM CIDS DIR Z064H000030D TBD

261200 CHECK FDU ENGi SUPPLY (i=1 or 2) NO MAINT. ACTION if no log book complaint TFU 261234020 N

Part Affected P/N Corrective P/NFDU 7304-00-01 7304-01-02

261300 CHECK FDU APU LOOP A (or B) WARN CKT No MAINT. ACTION if APU FDU test does not confirm the fault message TFU 261300001 N

Part Affected P/N Corrective P/NFDU 3720-00-00 TBD

Revision 31 PART A





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

Airbus_SIL 23-039 N

Part Affected P/N Corrective P/NDIRECTOR-CIDS Z014H000131A Z014H000231BDIRECTOR-CIDS Z014H000131A Z014H000131A_AMDT_BDIRECTOR-CIDS Z014H000031A Z014H000231BDIRECTOR-CIDS Z014H000031A Z014H000031A_AMDT_B

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


DIRECTOR-CIDS Z014H000131A Z014H000131A_AMDT_BDIRECTOR-CIDS Z014H000031A Z014H000031A_AMDT_BDIRECTOR-CIDS Z014H000031A Z014H000231BDIRECTOR-CIDS Z014H000131A Z014H000231B

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

SIL 23-039 Rev6

Airbus_SIL 23-039 N


DIRECTOR-CIDS Z014H000131A Z014H000231BDIRECTOR-CIDS Z014H000131A Z014H000131A_AMDT_BDIRECTOR-CIDS Z014H000031A Z014H000231BDIRECTOR-CIDS Z014H000031A Z014H000031A_AMDT_B

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

DIRECTOR-CIDS Z014H000031A Z014H000031A_AMDT_BDIRECTOR-CIDS Z014H000031A Z014H000231BDIRECTOR-CIDS Z014H000131A Z014H000231B

Revision 31 PART A





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


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


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]

TFU 275134025 N


SFCC 49-117-10 49-170-11SFCC 49-170-07 49-170-11

Revision 31 PART A





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


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)

NO MAINT ACTION if no log book complaint Y


SDAC 350E5161122 350E5151331SDAC 350E5151022 350E5151331

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


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.

TFU 275134025 N


SFCC 49-170-07 49-170-11

SFCC 49-117-10 49-170-11

Revision 31 PART A





281500 FUEL INTERCELL TRANSFERXFRVALVE29QM/72QM/10QP

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.

AMM_Task 281500740002AMM_Task 284600740001TFU 281500009

N


COMPUTER-FQI ALL P/N

2 842 34 FUE L Q UA NTI TY FQ IC 3 QT N O MA INT. A CTI ON i f FQ IC g ra de s re ma in s at 1 a fte r FQ IC te st t hr ou gh CFD S.

Associated with ECAM warning : 28-00 FQI CH1(2) FAULT

TFU 284234030 N


COMPUTER-FQI SIC5059XXXX05 SIC5059XXXX07COMPUTER-FQI SIC5059XXXX06 SIC5059XXXX07

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.

TFU 284200038 Y


COMPUTER-FQI SIC5059XXXX05 FQIC STAGE 8COMPUTER-FQI SIC5059XXXX07 FQIC STAGE 8

COMPUTER-FQI SIC5059XXXX06 FQIC STAGE 8

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



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

Revision 31 PART A





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/NCOMPUTER-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 (AMM

28-46-00-740-001). If the test shows NO FAULT then no further action is required.

N

Part Affected P/N Corrective P/NLEVEL SENSING ALL P/N

301151 R(L) WAI FILTER OR VALVE 10DL (9DL) NO MAINT. ACTION if not associated with ECAM warning. TSM_Task ATA30TFU 301100014

Y


ZONE CONTROLLER 775A0000-07 775A0000-08

307151 DRAINMAST HEATER AFT (FWD) NO MAINT. ACTION if no blockage or system malfunction reported. Airbus_SB 30-1030TFU 307100002

N


DRAIN MAST ASSY 4-60000H840-00 4-60000H882-00DRAIN MAST ASSY 4-60000H800-00 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.

Airbus_SB 30-1030TFU 307100003TFU 307100002

N


DRAIN MAST ASSY 4-60000H800-00 4-60000H882-00


Revision 31 PART A





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 SY

4-60000H800-00 or DRAIN MAST ASSY 4-60000H840-00 is installed.NO MAINT. ACTION if no blockage or system malfunction reported.

Airbus_SB 30-1030

TFU 307100003TFU 307100002

N

Part Affected P/N Corrective P/NDRAIN MAST ASSY 4-60000H800-00 4-60000H882-00DRAIN MAST ASSY 4-60000H840-00 4-60000H882-00

3 071 51 DRA IN MAS T HE ATE R MI D V al id o nly i f Mo d 2 159 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



N




N



Revision 31 PART A

ATA F il M R k D X R f F






Airbus_SB 30-1030TFU 307100003TFU 307100002

N


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



N



Airbus_SB 30-1030TFU 307100003TFU 307100002

N



N


Revision 31 PART A







Airbus_SB 30-1030TFU 307100003TFU 307100002

N


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



N



N



Airbus_SB 30-1030TFU 307100003TFU 307100002

N



Revision 31 PART A






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


311234 FLPi NO CFDIU DATA (i=1 or 2) Wrong ATA chapter. Should be 313434 instead. N

Part Affected P/N Corrective P/NSFCC 49-170-11 TBDSFCC 49-117-09 TBDSFCC 49-117-10 TBD

313234 RADARi: NO DATA FROM CFDIU (i=1 or 2) NO MAINT. ACTION TFU 344100010 Y

Part Affected P/N Corrective P/NRADAR 204-1217-0421 VSB RTA-4A-34-173

RADAR 204-1217-0418 VSB RTA-4A-34-173

313234 LGCIU i:NO DATA FROM CFDS (i=1 or 2) Appears after a CFDIU power down, NO MAINTENANCE ACTION TFU 323134043 N

Part Affected P/N Corrective P/NLGCIU 664700500A4A 664700500A4B

313234 CFDIU(1TM1)/HFi(1REi) (i=0,1 or 2) No maintenance action if no logbook complaint. N

Part Affected P/N Corrective P/NTRANSCEIVER-HF 964-0452-001 TBD

Revision 31 PART A






313234 RADARi: NO DATA FROM CFDIU (i=1 or 2) NO MAINT. ACTION TFU 344100010 Y

Part Affected P/N Corrective P/NRADAR 204-1217-0421 VSB RTA-4A-34-173RADAR 204-1217-0418 VSB RTA-4A-34-173

313234 LGCIU i:NO DATA FROM CFDS (i=1 or 2) Appears after a CFDIU power down, NO MAINTENANCE ACTION TFU 323134043 N


313234 CFDIU(1TM1)/HFi(1REi) (i=0,1 or 2) No maintenance action if no logbook complaint. N

Part Affected P/N Corrective P/NTRANSCEIVER-HF 964-0452-001 TBD

313316 ACCELEROMETER ACCELEROMETER Class II fault message with Maint STS.Apply TSM procedure.

TSM_Task 313300810805MPD_Task 313000-04-1

N


FDIU ED43A1D2 ED43A1D5FDIU ED43A1D3 ED43A1D5

313355 DFDR PLAYBACK NO MAINTENANCE ACTION.EMBODY VSB SFIM FDIU/360-31-090

N


FDIU ED43A1D3 ED43A1D4

Revision 31 PART A






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


DMU 795040-30-001 795040-31-002

313652 DAR TAPE LOW No Maintenance Action required N


DMU 795040-30-001 795040-31-002

313652 DAR No Maintenance Action required N


DMU 795040-30-001 795040-31-002

Revision 31 PART A





g

313652 DAR TAPE LOW No Maintenance Action required N

Part Affected P/N Corrective P/NDMU 795040-30-001 795040-31-002

316322 DU EWD(4WT1)/ECP(6WT) No maintenance action required if no logbook complaint. TFU 316100008 Y

Part Affected P/N Corrective P/NEIS II SOFTWARE SXT4EE2SA050A SXT3DE2SA0700EIS II SOFTWARE SXT3CE2SA0420 SXT3DE2SA0700

316322 DU ND CAPT(3WT1)/ND CAPT POT(8WT1) No maintenance action required if no logbook complaint. TFU 316100008 Y


316322 DU ND FO(3WT2)/ND FO POT(8WT2) No maintenance action required if no logbook complaint. TFU 316100008 Y

Part Affected P/N Corrective P/NEIS II SOFTWARE SXT3CE2SA0420 SXT3DE2SA0700EIS II SOFTWARE SXT4EE2SA050A SXT3DE2SA0700

316322 DU PFD CAPT(2WT1)/PFD CAPT POT(7WT1) No maintenance action required if no logbook complaint. TFU 316100008 Y


Revision 31 PART A





316322 DU PFD FO(2WT2)/PFD FO POT(7WT2) No maintenance action required if no logbook complaint. TFU 316100008 Y


316322 DU SD(4WT2)/ECP(6WT) No maintenance action required if no logbook complaint. TFU 316100008 Y


316322 DU EWD(4WT1)/ECP(6WT) No maintenance action required if no logbook complaint. TFU 316100008 Y


316322 DU ND CAPT(3WT1)/ND CAPT POT(8WT1) No maintenance action required if no logbook complaint. TFU 316100008 Y


316322 DU ND FO(3WT2)/ND FO POT(8WT2) No maintenance action required if no logbook complaint. TFU 316100008 Y


Revision 31 PART A





316322 DU PFD CAPT(2WT1)/PFD CAPT POT(7WT1) No maintenance action required if no logbook complaint. TFU 316100008 Y


316322 DU PFD FO(2WT2)/PFD FO POT(7WT2) No maintenance action required if no logbook complaint. TFU 316100008 Y


316322 DU SD(4WT2)/ECP(6WT) No maintenance action required if no logbook complaint. TFU 316100008 Y


316334 HUDC: NO DMC 1 DATA NO MAINT. ACTION TFU 343500003 N

Part Affected P/N Corrective P/NHUDC 9615433401 9615433402

316334 AFS:CHK DMCi-FMGCj CKT (i=1 or 2) (j=1 or 2) NO MAINT. ACTION required if no log book complaint N

Part Affected P/N Corrective P/NFMGC ALL P/N TBD

Revision 31 PART A



323171 LGCIU i 05GAi (i=1 or 2) NO MAINT. ACTION TFU 323134043 N


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).

N

Part Affected P/N Corrective P/NFWC 350E017271616 350E053020707FWC 350E018312020 350E053020707FWC 350E053020303 350E053020707FWC 350E053020606 350E053020707FWC 350E018301919 350E053020707FWC 350E053020404 350E053020707

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)

N


FWC 350E053020404 350E053020707FWC 350E053020303 350E053020707FWC 350E053020606 350E053020707FWC 350E018312020 350E053020606FWC 350E018301919 350E053020707

FWC 350E017271616 350E053020707

Revision 31 PART A





324224 SDACI:NO DATA FROM BSCU1 (i=1 or 2) NO MAINT. ACTION if no Log Book complaint N


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).

N

Part Affected P/N Corrective P/NFWC 350E017271616 350E053020707FWC 350E018312020 350E053020707FWC 350E053020303 350E053020707FWC 350E053020606 350E053020707FWC 350E018301919 350E053020707FWC 350E053020404 350E053020707

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)

N


FWC 350E053020404 350E053020707FWC 350E053020303 350E053020707FWC 350E053020606 350E053020707FWC 350E018312020 350E053020606FWC 350E018301919 350E053020707FWC 350E017271616 350E053020707

324224 SDACI:NO DATA FROM BSCU1 (i=1 or 2) NO MAINT. ACTION if no Log Book complaint N


SDAC 350E5161122 350E5151331SDAC 350E5151022 350E5151331

Revision 31 PART A





324234 SDACi:NO DATA FROM BSCU2 (i=1 or 2) NO MAINT. ACTION if no Log Book complaint N


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

TFU 324234049Airbus_SB 32-1318

N

Part Affected P/N Corrective P/NBSCU E21327003 E21327005BSCU E21327004 E21327005BSCU E21327001 E21327005

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

TFU 324234049Airbus_SB 32-1318

N


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


BSCU E21327003 E21327004

Revision 31 PART A





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


N



N


BSCU E213270B1 TBD


N


BSCU E213270B1 TBD


N


BSCU E213270B1 TBD

Revision 31 PART A






N



N



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


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


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

Y

Revision 31 PART A





are embodied.

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


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


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.

Y


324934 SDACi:NO DATA FROM TPIU (i=1 or 2) NO MAINT. ACTION if no Log Book complaint N

Part Affected P/N Corrective P/NSDAC 350E5151022 350E5151331

SDAC 350E5161122 350E5151331

Revision 31 PART A


3 251 51 S TE ER ING E LE CTRO H YDR AU LI C M ODU LE N MAINT ACTION if f lt t i d ft L di G f f ll t i N




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


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


PHC 1663214200 1663214301

Revision 31 PART A


341119 AOA SNSRi (3FPi)/ ADIRUi(1FPi) (i 1 2 or 3) NO MAINTENANCE ACTION if appears after an AOA test TFU 341000017 N




341119 AOA SNSRi (3FPi)/ ADIRUi(1FPi) (i=1, 2 or 3) NO MAINTENANCE ACTION if appears after an AOA test. TFU 341000017 N

Part Affected P/N Corrective P/NADIRU 465020-0303-0308 465020-0303-0309

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/NPHC 1663214200 1663214301

341119 AOA SNSRi (3FPi)/ ADIRUi(1FPi) (i=1, 2 or 3) NO MAINTENANCE ACTION if appears after an AOA test. TFU 341000017 N


ADIRU 465020-0303-0308 465020-0303-0309

341119 AOA SENSOR 3FPi (i=1 , 2 or 3) Associated with the ECAM warning ANTI ICE CAPT (F/O,STBY) AOA. TFU 303100016

Other TSM-ATA30TFU 303134006

N


PHC 1663214200 1663214301

341234 AFS:ADIRU1/2/3 DISAGREE NO MAINT. ACTION if not associated to any message in the ADIRU Bite TFU 229100009 Y


FAC B397CAM0101 B397BAM0509FAC B397BAM0407 B397BAM0509FAC B397BAM0406 B397BAM0509

FAC B397CAM0102 B397BAM0509

Revision 31 PART A


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/NFAC B397AAM0508 B397BAM0509FAC B397AAM0507 B397BAM0509FAC B397AAM0509 B397BAM0509FAC B397AAM0510 B397BAM0509



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


SFCC 49-117-06 49-117-07

341234 AFS:ADIRU1/2/3 DISAGREE No maintenance action if no logbook complaint TFU 220000012 Y


FAC B397AAM0507 B397BAM0513FAC B397AAM0508 B397BAM0513FAC B397BAM0406 B397BAM0513FAC B397BAM0407 B397BAM0513

Revision 31 PART A


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 RADARi: NO DATA FROM ADIRU (i=1 or 2) The fault appears during ground test. Repeat test. If result OK no further MAINTACTION required.

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.

N

Part Affected P/N Corrective P/NRADAR 066-50008-407 TBDRADAR 066-50008-405 TBDRADAR 066-50008-409 TBD

341234 ADIRUi+3(1FPi+3) ADRBUS /WXRi(1SQi) ( i = 1or 2)

No maintenance action required if no logbook complaint. Y


RADAR 822-1710-202 822-1710-203RADAR 822-1710-201 822-1710-203

341234 AFS:ADIRU1/2/3 DISAGREE NO MAINT.ACTION IF NO LOGBOOK COMPLAINT.Corrected by SB 34-1122 that cover pitot re-location

N

Part Affected P/N Corrective P/NPROBE-PITOT PRE SB 34-1122 POST SB 34-1122

341234 QUALIFIER D1/2/ WXR1(1SQ1) No maintenance action if no logbook compaint. N


Revision 31 PART A


341234 RADARi: NO DATA FROM ADIRU (i=1 or 2) NO MAINT. ACTION if no log book complaint N




3 3 O O U ( o ) O C O o og boo co p a t

Part Affected P/N Corrective P/NRADAR 622-5132-020 VSB WRT-701X_34-68RADAR 622-5132-120 VSB WRT-701X_34-77

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.

N




FAC B397AAM0508 B397BAM0509FAC B397AAM0507 B397BAM0509FAC B397AAM0509 B397BAM0509FAC B397AAM0510 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


SFCC 49-117-06 49-117-07

Revision 31 PART A


341234 AFS:ADIRU1/2/3 DISAGREE No maintenance action if no logbook complaint TFU 220000012 Y




g p

Part Affected P/N Corrective P/NFAC B397AAM0507 B397BAM0513FAC B397AAM0508 B397BAM0513FAC B397BAM0406 B397BAM0513FAC B397BAM0407 B397BAM0513

341234 RADARi: NO DATA FROM ADIRU (i=1 or 2) The fault appears during ground test. Repeat test. If result OK no further MAINTACTION required.

V en dor _S IL 9 5- 29 Re v1 N


RADAR 204-1217-0418 VSB RTA-4A-34-173RADAR 204-1217-0421 VSB RTA-4A-34-173

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.

N


341234 ADIRUi+3(1FPi+3) ADRBUS /WXRi(1SQi) ( i = 1or 2)

No maintenance action required if no logbook complaint. Y


RADAR 822-1710-202 822-1710-203RADAR 822-1710-201 822-1710-203

Revision 31 PART A


341234 AFS:ADIRU1/2/3 DISAGREE NO MAINT.ACTION IF NO LOGBOOK COMPLAINT. N




Corrected by SB 34-1122 that cover pitot re-location

Part Affected P/N Corrective P/NPROBE-PITOT PRE SB 34-1122 POST SB 34-1122

341234 QUALIFIER D1/2/ WXR1(1SQ1) No maintenance action if no logbook compaint. N


341234 RADARi: NO DATA FROM ADIRU (i=1 or 2) NO MAINT. ACTION if no log book complaint N


RADAR 622-5132-020 VSB WRT-701X_34-68RADAR 622-5132-120 VSB WRT-701X_34-77

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.

N


RADAR 066-50008-409 TBDRADAR 066-50008-407 TBDRADAR 066-50008-405 TBD

343234 ILSi BAD DATA FROM CFDIU (i=1 or 2) NO MAINT. ACTION N


Revision 31 PART A


343522 HUD - OHU NO MAINT. ACTION if no log book complaint. TFU 343500003 Y




Part Affected P/N Corrective P/NHUDC 9615433402 V65 SOFTWAREHUDC 9615433401 V65 SOFTWARE

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


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


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


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


343631 MMR1 (40RT1)/GPWC (1WZ) NO MAINT. ACTION required Y




Part Affected P/N Corrective P/NGPWC 9650976003102 9650976003206

343631 NO MLSi DATA (i=1 or 2) No maintenance action if no logbook complaint Y

Part Affected P/N Corrective P/NAMU AMU3514ES01 TBDAMU AMU3514CS01 TBDAMU AMU3514DS01 TBDAMU AMU3514BS01 TBD

343631 ILSi RECEIVER (i=1 or 2) NO MAINT. ACTION if no Log book complaint TFU 343600004 Y


RECEIVER 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


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


Revision 31 PART A


343631 ILSi(2RTi) (i=1 or 2) This message is triggered when receiver not tuned to any station and a self test isperformed

N




performed.NO MAINT. ACTION required if no logbook complaint.

Part Affected P/N Corrective P/NRECEIVER ILS 622-9738-041 VSB COLLINS ILS-720-34-11RECEIVER ILS 622-9738-020 VSB COLLINS ILS-720-34-6

343631 MMR1 (40RT1)/GPWC (1WZ) NO MAINT. ACTION required Y

Part Affected P/N Corrective P/NGPWC 9650976003102 9650976003206

343631 NO MLSi DATA (i=1 or 2) No maintenance action if no logbook complaint Y

Part Affected P/N Corrective P/NAMU AMU3514ES01 TBDAMU AMU3514CS01 TBDAMU AMU3514DS01 TBD

AMU AMU3514BS01 TBD

343676 ILSi(2RTi) BITE FAULT (i=1 or 2) Ref TSM task 34 36 00 810 801 associated to ILS fault "34 36 31 ILSi RECEIVER" N


344111 RADAR i ANTENNA (i=1 or 2) NO MAINT ACTION if nologbook complaint TFU 344100007 N


Revision 31 PART A


344111 RADAR1 ANTENNA NO MAINT. ACTION if no log book complaint N





344111 RADAR i ANTENNA (i=1 or 2) NO MAINT ACTION if message recorded immediately after engine start (this i tem

concerns only 2 airlines)

N

Part Affected P/N Corrective P/NRADAR MI585306402 TBD

344111 WXR ANTENNA (11SQ) No maintenance action required if no logbook complaint. N

Part Affected P/N Corrective P/NRADAR 822-1710-202 822-1710-203RADAR 822-1710-201 822-1710-203

344111 RADAR i ANTENNA (i=1 or 2) NO MAINT ACTION if nologbook complaint TFU 344100007 N


344111 RADAR1 ANTENNA NO MAINT. ACTION if no log book complaint N


RADAR 622-5132-020 VSB WRT-701X_34-68RADAR 622-5132-120 VSB WRT-701X_34-77

Revision 31 PART A


344111 RADAR i ANTENNA (i=1 or 2) NO MAINT ACTION if message recorded immediately after engine start (this i temconcerns only 2 airlines)

N




y )


344111 WXR ANTENNA (11SQ) No maintenance action required if no logbook complaint. N


344112 RADAR1 CONTROL UNIT NO MAINT. ACTION if no log book complaint N


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


344112 RADAR1 CONTROL UNIT NO MAINT. ACTION if no log book complaint N


RADAR 622-5132-120 VSB WRT-701X_34-77

RADAR 622-5132-020 VSB WRT-701X_34-68

Revision 31 PART A


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





344133 RADARi TRANSCEIVER (i=1 or 2) NO MAINT. ACTION if no log book complaint TFU 344100007 N


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


Revision 31 PART A


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

N




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


344133 RADARi TRANSCEIVER (i=1 or 2) NO MAINT. ACTION if no log book complaint TFU 344100007 N


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


344133 RADAR1 TRANSCEIVER NO MAINT. ACTION if no log book complaint N


Revision 31 PART A


344133 RADARi TRANSCEIVER (i=1 or 2) NO MAINT ACTION if message recorded immediately after engine start (this i temconcerns only 2 airlines).

Y





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").

N



344133 WXRi(1SQi) (i= 1 or 2) No maintenance action if no logbook complaint. N


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


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


RADAR 066-50008-407 TBD

RADAR 066-50008-409 TBDRADAR 066-50008-405 TBD

Revision 31 PART A


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

N




fault 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



N


RADAR 066-50008-405 TBD


N


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


RADAR 822-1710-201 822-1710-202

Revision 31 PART A


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



TCAS 4066010-905 TBDTCAS 4066010-904 TBDTCAS 066-50000-2X20 TBDTCAS 066-50000-1X08 TBDTCAS 4066010-903 TBDTCAS 940-300-001 TBD



TCAS 7517900-10002TCAS 822-1293-322TCAS 7517900-10003TCAS 622-8971-320TCAS 622-8971-322

Revision 31 PART A






Part Affected P/N Corrective P/NTCAS 4066010-905 TBDTCAS 4066010-904 TBDTCAS 066-50000-2X20 TBDTCAS 066-50000-1X08 TBDTCAS 4066010-903 TBDTCAS 940-300-001 TBD

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


TCAS 622-8971-320 N/ATCAS 622-8971-322 N/ATCAS 822-1293-322 N/A


Part Affected P/N Corrective P/NTCAS 066-50000-1X08 N/ATCAS 940-300-001 N/ATCAS 4066010-903 N/ATCAS 066-50000-2X20 N/ATCAS 4066010-904 N/ATCAS 4066010-905 N/A

344333 NO TCAS DATA No maintenance action required if no logbook complaint and if TCAS BITE is OK. TFU 344300011 N


TCAS 7517900-10002 N/ATCAS 7517900-10003 N/A

Revision 31 PART A






Part Affected P/N Corrective P/NTCAS 066-50000-1X08 N/ATCAS 066-50000-2X20 N/ATCAS 4066010-905 N/ATCAS 940-300-001 N/ATCAS 4066010-904 N/A





Part Affected P/N Corrective P/NTCAS 7517900-10002 N/ATCAS 7517900-10003 N/A


Part Affected P/N Corrective P/NTCAS 622-8971-320 N/ATCAS 622-8971-322 N/ATCAS 822-1293-322 N/A

Revision 31 PART A






Part Affected P/N Corrective P/NTCAS 066-50000-1X08 N/ATCAS 940-300-001 N/ATCAS 4066010-903 N/ATCAS 066-50000-2X20 N/ATCAS 4066010-904 N/ATCAS 4066010-905 N/A



TCAS 7517900-10002 N/ATCAS 7517900-10003 N/A


Part Affected P/N Corrective P/NTCAS 066-50000-1X08 N/ATCAS 066-50000-2X20 N/ATCAS 4066010-905 N/ATCAS 940-300-001 N/ATCAS 4066010-904 N/A



TCAS 822-1293-322 N/ATCAS 622-8971-320 N/A

TCAS 622-8971-322 N/A

Revision 31 PART A







344334 TCAS ARINC 429 No maintenance action required if no logbook complaint and if TCAS BITE is OK TFU 344300006 N

Part Affected P/N Corrective P/NTCAS 4066010-903 4066010-905

3 443 34 TCA S UN TRA CE ABL E N o ma int ena nce ac ti on r equ ir ed i f no l og bo ok T CAS co mp lai nt a nd i f T CA S BI TE i sOK.

TFU 344300006 N


344334 TCAS (1SG) No maintenance action required if no logbook complaint and if TCAS BITE is OK. TFU 344300004 N


TCAS 066-50000-0208 TPA-81A-34-75REV1TCAS 066-50000-0108 TPA-81A-34-61REV2TCAS 066-50000-0102 N/ATCAS 066-50000-0203 TPA-81A-34-72REV1

Revision 31 PART A


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-34-75REV1TCAS 066-50000-0108 TPA-81A-34-61REV2TCAS 066-50000-0203 TPA-81A-34-72REV1



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


TCAS 4066010-904 N/ATCAS 940-300-001 N/ATCAS 4066010-905 N/ATCAS 066-50000-2X20 N/ATCAS 066-50000-1X08 N/A

Revision 31 PART A










Part Affected P/N Corrective P/NTCAS 4066010-904 N/ATCAS 940-300-001 N/A

TCAS 4066010-905 N/ATCAS 066-50000-1X08 N/ATCAS 066-50000-2X20 N/A

344334 TCAS ARINC 429 No maintenance action required if no logbook complaint and if TCAS BITE is OK TFU 344300006 N


Revision 31 PART A


3 443 34 TCA S UN TRA CE ABL E N o ma int ena nce ac ti on r equ ir ed i f no l og bo ok T CAS co mp lai nt a nd i f T CA S BI TE i sOK.

TFU 344300006 N






Part Affected P/N Corrective P/NTCAS 066-50000-0208 TPA-81A-34-75REV1TCAS 066-50000-0108 TPA-81A-34-61REV2TCAS 066-50000-0102 N/ATCAS 066-50000-0203 TPA-81A-34-72REV1

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

TCAS 066-50000-0108 TPA-81A-34-61REV2TCAS 066-50000-0203 TPA-81A-34-72REV1



TCAS 7517900-10003 N/ATCAS 7517900-10002 N/A

Revision 31 PART 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 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

Part Affected P/N Corrective P/NTCAS 4066010-904 N/ATCAS 940-300-001 N/ATCAS 4066010-905 N/ATCAS 066-50000-2X20 N/ATCAS 066-50000-1X08 N/A





Revision 31 PART A






Part Affected P/N Corrective P/NTCAS 4066010-904 N/ATCAS 940-300-001 N/ATCAS 4066010-905 N/ATCAS 066-50000-1X08 N/ATCAS 066-50000-2X20 N/A

345000 MODE S i (i = 1 or 2) No maintenance action required if no logbook complaint and if TCAS BITE is OK. TFU 344300006 N


TCAS 4066010-903 4066010-905

345133 DME-i TRANSCEIVER (i=1 or 2) NO MAINT. ACTION if no log book complaints TFU 345100008 N


DME 622-4540-022 VSB DME-700-34-27

DME 622-4540-023 VSB DME-700-34-27DME 622-4540-021 VSB DME-700-34-27DME 622-4540-020 VSB DME-700-34-27

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

TFU 345100008 Y

Part Affected P/N Corrective P/NDME 622-4540-023 VSB DME-700-34-33DME 622-4540-023 VSB DME-700-34-27

Revision 31 PART A


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

345133 DME-i TRANSCEIVER (i=1 or 2) NO MAINT. ACTION if no log book complaints TFU 345100008 N

Part Affected P/N Corrective P/NDME 622-4540-022 VSB DME-700-34-27DME 622-4540-023 VSB DME-700-34-27DME 622-4540-021 VSB DME-700-34-27DME 622-4540-020 VSB DME-700-34-27

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

TFU 345100008 Y

Part Affected P/N Corrective P/NDME 622-4540-023 VSB DME-700-34-33DME 622-4540-023 VSB DME-700-34-27

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


TRANSPONDER-ATC 7517800-10005 TBD

Revision 31 PART A


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

P Aff d P/N C i P/N





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


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


TCAS 7517900-10002 N/ATCAS 7517900-10003 N/A

Revision 31 PART 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 3fault 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


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


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


CFDIU ALL P/N

Revision 31 PART A


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

N





Part Affected P/N Corrective P/NRECEIVER 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/NCFDIU ALL P/N

345332 ADF-i RECEIVER (i=1 or 2) NO MAINT. ACTION if no log book complaint. N


RECEIVER ADF 622-5222-020 VSB ADF-700-43-27RECEIVER ADF 622-5222-020 VSB ADF-700-34-20RECEIVER ADF 622-5222-020 VSB ADF-700-34-21

345531 VOR i : VOR RECEIVER (=1 or 2) NO MAINT ACTION if no logbook complaint TFU 345500013TFU 345500009

N

Part Affected P/N Corrective P/NRECEIVER-VOR 622-5220-020 VSB_700-34-19RECEIVER-VOR 622-5220-020 VSB_700-34-10_REV1

345531 AFS : VOR i (i=1 or 2) NO MAINT. ACTION if no logbook complaint Y


Revision 31 PART A


345531 VOR i : VOR RECEIVER (=1 or 2) NO MAINT ACTION if no logbook complaint TFU 345500013TFU 345500009

N





Part Affected P/N Corrective P/NRECEIVER-VOR 622-5220-020 VSB_700-34-19RECEIVER-VOR 622-5220-020 VSB_700-34-10_REV1

345531 AFS : VOR i (i=1 or 2) NO MAINT. ACTION if no logbook complaint Y


345572 VORi: VOR RECEIVER (i=1 or 2) NO MAINT. ACTION if no log book complaint. TFU 345500010 N

Part Affected P/N Corrective P/NRECEIVER-VOR 2041231-3610 VSB_RVA-36A-34-54

3 611 34 S DA Ci :NO D AT A FRO M B MC j ( i=1 o r 2 ) ( j=1 o r

2)

NO MAINT. ACTION if no logbook complaint N


SDAC 350E5161122 350E5151331SDAC 350E5151022 350E5151331

3 831 00 L IQ D L VL X MTR ( 40 MG ) A ND L IQ D L VL S NS R(41MG)

Software anomalyThe 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


OBRM CIDS DIR Z064H000030F Z064H000031AOBRM CIDS DIR Z064H000030D Z064H000031A

OBRM CIDS DIR Z064H000030E Z064H000031B

Revision 31 PART A


383134 VSC NO MAINT. ACTION Airbus_SB 38-1044Vendor_SB 4440403802TFU 383100022

Y





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.


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.


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


492316 LCDT SENSOR P29 No MAINT. ACTION Airbus_SB 49-1061 Y





ECB 4500001B 4500003HECB 4500001A 4500003HECB 4500003G 4500003HECB 4500001 4500003HAPU APU APS3200

493211 FUEL CTL UNIT P19 NO MAINT. ACTION if no logbook complaint Airbus_SB 49-1053 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


SDAC 350E5151022 350E5151331

SDAC 350E5161122 350E5151331

499414 OIL PRESS SW P14 NO MAINT. ACTION if no logbook complaint N


ECB 304817-1 304817-2

Revision 31 PART A


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

N





APU 3800278-2APU 3800278-4APU 3800278-3

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


DMC - EIS 1 ALL P/N

Revision 31 PART A


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





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


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


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


EIS II SOFTWARE SXT3CE2SA0420 SXT3DE2SA0700

Revision 31 PART A


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/NDMC EIS ALL 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/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.

TFU 732900033 N


ECU 1820M89P02 SB_73-1034ECU 1820M88P02ECU 1820M36P02 SB_73-1037ECU 1820M87P02

752420 ECU AIR,J7(8), ECU Must be disregarded if CFMI S/B 72-436 AIRBUS S/B 71-1014 embodied on theaircraft.

Airbus_SB 71-1014Vendor_SB 72-436

N

Part Affected P/N Corrective P/NECU 1519M83P03 1459M55P17ECU 1519M83P02 1820M27P01ECU 1459M55P16 1519M83P04ECU 1459M55P15

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


EEC SCN12C SCN12D

Revision 31 PART A


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.

N

Part Affected P/N Corrective P/NRADAR 822 1710 201 822 1710 202




RADAR 822-1710-201 822-1710-202

7 933 15 S DA Ci :E NG 2 O IL P RE SS X MTR 40 04 EN ( i=1 o r2)

Wrong FIN number. Should be 4003EN instead. All FWC in BASIC configuration (PreMod 24159) are affected (E2, E3, E4, F2).

N

Part Affected P/N Corrective P/NFWC PRE_STD_H2F3 POST_STD_H2F3

7 933 16 CHE CK N 4 BR G S CA V PR ES S X MTR i CI RCUI T4005EN (i=1 or 2)

NO MAINT. ACTION if EIU Ground Scanning result is RTOK TFU 793316001 N


EIU ALL_P/N 3957905005EIU ALL_P/N 3957905004

793415 CHECK OIL PRESS SWITCH 3EN(i) (i=1 or 2) No maintenance action is required if no logbook complaint when the message is

recorded in the PFR in flight phase 2 or phase 9.

Y


TPIS 1058-34

X XX XX X A DF- i:NO D AT A FRO M CON TRO L S OU RCE(i=1 or 2)

NO MAINT ACTION TFU 345300007 Y


RECEIVER ADF 204-1168-7513 VSB DFA-75A-34-49

Revision 31 PART A


X XX XX X V ORi NO DA TA F RO M CO NT ROL SO URC E ( i=1or2)

N O MA INT. A CTI ON. Me ssa ge tr ig ger ed ma in ly fo ll ow in g F MS r ese ts T FU 3 45 50 000 8 Y

Part Affected P/N Corrective P/NRECEIVER VOR 2041231 3610 VSB RVA 36A 34 54




RECEIVER-VOR 2041231-3610 VSB_RVA-36A-34-54

XXXXXX VHFi:NO DATA FROM CONTROL SOURCE (i=1, 2 or 3)

NO MAINT. ACTION TFU 231200007 N


X XX XX X IL S i : NO DA TA FRO M CO NTRO L S OURCE(i=1 or 2)



RECEIVER ILS 204-1230-3518 VSB RIA-35A-34-41CFDIU B401ACM0404

X XX XX X A DF- i : NO DA TA FRO M C ONT RO L S OUR CE

(i=1 or 2)

NO MAINT. ACTION TFU 345300006 Y


RECEIVER ADF 622-5222-020 VSB ADF-700-34-21RECEIVER ADF 622-5222-020 VSB ADF-700-43-27

X XX XX X V OR i : NO DA TA FRO M C ONT RO L S OUR CE(i=1 or 2)

NO MAINT. ACTION (mainly due to FMS resets). TFU 345500005 Y


RECEIVER-VOR 622-5220-020 VSB_700-34-10

Revision 31 PART A


X XX XX X DME i : NO D AT A FRO M C ON TRO L S OU RCE(i=1 or 2)

NO MAINT. ACTION Y

Part Affected P/N Corrective P/NDME 9599-614-03105 VSB TDM-709-34-012




DME 9599 614 03105 VSB TDM 709 34 012

XXXXXX VHFi:NO DATA FROM CONTROL SOURCE (i=1, 2 or 3)



X XX XX X IL S i : NO DA TA FRO M CO NTRO L S OURCE(i=1 or 2)



RECEIVER ILS 204-1230-3518 VSB RIA-35A-34-41CFDIU B401ACM0404

X XX XX X A DF- i : NO DA TA FRO M C ONT RO L S OUR CE

(i=1 or 2)

NO MAINT. ACTION TFU 345300006 Y


RECEIVER ADF 622-5222-020 VSB ADF-700-34-21RECEIVER ADF 622-5222-020 VSB ADF-700-43-27

X XX XX X V OR i : NO DA TA FRO M C ONT RO L S OUR CE(i=1 or 2)

NO MAINT. ACTION (mainly due to FMS resets). TFU 345500005 Y


RECEIVER-VOR 622-5220-020 VSB_700-34-10

Revision 31 PART A


X XX XX X DME i : NO D AT A FRO M C ON TRO L S OU RCE(i=1 or 2)

NO MAINT. ACTION Y

Part Affected P/N Corrective P/NDME 9599-614-03105 VSB TDM-709-34-012




DME 9599 614 03105 VSB TDM 709 34 012

Revision 31 PART A

ATA Cockpit Effect Remark Doc X Ref F

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 902215702-8

SIL 00-028 PART B : PFR Cockpit Effects



CPC 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

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


FLOW CTL VALVE 751A0000-06 751A0000-07

Revision 31 PART


2161 AIR:PACK i REGUL FAULT (i=1 or 2) When not associated with any maintenance message, check all sensors peripheral tothe pack controler.


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


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


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.


N


PACK TEMP CTLR ALL P/N

Revision 31 PART


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/NACSC ALL P/NPACK TEMP CTLR ALL P/N

2163 COND AFT (FWD) CAB DUCT OVHT Check Temp. sensor output resistance Airbus_SIL 21-049TFU 216318001

N

Part Affected P/N Corrective P/NZONE CONTROLLER ALL P/N N/A

2163 COND CKPT DUCT OVHT Check Temp. sensor output resistance Airbus_SIL 21-049

TFU 216318001

N


ZONE CONTROLLER ALL P/N N/A


N



Revision 31 PART


2163 COND CKPT DUCT OVHT Check Temp. sensor output resistance Airbus_SIL 21-049TFU 216318001

N






N



N




N




N



Revision 31 PART


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 B397AAM0509 B397BAM0510FAC B397BAM0407 B397BAM0510FAC B397BAM0508 B397BAM0510FAC B397BAM0509 B397BAM0510FAC B397CAM0102 B397BAM0510FAC B397AAM0507 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


FAC B397BAM0406 B397BAM0509FAC B397BAM0407 B397BAM0509FAC B397AAM0508 B397BAM0509FAC B397AAM0507 B397BAM0509

2200 AUTO FLT AP OFF Configuration Warning Y


2200 AUTO FLT A/THR OFF Configuration Warning Y


FMGC ALL P/N NONE

Revision 31 PART


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 B397AAM0509 B397BAM0510FAC B397BAM0407 B397BAM0510FAC B397BAM0508 B397BAM0510FAC B397BAM0509 B397BAM0510FAC B397CAM0102 B397BAM0510FAC B397AAM0507 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


FAC B397BAM0406 B397BAM0509FAC B397BAM0407 B397BAM0509FAC B397AAM0508 B397BAM0509FAC B397AAM0507 B397BAM0509

2200 AUTO FLT AP OFF Configuration Warning Y


2200 AUTO FLT A/THR OFF Configuration Warning Y


FMGC ALL P/N NONE

Revision 31 PART


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




DIRECTOR CIDS Z014H000031A TBD

2328 COM SATCOM FAULT No. Maint. Action if ECAM WARNING triggered when ADIRU 1+2+3 OFF N

Part Affected P/N Corrective P/NEIS II SOFTWARE SXT3FE2SA0410 SXT4EE2SA050AEIS II SOFTWARE SXT3CE2SA0420 SXT4EE2SA050A

2 400 E LE C BC L i FA UL T ( i=1 o r 2 ) N O MA INT. A CTI ON i f n o fa il ur e me ssa ge i n t he PF R, an d B CL te st th ru MCD U i sOK.

TFU 243800009TFU 243800022TFU 243800007Airbus_SB 24-1075

N

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


SMOKE DET AVNCS CG7GO CGDU2000-00

Revision 31 PART


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.

N


DIRECTOR-CIDS Z014H000030C Z014H000031ADIRECTOR-CIDS Z014H000030C Z014H000131A

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



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


SMOKE DET LAV GAI2800-02 TBDSMOKE DET LAV PAI2830-00 TBD

Revision 31 PART


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


SMOKE DET AVNCS CG7GO CGDU2000-00




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


DIRECTOR-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



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.

N



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


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.

N






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


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


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




SFCC 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.

TFU 279000028 N

Part Affected P/N Corrective P/NTHSA MODULE 9231-4-600 9231-5-600ELAC 3945122504 3945122505ELAC 3945122502 3945122505

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


Other FCOM_3.02.27TFU 279300040

N


2700 F/CTL SPD BRK DISAGREE Configuration warning Y


FCDC ALL_P/N

Revision 31 PART


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





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


Other FCOM_3.02.27TFU 279300040

N


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


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.

TFU 279000028 N


THSA MODULE 9231-4-600 9231-5-600ELAC 3945122504 3945122505ELAC 3945122502 3945122505




ELAC 3945122502 3945122505

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


Other FCOM_3.02.27TFU 279300040

N


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


LEVEL SENSING N/A

Revision 31 PART


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






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



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


LGCIU 664700500A4B 664700500A4D

Revision 31 PART


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


9599-607-14932 9599-607-14942

TRANSCEIVER-RADIO 9599-607-12333 9599-607-12352




ALTIMETERPHC 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


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


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


3100 DMU (MAINT STS) Associated with the message : CAGA MEMORY FAIL. TSM_Task TSM_ATA31TFU 313600013

N

Part Affected P/N Corrective P/NDMU 903116243B0B0G1 903116243B3D2J3DMU 903116243B0B0G0 903116243B3B3G4DMU 903116243B0D0J0 903116243B3B2G3




DMU 903116243B0D0J1 AND SUBSEQUENT STD

3100 CFDIU (MAINT STS) NO MAINT. ACTION if CFDIU power up test result is : CFDIU BITE MEMORY TSM_Task ATA31

TFU 313234031

N


CFDIU B401ACM0404 CFDIU WITH AMDT A

3100 DMU (MAINT STS) Associated with the message : CAGA MEMORY FAIL. TSM_Task TSM_ATA31TFU 313600013

N

Part Affected P/N Corrective P/NDMU 903116243B0B0G1 903116243B3D2J3DMU 903116243B0B0G0 903116243B3B3G4DMU 903116243B0D0J0 903116243B3B2G3

DMU 903116243B0D0J1 AND SUBSEQUENT STD

3200 L/G LGCIU 1 (2) FAULT NO MAINT. ACTION if BITE test OK TFU 323134043 N


LGCIU 664700500A4A 664700500A4B

Revision 31 PART


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


9599-607-14932 9599-607-14942


9599-607-12333 9599-607-12352




ALTIMETER

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


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


Revision 31 PART


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


9599-607-14932 9599-607-14942


9599-607-12333 9599-607-12352




ALTIMETER

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


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


3400 NAV GPWS FAULT No maintenance action is required if occurs on ground during Taxiing or Lining-up. TFU 344800002 Y


Revision 31 PART


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 TCAS FAULT No maintenance action is required if TCAS BITE test is OK If not OK ref to TSM TFU 344300004 N




3400 NAV TCAS FAULT No maintenance action is required if TCAS BITE test is OK. If not OK ref to TSM. TFU 344300004TFU 344300007

N

Part Affected P/N Corrective P/NTCAS 066-50000-0108 TPA-81A-34-75REV1TCAS 066-50000-0102 TPA-81A-34-61REV2TCAS 066-50000-0208 TPA-81A-34-72REV1TCAS 066-50000-0203 N/A

3400 NAV RAi FAULT (=1 or 2) NO MAINT ACTION if event happens at high altitude (above 8192 ft). TFU 344200007 N


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


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


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


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


ADM PG1152AC03 PG1152AC05


Airbus_SB 34-1084TFU 341000012

N


ADIRU HG1150AC05 HG1150AC06



N


RA ANTENNA 622-8701-002

Revision 31 PART


3400 NAV GPWS FAULT No maintenance action is required if occurs on ground during Taxiing or Lining-up. TFU 344800002 Y


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 TCAS FAULT No maintenance action is required if TCAS BITE test is OK. If not OK ref to TSM. TFU 344300006 N


3400 NAV TCAS FAULT No maintenance action is required if TCAS BITE test is OK. If not OK ref to TSM. TFU 344300004TFU 344300007

N


TCAS 066-50000-0108 TPA-81A-34-75REV1TCAS 066-50000-0102 TPA-81A-34-61REV2TCAS 066-50000-0208 TPA-81A-34-72REV1TCAS 066-50000-0203 N/A

3400 NAV RAi FAULT (=1 or 2) NO MAINT ACTION if event happens at high altitude (above 8192 ft). TFU 344200007 N


9599-607-14942 VSB ERT-530-34-35


9599-607-14942 VSB ERT-530-34-34



N

Part Affected P/N Corrective P/NRA ANTENNA 622-8701-002

Revision 31 PART



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


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


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


ADM PG1152AC03 PG1152AC05


Airbus_SB 34-1084TFU 341000012

N


ADIRU HG1150AC05 HG1150AC06

Revision 31 PART




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




SEQUENCEy p

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


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


Revision 31 PART


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




7700 ENG DUAL FAILURE NO MAINT. ACTION if occurs on ground during wet / snowy / icy weather, or afterde-icing/high press. cleaning.

TFU 344200005TFU 326100003TFU 344200013

TFU 344200003

Y


9599-607-14942 9599-607-12352


9599-607-12333 9599-607-12352


9599-607-14932 9599-607-12352


9599-607-12552 9599-607-12352

7700 ENG i EIU (Maintenance Status) DISREGARD THE MESSAGE if occurs after gear non retraction. TFU 323471043TFU 323173001

N

Part Affected P/N Corrective P/NLGCIU 664700500A4B 664700500A4C

Revision 31 PART



TFU 344200005TFU 326100003TFU 344200013TFU 344200003

Y



9599-607-14942 9599-607-12352


9599-607-12333 9599-607-12352

TRANSCEIVER RADIO 9599 607 14932 9599 607 12352





9599-607-14932 9599-607-12352

TRANSCEIVER-RADIO

ALTIMETER

9599-607-12552 9599-607-12352


N


7700 ENGi FADEC HI TEMP NO MAINT. ACTION if displayed before Engine start when ING/START selected.Disappear after a FADEC reset (>30 sec.)

TFU 752400002Other FCOM_3.02.18

N

Part Affected P/N Corrective P/NECU 1459M55P15 1459M55P17ECU 1519M83P02 1519M83P04

Revision 31 PART



TFU 344200005TFU 326100003TFU 344200013TFU 344200003

Y



9599-607-14942 9599-607-12352


9599-607-12333 9599-607-12352

TRANSCEIVER RADIO 9599 607 14932 9599 607 12352





9599-607-14932 9599-607-12352

TRANSCEIVER-RADIO

ALTIMETER

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


7700 ENGi OVSPD PROT FAULT Refer to FCOM 3.02.70 if it occurs at Engine start-up. Other FCOM_3.02.70TFU 732110004

N

Part Affected P/N Corrective P/NECU 1519M83P04 1519M83P06ECU 1820M27P01 1820M27P03ECU 1519M83P03 1519M83P06ECU 1459M55P16 1459M55P19ECU 1519M83P02 1519M83P06




ECU 1519M83P02 1519M83P06ECU 1459M55P17 1459M55P19ECU 1459M55P15 1459M55P19

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.

TFU 783100085 N

Part Affected P/N Corrective P/NECU 1820M36P06ECU 1820M87P07 1820M87P09ECU 1820M89P06ECU 1820M88P07 1820M88P09

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


ECU 1820M89P07 N/AECU 1820M36P07 N/A

Revision 31 PART


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.

TFU 783100078TFU 783100100

N


ECU 1519M83PXX 1820M88P09ECU 1459M55PXX 1820M87P09ECU 1820M89P06 1820M89P07ECU 1820M27PXXECU 1820M36P06 1820M36P07




ECU 1820M36P06 1820M36P07

7700 ENG OVSPD PROT FAULT Ref to FCOM 3.02.70. Other FCOM_3.02.70TFU 732000004 N


EEC ALL P/N SCN10AEEC ALL P/N SCN12C


N


ECU 1519M83P04 1519M83P06

ECU 1820M27P01 1820M27P03ECU 1519M83P03 1519M83P06ECU 1459M55P16 1459M55P19ECU 1519M83P02 1519M83P06ECU 1459M55P17 1459M55P19ECU 1459M55P15 1459M55P19


TFU 752400002Other FCOM_3.02.18

N


ECU 1459M55P15 1459M55P17ECU 1519M83P02 1519M83P04

Revision 31 PART


7700 ENG i BLEED STATUS FAULT (i=1 or 2) NO MAINTENANCE ACTION if occurs at ECU power up N

Part Affected P/N Corrective P/NECU 1519M83P02 (P03,P04,P05,P06) 1519M83P08ECU 1820M27P01 (P02, P03) 1820M27P05ECU 1459M55P15(P16,P17,P18,P19) 1459M55P21




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

N

Part Affected P/N Corrective P/NEEC SCN 15 N/AEEC SCN 16 N/A

7700 ENGi FUEL FILTER CLOG (i=1 or 2) No Maint. Action if warning triggered at engine start for less than 5 seconds. N


7700 ENG TYPE DISAGREE No Maint. Action if A/C is in ECU intermix configuration. N

Part Affected P/N Corrective P/NECU ECU STD 5 AIECU ECU STD 5 AH+ECU ECUSTD5AIECU ECU STD 5 AI+ECU ECUSTD5AHECU ECU STD 5 AH

Revision 31 PART



TFU 344200005TFU 326100003TFU 344200013TFU 344200003

Y



9599-607-14942 9599-607-12352


9599-607-12333 9599-607-12352

TRANSCEIVER-RADIO 9599-607-14932 9599-607-12352




ALTIMETERTRANSCEIVER-RADIOALTIMETER

9599-607-12552 9599-607-12352


N



TFU 344200005TFU 326100003TFU 344200013TFU 344200003

Y



9599-607-14942 9599-607-12352


9599-607-12333 9599-607-12352


9599-607-14932 9599-607-12352


9599-607-12552 9599-607-12352


N


LGCIU 664700500A4B 664700500A4C

Revision 31 PART



TFU 752400002Other FCOM_3.02.18

N

Part Affected P/N Corrective P/NECU 1459M55P15 1459M55P17ECU 1519M83P02 1519M83P04

7700 ENG DUAL FAILURE NO MAINT. ACTION if occurs on ground during wet / snowy / icy weather, or afterd i i /hi h l i

TFU 344200005TFU 326100003

Y




de-icing/high press. cleaning. TFU 326100003TFU 344200013TFU 344200003


9599-607-14942 9599-607-12352


9599-607-12333 9599-607-12352


9599-607-14932 9599-607-12352


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


N

Part Affected P/N Corrective P/NEEC ALL P/N SCN10AEEC ALL P/N SCN12C

Revision 31 PART



N

Part Affected P/N Corrective P/NECU 1519M83P04 1519M83P06ECU 1820M27P01 1820M27P03ECU 1519M83P03 1519M83P06ECU 1459M55P16 1459M55P19ECU 1519M83P02 1519M83P06ECU 1459M55P17 1459M55P19




ECU 1459M55P17 1459M55P19ECU 1459M55P15 1459M55P19

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.

TFU 783100085 N

Part Affected P/N Corrective P/NECU 1820M36P06ECU 1820M87P07 1820M87P09ECU 1820M89P06ECU 1820M88P07 1820M88P09

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


ECU 1820M89P07 N/AECU 1820M36P07 N/A

Revision 31 PART


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.

TFU 783100078TFU 783100100

N


ECU 1519M83PXX 1820M88P09ECU 1459M55PXX 1820M87P09ECU 1820M89P06 1820M89P07ECU 1820M27PXXECU 1820M36P06 1820M36P07





N


EEC ALL P/N SCN10AEEC ALL P/N SCN12C


N


ECU 1519M83P04 1519M83P06ECU 1820M27P01 1820M27P03ECU 1519M83P03 1519M83P06ECU 1459M55P16 1459M55P19ECU 1519M83P02 1519M83P06ECU 1459M55P17 1459M55P19ECU 1459M55P15 1459M55P19


TFU 752400002Other FCOM_3.02.18

N


ECU 1459M55P15 1459M55P17ECU 1519M83P02 1519M83P04

Revision 31 PART


7700 ENG i BLEED STATUS FAULT (i=1 or 2) NO MAINTENANCE ACTION if occurs at ECU power up N

Part Affected P/N Corrective P/NECU 1519M83P02 (P03,P04,P05,P06) 1519M83P08ECU 1820M27P01 (P02, P03) 1820M27P05ECU 1459M55P15(P16,P17,P18,P19) 1459M55P21

7700 ENG 2 FADEC FAULT No Maint action if no associated EEC fault message recorded in the PFR This is a N





N


7700 ENGi FUEL FILTER CLOG (i=1 or 2) No Maint. Action if warning triggered at engine start for less than 5 seconds. N


7700 ENG TYPE DISAGREE No Maint. Action if A/C is in ECU intermix configuration. N

Part Affected P/N Corrective P/NECU ECU STD 5 AIECU ECU STD 5 AH+ECU ECUSTD5AIECU ECU STD 5 AI+ECU ECUSTD5AHECU ECU STD 5 AH

Revision 31 PART



N





Revision 31 PART

ATA Class 3 message Remark Doc X Ref

212151 RECIRC FAN i OR SPLY (i=1 or 2) NO MAINT. ACTION TFU 216334044


215100 FLOW SEL NO MAINT. ACTION

SIL 00-028 PART C : Class 3 Fault messages




215152 MIXER FLAP DRIVE OR SPLY NO MAINT. ACTION TFU 216000003



216111 Pi COMP TEMP SENSOR (i=1 or 2) NO MAINT. ACTION TFU 216334044


216112 Pi COMP OVHT SENSOR (i=1 or 2) NO MAINT. ACTION TFU 216334044



Revision 31 PART


216115 Pi OUTLET TEMP SENSOR (i=1 or 2) NO MAINT. ACTION TFU 216334044


216117 Pi BLEED TEMP SENSOR (i=1 or 2) NO MAINT. ACTION TFU 216334044





216134 PACKi CONT NO MAINT. ACTION TFU 216134001TFU 216334044



216151 Pi RAM AIR IN ACTUATOR (i=1 or 2) NO MAINT. ACTION TFU 216334044


216152 Pi RAM AIR OUT ACTUATOR (i=1 or 2) NO MAINT. ACTION TFU 216334044


ZONE CONTROLLER 775A0000-07 775A0000-08ZONE CONTROLLER 775A0000-05 775A0000-08ZONE CONTROLLER 775A0000-06 775A0000-08

Revision 31 PART


216153 TURBINE BYPASS VALVE NO MAINT. ACTION TFU 216334044


216315 TEMP SENSOR CKPT DUCT NO MAINT. ACTION TFU 216334044





216315 TEMP SENSOR FWD CAB DUCT NO MAINT. ACTION TFU 216334044



216315 TEMP SENSOR CKPT DUCT NO MAINT. ACTION TFU 216334044


216315 TEMP SENSOR FWD CAB DUCT NO MAINT. ACTION TFU 216334044



Revision 31 PART


216316 TEMP SENSOR L/H AND R/H MIXER NO MAINT. ACTION TFU 216334044


216317 TEMP SENSOR AFT (FWD) CAB NO MAINT. ACTION TFU 216334044






216317 TEMP SENSOR CKPT NO MAINT. ACTION TFU 216334044



216317 TEMP SENSOR AFT (FWD) CAB NO MAINT. ACTION TFU 216334044


216317 TEMP SENSOR CKPT NO MAINT. ACTION TFU 216334044



Revision 31 PART


216318 CKPT DUCT OVHT SENSOR NO MAINT. ACTION TFU 216334044


216318 AFT (FWD) CAB DUCT OVHT SENSOR NO MAINT. ACTION TFU 216334044






216318 CKPT DUCT OVHT SENSOR NO MAINT. ACTION TFU 216334044



216318 AFT (FWD) CAB DUCT OVHT SENSOR NO MAINT. ACTION TFU 216334044


216334 ZONE CONT NO MAINT. ACTION TFU 216334044



Revision 31 PART


216334 NO PACK DATA FROM ECS NO MAINT. ACTION if zone cont. -5 fitted on A/C


216334 ZONE CONT NO MAINT. ACTION TFU 216334044






216334 NO PACK DATA FROM ECS NO MAINT. ACTION if zone cont. -5 fitted on A/C



216351 TRIM AIR VALVE CKPT (11HK) NO MAINT. ACTION TFU 216000004

Part Affected P/N Corrective P/NZONE CONTROLLER 775A0000-07 775A0000-08ZONE CONTROLLER 775A0000-05 775A0000-08ZONE CONTROLLER 775A0000-06 775A0000-08

216351 TRIM VALVE AFT (FWD) CAB NO MAINT. ACTION TFU 216000004


ZONE CONTROLLER 775A0000-07 775A0000-08ZONE CONTROLLER 775A0000-05 775A0000-08ZONE CONTROLLER 775A0000-06 775A0000-08

Revision 31 PART


216351 TRIM AIR VALVE CKPT (11HK) NO MAINT. ACTION TFU 216000004


216351 TRIM VALVE AFT (FWD) CAB NO MAINT. ACTION TFU 216000004





216352 TRIM AIR PRESS VALVE NO MAINT. ACTION TFU 216000003



2 283 34 FMG Ci (1 CA i) B US FM AC AR S /A TS U1 (1 TX 1)(i=1 or 2)

ATSU/ FMGCx protocol deviation when ATSU does receive answer from FMGCx (when in slavecondition). No maintenance action required.

TFU 460000002

Part Affected P/N Corrective P/NATSU PLAT SW LA2T0S111C1B0F1 LA2T0J13000C0F1ATSU PLAT SW LA2T0S162C0C0F1 LA2T0J13000C0F1

Revision 31 PART


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.

TFU 460000002

Part Affected P/N Corrective P/NTRANSCEIVER-VHF 822-1250-020 N/AATSU PLAT SW LA2T0J13002C0F1 LA2T0J1303A00F1ATSU PLAT SW LA2T0J13000C0F1 LA2T0J1303A00F1TRANSCEIVER-VHF 064-50000-2051 N/ATRANSCEIVER-VHF EVR750-04-0100A N/A




2 333 34 NO P ESM UX DA TA N o MA INT . A CT IO N i f n o ca bi n cr ew co mp la in t. Th is sp ur io us P ES B it e me ssa ge i s r ec or de d

when PES Bite is disabled in the CAM


DIRECTOR-CIDS Z010H000520A Z010H000521ADIRECTOR-CIDS Z010H0005119 Z010H000521A

233346 SEB 41LFT, 41RGT REF SIL HUGHES 1142000-130-03 NO MAINT. ACTION TFU 233300009


PES-MULTIPLEXER 1142300-131-XX VSB AVI-9332







Revision 31 PART



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.

TFU 233300009





DIRECTOR-CIDS Z010H0005119 Z010H000520A

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


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


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


GPCU 740121B VENDOR SIL 229GPCU 740121A VENDOR SIL 229

Revision 31 PART


244134 GPCU NO MAINT. ACTION


284216 L(R) CADENSICON 19QTi NO MAINT. ACTION TFU 284234029TFU 284234016

P t Aff t d P/N C ti P/N





CADENSICON 796-809-5 796-809-6

284216 C CADENSICON 20QT NO MAINT. ACTION TFU 284234029


CADENSICON 796-809-5 796-809-6


Part Affected P/N Corrective P/NCADENSICON 796-809-5 796-809-6

284216 C CADENSICON 20QT NO MAINT. ACTION TFU 284234029


CADENSICON 796-809-5 796-809-6

Revision 31 PART C



Part Affected P/N Corrective P/NCADENSICON 796-809-5 796-809-6

301151 WAI FILTER OR VALVE 9DL (10DL) NO MAINT. ACTION TFU 216000003







303134 PHC 6 DA 1(2,3) NO MAINT. ACTION. Other TSM-ATA30TFU 303134006


PHC 1663214200 1663214301

313234 CFDIU(1TW)/ATSU1(1TX1) Protocol problem between ATSU and CFDIUNo maintenace action required

TFU 460000002


313234 CFDIU (1TW)/WXRi (1SQi) ( i=1 or 2) No maintenance act ion required i f no logbook complaint.


RADAR 822-1710-201 822-1710-202

Revision 31 PART C


313234 CFDIU(1TW)/ATSU1(1TX1) Protocol problem between ATSU and CFDIUNo maintenace action required

TFU 460000002


313234 CFDIU (1TW)/WXRi (1SQi) ( i=1 or 2) No maintenance act ion required i f no logbook complaint.





315534 SDACi (i=1 or 2) NO MAINT. ACTION if associated with codes 2000 to 2005 TFU 315500002


315534 SDACi(1WVi)/ATSU1(1TX1) (i=1 or 2) nullNo maintenance action required

TFU 460000002


315534 SDACi (i=1 or 2) NO MAINT. ACTION if associated with codes 2000 to 2005 TFU 315500002


SDAC 350E5151022 350E5151331SDAC 350E5161122 350E5151331

Revision 31 PART C


315534 SDACi(1WVi)/ATSU1(1TX1) (i=1 or 2) nullNo maintenance action required

TFU 460000002


316334 DMC(1WTi/3)/ATSU(1TX1) ( i=1 or 2) Label 316 (wind direction) not properly received by the ATSUNo maintenance action required

TFU 460000002






ATSU PLAT SW LA2T0S111C1B0F1 LA2T0J13000C0F1ATSU PLAT SW LA2T0S162C0C0F1 LA2T0J13000C0F1

323171 LGCIUi(5GAi)/RMPj(1RGj) ( i=1 or 2)(j=1, 2 or 3) NO MAINTENANCE ACTION if t riggered during take-off and landing phases TFU 231300023

Part Affected P/N Corrective P/NRMP C12848AA01 C12848CA01

3 412 00 CHE CK A DI RUi R S TA TIC P HCj I NTE RF AC E(i=1, 2 or 3) (j=1, 2 or 3)

NO MAINT. ACTION TFU 303100013


PHC 1663214200 1663214301

3 412 00 CHE CK A DI RUi L ST AT IC PH Cj IN TE RFA CE(i=1, 2 or 3) (j=1, 2 or 3)



PHC 1663214200 1663214301

Revision 31 PART C


341200 No access to ZONT PHC1(2,3) INTERFACE NO MAINT. ACTION TFU 303100013


3 412 00 CHE CK A DI RUi A OA P HCj I NTE RF ACE (i =1 , 2or 3) (j=1, 2 or 3)







PHC 1663214200 1663214301

3 412 00 CHE CK A DI RUi P ITO T P HCj INTE RF AC E ( i=1, 2or 3) (j=1, 2 or 3)



PHC 1663214200 1663214301

3 412 00 CHE CK A DI RUi R S TA TIC P HCj I NTE RF AC E(i=1, 2 or 3) (j=1, 2 or 3)



3 412 00 CHE CK A DI RUi L ST AT IC PH Cj IN TE RFA CE(i=1, 2 or 3) (j=1, 2 or 3)



PHC 1663214200 1663214301

Revision 31 PART C


341200 No access to ZONT PHC1(2,3) INTERFACE NO MAINT. ACTION TFU 303100013


3 412 00 CHE CK A DI RUi A OA P HCj I NTE RF ACE (i =1 , 2or 3) (j=1, 2 or 3)






PHC 1663214200 1663214301

3 412 00 CHE CK A DI RUi P ITO T P HCj INTE RF AC E ( i=1, 2or 3) (j=1, 2 or 3)



PHC 1663214200 1663214301

341234 NO DATA FROM ADIRS NO MAINT. ACTION if appears in Phase 1,2 or 10 . Other TSM-ATA21


3 412 34 A DIRU 3( 1FP 3) A DR BU S/ WX Ri (1 SQi ) ( i = 1 o r2)

No maintenance action required if no logbook complaint.


RADAR 822-1710-201 822-1710-203RADAR 822-1710-202 822-1710-203

Revision 31 PART C




Part Affected P/N Corrective P/NRADAR 622-5132-623 TBD

3 412 34 A DIRU i( 1FP i) I R B US / WX Rj (1S Qj ) ( i = 1, 2 o r 3and j = 1 or 2)






RADAR 822-1710-202 822-1710-203RADAR 822-1710-201 822-1710-203

341234 NO DATA FROM ADIRS NO MAINT. ACTION if appears in Phase 1,2 or 10 . Other TSM-ATA21





RADAR 822-1710-201 822-1710-203RADAR 822-1710-202 822-1710-203




RADAR 622-5132-623 TBD

Revision 31 PART C


3 412 34 A DIRU i( 1FP i) I R B US / WX Rj (1S Qj ) ( i = 1, 2 o r 3and j = 1 or 2)



344233 RAi (2SAi)/WXRj (1SQj) (i=1 or 2) (j=1 or 2) No maintenance action required if no logbook complaint.





345233 ATCi (1SHi)/TCAS (1SG) (i = 1 or 2) No maintenance action required. CLASS 3 fault message is triggered if ATC transponder instandby.

Part Affected P/N Corrective P/NTCAS 7517900-10003 AS PER DESIGNTCAS 7517900-10002 AS PER DESIGN

462134 ATSU1(1TX1) nullNo maintenance action required.

TFU 460000002

Part Affected P/N Corrective P/NATSU PLAT SW LA2T0S162C0C0F1 LA2T0J13000C0F1ATSU PLAT SW LA2T0S111C1B0F1 LA2T0J13000C0F1

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

Revision 31 PART C


462134 ATSU1(1TX1) nullNo maintenance action required.

TFU 460000002

Part Affected P/N Corrective P/NATSU PLAT SW LA2T0S162C0C0F1 LA2T0J13000C0F1ATSU PLAT SW LA2T0S111C1B0F1 LA2T0J13000C0F1

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

710000 BALANCE ENGi (N1 NB VIB) (i=1 or 2) NO MAINT. ACTION if no log book entry concerning Engin vibrations. TFU 773234005

Part Affected P/N Corrective P/NEVMU 241-211-000-021 241-211-000-031

710000 CHECK ENGi (N2 NB VIB) (i=1 or 2) NO MAINT. ACTION if no log book entry concerning Engin vibrations. TFU 773234005


710000 BALANCE ENGi (N1 NB VIB) (i=1 or 2) NO MAINT. ACTION if no log book entry concerning Engin vibrations. TFU 773234005


EVMU 241-211-000-021 241-211-000-031

Revision 31 PART C


710000 CHECK ENGi (N2 NB VIB) (i=1 or 2) NO MAINT. ACTION if no log book entry concerning Engin vibrations. TFU 773234005


715100 J4, ADC2 (*) ENG1A (1B(2A)(2B) NO MAINT. ACTION TFU 732900012





ECU 1519M83P02 1519M83P04ECU 1459M55P16 1459M55P17ECU 1459M55P15 1459M55P17ECU 1519M83P03 1820M27P01

715100 J3, ADC1 (*) ENG1A (1B)(2A)(2B) NO MAINT. ACTION TFU 732900012

Part Affected P/N Corrective P/NECU 1459M55P15 1459M55P17ECU 1519M83P03 1820M27P01ECU 1519M83P02 1519M83P04ECU 1459M55P16 1459M55P17

715100 J4, ADC2 (*) ENG1A (1B(2A)(2B) NO MAINT. ACTION TFU 732900012


ECU 1519M83P02 1519M83P04ECU 1459M55P16 1459M55P17ECU 1459M55P15 1459M55P17ECU 1519M83P03 1820M27P01

Revision 31 PART C


715100 J3, ADC1 (*) ENG1A (1B)(2A)(2B) NO MAINT. ACTION TFU 732900012

Part Affected P/N Corrective P/NECU 1459M55P15 1459M55P17ECU 1519M83P03 1820M27P01ECU 1519M83P02 1519M83P04ECU 1459M55P16 1459M55P17

732500 CHECK EIU-WHCi INTERFACE (i=1 or 2) Check/Confirm that EIU/WHC interface is defective TFU 304034002





WHC 6664202-3 6664287-0

753180 BLD SNSR, J15, ECU (*) ENG1A (1B)(2A)(2B) NO MAINT.ACTION IF SB 72-1005 NOT EMBODIED ON THE A/C TFU 732900025

Part Affected P/N Corrective P/NECU 1820M27P01 SB_72-1005ECU 1459M55P17 SB_72-1005ECU 1519M83P04 SB_72-1005

753180 CWB3, WB3 SENS, J15 ENG1A (1B)(2A)(2B) NO MAINT. ACTION if SB 72-1005 not embodied on the A/C TFU 732900025


ECU 1519M83P03 SB_72-1005ECU 1519M83P02 SB_72-1005ECU 1459M55P15 SB_72-1005ECU 1459M55P16 SB_72-1005

Revision 31 PART C


753180 VTURI, BLD SNSR, ECU* ENG1A (1B)(2A)(2B) NO MAINT. ACTION IF SB 72-1005 NOT EMBODIED ON THE A/C. TFU 722900025


753180 BLD SNSR, J15, ECU (*) ENG1A (1B)(2A)(2B) NO MAINT.ACTION IF SB 72-1005 NOT EMBODIED ON THE A/C TFU 732900025





753180 CWB3, WB3 SENS, J15 ENG1A (1B)(2A)(2B) NO MAINT. ACTION if SB 72-1005 not embodied on the A/C TFU 732900025


ECU 1519M83P03 SB_72-1005ECU 1519M83P02 SB_72-1005ECU 1459M55P15 SB_72-1005ECU 1459M55P16 SB_72-1005

753180 VTURI, BLD SNSR, ECU* ENG1A (1B)(2A)(2B) NO MAINT. ACTION IF SB 72-1005 NOT EMBODIED ON THE A/C. TFU 722900025


Revision 31 PART C

ATA CFDS anomalies Remark Doc X Ref

2126 VENT AVNCS SYS FAULT during Ditching testprocedure.

VENT AVNCS SYS FAULT during Ditching test procedure.Reset AEVC C/B at the end of the Ditching test procedure.

TFU 212600010

Part Affected P/N Corrective P/NAEVC ALL P/N NONE

2131 Spurious message OUTFLOW VALVE ELEK i(04) may be triggered during system calibrationtest in MAN MODE.

Spurious message OUTFLOW VALVE ELEK i (04) may be triggered during system calibration testin MAN MODE.Repeat test in AUTO MODE.

TFU 213134006Other TSM-ATA21


SIL 00-028 PART D : CFDS anomalies



CPC 902215702-7 902215702-8

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


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






ZONE CONTROLLER 775A0000-06 775A0000-07ZONE CONTROLLER 775A0000-05 775A0000-07

Revision 31 PART


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.

Part Affected P/N Corrective P/NZONE CONTROLLER 775A0000-05 775A0000-07ZONE CONTROLLER 775A0000-06 775A0000-07

2 163 No s of twa re n umb er i n P /N of Z on e C on t. N o so ft wa re n umb er i n P /N o f Zo ne Co nt.






2163 No access to ZONE CONT menu when PACKC/B is pulled.

No access to ZONE CONT menu when PACK C/B is pulled.


2 163 No A /C i den t i n t he pr evi ou s le g r ep or t N o A /C id en t i n th e p re vi ous l eg r epo rtNO MAINT. ACTION



2163 Leg counting deviation at leg 99 Leg counting deviation at leg 99



Revision 31 PART





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

P t Aff t d P/N C ti P/N








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 No s of twa re n umb er i n P /N of Z on e C on t. N o so ft wa re n umb er i n P /N o f Zo ne Co nt.


Revision 31 PART


2163 No access to ZONE CONT menu when PACKC/B is pulled.

No access to ZONE CONT menu when PACK C/B is pulled.


2 163 No A /C i den t i n t he pr evi ou s le g r ep or t N o A /C id en t i n th e p re vi ous l eg r epo rtNO MAINT. ACTION


ZONE CONTROLLER 775A0000 05 775A0000 07





2163 Leg counting deviation at leg 99 Leg counting deviation at leg 99



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.

TFU 227000014


FMGC B398AAM0408 B398AAM0409FMGC B398BCM0104 B398BCM0106FMGC B398BAM0205 B398BAM0206

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


FAC ALL P/N B397AAM0509FAC ALL P/N B397AAM0508DMC - EIS 1 ALL P/N

Revision 31 PART


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.

TFU 227000014


FMGC B398AAM0408 B398AAM0409FMGC B398BCM0104 B398BCM0106FMGC B398BAM0205 B398BAM0206

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


Revision 31 PART


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


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




FCDC 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.

Part Affected P/N Corrective P/NRMP 899-0850-003 TBDRMP 899-0850-002 TBDRMP 899-0850-004 TBD

228334 FMGCi FMGCi Class 2 Fault message without associated Maintenance status.Apply TSM procedure

MPD_Task 279000-07


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.

Part Affected P/N Corrective P/NRMP 899-0850-003 TBDRMP 899-0850-002 TBDRMP 899-0850-004 TBD

Revision 31 PART


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


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


OBRM CIDS DIR Z064H000031B Z064H000031DOBRM CIDS DIR Z064H000031A Z064H000031C

Revision 31 PART


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).


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

Airbus_SB 23-1278





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.


OBRM CIDS DIR Z064H000030F Z064H000031COBRM CIDS DIR Z064H000031A Z064H000031DOBRM CIDS DIR Z064H000031B

Revision 31 PART


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).





OBRM CIDS DIR Z064H000030F Z064H000031ADIRECTOR-CIDS Z014H000030C Z014H000131AOBRM CIDS DIR Z064H000030F Z064H000031BDIRECTOR-CIDS Z014H000030C Z014H000031A

2 351 Fa ul ts mi ssi ng i n A ud io P re vio us a nd la st l egreports

Faults missing in Audio Previous and last leg reportsRefer to messages in the PFR.

TFU 235100013TFU 235100009

Part Affected P/N Corrective P/NAMU AMU2790DA03 AMU2790DB06AMU AMU2790CA03 AMU2790CB06AMU PRE VSB 2790-23-007 VSB 2790-23-007

AMU 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/NAMU 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




TFU 235100013TFU 235100009

Part Affected P/N Corrective P/NAMU AMU2790DA03 AMU2790DB06AMU AMU2790CA03 AMU2790CB06AMU PRE VSB 2790-23-007 VSB 2790-23-007AMU AMU2790EA03 AMU2790EB06AMU PRE VSB 2790-23-006 VSB 2790-23-006



TFU 235100013TFU 235100009





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



TFU 235100013TFU 235100009


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

Revision 31 PART D




TFU 235100013TFU 235100009

Part Affected P/N Corrective P/NAMU PRE VSB 2790-23-007 VSB 2790-23-007AMU PRE VSB 2790-23-006 VSB 2790-23-006AMU AMU2790EA03 AMU2790EB06AMU AMU2790DA03 AMU2790DB06AMU AMU2790CA03 AMU2790CB06



TFU 235100013TFU 235100009





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



TFU 235100013TFU 235100009


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


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

CFDS1(1TM)/CIDS(10yRH)-SDFy.Part Affected P/N Corrective P/N





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.


Revision 31 PART D


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

TFU 243800009TFU 243800007





BCL 35-0L5-1005-08

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


BCL 35-0L5-1005-08

Revision 31 PART D


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


GPCU 740121B VENDOR SIL 229GPCU 740121A




GPCU 740121A

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


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.

TFU 279500033


FCDC 115370-0105 115370-1118FCDC 115370-0106 115370-1118FCDC 115370-1016 115370-1118

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




FCDC 115370 0105 115370 1118FCDC 115370-0106 115370-1118FCDC 115370-1016 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.

TFU 279500033

Part Affected P/N Corrective P/NFCDC 115370-0105 115370-1118FCDC 115370-0106 115370-1118FCDC 115370-1016 115370-1118

Revision 31 PART D


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


FCDC 115370-0105 115370-1118FCDC 115370-0106 115370-1118FCDC 115370-1016 115370-1118

279300 Ultimely flash of AIL SERVO FAULT in case of ELAC 1 (or 2) fault during GROUND SCANNING





FCDC 115370-0105 115370-0106

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


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


279334 AFS:ELACi AFS:ELACiNO MAINT. ACTION if associated to B SYS LO PRESS (respectively Y SYS LO PRESS).


Revision 31 PART D


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


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


FCDC 115370-0105 115370-0106




279334 AFS:ELACi AFS:ELACiNO MAINT. ACTION if associated to B SYS LO PRESS (respectively Y SYS LO PRESS).


2 794 34 S EC 2 OR IN PU T O F L( R) THRO TT LE CTL UN IT8KSi

Class 2 Fault message SEC2 OR INPUT OF L(R) THROTTLE CTL UNIT 8KSi without associatedMaintenance status. Apply TSM procedure

MPD_Task 279000-07


279434 SEC3 OR WIRING FROM SFCC i Class 2 Fault message SEC3 OR WIRING FROM SFCC i without associated Maintenance status.Apply TSM procedure

MPD_Task 279000-07


FCDC 115370-0105 115370-0106FCDC 115370-0105 115370-1016

Revision 31 PART D


2 794 34 S EC 2 OR IN PU T O F L( R) THRO TT LE CTL UN IT8KSi

Class 2 Fault message SEC2 OR INPUT OF L(R) THROTTLE CTL UNIT 8KSi without associatedMaintenance status. Apply TSM procedure

MPD_Task 279000-07


279434 SEC3 OR WIRING FROM SFCC i Class 2 Fault message SEC3 OR WIRING FROM SFCC i without associated Maintenance status.Apply TSM procedure

MPD_Task 279000-07


FCDC 115370-0105 115370-0106FCDC 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


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


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


Revision 31 PART D


3132 NO DMC1 DATA recorded in CFDIU groundscanning

NO DMC1 DATA recorded in CFDIU ground scanningNO MAINT. ACTION.

TFU 313234030


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


3132 D li ti f F lt i PFR D li ti f F lt i PFR TFU 313234029




3132 Duplication of Fault message in PFR. Duplication of Fault message in PFR. TFU 313234029


CFDIU B401ACM0404 B401ACM0606

3132 Incoherent PFR Fault messages sent by the EIU. Incoherent PFR Fault messages sent by the EIU. TFU 313234029


EIU 3957900611 3957900612

3132 Incoherent PFR recording time in the PFRheader.

Incoherent PFR recording time in the PFR header due to Flight phases transitions anomalies. TFU 313234029



Revision 31 PART D


3132 Incomplete PFR Fault messages. Incomplete PFR Fault messages due to power supply transients. TFU 313234029


3132 Mixed GMT in PFR Mixed GMT in PFR due to power transients. 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 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



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



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


CFDIU B401ACM0506 TBD

Revision 31 PART D


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


3132 NO DMC1 DATA recorded in CFDIU groundscanning

NO DMC1 DATA recorded in CFDIU ground scanningNO MAINT. ACTION.

TFU 313234030



Revision 31 PART D


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


3132 Duplication of Fault message in PFR. Duplication of Fault message in PFR. TFU 313234029








EIU 3957900611 3957900612

3132 Incoherent PFR recording time in the PFRheader.

Incoherent PFR recording time in the PFR header due to Flight phases transitions anomalies. TFU 313234029



3132 Incomplete PFR Fault messages. Incomplete PFR Fault messages due to power supply transients. TFU 313234029



Revision 31 PART D


3132 Mixed GMT in PFR Mixed GMT in PFR due to power transients. 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


3132 PFR with NO FAULT / NO WARNING. PFR with NO FAULT / NO WARNING due to Flight phases transit ions anomalies. TFU 313234029




g pNO MAINT. ACTION.



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



3132 DIFFICULTIES FOR FILTER LOADING SOME DIFFICULTIES MAY BE ENCOUNTERED WHEN USING ANY OF THE PDL IN SERVICEBUT THE SFIM.

TFU 313234038


CFDIU B401ACM0505 N/ACFDIU B401ACM0506 N/A

Revision 31 PART D


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.


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.


AMU AMU2790CA03

Revision 31 PART D


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.


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.


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


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.


RADAR 204 1217 0418 VSB RTA 4A 34 173





3 132 34 CFDS pr omp t n ot a va il ab le on MCDU a t C FDIUpower up.

CFDS prompt not available on MCDU at CFDIU power up.Wait 1 minute after CFDIU power up to get the CFDS prompt on the MCDU.


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.


RECEIVER ADF 204-1168-7513RECEIVER ADF 622-5222-020

Revision 31 PART D


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.


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.


RMP 899-0850-003RMP 899-0850-004RMP 899-0850-002

Revision 31 PART D


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

RECEIVER-VOR 2041231-3610RECEIVER-VOR 2041231-3622RECEIVER-VOR 2041231-3613RECEIVER-VOR 2041231-3623




RECEIVER 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.



3 133 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.


SOFTWARE-FDIMU F320-001-8802

3135 Bad PRINT OUT FORMAT. Bad PRINT OUT FORMAT.NO MAINT ACTION

TFU 313522001


PRINTER 8055154501 POST VSB M3367

Revision 31 PART D


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.

Vendor_SB C19298A3MPD_Task 315000-03AMM_Task 316000740Vendor_SB C19366A3

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

TFU 324234049Airbus_SB 32-1318


Revision 31 PART D


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

TFU 324234049Airbus_SB 32-1318





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


Revision 31 PART D


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


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


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.





LGCIU 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".


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.



Revision 31 PART D


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


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


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


LGCIU 664700500A4A 664700500A4B

Revision 31 PART D


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".



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.



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.


LGCIU 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.


LGCIU 664700500A4C 664700500A4DLGCIU 664700500A4B 664700500A4D

Revision 31 PART D


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.


HUDC 9615433401 9615433402

3441 Bad LRU identification Bad LRU identification TFU 344100007




3441 Bad LRU identification. Bad LRU identification.NO MAINT. ACTION

TFU 344100007


3 441 B la nk p ag es or e rr ati c Da ta i n P re vi ou s Le gReport.

Blank pages or erratic Data in Previous Leg Report.NO MAINT. ACTION

TFU 344100007


3441 Spurious fault messageFMGC(1CA1)/GPWC(1WZ) and FMGC1 MAGTRK following a Ground Scanning or BITE testofthe GPWC.

Spurious fault message FMGC(1CA1)/GPWC(1WZ) and FMGC1 MAG TRK following a GroundScanning or BITE test of the GPWC.NO MAINT. ACTION.

TFU 344800003

Part Affected P/N Corrective P/NGPWC 9650676020 SOFTWARE MOD 1

Revision 31 PART D


3441 Bad LRU identification. Bad LRU identification.NO MAINT. ACTION

TFU 344100007


3 441 B la nk p ag es or e rr ati c Da ta i n P re vi ou s Le gReport.

Blank pages or erratic Data in Previous Leg Report.NO MAINT. ACTION

TFU 344100007


3441 Spurious fault message Spurious fault message FMGC(1CA1)/GPWC(1WZ) and FMGC1 MAG TRK following a Ground TFU 344800003




3441 Spurious fault messageFMGC(1CA1)/GPWC(1WZ) and FMGC1 MAGTRK following a Ground Scanning or BITE testofthe GPWC.

Spurious fault message FMGC(1CA1)/GPWC(1WZ) and FMGC1 MAG TRK following a GroundScanning or BITE test of the GPWC.NO MAINT. ACTION.

TFU 344800003


3443 Wrong ATA for fault message CFDIU BUS CFDIU BUS message with ATA 45 instead of 313234

Part Affected P/N Corrective P/NTCAS 4066010-904 TBD

3 448 S pu ri ou s me ss age 22 83 34 FMG C( 1CA 1)/ GP WC(1WZ) may be triggered

Spurious message 228334 FMGC(1CA1)/GPWC (1WZ) may be triggeredNO MAINT. ACTION if appears after a GPWC test via the CFDS

TFU 344800003


GPWC 9650676020 SWMOD1GPWC 9650676020 SOFTWARE MOD 1

Revision 31 PART D


3448 FMGC MAG TRK on MCDU may be displayedafter a GPWC ground scan. via the CFDS

FMGC MAG TRK on MCDU may be displayed after a GPWC ground scan. via the CFDSNO MAINT. ACTION.

TFU 344800003


3 448 B ad le g i ncr eme nta ti on o f G PW S Pr evi ou s Le gReports.

Bad leg incrementation of GPWS Previous Leg Reports.NO MAINT. ACTION.

TFU 344800004


3 448 L os s o f fa ul t me ssa ge s i n t he G PWC P rev iou sLeg Reports.

Loss of fault messages in the GPWC Previous Leg Reports.NO MAINT. ACTION

TFU 344800004





GPWC 9650676020 SOFTWARE MOD 1

3448 Same message with same date and GMT but different leg numbers in the Previous Leg Reports.NO MAINT. ACTION

TFU 344800004



3 448 S pu ri ou s me ss age 22 83 34 FMG C( 1CA 1)/ GP WC(1WZ) may be triggered

Spurious message 228334 FMGC(1CA1)/GPWC (1WZ) may be triggeredNO MAINT. ACTION if appears after a GPWC test via the CFDS

TFU 344800003


GPWC 9650676020 SWMOD1GPWC 9650676020 SOFTWARE MOD 1

Revision 31 PART D


3448 FMGC MAG TRK on MCDU may be displayedafter a GPWC ground scan. via the CFDS

FMGC MAG TRK on MCDU may be displayed after a GPWC ground scan. via the CFDSNO MAINT. ACTION.

TFU 344800003


3 448 B ad le g i ncr eme nta ti on o f G PW S Pr evi ou s Le gReports.

Bad leg incrementation of GPWS Previous Leg Reports.NO MAINT. ACTION.

TFU 344800004


3 448 L os s o f fa ul t me ssa ge s i n t he G PWC P rev iou sLeg Reports.

Loss of fault messages in the GPWC Previous Leg Reports.NO MAINT. ACTION

TFU 344800004






3448 Same message with same date and GMT but different leg numbers in the Previous Leg Reports.NO MAINT. ACTION

TFU 344800004



3 451 Wr ong id en ti fic ati on o f D ME : Me ssa ge : DME -0TRANSCEIVER

Wrong identification of DME : Message : DME-0 TRANSCEIVER TFU 345100009


DME 622-4540-022 622-4540-023

Revision 31 PART D


3453 NO access to the ADF Last Leg Report after 64 legs flown without fault recorded in BITENO MAINT. ACTION

Part Affected P/N Corrective P/NRECEIVER ADF 622-5222-020 VSB ADF-700-34-27

3455 No access to the VOR Last Leg Report after 64legs flown without fault recorded in BITE.

No access to the VOR Last Leg Report after 64 legs flown without fault recorded in BITE.NO MAINT. ACTION.

Part Affected P/N Corrective P/NRECEIVER-VOR 622-5220-020 VSB_700-34-21

3458 "GPSSU(1SNi) When MMR installed on the A/C, GPSSU messages (ex: 345831 "GPSSU(1SNi)) mean GPS partof the MMR.

TSM_Task 345800810





ADIRU ALL P/N

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


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

TFU 460000002AMM_Task 462100610AMM_Task 462100610


Revision 31 PART D


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


ATSU PLAT SW LA2T0S162C0C0F1 LA2T0S111C1B0F1







LRU identification AOC database not displayed on LRU ident MCDU page.For Honeywell AOC, all P/N are displayed on AOC CONFIGURATION page

AMM_Task 462100610TFU 460000002




(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



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


Revision 31 PART D


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


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.



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

TFU 460000002AMM_Task 462100610AMM T k 462100610




LA2T0S111C1B0000) and not disk P/N(LA2T0S162C0C0F1 or LA2T0S111C1B0F1)

The correct P/N for A/C interface S/W ends with F1 AMM_Task 462100610











Revision 31 PART D







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


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


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.


Revision 31 PART D


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





ECB 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.


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."


EEC 808050-4-056 SCN18EEC 824972-2-010 SCN18

Revision 31 PART D


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.

TFU 732534005

Part Affected P/N Corrective P/NEIU 3957900609 3957900613EIU 3957900612 3957900613EIU 3957900611 3957900612EIU 3957900610 3957900613

7325 Fault message CHECK 16(17) HB RELAYCIRCUIT OR EIUi RT OK in EIU groundscanning.

Fault message CHECK 16(17) HB RELAY CIRCUIT OR EIUi RT OK in EIU ground scanning.NO MAINT. ACTION when RT OK (Result Test OK) is mentioned.

TFU 732534005





7325 GARBLED FADEC fault messages in the PFR. GARBLED FADEC fault messages in the PFR.For maint. action ref. to the FADEC LAST LEG REPORT.

TFU 732500008TFU 732500007


EIU 3957900612 3957905014EIU 3957905004 3957905005EIU 3957900613

7325 When RTOK recorded in the GND SCAN results. When RTOK recorded in the GND SCAN results.Disregard, ref AMM EIU GND SCAN procedure.

Part Affected P/N Corrective P/NEIU ALL_P/N 3957900613EIU ALL_P/N 3957905004

Revision 31 PART D


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.

TFU 732534005


7325 Fault message CHECK 16(17) HB RELAYCIRCUIT OR EIUi RT OK in EIU groundscanning.

Fault message CHECK 16(17) HB RELAY CIRCUIT OR EIUi RT OK in EIU ground scanning.NO MAINT. ACTION when RT OK (Result Test OK) is mentioned.

TFU 732534005





7325 GARBLED FADEC fault messages in the PFR. GARBLED FADEC fault messages in the PFR.For maint. action ref. to the FADEC LAST LEG REPORT.

TFU 732500008TFU 732500007


EIU 3957900612 3957905014EIU 3957905004 3957905005EIU 3957900613

7325 When RTOK recorded in the GND SCAN results. When RTOK recorded in the GND SCAN results.Disregard, ref AMM EIU GND SCAN procedure.

Part Affected P/N Corrective P/NEIU ALL_P/N 3957900613EIU ALL_P/N 3957905004

Revision 31 PART D


7329 NVM FAULT DATA NOT RETRIEVABLE NVM FAULT DATA NOT RETRIEVABLE TFU 732900031

Part Affected P/N Corrective P/NECU 1519M83P02 1519M83P04ECU 1519M83P03ECU 1459M55P16 1820M27P01

7329 ENG OVSPD PROT FAULT associated withHMU, J7 during FADEC ground test

ENG OVSPD PROT FAULT associated with HMU, J7 during FADEC ground testTo be confirmed by a new test. If not confirmed, NO MAINT. ACTION.

TFU 732900025


ECU 1519M83P03ECU 1459M55P16 1820M27P01ECU 1519M83P02 1519M83P04

7329 ENG i FADEC A(B) FAULT d i FADEC GND ECAM i ENG i FADEC A(B) FAULT TFU 732900025




7329 ENG i FADEC A(B) FAULT during FADEC GNDTEST

ECAM warning ENG i FADEC A(B) FAULTNO MAINT. ACTION if associated with WB3 SENS,J15,ECU during FADEC ground test.

TFU 732900025


ECU 1519M83P02 1519M83P04ECU 1459M55P16 1820M27P01ECU 1459M55P15 1459M55P17ECU 1519M83P03

7329 NVM FAULT DATA NOT RETRIEVABLE NVM FAULT DATA NOT RETRIEVABLE TFU 732900031

Part Affected P/N Corrective P/NECU 1519M83P02 1519M83P04ECU 1519M83P03ECU 1459M55P16 1820M27P01

Revision 31 PART D


7329 ENG OVSPD PROT FAULT associated withHMU, J7 during FADEC ground test

ENG OVSPD PROT FAULT associated with HMU, J7 during FADEC ground testTo be confirmed by a new test. If not confirmed, NO MAINT. ACTION.

TFU 732900025

Part Affected P/N Corrective P/NECU 1519M83P03ECU 1459M55P16 1820M27P01ECU 1519M83P02 1519M83P04

7329 ENG i FADEC A(B) FAULT during FADEC GNDTEST

ECAM warning ENG i FADEC A(B) FAULTNO MAINT. ACTION if associated with WB3 SENS,J15,ECU during FADEC ground test.

TFU 732900025


ECU 1519M83P02 1519M83P04ECU 1459M55P16 1820M27P01ECU 1459M55P15 1459M55P17ECU 1519M83P03




7732 Wrong date in the EVMU Last Leg Report Wrong date in the EVMU Last Leg Report TFU 773234020


EVMU 241-211-000-021 241-211-000-031

7 831 Th ro ttl e l eve r s ti ll a ct ive d ur ing 60 se co nds i f

thrust reverser test interrupted with MCDU Menukey.

Throttle lever still active during 60 seconds if thrust reverser test interrupted with MCDU Menu key.

The operator must leave the Test function with the RETURN key instead of the MCDU Menu key.

TFU 783100014


ECU ALL P/N 1459M55P17ECU ALL P/N 1519M83P04

Revision 31 PART D

ATA Failure Messages Phases Source Part Affected PN

XXXXXX GR-OU-ND 08 09 CFDIU B401ACM0506CFDIU B401ACM0507

XXXXXX GN-D 08 09 CFDIU B401ACM0506CFDIU B401ACM0507

2131 CAB_PR_LO_DIFF_PR 06 07 CPC 902215702-8CPC 902215702-7

2161 AIR_PACK_1$2_FAULT 03 04 ACSC ALL P/NPACK TEMP CTLR ALL P/N

SIL 00-028 PART E : Filter Content (faults)



PACK TEMP CTLR ALL P/N

2200 AUTO_FLT_AP_OFF 02 03 04 08 09 FMGC ALL P/N

2200 AUTO_FLT_A/THR_OFF 08 09 FMGC ALL P/N

226634 DMC$:_NO__FAC$__DATA DMC - EIS 1 ALL P/N

Revision 31 PART


228212 AFS:_MCDU AFS FMGC ALL P/N

228212 MCDU3(3CA3)/ATSU1(1TX1) ATSU ATSU PLAT SW LA2T0S111C1B0F1

228334 AFS:FMGC$_(FM$) AFS FMGC B398BAM0205FMGC B398BCM0104FMGC B398AAM0408

228334 AFS:FMGC$/ATHR_ENGD_FDBK 08 09 AFS FMGC B398AAM0XXXFMGC B398BAM0XXX




FMGC B398BAM0XXXFMGC B398BCM0XXX

228334 AFS:FMGC$(DO_NOT_REMOVE) AFS FMGC C13042AA01FMGC C13043AA01FAC PRE_STD_B397BAM06

228334 AFS:FMGC AFS FMGC B398AAM0410FMGC B546CCM0101FMGC B398BAM0207FMGC B546CAM0101FMGC B546BAM0203

231100 ICAO_ADDRESS/HF$(3RE$) HFDR 822-0990-003

Revision 31 PART


231133 HFDR$(3RE$)/ATSU1(1TX1) CFDIU B401ACM0505CFDIU B401ACM0506CFDIU B401ACM0507CFDIU B401ACM0404

231133 NO_HF1_DATA 02 CFDS TRANSCEIVER-HF 964-0452-012TRANSCEIVER-HF 964-0452-001

231233 NO_ VHF3_ DATA CFDS CFDIU C12860AA02

231233 VHF0(1RC0) 02 TRANSCEIVER-VHF 822-1047-030TRA NS CE IV ER- VHF 8 22 -10 47 -02 0




TRA NS CE IV ER VHF 8 22 10 47 02 0

231313 RMP$(1RG$)/RMP$(1RG$) 02 RMP C12848AA01RMP C12848CA01

232834 SDU1(5RV1)/ATSU1(1TX1) ATSU PLAT SW LA2T0S162C0C0F1

240000 POWER_SUPPLY_INTERRUPT 01 02 09 10 EIS 3 EIS II SOFTWARE SXT3FE2SA0410EIS II SOFTWARE SXT3CE2SA0420

Revision 31 PART




240000 POWER_SUPPLY_INTERRUPT CIDS 1 DIRECTOR-CIDS Z014H000131ADIRECTOR-CIDS Z014H000231BDIRECTOR-CIDS Z014H000031A

240000 POWER_SUPPLY_INTERRUPT CIDS 2 DIRECTOR-CIDS Z014H000131ADIRECTOR-CIDS Z014H000231B




DIRECTOR-CIDS Z014H000031A

242255 AFS:28V_PWR_11XU1 02 09 10 AFS FMGC ALL P/N

243251 SDAC$:NO_TR1_CURRENT ______1PU1 SDAC 350E5161122SDAC 350E5151022

243834 SDAC$:NO_DATA_FROM BCL SDAC 350E5161122SDAC 350E5151022

Revision 31 PART


2700 F/CTL_SPD_BRK_DISAGREE FCDC ALL_P/N

275134 SDAC$:NO_DATA_FROM SFCC SDAC 350E5161122SDAC 350E5151022

284248 FUEL_QUANTITY___________ R_ULTRACOMP_52QT 06 FUEL COMPUTER-FQI SIC5059XXXX05COMPUTER-FQI SIC5059XXXX07COMPUTER-FQI SIC5059XXXX06

301151 $$$WAI_FILTER_OR_VALVE ZONE CONTROLLER 775A0000-07




301151 $$WAI_FILTER_OR_VALVE ZONE CONTROLLER 775A0000-07

313234 _RADAR$___NO DATA FROM_CFDIU RADAR 204-1217-0421RADAR 204-1217-0418

313522 AFS:PRINTER AFS PRINTER ALL P/N

Revision 31 PART


316322 DU_PFD_FO(2WT2)/________ PFD_FO_POT(7WT2) EIS II SOFTWARE SXT3CE2SA0420EIS II SOFTWARE SXT4EE2SA050A

316322 DU_ND_FO(3WT2)/_________ ND_FO_POT(8WT2) EIS II SOFTWARE SXT3CE2SA0420EIS II SOFTWARE SXT4EE2SA050A

316322 DU_PFD_CAPT(2WT1)/______ PFD_CAPT_POT(7WT1) EIS II SOFTWARE SXT4EE2SA050AEIS II SOFTWARE SXT3CE2SA0420

316322 DU_ND_CAPT(3WT1)/_______ ND_CAPT_POT(8WT1) EIS II SOFTWARE SXT4EE2SA050AEIS II SOFTWARE SXT3CE2SA0420




316322 DU_SD(4WT2)/____________ ECP(6WT) EIS II SOFTWARE SXT3CE2SA0420EIS II SOFTWARE SXT4EE2SA050A

316322 DU_EWD(4WT1)/___________ ECP(6WT) EIS II SOFTWARE SXT4EE2SA050AEIS II SOFTWARE SXT3CE2SA0420

3200 L/G_SHOCK_ABSORBER_FAULT 08 09 TRANSCEIVER-RADIOALTIMETER

9599-607-14932


9599-607-12333

Revision 31 PART


3200 BRAKES_HOT BSCU ALL P/N

324418 SDAC$:LH_Y_BRK_PRESS XDCR_63GG FWC 350E053020606

324418 SDAC$:RH_Y_BRK_PRESS XDCR_62GG FWC 350E053020606

324553 PARK_BRAKE_SELECTOR_____ VALVE(102GG)/BSCU(10GG)

01 02 BSCU 1 BSCU E21327003BSCU E21327001BSCU E21327004




BSCU E21327004

324553 PARK_BRAKE_SELECTOR_____ VALVE(102GG)/BSCU(10GG)

01 02 BSCU 2 BSCU E21327003BSCU E21327001BSCU E21327004

340000 NAV GPWS FAULT 02 03 04 08 09 RECEIVER ILS 204-1230-3518

341234 AFS:ADIRU1/2/3_DISAGREE FAC B397AAM0508FAC B397AAM0507FAC B397AAM0509FAC B397AAM0510

Revision 31 PART


341234 ADIRU$$$($FP$$$)_ADRBUS/ WXR$($SQ$) 02 RADAR 822-1710-202RADAR 822-1710-201

341234 AFS:ADIRU1/2/3_DISAGREE FAC B397CAM0101FAC B397BAM0407FAC B397BAM0406FAC B397CAM0102

341234 AFS:ADIRU1/2/3_DISAGREE FAC B397AAM0507FAC B397AAM0508FAC B397BAM0406

FAC B397BAM0407

343522 HUD_OHU HUDC 9615433402HUDC 9615433401




343631 MMR1(40RT1)/GPWC(1WZ) GPWC 9650976003102

343631 ILS$_RECEIVER RECEIVER ILS 204-1230-3518RECEIVER ILS 204-1230-3518

343631 AFS:ILS AFS FMGC ALL P/N

Revision 31 PART


343631 FWC$_:NO_DATA_FROM ILS 02 07 RECEIVER ILS 622-9738-020

343631 NO_MLS_$_DATA CFDS AMU AMU3514ES01AMU AMU3514CS01AMU AMU3514DS01AMU AMU3514BS01

344133 RADAR1_TRANSCEIVER RADAR MI585306402

345133 AFS:DME AFS DME 622-4540-023DME 622-4540-023




345133 AFS:DME AFS FMGC C13043AA01

345331 NO_ADF_$_DATA CFDS CFDIU ALL P/N

345531 AFS:VOR AFS FMGC ALL P/N

Revision 31 PART


383100 LIQD_LVL_XMTR_(40MG)_ AND_LIQD_LVL_SNSR(41MG)_ TOILET OBRM CIDS DIR Z064H000030FOBRM CIDS DIR Z064H000030DOBRM CIDS DIR Z064H000030E

383134 VSC VSC VSC 14404-011A

383141 TOILET_ASSY_LAV_$_ TOILET OBRM CIDS DIR Z064H000030DOBRM CIDS DIR Z064H000030DOBRM CIDS DIR Z064H000030E

383163 LIQD_LVL_XMTR_(40MG)_ TOILET OBRM CIDS DIR Z064H000030DOBRM CIDS DIR Z064H000030EOBRM CIDS DIR Z064H000030F




OBRM CIDS DIR Z064H000030F

492316 LCDT_SENSOR_P29 APU ECB 4500001BECB 4500001AECB 4500003GECB 4500001APU APU APS3200

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




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






7700 DUAL_ENGINE_FAILURE 02 03 04 08 09 TRANSCEIVER-RADIOALTIMETER

9599-607-14942


9599-607-12333


9599-607-14932


9599-607-12552

Revision 31 PART


793415 CHECK_OIL_PRESS_SWITCH 3EN 02 09 TPIS TPIS 1058-34

XXXXXX ADF-$:NO_DATA_FROM ______CONTROL_SOURCE RECEIVER ADF 622-5222-020RECEIVER ADF 622-5222-020

XXXXXX ADF-$:NO_DATA_FROM CONTROL_SOURCE RECEIVER ADF 204-1168-7513

XXXXXX VOR-$:NO_DATA_FROM ______CONTROL_SOURCE RECEIVER-VOR 622-5220-020




XXXXXX VOR-$:NO_DATA_FROM CONTROL_SOURCE RECEIVER-VOR 2041231-3610

XXXXXX DME-$:NO_DATA_FROM ________CONTROL_SOURCE DME 9599-614-03105

Revision 31 PART

A320 Sil 00-028 CFDS Anomalies

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