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CUSTOMER SERVICES DIRECTORATE AIRBUS1 ROND POINT MAURICE BELLONTE
31707 BLAGNAC CEDEX FRANCE
TELEPHONE + 33 (0)5 61 93 33 33
TELEX AIRBU 530526F SERVICE INFORMATION LETTER
SIL NUMBER: 00-028
PAGE: 1 of 9 + Appendix
CREATION DATE: Nov 30/1989
REVISION: 29
REVISION: DATE: 31-MAR-06
SUBJECT:
ATA CHAPTER:
AIRCRAFT TYPE:
APPLICABILITY:
1. PURPOSE:
Centralized Fault Display System (CFDS) Anomalies
A318, A319, A320, A321
All Aircraft
The present SIL identifies all the known CFDS anomalies/BITE deviations. It is intended to be usedby maintenance engineering as a synthetic document, providing a short description of each deviation,as well as the affected part and the corrective action, with a cross-reference to the relevantTFU/TSM procedure. The fault messages/warnings or behaviours which should be known by linemaintenance teams, are covered by the Trouble Shooting Manual.
More precisely, the messages/behaviours described in this SIL are those for which the conditions ofoccurrence are precise/known and reproducible. In addition are mentioned messages/behaviours forwhich a statistical survey revealed a too high number of occurrences (more than 1 every 5 flightsper aircraft without any logbook complaint).
The last part of this SIL gives the filter content.
Each operator is responsible for uploading and updating the filter database, according to the partnumbers of equipment fitted on their aircraft.
00
0. REASON FOR REVISION:
Update of data. See Section 5 for detailed list of evolutions. Procedure to download SIL 00-028 and associated files from AOLS.
CUSTOMER SERVICES DIRECTORATE AIRBUS1 ROND POINT MAURICE BELLONTE
31707 BLAGNAC CEDEX FRANCE
TELEPHONE + 33 (0)5 61 93 33 33
TELEX AIRBU 530526F SERVICE INFORMATION LETTER
SIL NUMBER: 00-028
PAGE: 2 of 9 + Appendix
CREATION DATE: Nov 30/1989
REVISION: 29
REVISION: DATE: 31-MAR-06
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, whichrequest specific maintenance 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:
1. The ATA chapter of the message or anomaly.
2. The description of the message which is considered as non justified under some conditions.
3. Specific maintenance action to be performed or some remarks about the anomaly.
4. The computer affected by the anomaly.
5. The Part Number (P/N) of the affected computer.
6. The corrective P/N.
7. The reference of the TFU/TSM to obtain more details about the anomaly.
8. The A/C type involved.
9. The indication whether AIRBUS recommended (Y) or not (N) to filter a message/warning.
Nota 2: New/revised items are highlighted by a vertical adjacent “NEW” in the margin.
Nota 3:Lower-case letters such as “i” or ”j” represent a variable integer (usually 1, 2, or 1 to 3).
“i” and “j” are used in the messages.
“X” represents any alphanumeric character in the part numbers
CUSTOMER SERVICES DIRECTORATE AIRBUS1 ROND POINT MAURICE BELLONTE
31707 BLAGNAC CEDEX FRANCE
TELEPHONE + 33 (0)5 61 93 33 33
TELEX AIRBU 530526F SERVICE INFORMATION LETTER
SIL NUMBER: 00-028
PAGE: 3 of 9 + Appendix
CREATION DATE: Nov 30/1989
REVISION: 29
REVISION: DATE: 31-MAR-06
Nota 4:For each item, carefully check that the part number fitted on your aircraft corresponds to theaffected P/N mentioned in the SIL. Otherwise, the remark is not applicable to your A/C.
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 on the MCDU or in MFT.
Nota 6: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.
Nota 7: Anytime the P/N of a computer is changed on the A/C, it is recommended to update the filtercontent, using information which are in Part E of this SIL.
Nota 8: Part E of this SIL - Filter Content - is available on floppy disk - called“FilenvXX.320” (XX: Revision number).For customization, refer to Maintenance Filter Tool (MFT) - SIL 00-088.
3. MATERIAL INFORMATION
Not Applicable
4. PROCUREMENT INFORMATION
Not Applicable
CUSTOMER SERVICES DIRECTORATE AIRBUS1 ROND POINT MAURICE BELLONTE
31707 BLAGNAC CEDEX FRANCE
TELEPHONE + 33 (0)5 61 93 33 33
TELEX AIRBU 530526F SERVICE INFORMATION LETTER
SIL NUMBER: 00-028
PAGE: 4 of 9 + Appendix
CREATION DATE: Nov 30/1989
REVISION: 29
REVISION: DATE: 31-MAR-06
5. LIST OF EVOLUTIONS
PART ATA ITEMS TYPE REMARKA 228334 FMGCi (1CAj)/RMPi (1RGi)/ILSi (1RTi) Revised Wording
A 231133 HF1 COUPLER (4RE1)/FEEDER HF1 (6RE1)/ANTENNA(5RE1) New
A 316322 DU ND CAPT(3WK1)/ND CAPT POT(8WK1) NewA 316322 DU ND FO(3WK2)/ND FO POT(8WK2) NewA 316322 DU PFD CAPT(1WK1)/PFD CAPT POT(7WK1) NewA 316322 DU PFD FO(1WK2)/PFD FO POT(7WK2) NewA 316322 DU EWD(2WK1)/ECP(6WM) NewA 316322 DU SD(2WK2)/ECP(6WM) NewA 341234 QUALIFIER Di/WXRj (1SQj) (i = 1 or 2 and j = 1 or 2) New
A 341234 ADIRUi+3(1FPi+3) ADRBUS/WXRj(1SQj)(i = 1 or 2 and j = 1 or 2) Revised Wording + P/N
A 344133 WXRi (1SQi) (i = 1 or 2) New
A 344133 DMCi: NO WXRj CHj DATA(i = 1, 2 or 3 and j = 1 or 2) Revised Wording
A 344300 DMC(i): NO TCAS DATA (i = 1 or 2) Revised Wording + P/NA 344333 FWC(i): NO DATA FROM TCAS (i = 1 or 2) Revised Wording + P/NA 344333 NO TCAS DATA Revised Wording + P/NA 344334 ATC(i): NO DATA FROM TCAS (i = 1 or 2) Revised Wording + P/NA 344334 TCAS (1SG) Revised Wording + P/NA 345233 QUALIFIER Ci/WXRj (1SQj) (i = 1 or 2 and j = 1 or 2) NewA 345233 ATCi (1SHi)/TCAS (100SG) source TCAS (i = 1 ou 2) NewA 345233 NO ATCi DATA source CFDS (i = 1 or 2) Revised Wording + P/NA 345233 ATCi (1SHi)/TCAS (1SG) source TCAS (i = 1 ou 2) Revised Add TFU ref.B 2161 AIR:PACK i REGUL FAULT Revised WordingB 3443 NAV TCAS FAULT Revised Add TFU ref.C 313234 CFDIU (1TW)/WXRi (i = 1 or 2) NewC 341234 ADIRU3 (1FP3) ADR BUS/WXRi (1SQi) (i = 1 or 2) NewE 2161 AIR_PACK_1$2_FAULT Revised Wording
E 316322 DU_ND_CAPT(3WK1)/_______ND_CAPT_POT(8WK1) New
E 316322 DU_ND_FO(3WK2)/__________ND_FO_POT(8WK2) New
E 316322 DU_PFD_CAPT(1WK1)/_______PFD_CAPT_POT(7WK1) New
E 316322 DU_PFD_FO(1WK2)/________PFD_FO_POT(7WK2) New
E 316322 DU_EWD(2WK1)/__________ECP(6WM) New
CUSTOMER SERVICES DIRECTORATE AIRBUS1 ROND POINT MAURICE BELLONTE
31707 BLAGNAC CEDEX FRANCE
TELEPHONE + 33 (0)5 61 93 33 33
TELEX AIRBU 530526F SERVICE INFORMATION LETTER
SIL NUMBER: 00-028
PAGE: 5 of 9 + Appendix
CREATION DATE: Nov 30/1989
REVISION: 29
REVISION: DATE: 31-MAR-06
E 316322 DU_SD(2WK2)/____________ECP(6WM) New
E 341234 ADIRU$($FP$)_IR_BUS/____WXR$($SQ$) New
E 341234 ADIRU$$$($FP$$$)_ADRBUS/WXR$($SQ$) New
E 345233 NO_ATC_$_DATA__ Revised Wording + P/N
6. PROCEDURE TO DOWNLOAD FILES ATTACHED TO SIL ON AOLS
1/ Procedure to download SIL .pdf files:
- under Technical Publication select Engineering Technical Documentation,- select Document Type and SIL Number then click on the SEARCH button,- once selected SIL is opened, it is possible either to print or to save on disk.
2/ Procedure to download attached files to SIL 00-028:
Following files can be downloaded through the Airbus OnLine Services (AOLS) FTP:
- AIRBUS Filter Envelop (FILENVxx.320 [xx=REV]),- AIRBUS FILTER DATABASE label to be stuck onto the floppy.
Procedure to download:
- select FTP Site under General Services menu,- click on ASSOCIATED DOCUMENTS for SIL under the main ROOT,- 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.
CUSTOMER SERVICES DIRECTORATE AIRBUS1 ROND POINT MAURICE BELLONTE
31707 BLAGNAC CEDEX FRANCE
TELEPHONE + 33 (0)5 61 93 33 33
TELEX AIRBU 530526F SERVICE INFORMATION LETTER
SIL NUMBER: 00-028
PAGE: 6 of 9 + Appendix
CREATION DATE: Nov 30/1989
REVISION: 29
REVISION: DATE: 31-MAR-06
LIST OF ABREVIATIONS
SIGLUM TITLEACARSACSCACPADIRUADFADRAEVCAFSAIDSAMMAMUAOAAPUASSYATAATCA/PA/THRATIMSBCLBITEBMCBSCUCAMCFDIUCFDSCHCCIDSCPCCVCC/BDCDFDRDLRBDLSDMCDME
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 SystemAircraft Maintenance ManualAudio Management UnitAngle-Of-AttackAuxiliary Power UnitAssemblyAir Transport AssociationAir Traffic ControlAutopilotAuto ThrustAir Traffic and Information Management SystemBattery Charge LimiterBuilt-in Test EquipmentBleed Monitoring ComputerBraking & Steering Control UnitCabin Assignment ModuleCentralized Fault Detection Interface UnitCentralized Fault Display SystemCargo Heat ControllerCabin Intercommunication Data SystemCabin Pressure ControllerCargo Ventilation ControllerCircuit BreakerDirect CurrentDigital Flight Data RecorderData Loader Routing BoxData Loader SelectorDisplay management ComputerDistance Measuring Equipment
CUSTOMER SERVICES DIRECTORATE AIRBUS1 ROND POINT MAURICE BELLONTE
31707 BLAGNAC CEDEX FRANCE
TELEPHONE + 33 (0)5 61 93 33 33
TELEX AIRBU 530526F SERVICE INFORMATION LETTER
SIL NUMBER: 00-028
PAGE: 7 of 9 + Appendix
CREATION DATE: Nov 30/1989
REVISION: 29
REVISION: DATE: 31-MAR-06
SIGLUM TITLEDMCUDMUDUECAMECBECSECUEFDUEIUELACEVMUFADECFACFCDFCDCFCOMFCUFCVFDIMUFDIUFGFINFLFMFMGCFMGSFMSFQI CHFQICFTFWCFWDF/CTLF/DGCUGPWCGPCUGWHFHPHPVHUD
Drain Mast Central UnitData Management UnitDisplay UnitElectronic Centralized Aircraft MonitorElectronic Control BoxEnvironmental 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 ValveFlight Data Interface Management UnitFlight Data Interface UnitFlight GuidanceFunctional Item NumberFlight LevelFlight ManagementFlight Management & Guidance ComputerFlight Management & Guidance SystemFlight Management SystemFuel Quantity Indicator ChannelFuel Quantity Indication ComputerFeetFlight Warning ComputerForwardFlight ControlFlight DirectorGround Control UnitGround Proximity Warning ComputerGround Power Control UnitGross WeightHigh FrequencyHigh PressureHigh Pressure ValveHead Up Display
CUSTOMER SERVICES DIRECTORATE AIRBUS1 ROND POINT MAURICE BELLONTE
31707 BLAGNAC CEDEX FRANCE
TELEPHONE + 33 (0)5 61 93 33 33
TELEX AIRBU 530526F SERVICE INFORMATION LETTER
SIL NUMBER: 00-028
PAGE: 8 of 9 + Appendix
CREATION DATE: Nov 30/1989
REVISION: 29
REVISION: DATE: 31-MAR-06
SIGLUM TITLEHUDCILSISISLGCIULOPLRUL/G
Head Up display ComputerInstrument Landing SystemIntegrated Standby Instrument SystemLanding Gear control & Interface UnitLow Oil Pressure Line Replacement UnitLine Replacement UnitLanding Gear
MMCDUMELMFTMLGMMMMELMPDMRBMSNMTBFMTBRMTBURMUNDNLGNMOBRMOVHTPAPCPCUPDUPESPFDPFRPHCPRAMPRVPTTPTUP/NQARRARFI
Mach NumberMulti-purpose Control and Display UnitMaster Equipment ListMaintenance Filter ToolMain Landing GearMaintenance ManualMaster Minimum Equipment ListMaintenance Planning DocumentMaintenance Review BoardManufacturer Serial NumberMean Time Between FailuresMean Time Between RemovalMean Time Between Unscheduled RemovalManagement UnitNavigation DisplayNose Landing GearNautic MilesOn Board Replaceable ModuleOverheatPublic AddressPack ControllerPower control UnitPower Distribution UnitPassenger Entertainment SystemPrimary Flight DisplayPost Flight ReportProbe Heat ComputerPre-Recorded Announcement and MusicPressure Regulator ValvePush-To-TalkPower Transfer UnitPart NumberQuick Access RecorderRadio AltimeterRequest For Information
CUSTOMER SERVICES DIRECTORATE AIRBUS1 ROND POINT MAURICE BELLONTE
31707 BLAGNAC CEDEX FRANCE
TELEPHONE + 33 (0)5 61 93 33 33
TELEX AIRBU 530526F SERVICE INFORMATION LETTER
SIL NUMBER: 00-028
PAGE: 9 of 9 + Appendix
CREATION DATE: Nov 30/1989
REVISION: 29
REVISION: DATE: 31-MAR-06
SIGLUM TITLERFRRMPSBSDACSDCUSDISECSFCCSFCSSFESILSRMTATTBDTEMTFUTHSTLTTPIUTRUTSMULDUPPR CRG DETVHFVORWAIWAIVWDBWHCWRXZC
Request For RevisionRadio Management PanelService BulletinSystem Data Acquisition ConcentratorSmoke Detection Control UnitSpares Data ImprovementSpoiler Elevator ComputerSlat/Flap Control ComputerSlat/Flap Control SystemSupplier Furnished EquipmentService Information LetterStructural Repair ManualTurn Around TimeTo Be DefinedTool and Equipment ManualTechnical Follow-UpTrimmable Horizontal StabilizerTemperature Limitation ThermostatTyre Pressure Indicating ComputerTransformer Rectifier UnitTrouble Shooting ManualUnit Load DeviceUpper Cargo Smoke DetectorVery High FrequencyVHF Omnidirectional RangeWing Anti-IceWing Anti-ice ValveWall Disconnect BoxWindow Heat ComputerWeather Radar TransceiverZone Controller
Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART A : Failure Messages
ATA Filter
000000 NO DATA NO MAINT. ACTION CFDIU B401ACM0505
----
B401ACM0506
Associated P/N : ----
No
212853 FWD CARGO FAN OR SPLY 6H NO MAINT. ACTION if power supply between FAN and CVC is OK, 115 V 3 phases. (Minimum value : 110 V)
CVC 600615-01-500
600615-00-502
----
600615-01-502
600615-00-503
TFU 212854002
Associated P/N : ----
No
212854 AFT CARGO FAN OR SPLY 35 NO MAINT. ACTION if power supply between FAN and CVC is OK, 115 V 3 phases. (Minimum value : 110 V)
CVC 600615-01-500
600615-00-502
----
600615-01-502
600615-00-503
TFU 212854002
Associated P/N : ----
No
215151 Pi FLOW CONTROL VALVE Associated to Maintenance Status PACK 1(2) , NO MAINT. ACTION if Bite test OK
FCV 751A0000-06
----
751A0000-07 TFU 215151004
Associated P/N : ----
No
216334 EIUi : NO ZONE CONTP(S) DATA
Associated with ECAM warning : ENG1(2) BLEED STATUS FAULT. NO MAINT. ACTION
ZC 775A0000-06
EIU CFMI
775A0000-07 TFU 216334051/ TFU 732900029 / TSM ATA 75
Associated P/N : ----
No
1Part A : page Revision 29
Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART A : Failure Messages
ATA Filter
216334 EIUi NO ZONE CONTP(S) DATA
NO MAINT. ACTION If not associated to Maintenance Status : ENG1(2)EIU
EIU 3957900609
395790061039579006113957905003
----
3957900612
3957905004
TFU 732534005 / TFU 732534042 / TSM ATA 71
Associated P/N : ----
No
216334 NO ZONE CTL DATA NO MAINT. ACTION, Could be intermittent (INTM). ZC 775A0000-06
B401ACM0404
775A0000-07 TFU 216334051
Associated P/N : CFDIU
No
216334 SDACi: NO DATA FROMECS i
NO MAINT. ACTION if occurs in phase 6 ZC 775A0000-06
----
775A0000-07 TFU 216334051
Associated P/N : ----
No
226634 DMCi : No FACj DATA No Maintenance action DMC ALL P/N
----
9615325050
(Soft std DMC V50)
Associated P/N : ----
Yes
228112 FCU (2CA) BUS CP-L/WRX 1 (1SQ1)
If no logbook associated logbook complaint, No maintenance action is required.
RADAR 066-50008-301
----
066-50008-405
Soft 05
Associated P/N : ----
No
2Part A : page Revision 29
Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART A : Failure Messages
ATA Filter
228112 FCU(2CA)CP-L BUS/WXRi(1SQi) (i = 1 or 2)
No maintenance action required if no logbook complaint. RADAR 822-1710-201
----
822-1710-202
Associated P/N : ----
No
228112 FCU(2CA)CP-R BUS/WXRi(1SQi) (i = 1 or 2)
No maintenance action required if no logbook complaint. RADAR 822-1710-201
----
822-1710-202
Associated P/N : ----
No
228112 FCU(3CA)CP-L BUS/WXRi 1SQi (I=1 or 2)
NO MAINT. ACTION if recorded during Engine Start (flight phase 02) or during switching from WXR1 to WXR2 and no associated cockpit effect.
RADAR 822-1710-201
----
822-1710-202
Associated P/N : ----
No
228112 FCU(3CA)CP-R BUS/WXRi 1SQi (I=1 or 2)
NO MAINT. ACTION if recorded during Engine Start (flight phase 02) or during switching from WXR1 to WXR2 and no associated cockpit effect.
RADAR 822-1710-201
----
822-1710-202
Associated P/N : ----
No
228112 RADARi:NO DATA FROMEFIS i PANEL
NO MAINT. ACTION if no log book complaint RADAR 622-5132-020
622-5132-120
----
VSB WRT-701X-34-68
VSB WRT-701X-34-77
Associated P/N : ----
No
3Part A : page Revision 29
Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART A : Failure Messages
ATA Filter
228212 AFS:MCDUi NO MAINT. ACTION if no log book complaint FMGC ALL P/N
----
NONE TFU 229100011
Associated P/N : ----
Yes
228212 MDCU3(3CA3)/ATSU1(1TX1) No maintenance action if MCDU 3 not installed. Can be filtered if MCDU 3 not installed
ATSU host platform S/W
LA2T0S111C1B0F1
----
LA2T0J13000C0F1 TFU 46 00 00 002
Associated P/N : ----
Yes
228334 AFS:FMGC$(DO NOT REMOVE)NO MAINT. ACTION
FAC FAC pre Std
B397BAM0617
C13042xA01
B397BAM0617
Associated P/N : FMGC PEGA
Yes
228334 AFS:FMGCi NO MAINT ACTION IF MESSAGE NOT ASSOCIATED WITH ANY ECAM WARNING AND COCPIT EFFECT
FMGC B546BAM0203
B546CCM0101B546CAM0101B398AAM0410
B398BAM0207
----
B546BAM0206
B546CAM0102B546CCM0104
TFU229100055
Associated P/N : ----
Yes
B546BCM0205C13042AA01
228334 AFS:FMGCi (FMi) NO MAINT. ACTION if no log book complaint FMGC B398AAM0408
B398BAM0205B398BCM0104
----
B398AAM0409
B398BAM0206B398BCM0106
TFU 229100010
Associated P/N : ----
Yes
4Part A : page Revision 29
Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART A : Failure Messages
ATA Filter
228334 AFS:FMGCi/ATHR ENGDFDBK
NO MAINT. ACTION if not associated with ECAM WARNING : AUTO FLT A/THR OFF.
FMGC (LEGACY)
B398AAM0xxx
B398BAM0xxxB398BCM0xxx
----
TBD
Associated P/N : ----
Yes
228334 FMGCi (1CAi)/RMPi(1RGi)/ILSi(2RTi)
No maintenance action if not logbook complaint ILS 066-50006-X202
(Allied)622-9738-041(Collins)
----
TBD
(Allied)822-0298-020
Associated P/N : ----
No
(Collins)
228334 FMGCi(1CAi) BUS MMR/MMRi (40RTi)
Reset MMR1 when I equal 1 (Reset MMR2 when i equal 2). If in the Ground Scanning "FMGC BUS ILS/MMR" or in the TSD "PORT B RX FAIL" are visible carry out associated TSM task.
MMR 822-1152-121
----
VSB Collins
GLU 920-34-19
TSM task 34 36 00 810 870/871
Associated P/N : ----
No
228334 FMGCi(1CAj)/RMPi(1RGi)/ILSi(1RTi)
No maintenance action if no FM auto reset reported in the logbook.
FMGC All P/N
----
N/A SIL 22-037 & SIL 22-038
Associated P/N : ----
No
228334 FMGECi(1CAi)/RMPi(1RGi)/ILSi(1RTi)
No maintenance action if no logbook entry ILS 622-9738-041
(Collins)
----
N/A
Associated P/N : ----
No
5Part A : page Revision 29
Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART A : Failure Messages
ATA Filter
230000 DIR1 (101RH)/OBRM Maintenance advise: A CIDS interface and power-up test must be performed to confirm validity of the failure and to clear the failure message from the ground report.
CIDS DIR
Z064H000030F
Z064H000031AZ064H000031B
----
TBD (end 2005)
Associated P/N : ----
No
231100 CHECK HF (i) ANTENNACIRCUIT
NO MAINT ACTION if no log book entry HF TRANSCEIVER
622-5272-020
----
VSB HFS-700-36 TFU 231100002
Associated P/N : ----
No
231100 ICAO ADDRESS/HFi(3REi) NO MAINT. ACTION. This message is triggered if Datalink not activated (MOD 31286) and CFDIU Label 157 not received within 30s after HFDR power-up. This message is associated with CLASS3 Fault message "462134 ATSU(1TX1)/ HFi(3Ri)"
HFDR 822-0990-003
Collins HFS900D
----
TBD
Associated P/N : ----
Yes
231133 HF1 COUPLER(4RE1)/FEEDER HF1(6RE1)/ANTENNA(5RE)
No maintenance action if no logbook compaint. COUPLER
792-6140-001
----Associated P/N : ----
No
231133 HFDRi(3REi)/ATSU1(1TX1)Source ACARS MU
NO MAINT. ACTION when HFDR not activated and CFDIU PRE STD 9B (Source name "ACARS MU" in the PFR)
ATSU HOST Platform S/W
LA2T0J13000C0F1
LA2T0J13002C0F1
B401ACM0507
C12860AA02 TFU 46 00 00 002
Associated P/N : CFDIU
Yes
6Part A : page Revision 29
Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART A : Failure Messages
ATA Filter
231133 NO HF 1 DATASource CFDS
No Maint. Action if triggered in phase 02. HF Transceiver
964-0452-001
964-0452-012
----
TBD
Associated P/N : ----
No
231211 CHECK VHF 1 ANTENNACIRCUIT
NO MAINT. ACTION if VSB mentioned in Corrective P/N not incorporated.
VHF 622-5219-020
----
VSB VHF-700-23-36
VSB VHF-700-23-30
TFU 231200011
Associated P/N : ----
No
231233 NO VHF3 DATA NO MAINT. ACTION when VHF3 not installed CFDS C12860AA02
(STD 9B)
----
CFDIU STD 10 TBC
Associated P/N : ----
Yes
231233 VHF 3 TRANSCEIVER NO MAINT. ACTION if no log book complaint VHF 622-5219-020
----
VSB VHF-700-23-38
Associated P/N : ----
No
231233 VHF0(1RC0) NO MAINT. ACTION if occurs in phase 02 VHF3 822-1047-030
----
N/A
Associated P/N : ----
Yes
7Part A : page Revision 29
Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART A : Failure Messages
ATA Filter
231313 RMPi(1RGi)/RMPj(1RGj) NO MAINT. ACTION required RMP C12848AA01
C12848CA01
----
TBD
Associated P/N : ----
Yes
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).
ATSU host platform S/W
LA2T0S162C0C0F1
----
LA2T0S111C1B0F1 TFU 46 00 00 002
Associated P/N : ----
Yes
237300 FAP1 (120RH)/DIR2/CAM
Maintenance advise: A CIDS interface and power-up test should be performed to confirm validity of the failure message. The associated time may be completely erroneous.
CIDS SDF
Z064H000030F
Z064H000031AZ064H000031B
----
TBD (end 2005)
Associated P/N : ----
No
237300 FAP1 (120RH)/DIR1/CAM Maintenance advise: To check the validity of the FAP failure message, please select the FAP status page. Should any anomaly is visible on subject page, please refer to the corresponding trouble shooting task.
CIDS DIR
Z064H000030F
Z064H000031AZ064H000031B
----
TBD (end 2005)
Associated P/N : ----
No
237300 FAP1 (120RH)/DIR2/CAM Maintenance advise: To check the validity of the FAP failure message, please select the FAP status page. Should any anomaly is visible on subject page, please refer to the corresponding trouble shooting task.
CIDS DIR
Z064H000030F
Z064H000031AZ064H000031B
----
TBD (end 2005)
Associated P/N : ----
No
8Part A : page Revision 29
Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART A : Failure Messages
ATA Filter
237313 AAP (126RH) ATT 4L Maintenance advise: If an AAP failure message is recorded into the PFR, perform a visual check of the AAP¨operation to determine the validity of the fault message.
CIDS DIR
Z064H000030F
----
Z064H000031A
Z064H000031B
Associated P/N : ----
No
237313 AAP (126RH) ATT 4L/DEU B (300RH7)
Maintenance advise: If an AAP failure message is recorded into the PFR, perform a visual check of the AAP¨operation to determine the validity of the fault message.
CIDS DIR
Z064H000030F
----
Z064H000031A
Z064H000031B
Associated P/N : ----
No
237322 AIP (320RH1) ATT 1L Maintenance advise: A CIDS interface and power-up test should be performed to confirm validity of the failure message. The associated time may be completely erroneous.
CIDS SDF
Z064H000030F
Z064H000031AZ064H000031B
----
TBD (end 2005)
Associated P/N : ----
No
237322 AIP (320RH9) ATT 4L Maintenance advise: A CIDS interface and power-up test should be performed to confirm validity of the failure message. The associated time may be completely erroneous.
CIDS SDF
Z064H000030F
Z064H000031AZ064H000031B
----
TBD (end 2005)
Associated P/N : ----
No
237334 CIDS2(102RH) NO MAINT. ACTION. Associated with MAINT STATUS TEMP CTL 1 and TEMP CTL 2. problem of a discrete label status computed by the CIDS2 and used by ACSC 1 and 2.
ACSC 1803A0000-03
----
TBD EYDCC Technical note P2161ME0308866-V1
Associated P/N : ----
No
9Part A : page Revision 29
Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART A : Failure Messages
ATA Filter
237334 DIR1 (101RH) -SDF Maintenance advise: A CIDS interface and power-up test should be performed to confirm validity of the failure message. The associated time may be completely erroneous.
CIDS SDF
Z064H000030F
Z064H000031AZ064H000031B
----
TBD (end 2005)
Associated P/N : ----
No
237334 DIR1 (101RH) BUS/DIR2 (102RH)
Maintenance advise: A CIDS interface and power-up test should be performed to confirm validity of the failure message. The associated time may be completely erroneous.
CIDS SDF
Z064H000030F
Z064H000031AZ064H000031B
----
TBD (end 2005)
Associated P/N : ----
No
237334 NO CIDS 1(2) DATA Please refer to TFU 23 73 00 083 CIDS Z010H000abcd
abcd=3113 or 3117or 5115 or 5117 or5118 or 5119 or
520A or 521A
CFDS
TBD TFU 23 73 00 083
Associated P/N : ALL P/N
Yes
237334 NO CIDS 1(2) DATA (INTM) Please refer to TFU 23 73 00 083 CIDS Z010H000abcd
abcd= 3113 or 3117or 5115 or 5117 or5118 or 5119 or
520A or 521A
CFDS
TBD TFU 23 73 00 083
Associated P/N : ALL P/N
No
24 P-OW-ER CONSUMPTION NO MAINT ACTION if no log book complaint BCL 35-0L5-1003-06
----
35-0L5-1004-07 TFU 243800008
Associated P/N : ----
No
10Part A : page Revision 29
Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART A : Failure Messages
ATA Filter
240000 POWER SUPPLY INTERRUPT NO MAINTENANCE ACTION ILS 066-50008-0301
----
066-50008-0405
Associated P/N : ----
No
240000 POWER SUPPLY INTERRUPTSource EIS 1(2)(3)
No Maintenance action if occurs during PWR transfer: Phase 01 and 02 (Engine start-up), Phase 09 and 10 (Engine Shut Down).
DMC EIS II Soft
SXT3F-E2SA-0410
SXT3C-E2SA-0420
----
EIS II Soft Std S5
Associated P/N : ----
Yes
242151 IDGi DISCONNECTED Check Class 3 Fault messages. GPCU 740121A
----
740121B
(SB24-1077)
TFU 244100002 / TSM ATA 24
Associated P/N : ----
No
242151 IDGi OIL LEVEL SENSOR/GCUi - Source EPGS
Quality issue affecting component inside the GCU. Ony GCUs manufactured before Nov 2002 are affected. When message is triggered, the GCU should be removed and sent to vendor Hamilton Sundstrand for repair.
GCU 767584J
----
TFU 24.21.00.039
Associated P/N : ----
No
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)
FMGC All P/N
----
N/A
Associated P/N : ----
Yes
11Part A : page Revision 29
Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART A : Failure Messages
ATA Filter
242300 CHECK GCU APU PIN C1, C5GEN APU PIN A9, A10
1.If associated with a generator trip : remove the APU generator, otherwise, NO MAINT.ACTION. 2.If APU GEN FAULT imediately after APU start,reset APU GEN P/B SW. on OVHD panel.
GCU 740120A
740120B
----
740120C
(SB 24-1074)
TFU 244100008
Associated P/N : ----
No
243251 SDACi: NO TR1 CURRENT1PU1
At APU start NO MAINT. ACTION SDAC 35-0E5-1510-22
35-0E5-1611-22
----
35-0E5-1513-31 TFU 315500003
Associated P/N : ----
Yes
243834 SDACi : NO DATA FROMBCLi
NO MAINT. ACTION if no Log Book complaint. SDAC 35-0E5-1510-22
35-0E5-1611-22
----
35-0E5-1513-31
Associated P/N : ----
Yes
256200 SLIDE BTL XY/DEU B (300RHZ) with X=1, 3 or 4 and Y=R or L and Z=1, 6 or 8.
No maintenance action required. CIDS DIR
Z064H000030F
----
Z064H000031A
Z064H000031B
Associated P/N : ----
No
261000 WRG: CAN BUS A (or B) NO MAINT. ACTION if fault message displayed after a reset of CIDS or CIDS-SDF
CIDS DIR
Z064H000030D
Z064H000030EZ064H000030F
----
TBD SIL 23-039
Associated P/N : ----
No
12Part A : page Revision 29
Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART A : Failure Messages
ATA Filter
261200 CHECK FDU ENGi SUPPLY NO MAINT. ACTION if no log book complaint FDU 730400-01
----
730401-02 TFU 261234020
Associated P/N : ----
No
261300 CHECK FDU APULOOP A WARN CKT
No MAINT. ACTION if APU FDU test does not confirm the fault message
FDU 3720-00-00
----
TBD TFU 26 13 00 001
Associated P/N : ----
No
261300 CHECK FDU APULOOP B WARN CKT
No MAINT. ACTION if APU FDU test does not confirm the fault message
FDU 3720-00-00
----
TBD TFU 26 13 00 001
Associated P/N : ----
No
261734 SDCU CHANNEL 2 (10WQ) NO MAINT. ACTION if reset of the SDCU clears the message
SDCU RAI-2800-M0706
----
SB 92-1021 TFU 26 17 34 012
Associated P/N : ----
No
275100 SFCC1(2) orFLP PPU POWER
If associated with failure message FLP1(2) PCU VALVEBLOCK 23(24) CV. Corrective action: replace SFCC at the origin of the fault.
SFCC 49-170-11
From S/N 5813To S/N 5956
----
OIT 999.0047/05
Associated P/N : ----
No
13Part A : page Revision 29
Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART A : Failure Messages
ATA Filter
275100 SFCCi or FLAP PPU POWER - If recorded in PFR without associated warning, NO MAINTENANCE ACTION required. If recorded in the PFR with the associated Ecam Warning: "F/CTL FLAP SYSi FAULT" or "F/CTL FLAP LOCKED" performed a manual reset of the SFCC through the SFCC MCDU BITE menu: SFCC/WTB RESET.
SFCC 49117-10
(S/N 1732 to 1934)49170-07(S/N 1743 to 1904)
----
49-170-11 TFU 275134025
Associated P/N : ----
No
275100 SLT/FLT CSU 51CV ORWIRING TO SLT1(2)/FLP1(2)
If recorded in PFR without warning No MAINT. ACTION required. If Warning refer to TFU 27 51 00 004
SFCC 49170-11
----
49170-11 Amdt. A TFU 27 51 00 004
Associated P/N : ----
No
275134 SDACi: NO DATA FROM SFCC NO MAINT ACTION if no log book complaint SDAC 35-0E5-1510-22
35-0E5-1611-22
----
35-0E5-1513-31
Associated P/N : ----
Yes
275453 FLP1(2) PCUVALVEBLOCK 23(24) CV
If associated with failure message SFCC1(2) or FLP PPU POWER. Corrective action: replace SFCC at the origin of the fault.
SFCC 49-170-11
From S/N 5813To S/N 5956
----
OIT 999.0047/05
Associated P/N : ----
No
278100 SFCCi or SLAT PPU POWER If recorded in PFR without warning: NO MAINTENANCE ACTION required. If associated with Ecam Warning: "F/CTL SLAT SYSi FAULT" or "F/CTL SLAT LOCKED" performed a SFCC/WTB reset through the MCDU.
SFCC 49117-10
49170-07(S/N 1727 to 1906)
----
49-170-11 TFU 275134025
Associated P/N : ----
No
14Part A : page Revision 29
Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART A : Failure Messages
ATA Filter
2800 FUEL L(R) XFR VALVE OPEN If this ECAM message is reported, perform functional BITE test of the ICTVs - FLSS Status (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 the FLSS status and FLSS BITE show NO FAULT.
FQIC
----
TFU 281500003
Associated P/N : ----
No
284234 FUEL QUANTITY FQIC 3QT NO MAINT. ACTION if FQIC grades remains at 1 after FQIC test through CFDS. associated with ECAM warning : 28-00 FQI CH1(2) FAULT
FQIC SIC5059-xx-xx05
SIC5059-xx-xx06
----
SIC5059-xx-xx07 TFU 284234030
Associated P/N : ----
No
284634 FUEL LEVEL SENSINGL (or R) UNFULL SENSOR 25QJ1 (or 25QJ2 or 26QJ1 or 26QJ2)
NO MAINT. ACTION if triggered in flight phase 02 FLSCU ALL P/N
----
TBD
Associated P/N : ----
No
301151 R(L) WAI FILTER OR VALVE10DL (9DL)
NO MAINT. ACTION if not associated with ECAM warning.
ZC 775A0000-07
----
775A0000-08 TFU 301100014 / TSM ATA30
Associated P/N : ----
Yes
307151 DRAINMAST HEATER FWD AFT NO MAINT. ACTION if no blockage or system malfunction reported.
DMCU 4-60000H800
4-60000H840
----
4-60000H882
SB 30-1030
TFU 307100002
Associated P/N : ----
No
15Part A : page Revision 29
Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART A : Failure Messages
ATA Filter
307151 DRAINMAST HEATER FWD/AFT Replace the drainmast even if the fault is not confirmed on ground. This deviation has been identified. A correction will be incorporated in the next Drainmast
DRAINMAST
4-60000H880
----
4-60000H882
SB 30-1030
TFU 307100003
Associated P/N : ----
No
307151 DRAINMAST HEATER MID Valid only if Mod. 21598 embodied. NO MAINT. ACTION if no blockage or system malfunction reported.
DMCU 4-60000H800
4-60000H840
----
4-60000H882
SB 30-1030
TFU 307100002/307100003
Associated P/N : ----
No
307151 DRAINMAST HEATER MID Valid only if Mod 21598 embodied. Replace the drainmast even if the fault is not confirmed on ground. This anomaly has been identified. A correction will be incorporated in the next Drainmast.
DRAINMAST
4-60000H880
----
4-60000H882
SB 30-1030
TFU 307100003
Associated P/N : ----
No
313234 BAD DATA FROM CFDIU NO MAINT. ACTION ILS 622-9738-020
622-9738-041
B401ACM0404
VSB ILS-720-34-01
AI S/B: 34-1093
Associated P/N : CFDIU
No
313234 CFDIU(1TW)/HF(i) (3REi) No maintenance action if no logbook complaint. HF Transceiver
964-0452-001
----
TBD
Associated P/N : ----
No
16Part A : page Revision 29
Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART A : Failure Messages
ATA Filter
313234 LGCIU: NO DATA FROM CFDS Appears after a CFDIU power down, NO MAINTENANCE ACTION
LGCIU 664700500A4A
----
664700500A4B TFU 323134043
Associated P/N : ----
No
313234 RADAR x: NO DATA FROMCFDIU
NO MAINT. ACTION RADAR 204-1217-0418
204-1217-0421
----
VSB RTA-4A-34-173 TFU344100010
Associated P/N : ----
Yes
313352 QAR NO MAINT. ACTION if mentioned in Phase 1 in last leg report
FDIU 9026-16079-01B2
----
9026-16079-02B3 TFU 313300007
Associated P/N : ----
No
313352 QAR TAPE LOW NO MAINT. ACTION if mentioned in Phase 1 in last leg report
FDIU 9026-16079-01B2
----
9026-16079-02B3 TFU 313300007
Associated P/N : ----
No
313355 DFDR NO MAINT. ACTION if mentioned in Phase 1 in last leg report
FDIU 9026-16079-01B2
----
9026-16079-02B3 TFU 313300007
Associated P/N : ----
No
17Part A : page Revision 29
Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART A : Failure Messages
ATA Filter
313355 DFDR PLAYBACK NO MAINTENANCE ACTION. RECOMMENDED STEP: EMBODY VSB SFIM FDIU/360-31-090
FDIU ED43A1D3
----
ED43A1D4
Associated P/N : SSFDR
No
313634 NO DMU DATA (INTM) No Maintenance Action required DMU 795040-30-001
----Associated P/N : ----
No
313652 DAR No Maintenance Action required DMU 795040-30-001
----
795040-31-002
Associated P/N : ----
No
313652 DAR TAPE LOW No Maintenance Action required DMU 795040-30-001
----
795040-30-002
Associated P/N : ----
No
316322 DU EWD(2WK1)/ECP(2WM) No maintenance action required if no logbook complaint. EIS II Software
SXT3CE2SA0420
SXT4EE2SA050A
----
TBD
Associated P/N : ----
Yes
18Part A : page Revision 29
Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART A : Failure Messages
ATA Filter
316322 DU ND CAPT(3WK1)/ND CAPT POT(8WK1)
No maintenance action required if no logbook complaint. EIS II Software
SXT3CE2SA0420
SXT4EE2SA050A
----
TBD
Associated P/N : ----
Yes
316322 DU ND FO(3WK2)/ND FO POT(8WK2)
No maintenance action required if no logbook complaint. EIS II Software
SXT3CE2SA0420
SXT4EE2SA050A
----
TBD
Associated P/N : ----
Yes
316322 DU PFD CAPT(1WK1)/PFD CAPT POT(7WK1)
No maintenance action required if no logbook complaint. EIS II Software
SXT3CE2SA0420
SXT4EE2SA050A
----
TBD
Associated P/N : ----
Yes
316322 DU PFD FO(1WK2)/PFD FO POT(7WK2)
No maintenance action required if no logbook complaint. EIS II Software
SXT3CE2SA0420
SXT4EE2SA050A
----
TBD
Associated P/N : ----
Yes
316322 DU SD(2WK2)/ECP(2WM) No maintenance action required if no logbook complaint. EIS II Software
SXT3CE2SA0420
SXT4EE2SA050A
----
TBD
Associated P/N : ----
Yes
19Part A : page Revision 29
Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART A : Failure Messages
ATA Filter
316334 AFS:CHK DMCi-FMGCj CKT(i=1 or 2) (j=1 or 2)
NO MAINT. ACTION required if no log book complaint FMGC ALL P/N
----
TBD
Associated P/N : ----
No
316334 HUDC : CHECK DMC1 NO MAINT. ACTION HUDC 96154334-1
----
96154334-2 TFU 343500003
Associated P/N : ----
No
316334 HUDC : NO DMC1 DATA NO MAINT. ACTION HUDC 96154334-1
----
96154334-2 TFU 343500003
Associated P/N : ----
No
323171 CHECK LGCIU-PHC3 NO MAINT. ACTION if triggered in FWC flight phase 06 or 07 and if not associated with fault message "L/G EXT PROX SNSR 24GA(25GA) TGT POS"
BSCU E21327001
E21327003
----
TBD
Associated P/N : ----
No
323171 LGCIUi 05GAi NO MAINT. ACTION LGCIU 664700500A4A
----
664700500A4B TFU 323134043
Associated P/N : ----
No
20Part A : page Revision 29
Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART A : Failure Messages
ATA Filter
324224 SDACi:NO DATA FROMBSCU1+2
Wrong ATA REF. Should be 324234 instead. All FWC in BASIC configuration (Pre Mod 24159) are affected (E2, E3, E4, F2).
FWC 350E017271616
350E018301919350E018312020350E053020x0x
(x=3, 4, 6)
----
FWC STD H2F3
(Target: Oct 2005)
Associated P/N : ----
No
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).
FWC 350E017271616
350E018301919350E018312020350E053020x0x
(x=3, 4, 6)
----
FWC STD H2F3
(Target: Oct 2005)
Associated P/N : ----
No
324234 BSCU(10GG) NO MAINT. ACTION if the associated TSD shows fault code 530 AND if triggered on ground during Engine start or Engine shut-down AND A/C equipped with BSCS EMM (mod 26925).
BSCU E21327003 TBD
Associated P/N :
No
324234 SDAC : NO DATA FROM BSCU NO MAINT. ACTION if no Log Book complaint SDAC 35-0E5-1510-22
35-0E5-1611-22
----
35-0E5-1513-31
Associated P/N : ----
No
324234 SDAC : NO DATA FROM TPIU NO MAINT. ACTION if no Log Book complaint SDAC 35-0E5-1510-22
35-0E5-1611-22
----
35-0E5-1513-31
Associated P/N : ----
No
21Part A : page Revision 29
Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART A : Failure Messages
ATA Filter
324334 ABCU(95GG)/BRK SELECTOR VALVE(23GG)
NO MAINT. ACTION if triggered in flight phase 01 or 02 on A/C equipped with BSCS EMM (mod 26925)
BSCU E21327003
----
TBD
Associated P/N : ----
No
324418 SDACi: LH Y BRK PRESSXDCR 63GG. (i=1 OR 2)
A) NO MAINT ACTION if the fault message occurs in phase 06 and is not associated with the fault message "BRK ALTN PRESS TRANSDUCER 101GG" Source BSCU. B)Wrong FIN number coded in FWC BITE message. Should be 101GG instead.
FWC 350E053020606
(FWC H2F2)
Post MOD 26925
FWC H2F3
P/N TBD
Associated P/N : BSCU
Yes
324418 SDACi:RH Y BRK PRESSXDCR 62GG. (i=1 OR 2)
A) NO MAINT ACTION if the fault message occurs in phase 06 and is not associated with the fault message "BRK ALTN PRESS TRANSDUCER 100GG" Source BSCU. B) Wrong FIN number coded in FWC BITE message. Should be 100GG instead.
FWC 350E053020606
(FWC H2F2)
Post MOD 26925
FWC H2F3
P/N TBD
Associated P/N : BSCU
Yes
325151 STEERING ELECTROHYDRAULIC MODULE 6GC
No MAINT. ACTION if fault message triggered after Landing Gear free fall extension and code 58 (code 6A on A320 with BOGIE) has been recorded in BSCU BITE.
BSCU C202163 SERIES
C202452 SERIES
PRE MOD 26925
N/A
Associated P/N : ----
No
325151 STEERING ELECTRO-HYDMODULE (6GC)
No MAINT. ACTION if fault message triggered after Landing Gear free fall extension and code 654 has been recorded in BSCU BITE.
BSCU E21327 SERIES
PRE MOD 26925
N/A
Associated P/N : ----
No
22Part A : page Revision 29
Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART A : Failure Messages
ATA Filter
341119 AOA SENSOR 3FP1(2,3) Associated with the ECAM warning ANTI ICE CAPT (F/O,STBY) AOA.
PHC 1663214-200
----
1663214-301 TFU 303100016 / TFU 303134006 / TSM ATA 30
Associated P/N : ----
No
341119 AOA SNSRi (3FPi)/ADIRUi(1FPi)
NO MAINTENANCE ACTION if appears after an AOA test.
ADIRU 465020-0303-0308
----
465020-0303-0309 TFU 341000017
Associated P/N : ----
No
341234 ADIRU1+3 (1FP1+3)BUS IR/WXR1 (1SQ1)
If no logbook complaint, do not remove the RTA-4B from the aircraft. Power cycling the RTA-4B or executing the Radar Test on the MCDU will clear the nuisance fault if it continues to be displayed in Ground Scanning.
RTA-4B 066-50008-0405
066-50008-0407
----
066-50008-0409
Associated P/N : ----
No
341234 ADIRUi+3(1FPi+3) ADRBUS/WXRi(1SQi) (i = 1 or 2)
No maintenance action required if no logbook complaint. RADAR 822-1710-201
822-1710-202
----
822-1710-203
Associated P/N : ----
Yes
341234 AFS:ADIRU 1/2/3 DISAGREE NO MAINT. ACTION if not associated to any Message in the ADIRU Bite
FAC B397AAM0507/0508
B397BAM0406/0407
----
B397BAM0509
B397AAM0509B397CAM0101
TFU 229100009
Associated P/N : ----
Yes
23Part A : page Revision 29
Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART A : Failure Messages
ATA Filter
341234 AFS:ADIRU 1/2/3 DISAGREE NO MAINT.ACTION IF NO LOGBOOK COMPLAINT. Pitot Pre SB 34-1122
----
SB 34-1122
(Pitot re-location)
TFU220000012
Associated P/N : ----
No
341234 AFS:ADIRU 1/2/3 DISAGREE No maintenance action if no logbook complaint FAC B397AAM0507
B397AAM0508B397BAM0406B397BAM0407
----
B397BAM0513 TFU 220000012
Associated P/N : ----
Yes
341234 NO ADIRUi DATA CHECKWIRING TO SLT(FLP)i
When this message is followed by 27-51-34 SFCC1(2), 21(22)CV ignore this second message.
SFCC 49117-06
----
49117-07 TFU 275144003
Associated P/N : ----
No
341234 QUALIFIER Di/WXRj (1SQj)(i=1 or 2 and j= 1 or 2)
No maintenance action if no logbook compaint. RADAR 822-1710-201
----
822-1710-202
Associated P/N : ----
No
341234 RADARi: NO DATA FROMADIRU
The fault appears during ground test. Repeat test. If result OK no further MAINT ACTION required.
RADAR 204-1218-0418
204-1218-0421
----
SIL 95-29 Rev.1
Associated P/N : ----
No
24Part A : page Revision 29
Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART A : Failure Messages
ATA Filter
341234 RADARi:NO DATA FROMADIRU
NO MAINT. ACTION if no log book complaint RADAR 622-5132-020
622-5132-1120
----
VSB WRT-701X-34-68
VSB WRT-701X-34-77
Associated P/N : ----
No
343522 HUD OHU NO MAINT. ACTION if no log book complaint. HUDC 96154334-1
96154334-2
----
V65 SOFTWARE TFU 343500003
Associated P/N : ----
Yes
343631 AFS : ILS i NO MAINT. ACTION if occurs at the end of the flight FMGC All P/N
----
TBD
Associated P/N : ----
Yes
343631 FWCi :NO DATA FROMILSi
NO MAINT ACTION if occurs in flight phases 02 and 07. ILS 622-9738-020
----
622-9788-041
Associated P/N : ----
Yes
343631 ILS i RECEIVER NO MAINT. ACTION if no Log book complaint ILS 204-1230-3518
----
204-1230-3521
204-1230-3532
TFU 343600004
Associated P/N : ----
Yes
25Part A : page Revision 29
Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART A : Failure Messages
ATA Filter
343631 ILSi NO MAINT. ACTION if occurs in flight phase 02. ILS 622-9738-020
622-9738-041
----
NONE
Associated P/N : ----
Yes
343631 ILSi (2RTi) NO MAINT. ACTION required if no logbook complaint. When receiver not tuned to any station, a self test is performed and this spurious message may be triggered.
ILS 622-9738-041
622-9738-020
----
Collins VSB
ILS-720-34-11ILS-900-34-6
Associated P/N : ----
No
343631 MMR1 (40RT1)/GPWC (1WZ) NO MAINT. ACTION required EGPWS 965-0976-
003-102-102
----
965-0976-
003-206-206
Associated P/N : ----
Yes
343676 ILSi RECEIVER Ref TSM task 34 36 00 810 801 associated to ILS fault "34 36 31 ILSi RECEIVER"
ILS 622-9738-020
----
622-9738-041
Associated P/N : ----
No
343731 NO MLS (i) DATA No maintenance action if no logbook complaint AMU 3514xS01
----
TBD
Associated P/N : ----
Yes
26Part A : page Revision 29
Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART A : Failure Messages
ATA Filter
344111 RADAR 1 ANTENNA NO MAINT. ACTION if no log book complaint RADAR 622-5132-020
622-5132-120
----
VSB WRT-701X-34-68
VSB WRT-701X-34-77
Associated P/N : ----
No
344111 RADAR i ANTENNA NO MAINT ACTION if nologbook complaint RADAR 204-1217-0418
204-1217-0421
----
VSB RTA-4A-34-160
Rev.1
TFU 344100007
Associated P/N : ----
No
344111 RADAR i ANTENNA NO MAINT ACTION if message recorded immediately after engine start (this item concerns only 2 airlines)
RADAR MI 585306-402
----
TBD NONE
Associated P/N : ----
No
344111 WXR ANTENNA(11SQ) No maintenance action required if no logbook complaint. RADAR 822-1710-201
----
822-1710-202
Associated P/N : ----
No
344112 RADAR 1 CONTROL UNIT NO MAINT. ACTION if no log book complaint RADAR 622-5132-020
622-5132-120
----
VSB WRT-701X-34-68
VSB WRT-701X-34-77
Associated P/N : ----
No
27Part A : page Revision 29
Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART A : Failure Messages
ATA Filter
344112 WXR CTL PNL(3SQ)/WXRi(1SQi) (i = 1 or 2)
NO MAINT. ACTION if recorded during Engine Start (flight phase 02) or during switching from WXR1 to WXR2 and no associated cockpit effect.
RADAR 822-1710-201
----
822-1710-202
Associated P/N : ----
No
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 Task 31-60-00-740-002 "EIS Input TEST". If test ok, the WXR/DMC interface works properly and the WXR transceiver units should not be removed. If the test fails, apply corresponding TSM procedure 34-41-00-810-8x "Loss of Weather Radar Channel j bus identified by the EIS i".
RADAR 622-5132-622
622-5132-623
----
TBD
Associated P/N : ----
No
344133 RADAR 1 TRANSCEIVER NO MAINT. ACTION if no log book complaint RADAR 622-5132-020
622-5132-120
----
VSB WRT-701X-34-68
VSB WRT-701X-34-77
Associated P/N : ----
No
344133 RADAR i TRANSCEIVER NO MAINT ACTION if message recorded immediately after engine start (this item concerns only 2 airlines).
RADAR MI 585306-402
----
TBD NONE
Associated P/N : ----
Yes
344133 RADARi TRANSCEIVER NO MAINT. ACTION if no log book complaint RADAR 204-1218-0418
204-1218-0421
----
VSB RTA-4A-34-160
Rev.1
TFU 344100007
Associated P/N : ----
No
28Part A : page Revision 29
Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART A : Failure Messages
ATA Filter
344133 WXRi(1SQi)(i=1 or 2)
No Maint. Action if fault msg recorded in the PFR without cockpit effect and is associated with specific TSD (final 4 digits "0000"). The fault msg may be triggered if radar selected OFF and Pred Windshear scanning automatically activated during take-off or approach.
RADAR 066-50008-0405
066-50008-0407
----
066-50008-0409
Associated P/N : ----
No
344133 WXRi(1SQi)(i= 1 or 2)
No maintenance action if no logbook complaint. RADAR 822-1710-201
----
822-1710-202
Associated P/N : ----
No
344137 WXR MOUNTING TRAY(5SQ)/WXRi(1SQi) (i = 1 or 2)
No maintenance action required if no logbook complaint. RADAR 822-1710-201
----
822-1710-202
Associated P/N : ----
No
344233 RA1 (2SA1) +RA2 (2SA2) /WXR1 (1SQ1)
If no logbook complaint, do not remove the RTA-4B from the aircraft. Power cycling the RTA-4B or executing the Radar Test on the MCDU will clear the nuisance fault if it continues to be displayed in Ground Scanning.
RADAR 066-50008-0405
066-50008-0407
----
066-50008-0409
Associated P/N : ----
No
344233 RA1(2SA1)+RA2((2SA2)/WXRi (1SQi) (I=1 or 2)
NO MAINT. ACTION if recorded during Engine Start (flight phase 02) or during switching from WXR1 to WXR2 and no associated cockpit effect.
RADAR 822-1710-201
----
822-1710-202
Associated P/N : ----
No
29Part A : page Revision 29
Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART A : Failure Messages
ATA Filter
344300 DMC(i): NO TCAS DATA(i = 1 or 2)
No maintenance action required if no logbook complaint and if TCAS BITE is OK.
TCAS ACSS
7517900-10002
7517900-10003
----
TBD TFU 34.43.00.011
Associated P/N : ----
No
344300 DMC(i): NO TCAS DATA(i = 1 or 2)
No maintenance action required if no logbook complaint and if TCAS BITE is OK.
TCAS HONEYWELL
066-50000-1x08
066-50000-2x204066010-903/9044066010-905
940-300-001
----
TBD TFU 34.43.00.011
Associated P/N : ----
No
344300 DMC(i): NO TCAS DATA(i = 1 or 2)
No maintenance action required if no logbook complaint and if TCAS BITE is OK.
TCAS ROCKWELL
622-8971-320
622-8971-322822-1293-322
----
TBD TFU 34.43.00.011
Associated P/N : ----
No
344300 TCAS ARINC 429 NO MAINT ACTION if no logbook complaint. This deviation has been identified.
TCAS 4066010-903
----
4066010-905 TFU 344300006
Associated P/N : ----
No
344300 TCAS UNTRACEABLE NO MAINT ACTION if no log book TCAS complaint. TCAS 4066010-903
----
4066010-905 TFU 344300006
Associated P/N : ----
No
30Part A : page Revision 29
Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART A : Failure Messages
ATA Filter
344333 FWC(i): NO DATAFROM TCAS (i = 1 or 2)
No maintenance action required if no logbook complaint and if TCAS BITE is OK.
TCAS HONEYWELL
066-50000-1x08
066-50000-2x204066010-903/9044066010-905
940-300-001
----
TBD TFU 34.43.00.011
Associated P/N : ----
No
344333 FWC(i): NO DATAFROM TCAS (i = 1 or 2)
No maintenance action required if no logbook complaint and if TCAS BITE is OK.
TCAS ACSS
7517900-10002
7517900-10003
----
TBD TFU 34.43.00.011
Associated P/N : ----
No
344333 FWC(i): NO DATAFROM TCAS (i = 1 or 2)
No maintenance action required if no logbook complaint and if TCAS BITE is OK.
TCAS ROCKWELL
622-8971-320
622-8971-322822-1293-322
----
TBD TFU 34.43.00.011
Associated P/N : ----
No
344333 NO TCAS DATA No maintenance action required if no logbook complaint and if TCAS BITE is OK.
TCAS ROCKWELL
622-8971-320
622-8971-322822-1293-322
----
TBD TFU 34.43.00.011
Associated P/N : ----
No
344333 NO TCAS DATA No maintenance action required if no logbook complaint and if TCAS BITE is OK.
TCAS ACSS
7517900-10002
7517900-10003
----
TBD TFU 34.43.00.011
Associated P/N : ----
No
31Part A : page Revision 29
Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART A : Failure Messages
ATA Filter
344333 NO TCAS DATA No maintenance action required if no logbook complaint and if TCAS BITE is OK.
TCAS ROCKWELL
622-8971-320
622-8971-322822-1293-322
----
TBD TFU 34.43.00.011
Associated P/N : ----
No
344333 NO TCAS DATA No maintenance action required if no logbook complaint and if TCAS BITE is OK.
TCAS HONEYWELL
066-50000-1x08
066-50000-2x204066010-903/9044066010-905
940-300-001
----
TBD TFU 34.43.00.011
Associated P/N : ----
No
344333 NO TCAS DATA No maintenance action required if no logbook complaint and if TCAS BITE is OK.
TCAS ACSS
7517900-10002
7517900-10003
----
TBD TFU 34.43.00.011
Associated P/N : ----
No
344334 ATC(i): NO DATAFROM TCAS (i = 1 or 2)
No maintenance action required if associated to the TCAS fault message "344334 TCAS (1SG)" and if TCAS BITE is OK.
TCAS 066-50000-0203
066-50000-0102066-50000-0208066-50000-0108
----
TPA-81A-34-61 REV2
TPA-81A-34-72TPA-81A-34-75 REV1
TFU 34.43.00.004
Associated P/N : ----
No
344334 ATC(i): NO DATAFROM TCAS (i = 1 or 2)
No maintenance action if no logbook complaint and if TCAS BITE is OK.
TCAS ROCKWELL
622-8971-320
622-8971-322822-1293-322
----
TBD TFU 34.43.00.011
Associated P/N : ----
Yes
32Part A : page Revision 29
Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART A : Failure Messages
ATA Filter
344334 ATC(i): NO DATAFROM TCAS (i = 1 or 2)
No maintenance action if no logbook complaint and if TCAS BITE is OK.
TCAS HONEYWELL
066-50000-1x08
066-50000-2x204066010-903/9044066010-905
940-300-001
----
TBD TFU 34.43.00.011
Associated P/N : ----
Yes
344334 ATC(i): NO DATAFROM TCAS (i = 1 or 2)
No maintenance action if no logbook complaint and if TCAS BITE is OK.
TCAS ACSS
7517900-10002
7517900-10003
----
TBD TFU 34.43.00.011
Associated P/N : ----
Yes
344334 TCAS (1SG) No maintenance action required if no logbook complaint and if TCAS BITE is OK.
TCAS 066-50000-0203
066-50000-0102066-50000-0108066-50000-0208
----
TPA-81A-34-61-REV2
TPA-81A-34-72TPA-81A-34-75 REV1
TFU 34.43.00.004
Associated P/N : ----
No
344334 TCAS(1SG) No maintenance action required if no logbook complaint and if TCAS BITE is OK.
TCAS HONEYWELL
066-50000-1x08
066-50000-2x204066010-903/9044066010-905
940-300-001
----
TBD TFU 34.43.00.011
Associated P/N : ----
No
344334 TCAS(1SG) No maintenance action required if no logbook complaint and if TCAS BITE is OK.
TCAS ROCKWELL
622-8971-320
622-8971-322822-1293-322
----
TBD TFU 34.43.00.011
Associated P/N : ----
No
33Part A : page Revision 29
Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART A : Failure Messages
ATA Filter
344334 TCAS(1SG) No maintenance action required if no logbook complaint and if TCAS BITE is OK.
TCAS ACSS
7517900-10002
7517900-10003
----
TBD TFU 34.43.00.011
Associated P/N : ----
No
345000 MODE S i NO MAINT ACTION if no logbook complaint. TCAS 4066010-903
----
4066010-905 TFU 344300006
Associated P/N : ----
No
345133 AFS:DMEi NO MAINT ACTION if no log book complaint FMGC PEGASUS
C13042xA01
----
TBD
Associated P/N : ----
Yes
345133 AFS:DMEi Due to A/C out of emitter range. No Maint. Action if no Log Book complaint.
DME 622-4540-023
FMGC LEGACY
VSB DME 700-34-33
VSB DME 700-34-27
TFU 345100008
Associated P/N : B398BxM0xxx
Yes
345133 DME i TRANSCEIVER NO MAINT. ACTION if no log book complaints DME 622-4540-020
622-4540-021622-4540-022622-4540-023
----
VSB DME-700-34-27 TFU 345100008
Associated P/N : ----
No
34Part A : page Revision 29
Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART A : Failure Messages
ATA Filter
345212 ATC CTL PNL(2SH) This misbehavior will be corrected at the next standard of P/N 7517800-10005 and new ATC CTL PNL(3SH)
TCAS 7517800-10005
----
7517800-10005
Associated P/N : ----
No
345233 ATCi (1SH1) /TCAS (100SG) source TCAS (i = 1 or 2)
No maintenance action if not associated to ECAM WARNING "NAV TCAS FAULT". 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).
T2CAS 9000000-10110
----
TBD
Associated P/N : ----
No
345233 ATCi (1SH1) / TCAS (1SG)source TCAS (i = 1 or 2)
No Maint. Action if not associated to ECAM WARNING "NAV TCAS FAULT". 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).
TCAS 7517900-10002
7517900-10003
----
TFU 34.43.00.011
Associated P/N : ----
No
345233 NO ATC i DATASource CFDS (i = 1 or 2)
No maintenance action is required if no logbook complaint.
ATC 751-7800-10002
751-7800-10005
----
TBD
Associated P/N : ----
Yes
345233 QUALIFIER Ci/WXRj (1SQj)(i = 1 or 2 and j = 1 or 2)
No maintenance action if no logbook complaint. RADAR 822-1710-201
----
822-1710-202
Associated P/N : ----
No
35Part A : page Revision 29
Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART A : Failure Messages
ATA Filter
345331 ADF i RECEIVER NO MAINT. ACTION if no log book complaint. ADF 622-5222-020
----
VSB ADF-700-34-20
VSB ADF-700-34-21VSB ADF-700-43-27
Associated P/N : ----
No
345331 NO ADF(i) DATA No maintenance action when ADF 1 or/and 2 not installed on the aircraft.
CFDIU
----
N/A
Associated P/N : ----
Yes
345531 AFS : VOR i NO MAINT. ACTION if no logbook complaint FMGC All P/N
----
TBD
Associated P/N : ----
Yes
345531 VOR i : VOR RECEIVER NO MAINT ACTION if no logbook complaint VOR 622-5220-020
----
VSB 700-34-10 Rev 1
VSB 700-34-19
TFU 345500009 / TFU 345500013
Associated P/N : ----
No
345572 VOR i RECEIVER NO MAINT. ACTION if no log book complaint. VOR 204-1231-3610
----
VSB RVA-36A-34-54 TFU 345500010
Associated P/N : ----
No
36Part A : page Revision 29
Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART A : Failure Messages
ATA Filter
361134 SDAC:NO DATA FROM BMCi NO MAINT. ACTION if no logbook complaint SDAC 35-0E5-1510-22
35-0E5-1611-22
----
350E5-1513-31
Associated P/N : ----
No
383100 CHECK LAV (X) OR CHECKVAC LINE LEAKAGE
Disconnect 42MG XDCR, then, the spurious message will disappear
VSC 14404-001-1
----
14404-011A
SB 38-1027
TFU 383100003 / TSM ATA 38 / VSB 14404-38-01
Associated P/N : ----
No
383100 LIQD LVL XMTR (40MG)AND LIQD LVL SNSR (41MG)
The system operation can be checked on ground by using the MCDU toilet ground report or by checking the FAP Water/Waste page.
CIDS DIR
Z064H000030D
Z064H000030EZ064H000030F
----
Z064H000031A
Z064H000031B
TFU 38.31.00.026
Associated P/N : ----
Yes
383134 VSC NO MAINT. ACTION VSC 14404-011A
----
14404-011B TFU 38 31 00 022 SB 38-1044 REV2 VSB 14440403802
Associated P/N : ----
Yes
383141 TOILET ASSY LAV i(with i = A, D, E, or F)
The system operation can be checked on ground by using the MCDU toilet ground report or by checking the FAP Water/Waste page.
CIDS DIR
Z064H000030D
Z064H000030E
----
Z064H000031A
Z064H000031B
TFU 38.31.00.026
Associated P/N : ----
No
37Part A : page Revision 29
Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART A : Failure Messages
ATA Filter
383162 LIQD LVL XMTR (40MG) The system operation can be checked on ground by using the MCDU toilet ground report or by checking the FAP Water/Waste page.
CIDS DIR
Z064H000030D
Z064H000030EZ064H000030F
----
Z064H000031A
Z064H000031B
TFU 38.31.00.026
Associated P/N : ----
Yes
383168 DIFF PRESS XDCR NO MAINT. ACTION if 42MG XDCR has been disconnected.
VSC 14404-001-1
----
14404-011A
SB-38-1027
TFU 383100003 / TSM ATA 38
Associated P/N : ----
No
492318 LCDT Sensor P29 No MAINT. ACTION ECB 4500001
4500001A4500001B4500003G
APS 3200
4500003H AIRBUS SB: A320-49-1061
Associated P/N : APU
Yes
493211 FUEL CTL UNIT P19 NO MAINT. ACTION if no logbook complaint ECB 304817-1
36-300
304817-2 S/B A320-49-1053
Associated P/N : GTCP
No
496134 SDAC : NO DATA FROM ECB NO MAINT. ACTION if no Log Book complaint (GTCP36.300)
SDAC 35-0E5-1510-22
35-0E5-1611-22
----
35-0E5-1513-31
Associated P/N : ----
No
38Part A : page Revision 29
Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART A : Failure Messages
ATA Filter
499414 OIL PRESS SW P14 NO MAINT. ACTION if no logbook complaint ECB (GTCP 36-300)
304817-1
----
304817-2
Associated P/N : ----
No
499651 APU OIL HEATER(8093KM) NO MAINT. ACTION required on A/C post SB 49-1026 and APU 36-300 pre Honeywell VSB 49-6702 and ECB P/N 3888394-230300 or ECB P/N 304817-1 or ECB P/N 304817-2
APU 3800278-2
3800278-33800278-4
----Associated P/N : ----
No
520000 DOOR BTL XY/DEU B (300RHZ) with X=1, 3 or 4 and Y=R or L and Z=1, 6 or 8.
No maintenance action required. CIDS DIR
Z064H000030F
----
Z064H000031A
Z064H000031B
Associated P/N : ----
No
731150 FRV(CLOSED),J7(J8),ECUDuring FADEC motoring test
NO MAINTENANCE ACTION IF ECU 5.BE or 5.DE not fitted on A/C.
ECU 1820M89P02
1820M36P021820M88P021820M87P02
----
SB 73-1034
SB 73-1037
TFU 732900033
Associated P/N : ----
No
732160 DMCi:NO ECUi A(B) DATA No Maint. Action if it occurs in phase 02 at the end of an engine run (80KTS not reached) or after any FADEC reset.
ECU ALL P/N
DMC (EIS I)
N/A
Associated P/N : ----
Yes
39Part A : page Revision 29
Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART A : Failure Messages
ATA Filter
732160 ECU(Ei-4000KS)(i=1 or 2)
No Maint. Action if it occurs in phase 02 at the end of an engine run (80KTS not reached) or after any FADEC reset.
DMC EIS II Soft
SXT3F-E2SA-0410
SXT3C-E2SA-0420
CFM ENGINE
TBD
Associated P/N : ----
Yes
732234 DMCi: NO EECi A(B) DATA No Maint. Action if it occurs in phase 02 at the end of an engine run (80KTS not reached) or after any FADEC reset.
EEC ALL P/N
DMC (EIS I)
N/A
Associated P/N : ----
Yes
732234 EEC(Ei-4000KS)(i=1 or 2)
No Maint. Action if it occurs in phase 02 at the end of an engine run (80KTS not reached) or after any FADEC reset.
DMC EIS II Soft
SXT3F-E2SA-0410
SXT3C-E2SA-0420
IAE/PW ENGINE
TBD
Associated P/N : ----
Yes
752210 LPTC VLV,HMUDuring FADEC motoring test
No maintenance action if ECU 5.BE or 5.DE not fitted on A/C.
ECU 1820M89P02
1820M36P021820M88P021820M87P02
----
SB 73-1034
SB 73-1037
TFU 732900033
Associated P/N : ----
No
752420 ECU AIR,J7(8), ECU Must be disregarded if CFMI S/B 72-436 AIRBUS S/B 71-1014 embodied on the aircraft.
ECU 1459M55P15
1459M55P161519M83P021519M83P03
----
1459M55P17
1519M83P041820M27P01
Associated P/N : ----
No
40Part A : page Revision 29
Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART A : Failure Messages
ATA Filter
783100 HC/PROX SW/T/R UP ACT i Associated with Maint. Status Eng I FADEC. No Maint. Action if recorded during phase 07 or 08 and if there is no crew report.
EEC SCN12C
----
SCN12D TFU 783100080
Associated P/N : ----
No
793311 QUALIFIER Bi/WXRj (1SQj)(i=1 or 2 and j= 1 or 2)
NO MAINT. ACTION if recorded during Engine Start (flight phase 02) or during switching from WXR1 to WXR2 and no associated cockpit effect.
RADAR 822-1710-201
----
822-1710-202
Associated P/N : ----
No
793315 SDACi:ENG2 OIL PRESSXMTR 4004EN (i=1 or 2), Source ECAM 1 or ECAM 2.
Wrong FIN number. Should be 4003EN instead. All FWC in BASIC configuration (Pre Mod 24159) are affected (E2, E3, E4, F2).
FWC ALL P/N
----
FWC Std H2F3
(Target: Oct 2005)
Associated P/N : ----
No
793316 CHECK N4 BRG SCAV PRESSXMTR CIRCUIT 4005 EN
NO MAINT. ACTION if EIU Ground Scanning result is RTOK
EIU All P/N (IAE)
----
3957905004
3957905005
TFU 793316001
Associated P/N : ----
No
793415 CHECK OIL PRESS SWITCH3EN(i)
No maintenance action is required if no logbook complaint when the message is recorded in the PFR in flight phase 2 or phase 9.
TPIU 1058-34
----
TBD
Associated P/N : ----
Yes
41Part A : page Revision 29
Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART A : Failure Messages
ATA Filter
XXXXXX ADF i : NO DATAFROM CONTROL SOURCE
NO MAINT. ACTION ADF 622-5222-020
204-1168-7513
B401ACM0404
VSB ADF-700-34-21
VSB DFA-75A-34-49VSB ADF-700-34-27
TFU 345300006 / TFU 345300007
Associated P/N : CFDIU
Yes
XXXXXX DME : NO DATA FROM CONTROL SOURCE
NO MAINT. ACTION DME 9599-614-03105
----
VSB TDM-709-34-012
Associated P/N : ----
Yes
XXXXXX ILS i : NO DATA FROMCONTROL SOURCE
NO MAINT. ACTION ILS 20412303518
B401ACM0404
VSB RIA-35A-34-41 TFU 343600004
Associated P/N : CFDIU
No
XXXXXX VHFi:NO DATA FROMCONTROL SOURCE
NO MAINT. ACTION VHF 622-5219-020
B401ACM0404
VSB VHF-700-23-30 TFU 231200007
Associated P/N : CFDIU
No
XXXXXX VOR i : NO DATAFROM CONTROL SOURCE
NO MAINT. ACTION (mainly due to FMS resets). VOR 622-5220-020
20412313610
B401ACM0404
VSB VOR-700-34-10
VSB RVA-36A-34-54
TFU 345500005 / TFU 345500008
Associated P/N : CFDIU
Yes
42Part A : page Revision 29
Warning message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART B : PFR Warning Messages
ATA Filter
2131 CAB PR LO DIFF PR NO MAINT. ACTION if it occurs after a rapid flight profile change
CPC 902215702-7902215702-8
----
9022-15702-10 TFU 213100005
Associated P/N : ----
Yes
2131 CAB PRESS SYST i FAULT If this warning occurs on ground with ADIRS "OFF", Select ADIRS "ON". If the warning still present, ref TSM
CPC 902215702-7
----
902215702-8 TFU 213134005
Associated P/N : ----
No
2151 PACKi
(Maintenance Status)
Associated to P1(2) FLOW CTL VALVE NO MAINT. ACTION if Bite test OK
FCV 751A0000-06
----
751A0000-07 TFU 215151004
Associated P/N : ----
No
2161 AIR PACK 1+2 FAULT NO MAINT ACTION if it occurs at the flight beginning (PHASE 03 or 04).
PC ALL P/N
----
N/A
Associated P/N : ----
Yes
1Part B : page Revision 29
Warning message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART B : PFR Warning Messages
ATA Filter
2161 AIR:PACK i REGUL FAULT When not associated with any maintenance message, check all sensors peripheral to the pack controler.
PC All P/N
----
TFU 216134003 / SIL 21-049
Associated P/N : Sensor
No
2161 TEMP CTL 1 (or 2)
(Maintenance Status)
NO MAINT. ACTION if associated with fault message "237334 CIDS2(102RH) Source TEMP CTL". Status problem of a discrete label computed by the CIDS2 and used by ACSC 1 and 2.
ACSC 1803A0000-03
----
1803B0000-01 SB A320-21-1149 / VSB 1803A-21-02
Associated P/N : ----
No
2163 AFT(FWD) CAB DUCT OVHT Check Temp. sensor output resistance ZC All P/N
----
N/A TFU 216318001 / SIL 21-049
Associated P/N : ----
No
2163 CKPT DUCT OVHT Check Temp. sensor output resistance ZC All P/N
----
N/A TFU 216318001 / SIL 21-049
Associated P/N : ----
No
2Part B : page Revision 29
Warning message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART B : PFR Warning Messages
ATA Filter
2200 AUTO FLT A/THR OFF Configuration Warning FMGC All P/N
----
N/A N/A
Associated P/N : ----
Yes
2200 AUTO FLT AP OFF Configuration Warning FMGC All P/N
----
N/A N/A
Associated P/N : ----
Yes
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
FAC B397AAM0507/0508B397BAM0406/0407
----
B397BAM0509 TFU 226600004 / AMM ATA 34.13.00 pBlock 501
Associated P/N : ----
No
2200 YAW DAMPER SYS NO MAINT. ACTION if occurs at Engine start during strong wind conditions. Recentering the Yaw damper before Engine start with Electric Pump will avoid the message.
FAC B397AAM0507/0508B397BAM0406/0407B397BAM0508/0509B397CAM0101/0102
B397AAM0509/0510
----
B397BAM0510 TFU 226300005
Associated P/N : ----
No
3Part B : page Revision 29
Warning message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART B : PFR Warning Messages
ATA Filter
2300 COM SATCOM FAULT No. Maint. Action if ECAM WARNING triggered when ADIRU 1+2+3 OFF
DMC EIS II Soft
SXT3F-E2SA-0410SXT3C-E2SA-0420
----
EIS II STD S5
Associated P/N : ----
No
2400 ELEC BCL i FAULT NO MAINT. ACTION if no failure message in the PFR, and BCL test thru MCDU is OK.
BCL 35-0L5-1003-0635-0L5-1004-07
----
35-OL5-1005-08
(SB 24-1075)
TFU 243800007 / TFU 243800009/TFU 243800022
Associated P/N : ----
No
2600 SMOKE LAVATORY DET SMOKE If associated with the SDCU fault message "SMOKE DET LAV x" (x is the lavatory affected), ref the maintenance advice field of the TFU 261715003
SMOKE DET
GAI2800-02PAI2830-00
----
TBD TFU 261715003
Associated P/N : ----
No
2615 AVIONICS SMOKE If triggered on ground, associated with amber memo LAND ASAP no evidence of smoke, then FWC1 & FWC2 should be reset in order to clear the latch condition of the warning. This allows to prevent spurious LAND ASAP memo to be triggered at take-off.
SMOKE DET
CG7GO
----
CGDU2000-00 TFU 26 15 15 001
Associated P/N : ----
No
4Part B : page Revision 29
Warning message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART B : PFR Warning Messages
ATA Filter
261600 SMOKE AFT CRG BTL1
FAULT
Maintenance advise: Make sure that when AMM Task 26-16-00-710-001 "Operational test of the cargo-compartment Smoke-detection system by PTT" is performed, the PTT button is hold 20 seconds as recommended and activated only one time.
CIDS DIR Z014H000030C
----
Z014H000131A
Z014H000031A
Associated P/N : ----
No
261600 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" is performed, the PTT button is hold 20 seconds as recommended and activated only one time.
CIDS DIR Z014H000030C
----
Z014H000131A
Z014H000031A
Associated P/N : ----
No
261600 SMOKE FWD CRG BTL1
FAULT
Maintenance advise: Make sure that when AMM Task 26-16-00-710-001 "Operational test of the cargo-compartment Smoke-detection system by PTT" is performed, the PTT button is hold 20 seconds as recommended and activated only one time.
CIDS DIR Z014H000030C
----
Z014H000131A
Z014H000031A
Associated P/N : ----
No
261600 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" is performed, the PTT button is hold 20 seconds as recommended and activated only one time.
CIDS DIR Z014H000030C
----
Z014H000131A
Z014H000031A
Associated P/N : ----
No
5Part B : page Revision 29
Warning message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART B : PFR Warning Messages
ATA Filter
2700 F/CTL ALT LAW IF OCCURS AT ENGINE START,PERFORM ELACs RESET WITH ALL HYDRAULIC SYSTEMS DEPRESSURIZED.
ELAC 3945122502STD L69
----
3945122505 TFU279300040/FCOM 3 02 27
Associated P/N : ----
No
2700 F/CTL ELAC 2 PITCH FAULT At engine start, if associated with "THS ACTR SERVO MOT 1 9CE" maintenance message 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 button reset.
ELAC + THSA
3945122502(ELAC)3945122504(ELAC)9231-4-600 (THSA)
----
3945122505 (ELAC)
9231-5-600 (THSA)
TFU279000028
Associated P/N : ----
No
2700 F/CTL ELAC1(2) FAULT Even if associated with "ELAC1(2)" maintenance message, failure of opposite ELAC may be suspected. Apply TSM procedure.
FCDC115370-105115370-1016
----
N/A TFU 279500039
Associated P/N : ----
No
2700 F/CTL SPD BRK DISAGREE Configuration warning FCDC All P/N
----
N/A
Associated P/N : ----
Yes
6Part B : page Revision 29
Warning message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART B : PFR Warning Messages
ATA Filter
2751 F/CTL If associated with the PFR message "SFCC1(2) FLAP(SLAT)", reset the SFCC.
SFCC 49-170-07
----
AMDT C
49-170-11
TFU 27 51 34 027
Associated P/N : ----
No
275100 F/CTL FLAPS LOCKED If experienced at first A/C power-up when electrical power is powered from batteries ref TFU 275134026 MAINTENANCE ADVICE field.
SFCC 49117-1049170-07
----
Amdt A
49-170-11
TFU 275134026
Associated P/N : ----
No
278100 F/CTL SLATS LOCKED If experienced at first A/C power-up, when electrical power is supplied from batteries ref TFU 27134026 MAINTENANCE ADVICE field
SFCC 49117-1049170-07
----
49-170-11 Amdt A
49-170-11
TFU 275134026
Associated P/N : ----
No
2793 ELAC i PITCH FAULT IF NO MAINTENANCE MESSAGE associated : CHECK the PITCH CHANGE OVER DISCRETES LANE.
FCDC 115370-0105
----
115370-1016
115370-0106
TFU 279300028
Associated P/N : ----
No
7Part B : page Revision 29
Warning message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART B : PFR Warning Messages
ATA Filter
2800 R(L) WING TK LO LVL NO MAINT. ACTION if occurs at beginning of descent.
N/A
----
SB 28-1029 TFU 284615003
Associated P/N : ----
No
281500 FUEL INTERCELL TRANSFER
XFR VALVE (29QM)/((72QM)/(10QP)
If this ECAM message is reported, perform functional BITE test of the ICTVs - FLSS Status (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 the FLSS status and FLSS BITE show NO FAULT.
FQIC
----
TFU 281500009
Associated P/N : ----
No
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.
FQIC
----
TFU 284600009
Associated P/N : ----
No
8Part B : page Revision 29
Warning message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART B : PFR Warning Messages
ATA Filter
2900 BLUE RSVR Should be a warning, as RAT operation can be affected. Will be re-classified.
N/A
----
SB 29-1055 TFU 293400002 / TSM ATA 29/SIL29050
Associated P/N : ----
No
3000 ANTI ICE CAPT (F/O) TAT NO MAINT. ACTION if occurs on ground during wet / snowy / icy weather, or after de-icing/high-press cleaning
RA 9599-607-149329599-607-12333
1663214-200
9599-607-14942
9599-607-12352
TFU 303100017/326100003/344200003
Associated P/N : PHC
No
3000 ANTI ICE CAPT (F/O)PITOT DISREGARD the message if occurs after gear non-retraction. This deviation has been identified and will be cured at the next opportunaty of a new PHC std.
LGCIU 664700500A4B
----
66400500A4D TFU 323173001/323171043
Associated P/N : ----
No
3000 ANTI ICE L(R) WINDOW Occurs when windows Windshield are exposed to the sun in hot and dry atmosphere for more than one hour
WHC 666 4202-2666 4202-3666 4202-4666 4287-0
----
416-00318-001
416-00318-003
TFU 304200004
Associated P/N : ----
No
9Part B : page Revision 29
Warning message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART B : PFR Warning Messages
ATA Filter
3100 CFDIU
(Maintenance Status)
NO MAINT. ACTION if CFDIU power up test result is : CFDIU BITE MEMORY
CFDIU B401ACM0404
----
Amdt A TFU 313234031 / TSM ATA31
Associated P/N : ----
No
3100 DMU
(Maintenance Status)
Associated with the message : CAGA MEMORY FAIL.
DMU 903116243BOBOG0903116243BODOJ0903116243B0B0G1903116243B0D0J1
----
903116243B3B3G4
903116243B3B2G3903116243B3D2J3
TFU 313600013 / TSM ATA 31
Associated P/N : ----
No
and subsequent std
3200 BRAKES BSCU CH(i) FAULT If occurs at engine shutdown, reset the BSCU (FCOM 3.04.32)
BSCU All P/N
----
N/A TFU 32 42 34 041 / FCOM 3.04.32
Associated P/N : ----
No
3200 BRAKES HOT
Configuration warning.
This warning does not reflect a malfunction of the system. Instead, it is triggered to remind the flight crew that take-off is not permitted with brakes hot.
BSCU ALL P/N
----
N/A N/A
Associated P/N : ----
Yes
10Part B : page Revision 29
Warning message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART B : PFR Warning Messages
ATA Filter
3200 L/G SHOCK ABSORBER FAULT NO MAINT. ACTION if occurs on ground during wet / snowy / icy weather, or after de-icing/high-press cleaning
RA 9599-607-149329599-607-12333
----
9599-607-14942
9599-607-12352
TFU 326100003/344200003/344200005
Associated P/N : ----
Yes
3200 LGCIU i FAULT NO MAINT. ACTION if BITE test OK LGCIU 664700500A4A
----
664700500A4B TFU 323134043
Associated P/N : ----
No
3200 LGCIU i FAULT If not LGCIU faut message available in the PFR, refer to the Last Leg Report of the LGCIU
LGCIU 664700500A4C
----
664700500A4D
Associated P/N : ----
No
3400 NAV GPWS FAULT NO MAINT. ACTION if occurs on ground during taxiing or lining-up
ILS 622-9738-020
----
622-9738-041 TFU 344800002
Associated P/N : ----
Yes
11Part B : page Revision 29
Warning message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART B : PFR Warning Messages
ATA Filter
3400 NAV GPWS FAULT NO MAINT. ACTION if occurs on ground during Taxiing or Lining-up
ILS 20412303518
----
20412303521
20412303532
TFU 344800002
Associated P/N : ----
Yes
3400 NAV TCAS FAULT NO MAINT ACTION if TCAS BITE test is OK. If not OK ref TSM.
TCAS 066-50000-0203066-50000-0102066-50000-0208066-50000-0108
----
TPA-81A-3461 REV 2
TPA-81A-34-72TPA-81A-34-75 REV1
TFU 34.43.00.004 & 34.43.00.007
Associated P/N : ----
No
3400 NAV TCAS FAULT NO MAINT ACTION if TCAS BITE test is OK. If not OK ref to TSM.
TCAS 4066010-903
----
4066010-905 TFU 344300006
Associated P/N : ----
No
3410 ADRi
(Maintenance Status)
The MAINTENANCE STATUS may appear after performing the AOA SENSOR test. See maintenance advice given in TFU 34 10 00 017
ADIRU 465020-0303-0308
----
465020-0303-0309 TFU 341000017
Associated P/N : ----
No
12Part B : page Revision 29
Warning message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART B : PFR Warning Messages
ATA Filter
3410 ALTITUDE/AIRSPEED FLAGS
ON PFD WITHOUT ECAM WARNING "NAV ADRi FAULT".
SEE MAINTENANCE ACTIONS I N TFU 341000012
ADIRU HG1150AC05
----
HG1150AC06 TFU341000012
Associated P/N : ----
No
3410 NAV ADR x FAULT If associated to ADM fault message "34 11 17 ADIRUx : NO DATA FROM ADM 19FPx" ref MAINTENANCE ADVICE field of the TFU 341000021
ADM PG1152AC03
----
PG1152AC05 TFU 341000021
Associated P/N : ----
No
3410 NAV ADRx FAULT Associated to ADM fault messages. NO MAINTENANCE ACTION if AIR DATA parameters are valid on ground
ADIRU HG1150AC05
----
MOD 25882 TFU 341000016
Associated P/N : ----
No
3410 NAV ADRx FAULT No associated maintenance message(source ADR).Follow advice given in TFU341000012.
ADIRU HG1150AC05
----
HG1150AC06 TFU 341000012/SB34-1084
Associated P/N : ----
No
13Part B : page Revision 29
Warning message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART B : PFR Warning Messages
ATA Filter
3441 NAV PRED W/S DET FAULT If associated with fault message "DMCi: NO WXRj Chy DATA" (i=1, 2 or 3 ; j=1 or 2), perform SYSTEM TEST of both WXR units. If test ok, do not remove the WXR transceiver units. If the test fails, apply corresponding TSM procedure.
RADAR 622-5132-622622-5132-623
----
TBD
Associated P/N : ----
No
3441 RED WXR FLAG ON PFD
DURING ON/OFF SEQUENCE
NO Maint. Action if WXR RADAR works correctly after power on.
RADAR 204-1218-0418204-1218-0421
----
TFU344100014
Associated P/N : ----
No
3442 NAV RAi FAULT Apply Maintenance action described in TFU344200008 if correlated with both the PFR fault messages "LRAi TRANSCEIVER" and "LRAi ANTENNA"
RA ANTENNA
622-8701-002
----
S/N > 2014 TFU344200008/ SIL 95-01/AOT 34-03
Associated P/N : ----
No
3442 NAV RAi FAULT NO MAINT ACTION if event happens at high altitude (above 8192 ft).
RA 9599-607-14942
----
ERT-530-34-34
ERT-530-34-35
TFU 344200007
Associated P/N : ----
No
14Part B : page Revision 29
Warning message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART B : PFR Warning Messages
ATA Filter
3443 NAV TCAS FAULT
without associated Maintenance Fault message.
If CFDS PFR filter Database contains fault message "ATC1 (1SH1) / TCAS (1SG)" or "ATC2 (1SH2) / TCAS (1SG)", check if either one of these messages has been recorded in TCAS LAST LEG REPORT. Perform Maint. action accordingly.
TCAS 7517900-100027517900-10003
----
TBD TFU 34.43.00.011
Associated P/N : ----
No
3443 NAV TCAS FAULT
without associated Maintenance Fault message.
If CFDS PFR filter Database contains fault message "ATC1: NO DATA FROM TCAS" or "ATC2: NO DATA FROM TCAS", check if either one of these messages has been recorded in TCAS LAST LEG REPORT. Perform Maint. action accordingly.
TCAS 066-50000-1X08066-50000-2X20622-8971-320/322822-1293-322
940-300-001
----
TBD TFU 34.43.00.011
Associated P/N : ----
No
3600 AIR BLEED
(Maintenance Status)
NO MAINT. ACTION if the AIR BLEED MAINTENANCE STATUS is recorded in the PFR in phase 2, without any associated Fault Message.
BMC 785-002-61785-002-7
----
N/A
Associated P/N : ----
No
3800 VSC
(Maintenance Status)
NO MAINT ACTION VSC 14404-011A
----
14404-011B TFU 38 31 00 022 SB 38-1044 REV2 VSB 14440403802
Associated P/N : ----
Yes
15Part B : page Revision 29
Warning message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART B : PFR Warning Messages
ATA Filter
7700 DUAL ENGINE FAILURE NO MAINT. ACTION if occurs on ground during wet / snowy / icy weather, or after de-icing/high press. cleaning.
RA 9599-607-149329599-607-123339599-607-149429599-607-12552
----
9599-607-12352 TFU 326100003/344200003/344200005/344200013
Associated P/N : ----
Yes
7700 ENG BLEED STATUS FAULT NO MAINTENANCE ACTION if occurs at ECU power up
ECU 1459M55P15P16/P17/P18/P191519M83P02P03/P04/P05/P06
1820M27P01/P02/P03
----
1459M55P21
1519M83P081820M27P05
Associated P/N : ----
No
7700 ENG i EIU
(Maintenance Status)
DISREGARD THE MESSAGE if occurs after gear non retraction.
LGCIU 664700500A4B
----
664700500A4C TFU 323173001/323471043
Associated P/N : ----
No
7700 ENG i FADEC A(B) FAULT without the message : FADEC Cleared in some cases by the DMU and/or SDCU replacement.
DMU All P/N
post SB 26-005
VSB/RAI2800-26-005
for the SDCUVSB 795020-31-019
TFU 315300048/TFU 313600041
Associated P/N : SDCU
No
for the DMU
16Part B : page Revision 29
Warning message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART B : PFR Warning Messages
ATA Filter
7700 ENG i REVERSER FAULT No maintenance action is required when occurs during engine shut off phase (Engine master switch off)
ECU 1820M36P071820M89P07
----
N/A OIT/FOT 999.0111/99 TFU 78 31 00 098
Associated P/N : ----
No
7700 ENG OVSPD PROT FAULT Ref to FCOM 3.02.70. EEC All P/N
----
Partially corrected in:
- SCN12C(A1)- SCN10A(A5)
TFU 732000004
Associated P/N : ----
No
7700 ENG TYPE DISAGREE No Maint. Action if A/C is in ECU intermix configuration.
ECU ECU std 5AIECU std 5AI+ECU std 5AHECU std 5AH+
----Associated P/N : ----
No
7700 ENG X RESERVER FAULT if associated to the following fault message "HCU (TRDV), J5 (J6), ECU" at engine start, refer to FCOM TR 477-3 and AMM 71-00-00 page block 500 for alternate start procedure.
ECU 1820M36P061820M89P061820M87P071820M88P07
----
1820M87P09
1820M88P09
TFU 783100085
Associated P/N : ----
No
17Part B : page Revision 29
Warning message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART B : PFR Warning Messages
ATA Filter
7700 ENG1 REVERSER FAULT If this warning occurs during the thrust reverser test (through the ECU menu mode) 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 hydraulic ground card to confirm the fault.
ECU 1459M55Pxx1519M83Pxx1820M27Pxx1820M36P06
1820M89P06
----
1820M87P09
1820M88P091820M36P07
TFU 783100078/783100100
Associated P/N : ----
No
1820M88P07
7700 ENGi FADEC HI TEMP NO MAINT. ACTION if displayed before Engine start when ING/START selected. Disappear after a FADEC reset (>30 sec.)
ECU 1459M55P151519M83P02
----
1459M55P17
1519M83P04
TFU 752400002 / FCOM 3.02.18
Associated P/N : ----
No
7700 ENGi FUEL FILTER CLOG
(i=1 or 2)
No Maint. Action if warning triggered at engine start for less than 5 seconds.
FWC 350E053020606 (H2F2)
----
FWC H2F3
Associated P/N : ----
No
7700 ENGi OVSPD PROT FAULT Refer to FCOM 3.02.70 if it occurs at Engine start-up.
ECU 1459M55P15P16/P171519M83P02P03/P04
1820M27P01
----
1459M55P19
1519M83P061820M27P03
TFU 732110004
Associated P/N : ----
No
18Part B : page Revision 29
Warning message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART B : PFR Warning Messages
ATA Filter
7700 IGN A+B FAULT If appears when selecting Master Lever for Engine start, cycle EIU C/B and attempt a new Engine start.
EIU 3957900611395790061239579050-03
----
Amdt C TFU 743000082 / TFU 743000083
Associated P/N : ----
No
7711 ENG 1 FADEC FAULT No Maint action if no associated EEC fault message recorded in the PFR. This is a FADEC discrepency that occurs on V2500 A5 Engines only
EEC SCN 15SCN 16
----
N/A
Associated P/N : ----
No
7711 ENG 2 FADEC FAULT No Maint action if no associated EEC fault message recorded in the PFR. This is a FADEC discrepency that occurs on V2500 A5 Engines only
EEC SCN 15SCN 16
----
N/A
Associated P/N : ----
No
19Part B : page Revision 29
Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART C : Anomalies related to Class 3 Failure Messages
ATA
PARAMETER 26.1.320.10not available
NO MAINT. ACTION if occurs after alpha-call-up programmation of this parameter when A/C equipped with FWC C4/C5 and IAE engines.
DMU All P/N
35-0E0-1618-7070/71
90311624B3D2J3
FWCAssociated Part :
PARAMETER 26.1.320.01not available
NO MAINT. ACTION if occurs after alpha-call-up programmation of this parameter when A/C equipped with FWC C4/C5 and IAE engines.
DMU All P/N
35-0E0-1618-7070/71
90311624B3D2J3
FWCAssociated Part :
212151 RECIRC FAN i OR SPLY NO MAINT. ACTION ZC 775A0000-05
----
775A0000-06 TFU 216334044
----Associated Part :
212152 MIXER FLAP DRIVE NO MAINT. ACTION ZC 775A0000-05
----
775A0000-06 TFU 216000003
----Associated Part :
215100 FLOW SEL NO MAINT. ACTION ZC 775A0000-05
----
775A0000-06
----Associated Part :
1Part C : page Revision 29
Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART C : Anomalies related to Class 3 Failure Messages
ATA
215218 Pi BLEED TEMP SENSOR NO MAINT. ACTION ZC 775A0000-05
----
775A0000-06 TFU 216334044
----Associated Part :
216111 Pi COMP TEMP SENSOR NO MAINT. ACTION ZC 775A0000-05
----
775A0000-06 TFU 216334044
----Associated Part :
216112 Pi COMP OVHT SENSOR NO MAINT. ACTION ZC 775A0000-05
----
775A0000-06 TFU 216334044
----Associated Part :
216115 Pi OUTLET TEMP SENSOR NO MAINT. ACTION ZC 775A0000-05
----
775A0000-06 TFU 216334044
----Associated Part :
216134 PACKi CONT NO MAINT. ACTION ZC 775A0000-05
759A0000-06/-07
775A0000-06
759A0000-08
TFU 216134001 / TFU 216334044
PCAssociated Part :
2Part C : page Revision 29
Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART C : Anomalies related to Class 3 Failure Messages
ATA
216151 Pi RAM AIR IN ACTUATOR NO MAINT. ACTION ZC 775A0000-05
----
775A0000-06 TFU 216334044
----Associated Part :
216152 PiRAM AIR OUT ACTUATOR NO MAINT. ACTION ZC 775A0000-05/-06/-07
----
775A0000-08 TFU 216334044
----Associated Part :
216153 TURBINE BYPASS VALVE NO MAINT. ACTION ZC 775A0000-05
----
775A0000-06 TFU 216334044
----Associated Part :
216315 TEMP SENSOR FWD (AFT)CAB DUCT I
NO MAINT. ACTION ZC 775A0000-05
----
775A0000-06 TFU 216334044
----Associated Part :
216315 TEMP SENSOR COCKPITDUCT I
NO MAINT. ACTION ZC 775A0000-05
----
775A0000-06 TFU 216334044
----Associated Part :
3Part C : page Revision 29
Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART C : Anomalies related to Class 3 Failure Messages
ATA
216316 TEMP SENSOR R/H (L/H)MIXER I
NO MAINT. ACTION ZC 775A0000-05
----
775A0000-06 TFU 216334044
----Associated Part :
216317 TEMP SENSOR FWD (AFT)CAB I
NO MAINT. ACTION ZC 775A0000-05
----
775A0000-06 TFU 216334044
----Associated Part :
216317 TEMP SENSOR COCKPIT I NO MAINT. ACTION ZC 775A0000-05
----
775A0000-06 TFU 216334044
----Associated Part :
216318 FWD (AFT) CAB DUCTOVHT SENSOR I
NO MAINT. ACTION ZC 775A0000-05
----
775A0000-06 TFU 216334044
----Associated Part :
216318 COCKPIT DUCTOVHT SENSOR I
NO MAINT. ACTION ZC 775A0000-05
----
775A0000-06 TFU 216334044
----Associated Part :
4Part C : page Revision 29
Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART C : Anomalies related to Class 3 Failure Messages
ATA
216334 NO PACK DATA FROM ECS NO MAINT. ACTION if zone cont. -5 fitted on A/C
ZC 775A0000-05
304640-2
775A0000-06
ECBAssociated Part :
216334 ZONE CONT NO MAINT. ACTION ZC 775A0000-05
----
775A0000-06 TFU 216334044
----Associated Part :
216351 TRIM AIR VALVE COCKPIT NO MAINT. ACTION ZC 775A0000-05/-06/-07
----
775A0000-08 TFU 216000004
----Associated Part :
216351 TRIM VALVE FWD (AFT) CAB NO MAINT. ACTION ZC 775A0000-05/-06/-07
----
775A0000-08 TFU 216000004
----Associated Part :
216352 TRIM AIR PRESS VALVE I NO MAINT. ACTION ZC 775A0000-05
----
775A0000-07 TFU 216000003
----Associated Part :
5Part C : page Revision 29
Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART C : Anomalies related to Class 3 Failure Messages
ATA
223334 NO PES MUX DATA No MAINT. ACTION if no cabin crew complaint. This spurious PES Bite message is recorded when PES Bite is disabled in the CAM
CIDS Z010H0005119
Z010H000520A
----
Z010H000521A
----Associated Part :
228334 FMGCx(1CAx) BUS FMACARS/ATSU1(1TX1)
ATSU/ FMGCx protocol deviation when ATSU does receive answer from FMGCx (when in slave condition). No maintenance action required.
ATSU host platform S/W
LA2T0S162C0C0F1
LA2T0S111C1B0F1
----
LA2T0J13000C0F1 TFU 46 00 00 002
----Associated Part :
231233 VDR3(1RC3)/ATSU1(1TX1) NO MAINT. ACTION. ATSU LA2T0J13000C0F1
064-50000-2051
TBD TFU 46.00.00.002
VDRAssociated Part :
233346 SEB 42LFT, 42RGT REF SIL HUGHES 1142000-130-03 NO MAINT. ACTION
PES 1142300-131-xx
----
VSB AVI-93-32 TFU 233300009
----Associated Part :
233346 SEB 41LFT, 41RGT REF SIL HUGHES 1142000-130-03 NO MAINT. ACTION
PES 1142300-131-xx
----
VSB AVI-93-32 TFU 233300009
----Associated Part :
6Part C : page Revision 29
Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART C : Anomalies related to Class 3 Failure Messages
ATA
233600 NO SCU DATA No maintenance action if no cabin crew complaint. This message is recorded when the SCU pin prog 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.
CIDS Z01H0005119
----
Z010H000520A TFU 233300009
----Associated Part :
242100 CHECK GCUi PIN A8A,A9BIDGi PIN B7,B8 WIRING
GPCU 740121A
----
740121B
(S/B 24-1077)
TFU 244100002 / TSM ATA 24 pB 401
----Associated Part :
242200 CHECK FIRE HANDLE i ; RESET GEN i
NO MAINT. ACTION if Fire handle switches actuation not mentionned in the Log Book.
GPCU 740121A
----
740121B
(SB 24-1077)
TFU 244100004
----Associated Part :
242218 TDC AC SENSOR 50 XU i After a GPCU test, Generator 1& 2 P/B switches in the cockpit must be reset. Otherwise, this message will appear after the 2nd GPCU test
GPCU 740121A
740121B
----
Vdr SIL 229 TFU 244100003
----Associated Part :
244134 GPCU NO MAINT. ACTION GPCU 740121A
----
740121B
(SB-24-1077)
----Associated Part :
7Part C : page Revision 29
Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART C : Anomalies related to Class 3 Failure Messages
ATA
284216 CTR CADENSICON 20 QT NO MAINT. ACTION Cadensicon 796-809-5
----
796-809-6 TFU 284234029
----Associated Part :
284216 L(R) CADENSICON 19QTi NO MAINT. ACTION Cadensicon 796-809-5
----
796-809-6 TFU 284234029 / TFU 284234016
----Associated Part :
301151 R(L) WAI FILTER OR VALVE10DL(9DL)
NO MAINT. ACTION ZC 775A0000-05
----
775A0000-07 TFU 216000003
----Associated Part :
303134 PHC 6 DA 1(2,3) PHC 1663214-200
----
1663214-301 TFU 303134006 / TSM ATA 30
----Associated Part :
313234 CFDIU(1TW1)/ATSU1(1TX1) Protocol problem between ATSU and CFDIU. No maintenace action required.
ATSU host platform S/W
LA2T0S162C0C0F1
LA2T0S11C1B0F1
----
LA2T0J13000C0F1 TFU 46 00 00 002
----Associated Part :
8Part C : page Revision 29
Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART C : Anomalies related to Class 3 Failure Messages
ATA
313234 CFDIU(1TW)/WXRi (i = 1 or 2)
No maintenance action required if no logbook complaint.
RADAR 822-1710-201
----
822-1710-202
----Associated Part :
313334 NO CLOCK DATA NO MAINT. ACTION FDIU 9026-16079-01B2
----
9026-16079-02B3
----Associated Part :
313334 NO DMC1 DATA NO MAINT. ACTION FDIU 9026-16079-01B2
----
9026-16079-02B3
----Associated Part :
313334 NO FWCi DATA NO MAINT. ACTION FDIU 9026-16079-01B2
----
9026-16079-02B3
----Associated Part :
313334 NO CFDS DATA NO MAINT. ACTION FDIU 9026-16079-01B2
----
9026-16079-02B3
----Associated Part :
9Part C : page Revision 29
Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART C : Anomalies related to Class 3 Failure Messages
ATA
313334 NO SDAC 1 DATA NO MAINT. ACTION FDIU 9026-16079-01B2
----
9026-16079-02B3
----Associated Part :
313355 DFDR PLAY BACK NO MAINT. ACTION FDIU 9026-16079-01B2
----
9026-16079-02B3 TFU 313300007
----Associated Part :
313355 DFDR PLAYBACK Switch the recorder ground control P/B ON, then enter in the FDIU TEST MENU, check the DFDR status. NO MAINT. ACTION if associated with DFDR OPERATIVE NO PLAY BACK.
FDIU 9026-16079-01B2
9026-16079-01B3
----
9026-16079-02B4 TFU 3133000015
----Associated Part :
315534 SDAC i NO MAINT. ACTION if associated with codes 2000 to 2005
SDAC
35-0E5-1510-22
35-0E5-1611-22
----
35-0E5-1513-31 TFU 315500002
----Associated Part :
315534 SDACx(1WVx)/ATSU1(1TX1) ATSU host platform S/W
LA2T0S111C1B0F1
----
LA2T0J13000C0F1 TFU 46 00 00 002
----Associated Part :
10Part C : page Revision 29
Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART C : Anomalies related to Class 3 Failure Messages
ATA
316234 DMC(1WT2/3)/ATSU(1TX1) Label 316 (wind direction) not properly received by the ATSU. Item under investigation. This deviation has no operational impact as data only needed for ADS applications.
ATSU host platform S/W
LA2T0S162C0C0F1
----
LA2T0J13000C0F1
----Associated Part :
316234 DMC(1WT1/3)/ATSU(1TX1) Label 316 (wind direction) not properly received by the ATSU. Item under investigation. This deviation has no operational impact as data only needed for ADS applications. No maint. Action required.
ATSU host platform S/W
LA2T0S162C0C0F1
LA2T0S111C1B0F1
----
LA2T0J13000C0F1 TFU 46 00 00 002
----Associated Part :
341034 NO DATA FROM ADIRS NO MAINT. ACTION if appears in Phase 1,2 or 10 .
ZC 775A0000-05
----
775A0000-06 TSM ATA 21
----Associated Part :
341200 No access to ZONTPHC1(2,3) INTERFACE
NO MAINT. ACTION PHC 1663214-200
----
1663214-301 TFU 303100013
----Associated Part :
341200 CHECK ADIRU1 (2,3) R STAPHC1(2,3) INTERFACE
NO MAINT. ACTION PHC 1663214-200
----
1663214-301 TFU 303100013
----Associated Part :
11Part C : page Revision 29
Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART C : Anomalies related to Class 3 Failure Messages
ATA
341200 CHECK ADIRU1 (2,3) L STAPHC1(2,3) INTERFACE
NO MAINT. ACTION PHC 1663214-200
----
1663214-301 TFU 303100013
----Associated Part :
341200 CHECK ADIRU 1 (2,3) AOAPHC1(2,3) INTERFACE
NO MAINT. ACTION PHC 1663214-200
----
1663214-301 TFU 303100013
----Associated Part :
341200 CHECK ADIRU 1 (2,3) PITOPHC1(2,3) INTERFACE
NO MAINT. ACTION PHC 1663214-200
----
1663214-301 TFU 303100013
----Associated Part :
341234 ADIRU3(1FP3) ADR BUS/WXRi(1SQi) (i = 1 or 2)
No maintenance action required if no logbook complaint.
RADAR 622-5132-623
----
TBD
----Associated Part :
341234 ADIRU3(1FP3) ADR BUS/WXRi(1SQi) (i = 1 or 2)
No maintenance action required if no logbook complaint.
RADAR 822-1710-201
822-1710-202
----
822-1710-203
----Associated Part :
12Part C : page Revision 29
Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART C : Anomalies related to Class 3 Failure Messages
ATA
341234 ADIRUi(1FPi) IR BUS/WXRj(1SQj) (i = 1, 2 or 3 and j = 1 or 2)
No maintenance action required if no logbook complaint.
RADAR 822-1710-201
822-1710-202
----
822-1710-203
----Associated Part :
344233 RAi(2SAi)/WXRj(i = 1, 2 or 3 and j = 1 or 2)
No maintenance action required if no logbook complaint.
RADAR 822-1710-201
----
822-1710-202
----Associated Part :
345233 ATCi (1SH1) / TCAS (1SG)(i = 1 or 2)
No Maint. Action. CLASS 3 fault message is triggered if ATC transponder in standby.
TCAS 7517900-10002
7517900-10003
--------Associated Part :
462134 ATSU(1TX1)/HFi(3Ri) NO MAINT. ACTION. This message is triggered if there is no ATSU link with HFDR, i.e. (MOD 30625/30331 not installed).
HFDR 822-0990-003
COLLINS HFS900D
----
TBD
----Associated Part :
462134 ATSU1(1TX1) No maintenance action required. ATSU host platform S/W
LA2T0S162C0C0F1
LA2T0S111C1B0F1
----
LA2T0J13000C0F1 TFU 46 00 00 002
----Associated Part :
13Part C : page Revision 29
Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART C : Anomalies related to Class 3 Failure Messages
ATA
710000 BALANCE ENGi N1-NB-VIB NO MAINT. ACTION if no log book entry concerning Engin vibrations.
EVMU 241-211-000-021
----
241-211-000-031 TFU 773234005
----Associated Part :
710000 CHECK ENG i N2-NB-VIB NO MAINT. ACTION if no log book entry concerning Engin vibrations.
EVMU 241-211-000-021
----
241-211-000-031 TFU 773234005
----Associated Part :
715100 J3, ADC1 NO MAINT. ACTION ECU 1459M55P15
1519M83P02
1459M55P16
1519M83P03
----
1459M55P17
1519M83P04
1820M27P01
TFU 732900012
----Associated Part :
715100 J4, ADC2 NO MAINT. ACTION ECU 1459M55P15
1519M83P02
1459M55P16
1519M83P03
----
1459M55P17
1519M83P04
1820M27P01
TFU 732900012
----Associated Part :
732500 CHECK EIU WHC INTERFACE Check/Confirm that EIU/WHC interface is defective
WHC 6664-202-3
----
6664-287-0 TFU 304034002
----Associated Part :
14Part C : page Revision 29
Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART C : Anomalies related to Class 3 Failure Messages
ATA
753100 BLD SNSR,J15,ECU NO MAINT.ACTION IF SB 72-1005 NOT EMBODIED ON THE A/C
ECU 1459M55P17
1519M83P04
1820M27P01
----
SB 72-1005 TFU 732900025
----Associated Part :
753100 VTURI,BLD SNSR,ECU NO MAINT. ACTION IF SB 72-1005 NOT EMBODIED ON THE A/C.
ECU 1459M55P17
1519M83P04
1820M27P01
----
SB 72-1005 TFU 722900025
----Associated Part :
753100 CWB3 SENS, J15 ECU NO MAINT. ACTION if SB 72-1005 not embodied on the A/C
ECU 1459M55P15
1519M83P02
1459M55P16
1519M83P03
----
SB : 72-1005 TFU 732900025
----Associated Part :
753100 WB3 SENS, J15 ECU NO MAINT. ACTION if SB 72-1005 not embodied on the A/C
ECU 1459M55P15
1519M83P02
1459M55P16
1519M83P03
----
SB : 72-1005 TFU 732900025
----Associated Part :
15Part C : page Revision 29
Description of anomaly Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART D : Anomalies related to general use of CFDS
ATA
Sel. valve and LGCIU faults are covered by the fault message: "LGCIU i 05GAi". With the LGCIU std 4D, the following message "LGCIU i 05GAi / L/G SEL VALVE 40G0A" will be triggered in case of valve or LGCIU failure.
LGCIU 664700500A4B
664700500A4C
----
664700500A4D
----Associated Part :
Recording in the PFR of "empty" DMU messages in flight phase 2 or 5. No Maintenance Action required.
DMU 795040-31-002
----
TBD TFU 313600063
----Associated Part :
70 NVM FAULT DATA
NOT RETRIEVABLE
ECU 1459M55P15
1519M83P02
1459M55P16
1519M83P03
----
1459M55P17
1519M83P04
1820M27P01
TFU 732900031
----Associated Part :
21 GND failures report
in last leg report,
ZC 775A0000-05
775A0000-06
----
775A0000-07
----Associated Part :
1Part D : page Revision 29
Description of anomaly Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART D : Anomalies related to general use of CFDS
ATA
21 No A/C ident in the
previous leg report
NO MAINT. ACTION ZC 775A0000-05
----
775A0000-07
----Associated Part :
21 NO ACCEPTABLE FAILURE IN
26
NO MAINT. ACTION if no log book complaint.
ZC 775A0000-05
----
775A0000-06 TFU 216334047
----Associated Part :
21 No access to ZONE CONT
menu when PACK C/B is pulled.
Make sure all C/B are pushed ZC 775A0000-05
----
775A0000-06
----Associated Part :
21 No software number
in P/N of Zone Cont.
NO MAINT. ACTION ZC 775A0000-05
----
775A0000-07
----Associated Part :
2Part D : page Revision 29
Description of anomaly Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART D : Anomalies related to general use of CFDS
ATA
21 OUTFLOW VALVE ELEK i
(04)
If it occurs during system calibration test in MAN MODE, repeat test in AUTO MODE.
CPC 902215702-7
----
902215702-8 TFU 213134006 / TSM ATA 21
----Associated Part :
21 P.L.R. : Leg counting
deviation at leg 99
ZC 775A0000-05
----
775A0000-07
----Associated Part :
21 Test results
in coded form
ZC 775A0000-07
----
775A0000-07 TFU 216134002 / TFU 216334004 / TSM ATA 21
----Associated Part :
21 VENT AVNCS SYS FAULT
during Ditching test procedure.
Reset AEVC C/B at the end of the Ditching test procedure.
AEVC All P/N
----
NONE TFU 212600010 / FCOM chapter 3.04.91 rev.20/AMM 212600 PB 527
----Associated Part :
3Part D : page Revision 29
Description of anomaly Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART D : Anomalies related to general use of CFDS
ATA
216351 FAILURE NOT CLEARLY
IDENTIFIED
NO MAINT. ACTION if no log book complaint.
ZC 775A0000-06
775A0000-05
----
775A0000-06 TFU 216334047
----Associated Part :
22 22-83-34 FMGC (1CA1) /
GPWC (1WZ)
NO MAINT. ACTION if appears after a GPWC test via the CFDS
GPWC 965-0676-020
----
S/W Mod 1 TFU 344800003
----Associated Part :
22 Disregard the indication
RTOK in the AFS Bite report
NO MAINT. ACTION FAC All P/N
----
N/A
----Associated Part :
22 ELAC 1 & ELAC 2 messages
displayed in the ground scan if no hydraulic pressure
NO MAINT. ACTION if no Hydraulic pressure on the A/C
FAC All P/N
----
N/A TSM ATA 22
----Associated Part :
4Part D : page Revision 29
Description of anomaly Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART D : Anomalies related to general use of CFDS
ATA
22 FMGC MAG TRK on MCDU NO MAINT. ACTION if appears after a GPWC ground scan. via the CFDS
GPWC 965-0676-020
----
S/W Mod 1 TFU 344800003
----Associated Part :
22 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 is displayed on the PFD.
DMC ALL P/N
----
FAC --->
B397BAM0508
B397BAM0509
TFU 229700004
----Associated Part :
22 Wrong (Alternate) City
Pair on the PFR.
If Lateral revision at destination is used for inserting/changing Altn destination. Inserting/Modifying via init A page in pre-flight or via secondary flight plan will avoid this anomaly.
FMGC B398AAM0408
B398BAM0205
B398BCM0104
----
B398AAM0409
B398BAM0206
B398BCM0106
TFU 227000014
----Associated Part :
228334 FMGCi Class 2 Fault message without associated Maintenance status. Apply TSM procedure
FCDC 115370-0105
----
115370-1016
115370-0106
MPD Task : 313000-03-1
----Associated Part :
5Part D : page Revision 29
Description of anomaly Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART D : Anomalies related to general use of CFDS
ATA
228334 RMP1(2,3) : NO DATA FROM
FMGCi
Class 2 Fault message to be considered as a Class 3 message.
RMP 899-0850-002
899-0850-003
899-0850-004
----
NONE
----Associated Part :
23 Faults missing in Audio
Previous and last leg reports
Refer to messages in the PFR. AMU 2790(*)A03
2790(*)A03
2790(*)A03
* = C or D or E(3 or 4 or 5 boards)
----
VSB 2790-23-006
VSB 2790-23-007
P/N: 2790(*)B06
TFU 235100009/TFU 235100013
----Associated Part :
23 Wrong P/N of AMU and ACP
in the audio LRU identification
NO MAINT. ACTION AMU 2790(*)A03
2790(*)A03
2790(*)A03
* = C or D or E(3 or 4 or 5 boards)
----
VSB 2790-23-006
VSB 2790-23-007
P/N: 2790(*)B06
TFU 235100009/TFU 235100013
----Associated Part :
230000 BITE Test of the PES Maintenance advise: To determine the status of the PES video system, it is recommended to check, after aircraft is energized, the ground report of CIDS1/CIDS2 menu through the MCDU
CIDS DIR Z064H000030F
----
Z064H000031A
Z064H000031B
SB 23-1278
----Associated Part :
6Part D : page Revision 29
Description of anomaly Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART D : Anomalies related to general use of CFDS
ATA
230000 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 date indication in the ground report of the CIDS1 or CIDS2 or the CIDS1 or 2 Toilet system.
CIDS DIR Z064H000030F
Z064H000031A
Z064H000031B
----
TBD (end 2005)
----Associated Part :
230000 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 Leg Report of the CIDS1 or 2 Toilet system.
CIDS DIR Z064H000030F
Z064H000031A
Z064H000031B
----
TBD (end 2005)
----Associated 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) as it follows: Switchover of CIDS (CIDS1 passive, CIDS2 active, CIDS-SDF1
Maintenance advise: Perform a CIDS reset as described in Appendix 1 to recover the usual CIDS configuration (CIDS part and CIDS-SDF part from the same unit active at the same time).
CIDS DIR Z064H000030F
Z014H000030C
----
Z064H000031A
Z064H000031B
Z014H000131A
----
Z014H000031A
Associated Part :
230000 Video BITE Test
The test of the Video System through MCDU provides unreliable result. Only simultaneous CIDS and PES power-up initiate the PES BITE to be correctly reported (normal mode)
Maintenance advise: To determine the status of the PES video system, it is recommended to check, after aircraft is energized, the ground report of CIDS1/CIDS2 menu through the MCDU
CIDS DIR Z064H000031A
Z064H000031B
----
TBD (end 2005)
----Associated Part :
7Part D : page Revision 29
Description of anomaly Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART D : Anomalies related to general use of CFDS
ATA
2311 IMPOSSIBILITY TO USE
VHF3 IN VOICE MODE
NO MAINT.ACTION. IF AMU AMDT A , APPLY VSB 23-007.
AMU ALL P/N WITH
AMDT A
----
VSB 23-007
P/N: 2790(*)B06
TFU 235100013
----Associated Part :
237334 BITE Test of CIDS
The maintenance message "DIR2 (102RH) -SDF" is spuriously triggered during a system test of the smoke system through the MCDU with the following configuration: both CIDS directors
Maintenance advise: Subject configuration may be reproduced for trouble shooting purpose. Therefore, the validity of the failure message must be checked through a CIDS-SDF ground scanning.
CIDS DIR Z014H000030C
Z064H000030F
----
Z064H000031A
Z064H000031B
Z014H000131A
----
Z014H000031A
Associated Part :
24 After a GPCU test, NO
RESPONSE.
Reinitialize GPCU test GPCU 740121A
740121B
----
Vdr SIL 229
SB 740121-24-7
TFU 244100006
----Associated Part :
24 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
BCL All P/N
----
35-0L5-1005-08
(S/B 24-1075)
TFU 243800007 / TFU 243800009
----Associated Part :
8Part D : page Revision 29
Description of anomaly Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART D : Anomalies related to general use of CFDS
ATA
24 GCUi TEST NOT DONE
or IDGi RUNNING
NO MAINT. ACTION if appears after a GPCU test. Reinitialize the GPCU test.
GPCU 740121A
740121B
----
Vdr SIL 229 TFU 244100005
----Associated Part :
242334 GCU EMERG IN AVIONIC
STATUS
If test result is OK, no maintenance action Could be corrected in a next CFDIU std
GCU 520915 amdt 4
----
TBD TFU 313234035
----Associated Part :
261700 Operational check
of the Lavatory Smoke detection function as per AMM task 26-17-00-710-001 not possible in case DIR1 and DIR-SDF2 or DIR2 and DIR-SDF1 are active simultaneously (CIDS cross configuration).
CIDS DIR Z064H000030D
Z064H000030E
Z064H000030F
----
TBD
----Associated Part :
27 Interruption of SFCC-
CFDS communication when selecting the print option in the SFCC "SYSTEM DATA" pages.
reenter the SFCC MENU SFCC 49117-06/07
----
N/A TFU 275151047
----Associated Part :
9Part D : page Revision 29
Description of anomaly Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART D : Anomalies related to general use of CFDS
ATA
2700 During Ground Scanning,
MAINT STATUS F/CTL may be triggered without associated fault message 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.
FCDC 115370-0106
115370-105
115370-1016
----
115370-1118 TFU 27 95 00 033
----Associated Part :
2700 During Ground Scanning,
ECAM WARNING F/CTL AILERON SERVO FAULT may be triggered without associated fault message if the failure affects the servovalve or the POS XDCR or the SOLENOID valve signal.
TSM procedure should be followed using the ECAM WARNING as entry point.
FCDC 115370-0106
115370-105
115370-1016
----
115370-1118 TFU 279500033
----Associated Part :
279300 Ultimely flash of
AIL SERVO FAULT in case of ELAC 1 (or 2) fault during GROUND SCANNING
FCDC 115370-0105
----
115370-1016
115370-0106
----Associated Part :
279334 AFS:ELACi NO MAINT. ACTION if associated to B SYS LO PRESS (respectively Y SYS LO PRESS).
FAC All P/N
----
N/A
----Associated Part :
10Part D : page Revision 29
Description of anomaly Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART D : Anomalies related to general use of CFDS
ATA
279334 ELACi COM (MON) OR
BUS FROM FMGCi
Class 2 Fault message without associated Maintenance status. Apply TSM procedure
FCDC 115370-0105
----
115370-1016
115370-0106
MPD Task : 313000-03-1
----Associated Part :
279334 SEC3 OR BUS2 FROM ADR2
(ADR3 / IR2 / IR3)
Class 2 Fault message without associated Maintenance status. Apply TSM procedure
FCDC 115370-0105
----
115370-1016
115370-0106
MPD Task : 313000-03-1
----Associated Part :
279434 SEC2 OR INPUT OF L(R)
THROTTLE CTL UNIT 8KSi
Class 2 Fault message without associated Maintenance status. Apply TSM procedure
FCDC 115370-0105
----
115370-1016
115370-0106
MPD Task : 313000-03-1
----Associated Part :
279434 SEC3 OR WIRING FROM
SFCC i
Class 2 Fault message without associated Maintenance status. Apply TSM procedure
FCDC 115370-0105
----
115370-1016
115370-0106
MPD Task : 313000-03-1
----Associated Part :
11Part D : page Revision 29
Description of anomaly Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART D : Anomalies related to general use of CFDS
ATA
279534 OP FCDC FAIL DISCR Class 2 Fault message without associated Maintenance status. Apply TSM procedure
FCDC 115370-0105
----
115370-1016
115370-0106
MPD Task : 313000-03-1
----Associated Part :
301151 L(R) WAI FILTER
OR VALVE9(10) Associated with E/Ws 30.00 WING ANTI ICE SYS FAULT
Do not forget to use the Zone Cont. Class 3 report upon wing anti ice Ecam Warnings.
ZC 775A0000-05
----
775A0000-07 TFU 216334046 / 216334046/TSM ATA 30
----Associated Part :
31 BACK UP MODE DEVIATIONS DO NOT CHOOSE ECAM1/2,FDIU,SFCC1 WHEN DOING STEP 6 OF AMM TASK 31 32 00 710 002
CFDIU B401ACM0506
----
TBD TFU313234035
----Associated Part :
31 Bad counting of the
flight legs in the Class 3 Fault memory.
NO MAINT. ACTION DMU 903116243BOBOG0
903116243BODOJ0
903116243B0B0G1
903116243B0D0J1
----
903116243B3B3G4
9031116243B3B2G3
903116243B3D2J3
TFU 313600017
----
and subsequent std
Associated Part :
12Part D : page Revision 29
Description of anomaly Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART D : Anomalies related to general use of CFDS
ATA
31 Bad PRINT OUT FORMAT. NO MAINT. ACTION Printer 805515-4501
----
805515-4501
VSB M3367
TFU 313522001
----Associated Part :
31 DIFFICULTIES FOR FILTER
LOADING
SOME DIFFICULTIES MAY BE ENCOUNTERED WHEN USING ANY OUT OF THE PDL IN SERVICE BUT THE SFIM.
CFDIU B401ACM0505
B401ACM0506
----
N/A TFU313234038
----Associated Part :
31 Duplication of Fault
message in PFR.
CFDIU B401ACM0404
----
B401ACM0606 TFU 313234029
----Associated Part :
31 GR-OU-ND or GN-D - -
messages in phase 8/9
Generated by type 2 system. No maintenance Action.
CFDIU B401ACM0506
B401ACM0507
----
C12860AA02
----Associated Part :
13Part D : page Revision 29
Description of anomaly Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART D : Anomalies related to general use of CFDS
ATA
31 Incoherent PFR Fault
messages sent by the EIU.
Check EIU Previous Leg reports. EIU 3957900611
----
3957900612 TFU 313234029
----Associated Part :
31 Incoherent PFR recording
time in the PFR header.
Due to Flight phases transitions anomalies.
CFDIU B401ACM0404
----
B401ACM0506 TFU 313234029
----Associated Part :
31 Incomplete PFR Fault
messages.
Due to power transients. CFDIU B401ACM0404
----
B401ACM0506 TFU 313234029
----Associated Part :
31 Message NO RESPONSE,
PRESS RETURN after the start of DMC test.
To get the results, reenter DMC menu and access the "Test Result" item
DMC All P/N
----
None
----Associated Part :
14Part D : page Revision 29
Description of anomaly Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART D : Anomalies related to general use of CFDS
ATA
31 Mixed GMT in PFR Due to power transients. CFDIU B401ACM0404
----
B401ACM0506 TFU 313234029
----Associated Part :
31 NO "SYST" DATA (INTM) If no logbook complaint, NO MAINT ACTION. This message is generated by the CFDIU (Source : CFDS).
CFDIU B401ACM0506
----
TBD
----Associated Part :
31 NO DMC1 DATA recorded in
CFDIU ground scanning
NO MAINT. ACTION CFDIU B401ACM0404
----
B401ACM0506 TFU 313234030
----Associated Part :
31 NO FWC DATA recorded in
CFDIU last leg report.
NO MAINT. ACTION if no log book complaint.
CFDIU B401ACM0404
----
B401ACM0506 TFU 313234030
----Associated Part :
15Part D : page Revision 29
Description of anomaly Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART D : Anomalies related to general use of CFDS
ATA
31 P/N read through LRU
IDENT. Menu not in accordance with the actual P/N.
NO MAINT. ACTION FDIU 9026-16079-01B2
----
9026-16079-02B3 TFU 313300011
----Associated Part :
31 PFR with NO FAULT / NO
WARNING.
Due to Flight phases transitions anomalies.
CFDIU B401ACM0404
----
B401ACM0506 TFU 313234029
----Associated Part :
31 System source without
Fault message.
Under investigation. No Maint. Action. CFDIU B401ACM0404
----
B401ACM0506 TFU 313234029
----Associated Part :
31 Untimely print out of
real time failure and warning.
In flight pull, PRINTER C/B. CFDIU B401ACM0404
----
Amdt A TFU 313234026
----Associated Part :
16Part D : page Revision 29
Description of anomaly Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART D : Anomalies related to general use of CFDS
ATA
31 12 34 FLPi NO CFDIU DATA The ATA chapter of this message should be 313234 instead of 311234.
SFCC 49-117-09
49-117-10
49-170-11
----
TBD
----Associated Part :
313234 ADFi : NO DATA FROM
CFDIU
Class 2 Fault message to be considered as a Class 3 message.
ADF 204-1168-7513
622-5222-020
----
NONE
----Associated Part :
313234 AUDIO NO DATA FROM
CFDIU
Class 2 Fault message to be considered as a Class 3 message.
AMU 2790CA03
----
NONE
----Associated Part :
313234 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 B401ACM0507
C12860AA02
----
N/A
----Associated Part :
17Part D : page Revision 29
Description of anomaly Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART D : Anomalies related to general use of CFDS
ATA
313234 DME1(2,3) : NO DATA FROM
CFDIU
Class 2 Fault message to be considered as a Class 3 message.
DME 622-4540-023
9599-614-03105
----
NONE
----Associated Part :
313234 HFi : NO DATA FROM
CFDIU
Class 2 Fault message to be considered as a Class 3 message.
HF 622-5272-020
----
NONE
----Associated Part :
313234 NO DATA FROM CFDIU Class 2 Fault message to be considered as a Class 3 message.
ILS 204-1230-3518
622-5222-020
----
204-1230-3521
622-5222-041
----Associated Part :
313234 RMP1(2,3) : NO DATA FROM
CFDIU
Class 2 Fault message to be considered as a Class 3 message.
RMP 899-0850-002
899-0850-003
899-0850-004
----
NONE
----Associated Part :
18Part D : page Revision 29
Description of anomaly Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART D : Anomalies related to general use of CFDS
ATA
313234 VHF1(2,3) : NO DATA FROM
CFDIU
Class 2 Fault message to be considered as a Class 3 message.
VHF 204-1237-4417
----
NONE
----Associated Part :
313234 VOR 1(2,3) :NO DATA FROM
CFDIU
Class 2 Fault message to be considered as a Class 3 message.
VOR 204-1231-3610
622-5220-020
204-1231-3623
204-1231-3613204-1231-3622
----
NONE
----Associated Part :
313234 WRX i : NO DATA FROM
CFDIU
Class 2 Fault message to be considered as a Class 3 message.
WRX 204-1217-0418
204-1217-0421
----
VSB RTA-4A-34-173
----Associated Part :
313316 ACCELEROMETER Class 2 Fault message without associated Maintenance Status. Apply TSM procedure.
FDIU ED43A1D2
ED43A1D3
90261607902B3
----
ED43A1D5 MPD 313000-04-01
----Associated Part :
19Part D : page Revision 29
Description of anomaly Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART D : Anomalies related to general use of CFDS
ATA
32 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 664700500A4B
664700500A4C
----
664700500A4D
----Associated Part :
32 If a power interrupt of 10 ms or greater occurs after the transition from flight phase 1 to 2 with shock absorbers compressed any subsequent faults detected by the LGCIU will be logged in ground memory and not flight memory.
LGCIU 664700500A4B
664700500A4C
----
664700500A4D
----Associated Part :
32 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 664700500A4B
664700500A4C
----
664700500A4D
----Associated Part :
32 BSCU BITE report
Wrong DATE, TIME and FLIGHT PHASE due to lack of communciation with CFDIU at the time fault msg is recorded. CLASS 3 fault msg "CFDIU(1TW)/BSCU(10GG)"
CLASS 3 fault msg "CFDIU(1TW)/BSCU(10GG)" should be memorized in BSCU CLASS 3 REPORT. TIME and DATE displayed correspond to TIME and DATE at time of consultation and not time / date of event.
BSCU E21327001
E21327003
----
TBD
----Associated Part :
20Part D : page Revision 29
Description of anomaly Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART D : Anomalies related to general use of CFDS
ATA
32 During TPIU Bite test
"NO RESPONSE" message may appears on the MCDU
Restart the TPIU Bite test TPIU 1058-34
----
TBD
----Associated Part :
32 Menu Mode access
possible during flight
LGCIU 664700500A4A
----
664700500A4B TFU 323134043
----Associated Part :
32 No LGCIU fault message
in the PFR.
The first failure logged in an empty LGCIU memory is not transmitted to the CFDIU for PFR recording.
LGCIU 66700500A4C
----
664700500A4D
----Associated Part :
32 Nothing in the LGCIU
Last Leg report instead of "NO FAILURE"
LGCIU 664700500A4A
----
664700500A4B TFU 323134043
----Associated Part :
21Part D : page Revision 29
Description of anomaly Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART D : Anomalies related to general use of CFDS
ATA
32 Spurious NO DATA FROM
CFDS in the LGCIU Ground scanning, with date ???31
NO MAINT. ACTION LGCIU 664700500A4A
----
664700500A4B TFU 323134041
----Associated Part :
335100 EPSUs Battery Capacity
test not possible through the MCDU
AMM task 33-51-00-710-011 to be updated accordingly.
CIDS DIR Z064H000030D
Z064H000030E
Z064H000030F
----
TBD
----Associated Part :
335100 The Battery Capacity
test of the EPSUs through the MCDU is not possible.
Maintenance advise: Pending availability of the MCDU test, the alternate AMM Task 33-51-00-710-011-01 "Remove Batteries for capacity check" should be applied.
CIDS DIR Z064H000030F
----
Z064H000031A
Z064H000031B
----Associated Part :
34 Bad leg incrementation
of GPWS Previous Leg Reports.
NO MAINT. ACTION GPWC 965-0676-020
----
9650676-020
S/W MOD 1
TFU 344800004
----Associated Part :
22Part D : page Revision 29
Description of anomaly Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART D : Anomalies related to general use of CFDS
ATA
34 Bad LRU identification. NO MAINT. ACTION RADAR 204-1217-0418
204-1217-0421
----
VSB RTA-4A-34-161 TFU 344100007
----Associated Part :
34 Blank pages or erratic
Data in Previous Leg Report.
NO MAINT. ACTION RADAR 204-1217-0418
204-1217-0421
----
VSB RTA-4A-34-161 TFU 344100007
----Associated Part :
34 FMGC (1CA1) / GPWC (1WZ)
FMGC1 MAG TRK
Messages in the Ground Scanning and in the test result of the GPWC : NO MAINT. ACTION.
GPWC 965-0676-020
----
9650676-020
S/W MOD 1
TFU 344800003
----Associated Part :
34 Loss of fault messages
in the GPWC Previous Leg Reports.
NO MAINT. ACTION GPWC 965-0676-020
----
9650676-020
S/W MOD 1
TFU 344800004
----Associated Part :
23Part D : page Revision 29
Description of anomaly Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART D : Anomalies related to general use of CFDS
ATA
34 NO access to the ADF
Last Leg Report after 64 legs flown without fault recorded in BITE
NO MAINT ACTION ADF 622-5222-020
----
VSB ADF-700-34-27
----Associated Part :
34 No access to the VOR
Last Leg Report after 64 legs flown without fault recorded in BITE.
NO MAINTENANCE ACTION VOR 622-5220-020
----
VSB-700-34-21 NONE
----Associated Part :
34 No transmission of
external failure at detection but after power cut
NO MAINT. ACTION HUDC 96154334-1
----
96154334-2
----Associated Part :
34 Random and transient
pattern (2sec) during aproach, instead of the wanted symbology display.
NO MAINT ACTION HUDC 9615433402
----
V65
----Associated Part :
24Part D : page Revision 29
Description of anomaly Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART D : Anomalies related to general use of CFDS
ATA
34 same message with same
date and GMT but different leg numbers in the Previous Leg Reports.
NO MAINT. ACTION GPWC 965-0676-020
----
965-0676-020
S/W MOD 1
TFU 344800004
----Associated Part :
34 Wrong identification of
DME : Message : DME-0 TRANSCEIVER
DME 622-4540-022
----
622-4540-023 TFU 345100009
----Associated Part :
34 36 All ILS failures are
coded as MMR failures in the following case:
When the CFDIU is swapped from an 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.
CFDIU B401ACM0507
----
TBD
----Associated Part :
345831 "GPSSU(1SNi) when MMR installed on the A/C, GPSSU means GPS part of the MMR.
ADIRU All P/N
----
Ref TSM task: 34 58 00 810 805
----Associated Part :
25Part D : page Revision 29
Description of anomaly Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART D : Anomalies related to general use of CFDS
ATA
361100 WAI NO BLEED AIR ENG i
Associated with E/Ws 30.00 WING ANTI ICE L(R) VALVE OPEN
Do not forget to use the Zone Cont. Class 3 report upon wing anti ice Ecam Warnings.
ZC All P/N
----
775A0000-08 TFU 301100014
----Associated Part :
45 CFDIU BUS The ATA chapter of this message should be 313234 instead of 45.
TCAS 4066010-904
----
TBD
----Associated Part :
451334 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 wording shall be 313234 CFDIU(1TW)/CIDS(10yRH)-SDFy (with y=1 or 2) instead of 451334 CFDS1(1TM)/CIDS(10yRH)-SDFy.
CIDS DIR Z014H000030C
----
Z014H000031A
Z014H000131A
----Associated Part :
4621 GROUND SCANNING
ATSU failures may be missing in ground scanning report.
Always reset the ATSU before performing the ground scanning function.
ATSU host platform S/W
LA2T0S162C0C0F1
----
LA2T0S111C1B0F1
----Associated Part :
26Part D : page Revision 29
Description of anomaly Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART D : Anomalies related to general use of CFDS
ATA
4621 LINK TEST Before activating the link test function, select the VHF3 in DATA mode (if VHF3 in VOICE mode, the test fails).
ATSU host platform S/W
LA2T0S162C0C0F1
LA2T0S111C1B0F1
----
LA2T0J13000C0F1 AMM task : 46 21 00 710 00200
----Associated Part :
4621 LRU identification
A/C interfacce P/N displayed on LRU ident page is software P/N (LA2T0S162C0C000) and not disk P/N (LA2T0S162C0C0F1)
ATSU host platform S/W
LA2T0S162C0C0F1
LA2T0S111C1B0F1
----
LA2T0J13000C0F1 AMM tasks : 46 21 00 610 00100/120
----Associated Part :
4621 LRU identification
AOC database not displayed on LRU ident MCDU page.
AOC database P/N is accessible on AOC menu (MISC menu for Allied Signal AOC, and CONFIG menu for Rockwell Collins AOC).
ATSU host platform S/W
LA2T0S162C0C0F1
----
LA2T0S111C1B0F1 AMM tasks : 46 21 00 610 00300/320
----Associated Part :
4621 MCDU dual access AOC (Collins) simultaneously displayed and used on both MCDU, may induce to a MCDU protocol interuption leading to an ATSU time out. MCDU menu key has to be selected to recover ATSU normal mode. Only 1 MCDU must be used.
ATSU host platform S/W
LA2T0S162C0C0F1
----
LA2T0S111C1B0F1
----Associated Part :
27Part D : page Revision 29
Description of anomaly Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART D : Anomalies related to general use of CFDS
ATA
4621 PRINT FAILED A "PRINT FAILED" message can be displayed on MCDU, even if the print is successful.
ATSU host plateform S/W
LA2T0S162C0C0F1
----
LA2T0S111C1B0F1
----Associated Part :
4621 PRINT FUNCTION The "*" indicating the possibility to print is not always displayed. The "*" is systematicaly displayed after activating the PRINT function.
ATSU host platform S/W
LA2T0S162C0C0F1
----
LA2T0S111C1B0F1 TFU 46 00 00 002
----Associated Part :
4621 SYSTEM REPORT TEST
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).
ATSU host paltform S/W
LA2T0S162C0C0F1
LA2T0S162C0B0F1
----
LA2T0J13000C0F1 AMM task : 46 21 00 740 00100
----Associated Part :
4621 TSD DUMP After the DUMP TSD prompt 2 consecutives messages are displayed : "Waiting for response" &"No response" even if the function is properly performed.
ATSU host platform S/W
LA2T0S111C1B0F1
----
LA2T0J13000C0F1
----Associated Part :
28Part D : page Revision 29
Description of anomaly Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART D : Anomalies related to general use of CFDS
ATA
49 Messages may be
duplicated in the PFR.
ECB (GTCP 36-300)
304817-1
----
304817-2
----Associated Part :
49 Some messages are sent
with more than 48 characters
APU GTCP 36.300 ECB (GTCP 36-300)
304640-3
----
304817-1
----Associated Part :
73 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.
EIU 3957900609
3957900610
3957900611
3957900612
----
3957900613 TFU 732534005
----Associated Part :
73 ENG OVSPD PROT FAULT
associated with HMU, J7 during FADEC ground test
To be confirmed by a new test. If not confirmed, NO MAINT. ACTION.
ECU 1459M55P15
1519M83P02
1459M55P16
1519M83P03
----
1459M55P17
1519M83P04
1820M27P01
TFU 732900025
----Associated Part :
29Part D : page Revision 29
Description of anomaly Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART D : Anomalies related to general use of CFDS
ATA
73 GARBLED FADEC fault
messages in the PFR.
For maint. action ref. to the FADEC LAST LEG REPORT.
EIU 39579050-04 (IAE)
395900612 (CFMI)
395900613 (CFMI)
----
39579050-05 (IAE)
39579050-14(CFMI)
TFU732500008/TFU732500007
----Associated Part :
73 OIL TEMP SENSOR 4004 EN
RT OK in EIU ground scanning.
NO MAINT. ACTION when RT OK (Result Test OK) is mentioned.
EIU 3957900609
3957900610
3957900611
3957900612
----
3957900613 TFU 732534005
----Associated Part :
73 When RTOK recorded in
the GND SCAN results.
Disregard, ref AMM EIU GND SCAN procedure.
EIU All P/N
----
3957900613 (CFM)
39579050-04 (IAE)
----Associated Part :
7300 FADEC Ground Scanning
There is a specific sequence of events when running FADEC GROUND SCANNING which can lead 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 EEC self-test and then exit Menu Mode without selecting Ground Scanning."
EEC (Soft SCN17)
808050-4-056
824972-2-010
----
SCN18
----Associated Part :
30Part D : page Revision 29
Description of anomaly Remark Part P/Ns Affected Corrective P/N Doc X Ref
SIL 00-028 PART D : Anomalies related to general use of CFDS
ATA
77 Wrong date in the EVMU
Last Leg Report
Present date instead of actual date recorded in EVMU last leg report when No failure recorded and last leg corresponds to the day before.
EVMU 241-211-000-021
----
241-211-000-031 TFU 773234020
----Associated Part :
7700 ENG i FADEC A(B) FAULT NO MAINT. ACTION if associated with WB3 SENS,J15,ECU in FADEC ground test.
ECU 1459M55P15
1519M83P02
1459M55P16
1519M83P03
----
1459M55P17
1519M83P04
1820M27P01
TFU 732900025
----Associated Part :
78 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.
ECU ECU (CFMI)
----
1459M55P17
1519M83P04
TFU 783100014
----Associated Part :
31Part D : page Revision 29
ATA Failure Message
SIL 00-028 Part E : Filter ContentPhases Source Affected part and P/N
2131 CAB_PR_LO_DIFF_PR 06 07 902215702-7902215702-8
CPCCPC
2161 AIR_PACK_1$2_FAULT 03 04 ALL P/NPC
2200 AUTO_FLT_A/THR_OFF 08 09 All P/NFMGC
2200 AUTO_FLT_AP_OFF 02 03 04 All P/N08 09 FMGC
2700 F/CTL_SPD_BRK_DISAGREE All P/NFCDC
2800 FUEL_L_WING_TK_OVERFLOW 07 All P/NFQIC
1Part E : page Revision 29
ATA Failure Message
SIL 00-028 Part E : Filter ContentPhases Source Affected part and P/N
2800 FUEL_R_WING_TK_OVERFLOW 07 All P/NFQIC
3200 BRAKES_HOT All P/NBSCU
3200 L/G_SHOCK_ABSORBER_FAULT 09 08 9599-607-149329599-607-12333
RARA
3400 NAV_GPWS_FAULT 02 03 04 204-1230-3518622-9738-020
08 09 ILS P/N3ILS P/N1
3800 VSC 14404-011AVSC P/N1
7700 DUAL_ENGINE_FAILURE 02 03 04 9599-607-149329599-607-12333
08 09 RARA
2Part E : page Revision 29
ATA Failure Message
SIL 00-028 Part E : Filter ContentPhases Source Affected part and P/N
HUD All P/NHUDC
GN-D - - 08 09 B401ACM0506B401ACM0507
CFDIUCFDIU
GR-OU-ND 08 09 B401ACM0506B401ACM0507
CFDIUCFDIU
226634 DMC$:_NO__FAC$__DATA All P/NDMC
228212 AFS:_MCDU$ All P/NFMGC
228212 MCDU3(3CA3)/ATSU1(1TX1) LA2T0S111C1B0F1ATSU P/N1
3Part E : page Revision 29
ATA Failure Message
SIL 00-028 Part E : Filter ContentPhases Source Affected part and P/N
228334 AFS:FMGC$ B546BAM0203B546CCM0101B546CAM0101B398AAM0410B398BAM0207
FMGCFMGCFMGCFMGCFMGC
228334 AFS:FMGC$(DO_NOT_REMOVE) AFS B397BAM0617FAC pre Std
228334 AFS:FMGC$/ATHR_ENGD_FDBK 08 09 B398AAM0xxxB398BAM0xxxB398BCM0xxx
FMGCFMGCFMGC
228334 AFS:FMGC$_(FM$) B398AAM0408B398BAM0205B398BCM0104
FMGCFMGCFMGC
231100 ICAO_ADDRESS/HF$(3RE$) 822-0990-003HFDR CollinsHFS900D
231133 HFDR$(3RE$)/ATSU1(1TX1) LA2TOJ13000C0F1LA2TOJ13002C0F1
ATSU P/N2ATSU P/N4
4Part E : page Revision 29
ATA Failure Message
SIL 00-028 Part E : Filter ContentPhases Source Affected part and P/N
231133 NO_HF_1_DATA 02 CFDS 964-0452-001964-0452-012
HF TRANSCEIVHF TRANSCEIV
231233 NO_ VHF3_ DATA CFDS C12860AA02
Not installed
CFDIU
VHF3
231233 VHF0(1RC0) 02 822-1047-030VHF
231313 RMP$(1RG$)/RMP$(1RG$) 02 C12848AA01C12848CA01
RMPRMP
232834 SDU1(5RV1)/ATSU1(1TX1) LA2T0S162C0C0F1ATSU P/N3
237334 NO_CIDS_2_DATA 02 05 06 CFDS Z010H0003113(7)Z010H0005115(7)Z010H0005118(9)Z010H000520(1)A
CIDSCIDSCIDSCIDS
5Part E : page Revision 29
ATA Failure Message
SIL 00-028 Part E : Filter ContentPhases Source Affected part and P/N
237334 NO_CIDS_2_DATA_(INTM) 02 05 06 CFDS Z010H0003113(7)Z010H0005115(7)Z010H0005118(9)Z010H000520(1)A
CIDSCIDSCIDSCIDS
240000 POWER_SUPPLY_INTERRUPT 01 02 09 EIS 3 SXT3F-E2SA-0410SXT3C-E2SA-0420
10 DMC EIS II SoftDMC EIS II Soft
240000 POWER_SUPPLY_INTERRUPT 01 02 09 EIS 1 SXT3F-E2SA-0410SXT3C-E2SA-0420
10 DMC EIS II SoftDMC EIS II Soft
240000 POWER_SUPPLY_INTERRUPT 01 02 09 EIS 2 SXT3F-E2SA-0410SXT3C-E2SA-0420
10 DMC EIS II SoftDMC EIS II Soft
242255 AFS:28V_PWR_11XU1 02 09 10 All P/NFMGC
243251 SDAC$:NO_TR1_CURRENT ______1PU1
35-0E5-1510-2235-0E5-1611-22
SDACSDAC
6Part E : page Revision 29
ATA Failure Message
SIL 00-028 Part E : Filter ContentPhases Source Affected part and P/N
243854 SDAC$:NO_DATA_FROMBCL$
35-0E5-1510-2235-0E5-1611-22
SDACSDAC
275134 SDAC$:NO_DATA_FROMSFCC
35-0E5-1510-2235-0E5-1611-22
SDACSDAC
301151 _WAI_FILTER_OR_VALVE 775A0000-07ZC
313234 _RADAR$___NO DATAFROM_CFDIU
204-1217-0418204-1217-0421
RADARRADAR
316322 DU_EWD(2WK1)/___________ECP(2WM)
SXT3CE2SA0420SXT4EE2SA050A
EIS II Software
316322 DU_ND_CAPT(3WK1)/_______ND_CAPT_POT(8WK1)
SXT3CE2SA0420SXT4EE2SA050A
EIS II Software
7Part E : page Revision 29
ATA Failure Message
SIL 00-028 Part E : Filter ContentPhases Source Affected part and P/N
316322 DU_ND_FO(3WK2)/_________ND_FO_POT(8WK2)
SXT3CE2SA0420SXT4EE2SA050A
EIS II Software
316322 DU_PFD_CAPT(1WK1)/______PFD_CAPT_POT(7WK1)
SXT3CE2SA0420SXT4EE2SA050A
EIS II Software
316322 DU_PFD_FO(1WK2)/________PFD_FO_POT(7WK2)
SXT3CE2SA0420SXT4EE2SA050A
EIS II Software
316322 DU_SD(2WK2)/____________ECP(2WM)
SXT3CE2SA0420SXT4EE2SA050A
EIS II Software
324418 SDAC$:LH_Y_BRK_PRESSXDCR_63GG
06 350E053020606FWC
324418 SDAC$:RH_Y_BRK_PRESSXDCR_62GG
06 350E053020606FWC
8Part E : page Revision 29
ATA Failure Message
SIL 00-028 Part E : Filter ContentPhases Source Affected part and P/N
341234 ADIRU$$$($FP$$$)_ADRBUS/WXR$($SQ$)
2 822-1710-201822-1710-202
RADAR
341234 ADIRU$($FP$)_IR_BUS/____WXR$($SQ$)
2 822-1710-201822-1710-202
RADAR
341234 AFS:ADIRU1/2/3_DISAGREE B397AAM0507B397AAM0508B397BAM0406B397BAM0407
FACFACFACFAC
343522 HUD_OHU 96154334-196154334-2
HUDCHUDC
343631 AFS:ILS All P/NFMGC
343631 FWC$_:NO_DATA_FROMILS$
02 07 622-9738-020ILS P/N1
9Part E : page Revision 29
ATA Failure Message
SIL 00-028 Part E : Filter ContentPhases Source Affected part and P/N
343631 ILS$ 02 622-9738-020622-9738-041
ILS P/N1ILS P/N2
343631 ILS$_RECEIVER 204-1230-3518ILS P/N3
343631 MMR1(40RT1)/GPWC(1WZ) 9650976003102-xEGPWC
343731 NO_MLS_$_DATA 3514BS013514CS013514DS013514ES01
AMUAMUAMUAMU
344133 RADAR1_TRANSCEIVER 02 MI 585306-402RADAR
345133 AFS:DME$ 622-4540-023DME
10Part E : page Revision 29
ATA Failure Message
SIL 00-028 Part E : Filter ContentPhases Source Affected part and P/N
345133 AFS:DME$ C13042xA01FMGC
345233 ATC$_(1SH$)_/_TCAS_(1SG) TCAS 7517900-100027517900-10003
TCASTCAS
345233 NO_ATC_$_DATA__ CFDS 751-7800-10002751-7800-10005
ATC
345331 NO_ADF_$_DATA CFDS All P/N
Not installed
CFDIU
ADF1/ADF2
345531 AFS:VOR All P/NFMGC
383100 LIQD_LVL_XMTR_(40MG)_AND_LIQD_LVL_SNSR(41MG)_
TOILET Z064H000030DZ064H000030E
CIDS DIRCIDS DIR
11Part E : page Revision 29
ATA Failure Message
SIL 00-028 Part E : Filter ContentPhases Source Affected part and P/N
383134 VSC 14404-011AVSC P/N1
383141 TOILET_ASSY_LAV_$_ TOILET Z064H000030DZ064H000030E
CIDS DIRCIDS DIR
383162 LIQD_LVL_XMTR_(40MG)_ TOILET Z064H000030DZ064H000030E
CIDS DIRCIDS DIR
383162 LIQUID_LVL_XMTR 14403-003AVSC P/N2
492318 LCDT_SENSOR_P29 45000014500001A4500001B4500003G
ECB P/N1ECB P/N2ECB P/N3ECB P/N4
499651 APU_OIL_HEATER_(8093KM) APU 3888394-230300304817-1304817-23800278-4
ECBECBECBAPU
12Part E : page Revision 29
ATA Failure Message
SIL 00-028 Part E : Filter ContentPhases Source Affected part and P/N
499651 APU_OIL_HEATER_(8093KM) APU 3888394-230300304817-1304817-23800278-23800278-3
ECBECBECBAPUAPU
732160 DMC$:NO_ECU$A_DATA 02 All P/NECU
732160 DMC$:NO_ECU$B_DATA 02 All P/NECU
732160 ECU(E$-4000KS) 02 EIS 3 SXT3F-E2SA-0410SXT3C-E2SA-0420
DMC EIS II SoftDMC EIS II Soft
732160 ECU(E$-4000KS) 02 EIS 2 SXT3F-E2SA-0410SXT3C-E2SA-0420
DMC EIS II SoftDMC EIS II Soft
732160 ECU(E$-4000KS) 02 EIS 1 SXT3F-E2SA-0410SXT3C-E2SA-0420
DMC EIS II SoftDMC EIS II Soft
13Part E : page Revision 29
ATA Failure Message
SIL 00-028 Part E : Filter ContentPhases Source Affected part and P/N
732234 DMC$:NO_EEC$A_DATA 02 All P/NEEC
732234 DMC$:NO_EEC$B_DATA 02 All P/NEEC
732234 EEC(E$-4000KS) 02 EIS 3 SXT3F-E2SA-0410SXT3C-E2SA-0420
DMC EIS II SoftDMC EIS II Soft
732234 EEC(E$-4000KS) 02 EIS 2 SXT3F-E2SA-0410SXT3C-E2SA-0420
DMC EIS II SoftDMC EIS II Soft
732234 EEC(E$-4000KS) 02 EIS 1 SXT3F-E2SA-0410SXT3C-E2SA-0420
DMC EIS II SoftDMC EIS II Soft
793415 CHECK_OIL_PRESS_SWITCH3EN$
02 09 1058-34TPIS
14Part E : page Revision 29
ATA Failure Message
SIL 00-028 Part E : Filter ContentPhases Source Affected part and P/N
XXXXXX ADF-$:NO_DATA_FROMCONTROL_SOURCE
204-1168-7513ADF P/N1
XXXXXX ADF-$:NO_DATA_FROM______CONTROL_SOURCE
622-5222-020ADF P/N2
XXXXXX DME-$:NO_DATA_FROM________CONTROL_SOURCE
9599-614-03105DME
XXXXXX VOR-$:NO_DATA_FROMCONTROL_SOURCE
204-1231-3610VOR P/N1
XXXXXX VOR-$:NO_DATA_FROM______CONTROL_SOURCE
622-5220-020VOR P/N2
15Part E : page Revision 29