CFDS Trouble Shooting

CUSTOMER SERVICES DIRECTORATE AIRBUS1 ROND POINT MAURICE BELLONTE

31707 BLAGNAC CEDEX FRANCE

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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.



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SIL NUMBER: 00-028



REVISION: 29


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



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SIL NUMBER: 00-028



REVISION: 29


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



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SIL NUMBER: 00-028



REVISION: 29


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



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SIL NUMBER: 00-028



REVISION: 29


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.



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SIL NUMBER: 00-028



REVISION: 29


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



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SIL NUMBER: 00-028



REVISION: 29


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



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SIL NUMBER: 00-028



REVISION: 29


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



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SIL NUMBER: 00-028



REVISION: 29


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


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


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


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


No

1Part A : page Revision 29



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


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


No

226634 DMCi : No FACj DATA No Maintenance action DMC ALL P/N

----

9615325050

(Soft std DMC V50)


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


No




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


No

228112 FCU(2CA)CP-R BUS/WXRi(1SQi) (i = 1 or 2)


----

822-1710-202


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


No

228112 FCU(3CA)CP-R BUS/WXRi 1SQi (I=1 or 2)


RADAR 822-1710-201

----

822-1710-202


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


No




ATA Filter

228212 AFS:MCDUi NO MAINT. ACTION if no log book complaint FMGC ALL P/N

----

NONE TFU 229100011


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


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


Yes

B546BCM0205C13042AA01

228334 AFS:FMGCi (FMi) NO MAINT. ACTION if no log book complaint FMGC B398AAM0408

B398BAM0205B398BCM0104

----

B398AAM0409

B398BAM0206B398BCM0106

TFU 229100010


Yes




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


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


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


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


No

228334 FMGECi(1CAi)/RMPi(1RGi)/ILSi(1RTi)

No maintenance action if no logbook entry ILS 622-9738-041

(Collins)

----

N/A


No




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)


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


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


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


Yes




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


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


No

231233 NO VHF3 DATA NO MAINT. ACTION when VHF3 not installed CFDS C12860AA02

(STD 9B)

----

CFDIU STD 10 TBC


Yes

231233 VHF 3 TRANSCEIVER NO MAINT. ACTION if no log book complaint VHF 622-5219-020

----

VSB VHF-700-23-38


No

231233 VHF0(1RC0) NO MAINT. ACTION if occurs in phase 02 VHF3 822-1047-030

----

N/A


Yes




ATA Filter

231313 RMPi(1RGi)/RMPj(1RGj) NO MAINT. ACTION required RMP C12848AA01

C12848CA01

----

TBD


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).


LA2T0S162C0C0F1

----

LA2T0S111C1B0F1 TFU 46 00 00 002


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)


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)


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)


No




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


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


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)


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)


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


No




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)


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)


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


No




ATA Filter

240000 POWER SUPPLY INTERRUPT NO MAINTENANCE ACTION ILS 066-50008-0301

----

066-50008-0405


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


Yes

242151 IDGi DISCONNECTED Check Class 3 Fault messages. GPCU 740121A

----

740121B

(SB24-1077)

TFU 244100002 / TSM ATA 24


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


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


Yes




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


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


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


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


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


No




ATA Filter

261200 CHECK FDU ENGi SUPPLY NO MAINT. ACTION if no log book complaint FDU 730400-01

----

730401-02 TFU 261234020


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


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


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


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


No




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


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


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


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


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


No




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


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


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


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


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


No




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


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


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


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


No

313234 CFDIU(1TW)/HF(i) (3REi) No maintenance action if no logbook complaint. HF Transceiver

964-0452-001

----

TBD


No




ATA Filter

313234 LGCIU: NO DATA FROM CFDS Appears after a CFDIU power down, NO MAINTENANCE ACTION

LGCIU 664700500A4A

----

664700500A4B TFU 323134043


No

313234 RADAR x: NO DATA FROMCFDIU

NO MAINT. ACTION RADAR 204-1217-0418

204-1217-0421

----

VSB RTA-4A-34-173 TFU344100010


Yes

313352 QAR NO MAINT. ACTION if mentioned in Phase 1 in last leg report

FDIU 9026-16079-01B2

----

9026-16079-02B3 TFU 313300007


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


No

313355 DFDR NO MAINT. ACTION if mentioned in Phase 1 in last leg report

FDIU 9026-16079-01B2

----

9026-16079-02B3 TFU 313300007


No




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


No

313652 DAR No Maintenance Action required DMU 795040-30-001

----

795040-31-002


No

313652 DAR TAPE LOW No Maintenance Action required DMU 795040-30-001

----

795040-30-002


No

316322 DU EWD(2WK1)/ECP(2WM) No maintenance action required if no logbook complaint. EIS II Software

SXT3CE2SA0420

SXT4EE2SA050A

----

TBD


Yes




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


Yes

316322 DU ND FO(3WK2)/ND FO POT(8WK2)


SXT3CE2SA0420

SXT4EE2SA050A

----

TBD


Yes

316322 DU PFD CAPT(1WK1)/PFD CAPT POT(7WK1)


SXT3CE2SA0420

SXT4EE2SA050A

----

TBD


Yes

316322 DU PFD FO(1WK2)/PFD FO POT(7WK2)


SXT3CE2SA0420

SXT4EE2SA050A

----

TBD


Yes

316322 DU SD(2WK2)/ECP(2WM) No maintenance action required if no logbook complaint. EIS II Software

SXT3CE2SA0420

SXT4EE2SA050A

----

TBD


Yes




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


No

316334 HUDC : CHECK DMC1 NO MAINT. ACTION HUDC 96154334-1

----

96154334-2 TFU 343500003


No

316334 HUDC : NO DMC1 DATA NO MAINT. ACTION HUDC 96154334-1

----

96154334-2 TFU 343500003


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


No

323171 LGCIUi 05GAi NO MAINT. ACTION LGCIU 664700500A4A

----

664700500A4B TFU 323134043


No




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)


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)


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


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


No




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


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


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


No




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


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


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


No

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


822-1710-202

----

822-1710-203


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


Yes




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


No

341234 AFS:ADIRU 1/2/3 DISAGREE No maintenance action if no logbook complaint FAC B397AAM0507

B397AAM0508B397BAM0406B397BAM0407

----

B397BAM0513 TFU 220000012


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


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


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


No




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


No

343522 HUD OHU NO MAINT. ACTION if no log book complaint. HUDC 96154334-1

96154334-2

----

V65 SOFTWARE TFU 343500003


Yes

343631 AFS : ILS i NO MAINT. ACTION if occurs at the end of the flight FMGC All P/N

----

TBD


Yes

343631 FWCi :NO DATA FROMILSi

NO MAINT ACTION if occurs in flight phases 02 and 07. ILS 622-9738-020

----

622-9788-041


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


Yes




ATA Filter

343631 ILSi NO MAINT. ACTION if occurs in flight phase 02. ILS 622-9738-020

622-9738-041

----

NONE


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


No

343631 MMR1 (40RT1)/GPWC (1WZ) NO MAINT. ACTION required EGPWS 965-0976-

003-102-102

----

965-0976-

003-206-206


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


No

343731 NO MLS (i) DATA No maintenance action if no logbook complaint AMU 3514xS01

----

TBD


Yes




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


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


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


No

344111 WXR ANTENNA(11SQ) No maintenance action required if no logbook complaint. RADAR 822-1710-201

----

822-1710-202


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


No




ATA Filter

344112 WXR CTL PNL(3SQ)/WXRi(1SQi) (i = 1 or 2)


RADAR 822-1710-201

----

822-1710-202


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


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


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


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


No




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


No

344133 WXRi(1SQi)(i= 1 or 2)

No maintenance action if no logbook complaint. RADAR 822-1710-201

----

822-1710-202


No

344137 WXR MOUNTING TRAY(5SQ)/WXRi(1SQi) (i = 1 or 2)


----

822-1710-202


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


No

344233 RA1(2SA1)+RA2((2SA2)/WXRi (1SQi) (I=1 or 2)


RADAR 822-1710-201

----

822-1710-202


No




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


No



TCAS HONEYWELL

066-50000-1x08

066-50000-2x204066010-903/9044066010-905

940-300-001

----

TBD TFU 34.43.00.011


No



TCAS ROCKWELL

622-8971-320

622-8971-322822-1293-322

----

TBD TFU 34.43.00.011


No

344300 TCAS ARINC 429 NO MAINT ACTION if no logbook complaint. This deviation has been identified.

TCAS 4066010-903

----

4066010-905 TFU 344300006


No

344300 TCAS UNTRACEABLE NO MAINT ACTION if no log book TCAS complaint. TCAS 4066010-903

----

4066010-905 TFU 344300006


No




ATA Filter

344333 FWC(i): NO DATAFROM TCAS (i = 1 or 2)


TCAS HONEYWELL

066-50000-1x08

066-50000-2x204066010-903/9044066010-905

940-300-001

----

TBD TFU 34.43.00.011


No



TCAS ACSS

7517900-10002

7517900-10003

----

TBD TFU 34.43.00.011


No



TCAS ROCKWELL

622-8971-320

622-8971-322822-1293-322

----

TBD TFU 34.43.00.011


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


No


TCAS ACSS

7517900-10002

7517900-10003

----

TBD TFU 34.43.00.011


No




ATA Filter


TCAS ROCKWELL

622-8971-320

622-8971-322822-1293-322

----

TBD TFU 34.43.00.011


No


TCAS HONEYWELL

066-50000-1x08

066-50000-2x204066010-903/9044066010-905

940-300-001

----

TBD TFU 34.43.00.011


No


TCAS ACSS

7517900-10002

7517900-10003

----

TBD TFU 34.43.00.011


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


No


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


Yes




ATA Filter



TCAS HONEYWELL

066-50000-1x08

066-50000-2x204066010-903/9044066010-905

940-300-001

----

TBD TFU 34.43.00.011


Yes



TCAS ACSS

7517900-10002

7517900-10003

----

TBD TFU 34.43.00.011


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


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


No


TCAS ROCKWELL

622-8971-320

622-8971-322822-1293-322

----

TBD TFU 34.43.00.011


No




ATA Filter


TCAS ACSS

7517900-10002

7517900-10003

----

TBD TFU 34.43.00.011


No

345000 MODE S i NO MAINT ACTION if no logbook complaint. TCAS 4066010-903

----

4066010-905 TFU 344300006


No

345133 AFS:DMEi NO MAINT ACTION if no log book complaint FMGC PEGASUS

C13042xA01

----

TBD


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


No




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


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


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


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


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


No




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


No

345331 NO ADF(i) DATA No maintenance action when ADF 1 or/and 2 not installed on the aircraft.

CFDIU

----

N/A


Yes

345531 AFS : VOR i NO MAINT. ACTION if no logbook complaint FMGC All P/N

----

TBD


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


No

345572 VOR i RECEIVER NO MAINT. ACTION if no log book complaint. VOR 204-1231-3610

----

VSB RVA-36A-34-54 TFU 345500010


No




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


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


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


Yes

383134 VSC NO MAINT. ACTION VSC 14404-011A

----

14404-011B TFU 38 31 00 022 SB 38-1044 REV2 VSB 14440403802


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


No




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


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


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


No




ATA Filter

499414 OIL PRESS SW P14 NO MAINT. ACTION if no logbook complaint ECB (GTCP 36-300)

304817-1

----

304817-2


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


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


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


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


Yes




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


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


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


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


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


No




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


No

793311 QUALIFIER Bi/WXRj (1SQj)(i=1 or 2 and j= 1 or 2)


RADAR 822-1710-201

----

822-1710-202


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)


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


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


Yes




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


Yes

XXXXXX DME : NO DATA FROM CONTROL SOURCE

NO MAINT. ACTION DME 9599-614-03105

----

VSB TDM-709-34-012


Yes

XXXXXX ILS i : NO DATA FROMCONTROL SOURCE

NO MAINT. ACTION ILS 20412303518

B401ACM0404

VSB RIA-35A-34-41 TFU 343600004


No

XXXXXX VHFi:NO DATA FROMCONTROL SOURCE

NO MAINT. ACTION VHF 622-5219-020

B401ACM0404

VSB VHF-700-23-30 TFU 231200007


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


Yes


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


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


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


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


Yes

1Part B : page Revision 29



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)


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


No

2163 AFT(FWD) CAB DUCT OVHT Check Temp. sensor output resistance ZC All P/N

----

N/A TFU 216318001 / SIL 21-049


No

2163 CKPT DUCT OVHT Check Temp. sensor output resistance ZC All P/N

----

N/A TFU 216318001 / SIL 21-049


No




ATA Filter

2200 AUTO FLT A/THR OFF Configuration Warning FMGC All P/N

----

N/A N/A


Yes

2200 AUTO FLT AP OFF Configuration Warning FMGC All P/N

----

N/A N/A


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


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


No




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


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


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


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


No




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


No

261600 SMOKE AFT CRG BTL2

FAULT (if installed)



----

Z014H000131A

Z014H000031A


No

261600 SMOKE FWD CRG BTL1

FAULT



----

Z014H000131A

Z014H000031A


No

261600 SMOKE FWD CRG BTL2

FAULT (if installed)



----

Z014H000131A

Z014H000031A


No




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


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


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


No

2700 F/CTL SPD BRK DISAGREE Configuration warning FCDC All P/N

----

N/A


Yes




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


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


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


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


No




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


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


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


No




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


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


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


No




ATA Filter

3100 CFDIU


NO MAINT. ACTION if CFDIU power up test result is : CFDIU BITE MEMORY

CFDIU B401ACM0404

----

Amdt A TFU 313234031 / TSM ATA31


No

3100 DMU


Associated with the message : CAGA MEMORY FAIL.

DMU 903116243BOBOG0903116243BODOJ0903116243B0B0G1903116243B0D0J1

----

903116243B3B3G4

903116243B3B2G3903116243B3D2J3

TFU 313600013 / TSM ATA 31


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


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


Yes




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


Yes

3200 LGCIU i FAULT NO MAINT. ACTION if BITE test OK LGCIU 664700500A4A

----

664700500A4B TFU 323134043


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


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


Yes




ATA Filter

3400 NAV GPWS FAULT NO MAINT. ACTION if occurs on ground during Taxiing or Lining-up

ILS 20412303518

----

20412303521

20412303532

TFU 344800002


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


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


No

3410 ADRi


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


No




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


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


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


No

3410 NAV ADRx FAULT No associated maintenance message(source ADR).Follow advice given in TFU341000012.

ADIRU HG1150AC05

----

HG1150AC06 TFU 341000012/SB34-1084


No




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


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


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


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


No




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


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


No

3600 AIR BLEED


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


No

3800 VSC


NO MAINT ACTION VSC 14404-011A

----

14404-011B TFU 38 31 00 022 SB 38-1044 REV2 VSB 14440403802


Yes




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


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


No

7700 ENG i EIU


DISREGARD THE MESSAGE if occurs after gear non retraction.

LGCIU 664700500A4B

----

664700500A4C TFU 323173001/323471043


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




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


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


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+


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


No




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


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


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


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


No




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


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


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


No



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


215100 FLOW SEL NO MAINT. ACTION ZC 775A0000-05

----

775A0000-06


1Part C : page Revision 29



ATA

215218 Pi BLEED TEMP SENSOR NO MAINT. ACTION ZC 775A0000-05

----

775A0000-06 TFU 216334044


216111 Pi COMP TEMP SENSOR NO MAINT. ACTION ZC 775A0000-05

----

775A0000-06 TFU 216334044


216112 Pi COMP OVHT SENSOR NO MAINT. ACTION ZC 775A0000-05

----

775A0000-06 TFU 216334044


216115 Pi OUTLET TEMP SENSOR NO MAINT. ACTION ZC 775A0000-05

----

775A0000-06 TFU 216334044


216134 PACKi CONT NO MAINT. ACTION ZC 775A0000-05

759A0000-06/-07

775A0000-06

759A0000-08

TFU 216134001 / TFU 216334044

PCAssociated Part :




ATA

216151 Pi RAM AIR IN ACTUATOR NO MAINT. ACTION ZC 775A0000-05

----

775A0000-06 TFU 216334044


216152 PiRAM AIR OUT ACTUATOR NO MAINT. ACTION ZC 775A0000-05/-06/-07

----

775A0000-08 TFU 216334044


216153 TURBINE BYPASS VALVE NO MAINT. ACTION ZC 775A0000-05

----

775A0000-06 TFU 216334044


216315 TEMP SENSOR FWD (AFT)CAB DUCT I

NO MAINT. ACTION ZC 775A0000-05

----

775A0000-06 TFU 216334044


216315 TEMP SENSOR COCKPITDUCT I


----

775A0000-06 TFU 216334044





ATA

216316 TEMP SENSOR R/H (L/H)MIXER I


----

775A0000-06 TFU 216334044


216317 TEMP SENSOR FWD (AFT)CAB I


----

775A0000-06 TFU 216334044


216317 TEMP SENSOR COCKPIT I NO MAINT. ACTION ZC 775A0000-05

----

775A0000-06 TFU 216334044


216318 FWD (AFT) CAB DUCTOVHT SENSOR I


----

775A0000-06 TFU 216334044


216318 COCKPIT DUCTOVHT SENSOR I


----

775A0000-06 TFU 216334044





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


216351 TRIM AIR VALVE COCKPIT NO MAINT. ACTION ZC 775A0000-05/-06/-07

----

775A0000-08 TFU 216000004


216351 TRIM VALVE FWD (AFT) CAB NO MAINT. ACTION ZC 775A0000-05/-06/-07

----

775A0000-08 TFU 216000004


216352 TRIM AIR PRESS VALVE I NO MAINT. ACTION ZC 775A0000-05

----

775A0000-07 TFU 216000003





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


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.


LA2T0S162C0C0F1

LA2T0S111C1B0F1

----

LA2T0J13000C0F1 TFU 46 00 00 002


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


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

PES 1142300-131-xx

----

VSB AVI-93-32 TFU 233300009





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


242100 CHECK GCUi PIN A8A,A9BIDGi PIN B7,B8 WIRING

GPCU 740121A

----

740121B

(S/B 24-1077)

TFU 244100002 / TSM ATA 24 pB 401


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


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


244134 GPCU NO MAINT. ACTION GPCU 740121A

----

740121B

(SB-24-1077)





ATA

284216 CTR CADENSICON 20 QT NO MAINT. ACTION Cadensicon 796-809-5

----

796-809-6 TFU 284234029


284216 L(R) CADENSICON 19QTi NO MAINT. ACTION Cadensicon 796-809-5

----

796-809-6 TFU 284234029 / TFU 284234016


301151 R(L) WAI FILTER OR VALVE10DL(9DL)


----

775A0000-07 TFU 216000003


303134 PHC 6 DA 1(2,3) PHC 1663214-200

----

1663214-301 TFU 303134006 / TSM ATA 30


313234 CFDIU(1TW1)/ATSU1(1TX1) Protocol problem between ATSU and CFDIU. No maintenace action required.


LA2T0S162C0C0F1

LA2T0S11C1B0F1

----

LA2T0J13000C0F1 TFU 46 00 00 002





ATA

313234 CFDIU(1TW)/WXRi (i = 1 or 2)

No maintenance action required if no logbook complaint.

RADAR 822-1710-201

----

822-1710-202


313334 NO CLOCK DATA NO MAINT. ACTION FDIU 9026-16079-01B2

----

9026-16079-02B3


313334 NO DMC1 DATA NO MAINT. ACTION FDIU 9026-16079-01B2

----

9026-16079-02B3


313334 NO FWCi DATA NO MAINT. ACTION FDIU 9026-16079-01B2

----

9026-16079-02B3


313334 NO CFDS DATA NO MAINT. ACTION FDIU 9026-16079-01B2

----

9026-16079-02B3





ATA

313334 NO SDAC 1 DATA NO MAINT. ACTION FDIU 9026-16079-01B2

----

9026-16079-02B3


313355 DFDR PLAY BACK NO MAINT. ACTION FDIU 9026-16079-01B2

----

9026-16079-02B3 TFU 313300007


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


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


315534 SDACx(1WVx)/ATSU1(1TX1) ATSU host platform S/W

LA2T0S111C1B0F1

----

LA2T0J13000C0F1 TFU 46 00 00 002





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.


LA2T0S162C0C0F1

----

LA2T0J13000C0F1


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.


LA2T0S162C0C0F1

LA2T0S111C1B0F1

----

LA2T0J13000C0F1 TFU 46 00 00 002


341034 NO DATA FROM ADIRS NO MAINT. ACTION if appears in Phase 1,2 or 10 .

ZC 775A0000-05

----

775A0000-06 TSM ATA 21


341200 No access to ZONTPHC1(2,3) INTERFACE

NO MAINT. ACTION PHC 1663214-200

----

1663214-301 TFU 303100013


341200 CHECK ADIRU1 (2,3) R STAPHC1(2,3) INTERFACE


----

1663214-301 TFU 303100013





ATA

341200 CHECK ADIRU1 (2,3) L STAPHC1(2,3) INTERFACE


----

1663214-301 TFU 303100013


341200 CHECK ADIRU 1 (2,3) AOAPHC1(2,3) INTERFACE


----

1663214-301 TFU 303100013


341200 CHECK ADIRU 1 (2,3) PITOPHC1(2,3) INTERFACE


----

1663214-301 TFU 303100013


341234 ADIRU3(1FP3) ADR BUS/WXRi(1SQi) (i = 1 or 2)


RADAR 622-5132-623

----

TBD


341234 ADIRU3(1FP3) ADR BUS/WXRi(1SQi) (i = 1 or 2)


RADAR 822-1710-201

822-1710-202

----

822-1710-203





ATA

341234 ADIRUi(1FPi) IR BUS/WXRj(1SQj) (i = 1, 2 or 3 and j = 1 or 2)


RADAR 822-1710-201

822-1710-202

----

822-1710-203


344233 RAi(2SAi)/WXRj(i = 1, 2 or 3 and j = 1 or 2)


RADAR 822-1710-201

----

822-1710-202


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


462134 ATSU1(1TX1) No maintenance action required. ATSU host platform S/W

LA2T0S162C0C0F1

LA2T0S111C1B0F1

----

LA2T0J13000C0F1 TFU 46 00 00 002





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


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


715100 J3, ADC1 NO MAINT. ACTION ECU 1459M55P15

1519M83P02

1459M55P16

1519M83P03

----

1459M55P17

1519M83P04

1820M27P01

TFU 732900012


715100 J4, ADC2 NO MAINT. ACTION ECU 1459M55P15

1519M83P02

1459M55P16

1519M83P03

----

1459M55P17

1519M83P04

1820M27P01

TFU 732900012


732500 CHECK EIU WHC INTERFACE Check/Confirm that EIU/WHC interface is defective

WHC 6664-202-3

----

6664-287-0 TFU 304034002





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


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


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


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



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


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


70 NVM FAULT DATA

NOT RETRIEVABLE

ECU 1459M55P15

1519M83P02

1459M55P16

1519M83P03

----

1459M55P17

1519M83P04

1820M27P01

TFU 732900031


21 GND failures report

in last leg report,

ZC 775A0000-05

775A0000-06

----

775A0000-07


1Part D : page Revision 29



ATA

21 No A/C ident in the

previous leg report


----

775A0000-07


21 NO ACCEPTABLE FAILURE IN

26

NO MAINT. ACTION if no log book complaint.

ZC 775A0000-05

----

775A0000-06 TFU 216334047


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


21 No software number

in P/N of Zone Cont.


----

775A0000-07





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


21 P.L.R. : Leg counting

deviation at leg 99

ZC 775A0000-05

----

775A0000-07


21 Test results

in coded form

ZC 775A0000-07

----

775A0000-07 TFU 216134002 / TFU 216334004 / TSM ATA 21


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





ATA

216351 FAILURE NOT CLEARLY

IDENTIFIED


ZC 775A0000-06

775A0000-05

----

775A0000-06 TFU 216334047


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


22 Disregard the indication

RTOK in the AFS Bite report

NO MAINT. ACTION FAC All P/N

----

N/A


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





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


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


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


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





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


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


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


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





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.


Z064H000031A

Z064H000031B

----

TBD (end 2005)


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.


Z064H000031A

Z064H000031B

----

TBD (end 2005)


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).


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)





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


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.


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


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





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


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


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


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





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


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


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


279334 AFS:ELACi NO MAINT. ACTION if associated to B SYS LO PRESS (respectively Y SYS LO PRESS).

FAC All P/N

----

N/A





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


279334 SEC3 OR BUS2 FROM ADR2

(ADR3 / IR2 / IR3)


FCDC 115370-0105

----

115370-1016

115370-0106

MPD Task : 313000-03-1


279434 SEC2 OR INPUT OF L(R)

THROTTLE CTL UNIT 8KSi


FCDC 115370-0105

----

115370-1016

115370-0106

MPD Task : 313000-03-1


279434 SEC3 OR WIRING FROM

SFCC i


FCDC 115370-0105

----

115370-1016

115370-0106

MPD Task : 313000-03-1





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


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


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


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 :




ATA

31 Bad PRINT OUT FORMAT. NO MAINT. ACTION Printer 805515-4501

----

805515-4501

VSB M3367

TFU 313522001


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


31 Duplication of Fault

message in PFR.

CFDIU B401ACM0404

----

B401ACM0606 TFU 313234029


31 GR-OU-ND or GN-D - -

messages in phase 8/9

Generated by type 2 system. No maintenance Action.

CFDIU B401ACM0506

B401ACM0507

----

C12860AA02





ATA

31 Incoherent PFR Fault

messages sent by the EIU.

Check EIU Previous Leg reports. EIU 3957900611

----

3957900612 TFU 313234029


31 Incoherent PFR recording

time in the PFR header.

Due to Flight phases transitions anomalies.

CFDIU B401ACM0404

----

B401ACM0506 TFU 313234029


31 Incomplete PFR Fault

messages.

Due to power transients. CFDIU B401ACM0404

----

B401ACM0506 TFU 313234029


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





ATA

31 Mixed GMT in PFR Due to power transients. CFDIU B401ACM0404

----

B401ACM0506 TFU 313234029


31 NO "SYST" DATA (INTM) If no logbook complaint, NO MAINT ACTION. This message is generated by the CFDIU (Source : CFDS).

CFDIU B401ACM0506

----

TBD


31 NO DMC1 DATA recorded in

CFDIU ground scanning

NO MAINT. ACTION CFDIU B401ACM0404

----

B401ACM0506 TFU 313234030


31 NO FWC DATA recorded in

CFDIU last leg report.


CFDIU B401ACM0404

----

B401ACM0506 TFU 313234030





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


31 PFR with NO FAULT / NO

WARNING.

Due to Flight phases transitions anomalies.

CFDIU B401ACM0404

----

B401ACM0506 TFU 313234029


31 System source without

Fault message.

Under investigation. No Maint. Action. CFDIU B401ACM0404

----

B401ACM0506 TFU 313234029


31 Untimely print out of

real time failure and warning.

In flight pull, PRINTER C/B. CFDIU B401ACM0404

----

Amdt A TFU 313234026





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


313234 ADFi : NO DATA FROM

CFDIU


ADF 204-1168-7513

622-5222-020

----

NONE


313234 AUDIO NO DATA FROM

CFDIU


AMU 2790CA03

----

NONE


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





ATA

313234 DME1(2,3) : NO DATA FROM

CFDIU


DME 622-4540-023

9599-614-03105

----

NONE


313234 HFi : NO DATA FROM

CFDIU


HF 622-5272-020

----

NONE


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


313234 RMP1(2,3) : NO DATA FROM

CFDIU


RMP 899-0850-002

899-0850-003

899-0850-004

----

NONE





ATA

313234 VHF1(2,3) : NO DATA FROM

CFDIU


VHF 204-1237-4417

----

NONE


313234 VOR 1(2,3) :NO DATA FROM

CFDIU


VOR 204-1231-3610

622-5220-020

204-1231-3623

204-1231-3613204-1231-3622

----

NONE


313234 WRX i : NO DATA FROM

CFDIU


WRX 204-1217-0418

204-1217-0421

----

VSB RTA-4A-34-173


313316 ACCELEROMETER Class 2 Fault message without associated Maintenance Status. Apply TSM procedure.

FDIU ED43A1D2

ED43A1D3

90261607902B3

----

ED43A1D5 MPD 313000-04-01





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


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


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


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





ATA

32 During TPIU Bite test

"NO RESPONSE" message may appears on the MCDU

Restart the TPIU Bite test TPIU 1058-34

----

TBD


32 Menu Mode access

possible during flight

LGCIU 664700500A4A

----

664700500A4B TFU 323134043


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


32 Nothing in the LGCIU

Last Leg report instead of "NO FAILURE"

LGCIU 664700500A4A

----

664700500A4B TFU 323134043





ATA

32 Spurious NO DATA FROM

CFDS in the LGCIU Ground scanning, with date ???31

NO MAINT. ACTION LGCIU 664700500A4A

----

664700500A4B TFU 323134041


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


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.


----

Z064H000031A

Z064H000031B


34 Bad leg incrementation

of GPWS Previous Leg Reports.

NO MAINT. ACTION GPWC 965-0676-020

----

9650676-020

S/W MOD 1

TFU 344800004





ATA

34 Bad LRU identification. NO MAINT. ACTION RADAR 204-1217-0418

204-1217-0421

----

VSB RTA-4A-34-161 TFU 344100007


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


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


34 Loss of fault messages

in the GPWC Previous Leg Reports.


----

9650676-020

S/W MOD 1

TFU 344800004





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


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


34 No transmission of

external failure at detection but after power cut

NO MAINT. ACTION HUDC 96154334-1

----

96154334-2


34 Random and transient

pattern (2sec) during aproach, instead of the wanted symbology display.

NO MAINT ACTION HUDC 9615433402

----

V65





ATA

34 same message with same

date and GMT but different leg numbers in the Previous Leg Reports.


----

965-0676-020

S/W MOD 1

TFU 344800004


34 Wrong identification of

DME : Message : DME-0 TRANSCEIVER

DME 622-4540-022

----

622-4540-023 TFU 345100009


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


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





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


45 CFDIU BUS The ATA chapter of this message should be 313234 instead of 45.

TCAS 4066010-904

----

TBD


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.


----

Z014H000031A

Z014H000131A


4621 GROUND SCANNING

ATSU failures may be missing in ground scanning report.

Always reset the ATSU before performing the ground scanning function.


LA2T0S162C0C0F1

----

LA2T0S111C1B0F1





ATA

4621 LINK TEST Before activating the link test function, select the VHF3 in DATA mode (if VHF3 in VOICE mode, the test fails).


LA2T0S162C0C0F1

LA2T0S111C1B0F1

----

LA2T0J13000C0F1 AMM task : 46 21 00 710 00200


4621 LRU identification

A/C interfacce P/N displayed on LRU ident page is software P/N (LA2T0S162C0C000) and not disk P/N (LA2T0S162C0C0F1)


LA2T0S162C0C0F1

LA2T0S111C1B0F1

----

LA2T0J13000C0F1 AMM tasks : 46 21 00 610 00100/120


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).


LA2T0S162C0C0F1

----

LA2T0S111C1B0F1 AMM tasks : 46 21 00 610 00300/320


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.


LA2T0S162C0C0F1

----

LA2T0S111C1B0F1





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


4621 PRINT FUNCTION The "*" indicating the possibility to print is not always displayed. The "*" is systematicaly displayed after activating the PRINT function.


LA2T0S162C0C0F1

----

LA2T0S111C1B0F1 TFU 46 00 00 002


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


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.


LA2T0S111C1B0F1

----

LA2T0J13000C0F1





ATA

49 Messages may be

duplicated in the PFR.

ECB (GTCP 36-300)

304817-1

----

304817-2


49 Some messages are sent

with more than 48 characters

APU GTCP 36.300 ECB (GTCP 36-300)

304640-3

----

304817-1


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


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





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


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


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)


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





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


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


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



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


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


ATA Failure Message


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


ATA Failure Message


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


ATA Failure Message


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


ATA Failure Message


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





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


ATA Failure Message


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)


EIS II Software


ATA Failure Message


316322 DU_ND_FO(3WK2)/_________ND_FO_POT(8WK2)


EIS II Software

316322 DU_PFD_CAPT(1WK1)/______PFD_CAPT_POT(7WK1)


EIS II Software

316322 DU_PFD_FO(1WK2)/________PFD_FO_POT(7WK2)


EIS II Software

316322 DU_SD(2WK2)/____________ECP(2WM)


EIS II Software

324418 SDAC$:LH_Y_BRK_PRESSXDCR_63GG

06 350E053020606FWC

324418 SDAC$:RH_Y_BRK_PRESSXDCR_62GG

06 350E053020606FWC


ATA Failure Message


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


ATA Failure Message


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


ATA Failure Message


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


ATA Failure Message


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


ATA Failure Message


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






ATA Failure Message


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






793415 CHECK_OIL_PRESS_SWITCH3EN$

02 09 1058-34TPIS


ATA Failure Message


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


CFDS Trouble Shooting

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