CFDS Trouble Shooting
April 14, 2017 | Author: mohnishvarma | Category: N/A
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Description
AIRBUS
CUSTOMER SERVICES DIRECTORATE 1 ROND POINT MAURICE BELLONTE 31707 BLAGNAC CEDEX FRANCE TELEPHONE + 33 (0 )5 61 93 33 33
SERVICE INFORMATION LETTER
TELEX AIRBU 530526F
SUBJECT:
Centralized Fault Display System (CFDS) Anomalies
ATA CHAPTER:
00
AIRCRAFT TYPE:
A318, A319, A320, A321
APPLICABILITY:
All Aircraft
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. 1.
PURPOSE: The present SIL identifies all the known CFDS anomalies/BITE deviations. It is intended to be used by 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 relevant TFU/TSM procedure. The fault messages/warnings or behaviours which should be known by line maintenance teams, are covered by the Trouble Shooting Manual. More precisely, the messages/behaviours described in this SIL are those for which the conditions of occurrence are precise/known and reproducible. In addition are mentioned messages/behaviours for which a statistical survey revealed a too high number of occurrences (more than 1 every 5 flights per 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 part numbers of equipment fitted on their aircraft.
SIL NUMBER: PAGE: CREATION DATE: REVISION: REVISION: DATE:
00-028 1 of 9 + Appendix Nov 30/1989 29 31-MAR-06
CUSTOMER SERVICES DIRECTORATE
AIRBUS
1 ROND POINT MAURICE BELLONTE 31707 BLAGNAC CEDEX FRANCE TELEPHONE + 33 (0 )5 61 93 33 33 TELEX AIRBU 530526F
2.
SERVICE INFORMATION LETTER
RECOMMENDATIONS The appendix is divided into five parts, which are: A. The list of PFR failure messages (internal and external) which request specific maintenance action. B. The list of ECAM WARNINGS and MAINTENANCE STATUS shown on the PFR, which request 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 chapter associated 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 SIL NUMBER: PAGE: CREATION DATE: REVISION: REVISION: DATE:
00-028 2 of 9 + Appendix Nov 30/1989 29 31-MAR-06
CUSTOMER SERVICES DIRECTORATE
AIRBUS
1 ROND POINT MAURICE BELLONTE 31707 BLAGNAC CEDEX FRANCE TELEPHONE + 33 (0 )5 61 93 33 33 TELEX AIRBU 530526F
SERVICE INFORMATION LETTER
Nota 4:For each item, carefully check that the part number fitted on your aircraft corresponds to the affected 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 the position 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 filter content, 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
SIL NUMBER: PAGE: CREATION DATE: REVISION: REVISION: DATE:
00-028 3 of 9 + Appendix Nov 30/1989 29 31-MAR-06
AIRBUS
CUSTOMER SERVICES DIRECTORATE 1 ROND POINT MAURICE BELLONTE 31707 BLAGNAC CEDEX FRANCE TELEPHONE + 33 (0 )5 61 93 33 33
SERVICE INFORMATION LETTER
TELEX AIRBU 530526F
5.
LIST OF EVOLUTIONS
PART ATA A A A A A A A A A A A A A A A A A A A A A B B C C E E E E E E
ITEMS
228334 FMGCi (1CAj)/RMPi (1RGi)/ILSi (1RTi) HF1 COUPLER (4RE1)/FEEDER HF1 (6RE1)/ANTENNA 231133 (5RE1) 316322 DU ND CAPT(3WK1)/ND CAPT POT(8WK1) 316322 DU ND FO(3WK2)/ND FO POT(8WK2) 316322 DU PFD CAPT(1WK1)/PFD CAPT POT(7WK1) 316322 DU PFD FO(1WK2)/PFD FO POT(7WK2) 316322 DU EWD(2WK1)/ECP(6WM) 316322 DU SD(2WK2)/ECP(6WM) 341234 QUALIFIER Di/WXRj (1SQj) (i = 1 or 2 and j = 1 or 2) ADIRUi+3(1FPi+3) ADRBUS/WXRj(1SQj) 341234 (i = 1 or 2 and j = 1 or 2) 344133 WXRi (1SQi) (i = 1 or 2) DMCi: NO WXRj CHj DATA 344133 (i = 1, 2 or 3 and j = 1 or 2) 344300 DMC(i): NO TCAS DATA (i = 1 or 2) 344333 FWC(i): NO DATA FROM TCAS (i = 1 or 2) 344333 NO TCAS DATA 344334 ATC(i): NO DATA FROM TCAS (i = 1 or 2) 344334 TCAS (1SG) 345233 QUALIFIER Ci/WXRj (1SQj) (i = 1 or 2 and j = 1 or 2) 345233 ATCi (1SHi)/TCAS (100SG) source TCAS (i = 1 ou 2) 345233 NO ATCi DATA source CFDS (i = 1 or 2) 345233 ATCi (1SHi)/TCAS (1SG) source TCAS (i = 1 ou 2) 2161 AIR:PACK i REGUL FAULT 3443 NAV TCAS FAULT 313234 CFDIU (1TW)/WXRi (i = 1 or 2) 341234 ADIRU3 (1FP3) ADR BUS/WXRi (1SQi) (i = 1 or 2) 2161 AIR_PACK_1$2_FAULT DU_ND_CAPT(3WK1)/_______ 316322 ND_CAPT_POT(8WK1) DU_ND_FO(3WK2)/__________ 316322 ND_FO_POT(8WK2) DU_PFD_CAPT(1WK1)/_______ 316322 PFD_CAPT_POT(7WK1) DU_PFD_FO(1WK2)/________ 316322 PFD_FO_POT(7WK2) DU_EWD(2WK1)/__________ 316322 ECP(6WM)
TYPE
REMARK
Revised
Wording
New New New New New New New New Revised
Wording + P/N
New Revised
Wording
Revised Revised Revised Revised Revised New New Revised Revised Revised Revised New New Revised
Wording + P/N Wording + P/N Wording + P/N Wording + P/N Wording + P/N
Wording + P/N Add TFU ref. Wording Add TFU ref.
Wording
New New New New New
SIL NUMBER: PAGE: CREATION DATE: REVISION: REVISION: DATE:
00-028 4 of 9 + Appendix Nov 30/1989 29 31-MAR-06
CUSTOMER SERVICES DIRECTORATE
AIRBUS
1 ROND POINT MAURICE BELLONTE 31707 BLAGNAC CEDEX FRANCE TELEPHONE + 33 (0 )5 61 93 33 33 TELEX AIRBU 530526F
E E E E
6.
SERVICE INFORMATION LETTER
DU_SD(2WK2)/____________ ECP(6WM) ADIRU$($FP$)_IR_BUS/____ 341234 WXR$($SQ$) ADIRU$$$($FP$$$)_ADRBUS/ 341234 WXR$($SQ$) 345233 NO_ATC_$_DATA__ 316322
New New New Revised
Wording + P/N
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.
SIL NUMBER: PAGE: CREATION DATE: REVISION: REVISION: DATE:
00-028 5 of 9 + Appendix Nov 30/1989 29 31-MAR-06
CUSTOMER SERVICES DIRECTORATE
AIRBUS
1 ROND POINT MAURICE BELLONTE 31707 BLAGNAC CEDEX FRANCE TELEPHONE + 33 (0 )5 61 93 33 33 TELEX AIRBU 530526F
SERVICE INFORMATION LETTER
LIST OF ABREVIATIONS
SIGLUM ACARS ACSC ACP ADIRU ADF ADR AEVC AFS AIDS AMM AMU AOA APU ASSY ATA ATC A/P A/THR ATIMS BCL BITE BMC BSCU CAM CFDIU CFDS CHC CIDS CPC CVC C/B DC DFDR DLRB DLS DMC DME
TITLE Aircraft Communication Addressing & Reporting System Air Conditionning System Controler Audio Control Panel Air Data Inertial Reference Unit Automatic Direction Finder Air Data Reference Avionic Equipment Ventilation Controller Auto Flight System Aircraft Integrated Data System Aircraft Maintenance Manual Audio Management Unit Angle-Of-Attack Auxiliary Power Unit Assembly Air Transport Association Air Traffic Control Autopilot Auto Thrust Air Traffic and Information Management System Battery Charge Limiter Built-in Test Equipment Bleed Monitoring Computer Braking & Steering Control Unit Cabin Assignment Module Centralized Fault Detection Interface Unit Centralized Fault Display System Cargo Heat Controller Cabin Intercommunication Data System Cabin Pressure Controller Cargo Ventilation Controller Circuit Breaker Direct Current Digital Flight Data Recorder Data Loader Routing Box Data Loader Selector Display management Computer Distance Measuring Equipment SIL NUMBER: PAGE: CREATION DATE: REVISION: REVISION: DATE:
00-028 6 of 9 + Appendix Nov 30/1989 29 31-MAR-06
CUSTOMER SERVICES DIRECTORATE
AIRBUS
1 ROND POINT MAURICE BELLONTE 31707 BLAGNAC CEDEX FRANCE TELEPHONE + 33 (0 )5 61 93 33 33 TELEX AIRBU 530526F
SIGLUM DMCU DMU DU ECAM ECB ECS ECU EFDU EIU ELAC EVMU FADEC FAC FCD FCDC FCOM FCU FCV FDIMU FDIU FG FIN FL FM FMGC FMGS FMS FQI CH FQIC FT FWC FWD F/CTL F/D GCU GPWC GPCU GW HF HP HPV HUD
SERVICE INFORMATION LETTER
TITLE Drain Mast Central Unit Data Management Unit Display Unit Electronic Centralized Aircraft Monitor Electronic Control Box Environmental Control System Engine Control Unit Engine Fire Detection Unit Engine Interface Unit Elevator Aileron Computer Engine Vibration Monitoring Unit Full Authority Digital Engine Control Flight Augmentation Computer Flight Control Display Flight Control Data Concentrator Fuel Control and Management Computer Flight Control Unit Flow control Valve Flight Data Interface Management Unit Flight Data Interface Unit Flight Guidance Functional Item Number Flight Level Flight Management Flight Management & Guidance Computer Flight Management & Guidance System Flight Management System Fuel Quantity Indicator Channel Fuel Quantity Indication Computer Feet Flight Warning Computer Forward Flight Control Flight Director Ground Control Unit Ground Proximity Warning Computer Ground Power Control Unit Gross Weight High Frequency High Pressure High Pressure Valve Head Up Display SIL NUMBER: PAGE: CREATION DATE: REVISION: REVISION: DATE:
00-028 7 of 9 + Appendix Nov 30/1989 29 31-MAR-06
CUSTOMER SERVICES DIRECTORATE
AIRBUS
1 ROND POINT MAURICE BELLONTE 31707 BLAGNAC CEDEX FRANCE TELEPHONE + 33 (0 )5 61 93 33 33 TELEX AIRBU 530526F
SIGLUM HUDC ILS ISIS LGCIU LOP LRU L/G M MCDU MEL MFT MLG MM MMEL MPD MRB MSN MTBF MTBR MTBUR MU ND NLG NM OBRM OVHT PA PC PCU PDU PES PFD PFR PHC PRAM PRV PTT PTU P/N QAR RA RFI
SERVICE INFORMATION LETTER
TITLE Head Up display Computer Instrument Landing System Integrated Standby Instrument System Landing Gear control & Interface Unit Low Oil Pressure Line Replacement Unit Line Replacement Unit Landing Gear Mach Number Multi-purpose Control and Display Unit Master Equipment List Maintenance Filter Tool Main Landing Gear Maintenance Manual Master Minimum Equipment List Maintenance Planning Document Maintenance Review Board Manufacturer Serial Number Mean Time Between Failures Mean Time Between Removal Mean Time Between Unscheduled Removal Management Unit Navigation Display Nose Landing Gear Nautic Miles On Board Replaceable Module Overheat Public Address Pack Controller Power control Unit Power Distribution Unit Passenger Entertainment System Primary Flight Display Post Flight Report Probe Heat Computer Pre-Recorded Announcement and Music Pressure Regulator Valve Push-To-Talk Power Transfer Unit Part Number Quick Access Recorder Radio Altimeter Request For Information SIL NUMBER: PAGE: CREATION DATE: REVISION: REVISION: DATE:
00-028 8 of 9 + Appendix Nov 30/1989 29 31-MAR-06
CUSTOMER SERVICES DIRECTORATE
AIRBUS
1 ROND POINT MAURICE BELLONTE 31707 BLAGNAC CEDEX FRANCE TELEPHONE + 33 (0 )5 61 93 33 33 TELEX AIRBU 530526F
SIGLUM RFR RMP SB SDAC SDCU SDI SEC SFCC SFCS SFE SIL SRM TAT TBD TEM TFU THS TLT TPIU TRU TSM ULD UPPR CRG DET VHF VOR WAI WAIV WDB WHC WRX ZC
SERVICE INFORMATION LETTER
TITLE Request For Revision Radio Management Panel Service Bulletin System Data Acquisition Concentrator Smoke Detection Control Unit Spares Data Improvement Spoiler Elevator Computer Slat/Flap Control Computer Slat/Flap Control System Supplier Furnished Equipment Service Information Letter Structural Repair Manual Turn Around Time To Be Defined Tool and Equipment Manual Technical Follow-Up Trimmable Horizontal Stabilizer Temperature Limitation Thermostat Tyre Pressure Indicating Computer Transformer Rectifier Unit Trouble Shooting Manual Unit Load Device Upper Cargo Smoke Detector Very High Frequency VHF Omnidirectional Range Wing Anti-Ice Wing Anti-ice Valve Wall Disconnect Box Window Heat Computer Weather Radar Transceiver Zone Controller
SIL NUMBER: PAGE: CREATION DATE: REVISION: REVISION: DATE:
00-028 9 of 9 + Appendix Nov 30/1989 29 31-MAR-06
SIL 00-028 PART A : Failure Messages ATA 000000
Failure message NO
DATA
Remark
Part
P/Ns Affected
Corrective P/N
NO MAINT. ACTION
CFDIU
B401ACM0505
B401ACM0506
Associated P/N : ---212853
FWD CARGO FAN OR SPLY 6H
NO MAINT. ACTION if power supply between FAN and CVC CVC is OK, 115 V 3 phases. (Minimum value : 110 V)
600615-01-500 600615-00-502
Associated P/N : ---212854
AFT CARGO FAN OR SPLY 35
NO MAINT. ACTION if power supply between FAN and CVC CVC is OK, 115 V 3 phases. (Minimum value : 110 V)
600615-01-500 600615-00-502
Associated P/N : ---215151
Pi FLOW CONTROL VALVE
FCV
Associated to Maintenance Status PACK 1(2) , NO MAINT. ACTION if Bite test OK
751A0000-06
Associated P/N : ---216334
EIUi : NO ZONE CONT P(S) DATA
ZC
Associated with ECAM warning : ENG1(2) BLEED STATUS FAULT. NO MAINT. ACTION
775A0000-06
Associated P/N : ----
Part A : page
1
Doc X Ref
Filter No
---600615-01-502
TFU 212854002
No
TFU 212854002
No
TFU 215151004
No
TFU 216334051/ TFU 732900029 / TSM ATA 75
No
600615-00-503
---600615-01-502 600615-00-503
---751A0000-07
---775A0000-07
EIU CFMI
Revision 29
SIL 00-028 PART A : Failure Messages ATA 216334
Failure message EIUi NO ZONE CONT P(S) DATA
Remark
Part
P/Ns Affected
Corrective P/N
Doc X Ref
NO MAINT. ACTION If not associated to Maintenance Status : ENG1(2)EIU
EIU
3957900609 3957900610 3957900611 3957905003
3957900612
TFU 732534005 / TFU 732534042 / TSM ATA 71
No
TFU 216334051
No
3957905004
Associated P/N : ---216334
NO ZONE CTL DATA
ZC
NO MAINT. ACTION, Could be intermittent (INTM).
775A0000-06
---775A0000-07
Associated P/N : CFDIU 216334
SDACi: NO DATA FROM ECS i
NO MAINT. ACTION if occurs in phase 6
ZC
No Maintenance action
DMC
775A0000-06
DMCi : No FACj DATA
ALL P/N
B401ACM0404 TFU 216334051
775A0000-07
Associated P/N : ---226634
Filter
No
---Yes
9615325050 (Soft std DMC V50)
Associated P/N : ---228112
FCU (2CA) BUS CP-L/ WRX 1 (1SQ1)
RADAR 066-50008-301
If no logbook associated logbook complaint, No maintenance action is required.
No
066-50008-405 Soft 05
Associated P/N : ----
Part A : page
----
2
----
Revision 29
SIL 00-028 PART A : Failure Messages ATA 228112
Failure message FCU(2CA)CP-L BUS/ WXRi(1SQi) (i = 1 or 2)
Remark
Part
P/Ns Affected
No maintenance action required if no logbook complaint.
RADAR 822-1710-201
Associated P/N : ---228112
FCU(2CA)CP-R BUS/ WXRi(1SQi) (i = 1 or 2)
No maintenance action required if no logbook complaint.
RADAR 822-1710-201
Associated P/N : ---228112
FCU(3CA)CP-L BUS/ WXRi 1SQi (I=1 or 2)
NO MAINT. ACTION if recorded during Engine Start (flight phase 02) or during switching from WXR1 to WXR2 and no associated cockpit effect.
RADAR 822-1710-201
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
Associated P/N : ---228112
FCU(3CA)CP-R BUS/ WXRi 1SQi (I=1 or 2)
Associated P/N : ---228112
RADARi:NO DATA FROM EFIS i PANEL
RADAR 622-5132-020 622-5132-120
NO MAINT. ACTION if no log book complaint
Associated P/N : ----
Part A : page
3
Doc X Ref
Corrective P/N
Filter No
822-1710-202
---No
822-1710-202
---No
822-1710-202
---No
822-1710-202
---VSB WRT-701X-34-68 VSB WRT-701X-34-77
----
Revision 29
No
SIL 00-028 PART A : Failure Messages ATA
Failure message
228212
AFS:MCDUi
Remark
Part
P/Ns Affected
Corrective P/N
Doc X Ref
NO MAINT. ACTION if no log book complaint
FMGC
ALL P/N
NONE
TFU 229100011
Yes
TFU 46 00 00 002
Yes
Associated P/N : ---228212
MDCU3(3CA3)/ATSU1(1TX1)
No maintenance action if MCDU 3 not installed. Can be filtered if MCDU 3 not installed
228334
----
ATSU LA2T0S111C1B0F1 LA2T0J13000C0F1 host platform S/W
Associated P/N : ---AFS:FMGC$(DO NOT REMOVE) NO MAINT. ACTION
FAC
AFS:FMGCi
FMGC
FAC pre Std B397BAM0617
Filter
---Yes
B397BAM0617
Associated P/N : FMGC PEGA C13042xA01 228334
NO MAINT ACTION IF MESSAGE NOT ASSOCIATED WITH ANY ECAM WARNING AND COCPIT EFFECT
B546BAM0203 B546CCM0101 B546CAM0101 B398AAM0410 B398BAM0207 Associated P/N : ----
228334
AFS:FMGCi (FMi)
FMGC
NO MAINT. ACTION if no log book complaint
B398AAM0408 B398BAM0205 B398BCM0104
Associated P/N : ----
Part A : page
4
B546BAM0206
TFU229100055
Yes
TFU 229100010
Yes
B546CAM0102 B546CCM0104 B546BCM0205 C13042AA01 ---B398AAM0409 B398BAM0206 B398BCM0106
----
Revision 29
SIL 00-028 PART A : Failure Messages ATA 228334
Failure message AFS:FMGCi/ATHR ENGD FDBK
Remark
Part
P/Ns Affected
NO MAINT. ACTION if not associated with ECAM WARNING : AUTO FLT A/THR OFF.
FMGC B398AAM0xxx (LEGAC B398BAM0xxx Y) B398BCM0xxx
Corrective P/N
FMGCi (1CAi)/ RMPi(1RGi)/ILSi(2RTi)
ILS
No maintenance action if not logbook complaint
066-50006-X202 (Allied) 622-9738-041 (Collins)
----
MMR
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.
FMGCi(1CAj)/ RMPi(1RGi)/ILSi(1RTi)
No maintenance action if no FM auto reset reported in the FMGC logbook.
822-1152-121
(Allied) 822-0298-020 (Collins) ---VSB Collins GLU 920-34-19
Associated P/N : ---228334
All P/N
FMGECi(1CAi)/ RMPi(1RGi)/ILSi(1RTi)
ILS
No maintenance action if no logbook entry
622-9738-041 (Collins)
Associated P/N : ----
Part A : page
5
TSM task 34 36 00 810 870/871
No
---SIL 22-037 & SIL 22- No 038
N/A
Associated P/N : ---228334
No
TBD
Associated P/N : ---228334
Filter Yes
TBD
Associated P/N : ---228334
Doc X Ref
---No
N/A
----
Revision 29
SIL 00-028 PART A : Failure Messages ATA 230000
Failure message DIR1 (101RH)/OBRM
Remark
Part
P/Ns Affected
Corrective P/N
Maintenance advise: A CIDS interface and power-up test CIDS must be performed to confirm validity of the failure and to DIR clear the failure message from the ground report.
Z064H000030F Z064H000031A Z064H000031B
TBD (end 2005)
Associated P/N : ---231100
CHECK HF (i) ANTENNA CIRCUIT
HF 622-5272-020 TRANSC EIVER
NO MAINT ACTION if no log book entry
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
No maintenance action if no logbook compaint.
COUPLE 792-6140-001 R
822-0990-003 Collins HFS900D
VSB HFS-700-36
HF1 COUPLER(4RE1)/ FEEDER HF1(6RE1)/ANTENNA(5RE)
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 LA2T0J13000C0F1 HOST LA2T0J13002C0F1 Platform S/W
6
No
Yes
---No
---C12860AA02
Associated P/N : CFDIU
Part A : page
TFU 231100002
TBD
Associated P/N : ---231133
No
----
Associated P/N : ---231133
Filter
----
Associated P/N : ---231100
Doc X Ref
TFU 46 00 00 002
B401ACM0507
Revision 29
Yes
SIL 00-028 PART A : Failure Messages ATA 231133
Failure message NO HF 1 DATA Source CFDS
Remark
Part
P/Ns Affected
No Maint. Action if triggered in phase 02.
HF 964-0452-001 Transcei 964-0452-012 ver
CHECK VHF 1 ANTENNA CIRCUIT
NO MAINT. ACTION if VSB mentioned in Corrective P/N VHF not incorporated.
622-5219-020
---VSB VHF-700-23-36
NO VHF3 DATA
NO MAINT. ACTION when VHF3 not installed
CFDS
NO MAINT. ACTION if no log book complaint
VHF
VHF 3 TRANSCEIVER
C12860AA02 (STD 9B)
CFDIU STD 10 TBC
622-5219-020
VHF0(1RC0)
VHF3
NO MAINT. ACTION if occurs in phase 02
822-1047-030
Associated P/N : ----
Part A : page
7
Yes
---VSB VHF-700-23-38
Associated P/N : ---231233
No
----
Associated P/N : ---231233
TFU 231200011
VSB VHF-700-23-30
Associated P/N : ---231233
Filter No
TBD
Associated P/N : ---231211
Doc X Ref
Corrective P/N
No
---Yes
N/A
----
Revision 29
SIL 00-028 PART A : Failure Messages ATA 231313
Failure message RMPi(1RGi)/RMPj(1RGj)
Remark
Part
P/Ns Affected
Corrective P/N
NO MAINT. ACTION required
RMP
C12848AA01 C12848CA01
TBD
Associated P/N : ---232834
SDU1(5RV1)/ATSU1(1TX1)
Generated by ATSU when SATCOM not installed. Disregard when SATCOM not installed (This message may be displayed on PFR, System Test and Ground scanning).
ATSU LA2T0S162C0C0F1 host platform S/W
Associated P/N : ---237300
FAP1 (120RH)/ DIR2/CAM
Maintenance advise: A CIDS interface and power-up test CIDS SDF should be performed to confirm validity of the failure message. The associated time may be completely erroneous.
Z064H000030F Z064H000031A Z064H000031B
Associated P/N : ---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 Z064H000031A Z064H000031B
Associated P/N : ---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 Z064H000031A Z064H000031B
Associated P/N : ----
Part A : page
8
Doc X Ref
Filter Yes
---LA2T0S111C1B0F1
TFU 46 00 00 002
Yes
---No
TBD (end 2005)
---No
TBD (end 2005)
---No
TBD (end 2005)
----
Revision 29
SIL 00-028 PART A : Failure Messages ATA 237313
Failure message AAP (126RH) ATT 4L
Remark
Part
P/Ns Affected
Corrective P/N
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
AAP (126RH) ATT 4L/ DEU B (300RH7)
CIDS DIR
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.
AIP (320RH1) ATT 1L
Maintenance advise: A CIDS interface and power-up test CIDS SDF should be performed to confirm validity of the failure message. The associated time may be completely erroneous.
AIP (320RH9) ATT 4L
Maintenance advise: A CIDS interface and power-up test CIDS SDF should be performed to confirm validity of the failure message. The associated time may be completely erroneous.
Z064H000030F
Z064H000031B
Z064H000030F Z064H000031A Z064H000031B
----
Z064H000030F Z064H000031A Z064H000031B
CIDS2(102RH)
ACSC 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.
1803A0000-03
Associated P/N : ----
Part A : page
9
No
TBD (end 2005)
---No
TBD (end 2005)
Associated P/N : ---237334
No
Z064H000031A
Associated P/N : ---237322
No
----
Associated P/N : ---237322
Filter
Z064H000031B
Associated P/N : ---237313
Doc X Ref
---EYDCC Technical note P2161ME0308866V1
TBD
----
Revision 29
No
SIL 00-028 PART A : Failure Messages ATA 237334
Failure message DIR1 (101RH) -SDF
Remark
Part
P/Ns Affected
Corrective P/N
Maintenance advise: A CIDS interface and power-up test CIDS SDF should be performed to confirm validity of the failure message. The associated time may be completely erroneous.
Z064H000030F Z064H000031A Z064H000031B
TBD (end 2005)
Associated P/N : ---237334
DIR1 (101RH) BUS/ DIR2 (102RH)
Maintenance advise: A CIDS interface and power-up test CIDS SDF should be performed to confirm validity of the failure message. The associated time may be completely erroneous.
Z064H000030F Z064H000031A Z064H000031B
NO CIDS 1(2) DATA
CIDS
Please refer to TFU 23 73 00 083
Z010H000abcd abcd=3113 or 3117 or 5115 or 5117 or 5118 or 5119 or
Filter No
---No
TBD (end 2005)
Associated P/N : ---237334
Doc X Ref
---TBD
TFU 23 73 00 083
Yes
TFU 23 73 00 083
No
TFU 243800008
No
520A or 521A Associated P/N : ALL P/N 237334
NO CIDS 1(2) DATA (INTM)
CIDS
Please refer to TFU 23 73 00 083
CFDS
Z010H000abcd TBD abcd= 3113 or 3117 or 5115 or 5117 or 5118 or 5119 or 520A or 521A Associated P/N : ALL P/N
24
P-OW-ER CONSUMPTION
NO MAINT ACTION if no log book complaint
BCL
35-0L5-1003-06
Associated P/N : ----
Part A : page 10
CFDS
35-0L5-1004-07
----
Revision 29
SIL 00-028 PART A : Failure Messages ATA 240000
Failure message POWER SUPPLY INTERRUPT
Remark
Part
P/Ns Affected
Corrective P/N
NO MAINTENANCE ACTION
ILS
066-50008-0301
066-50008-0405
Associated P/N : ---240000
POWER SUPPLY INTERRUPT Source 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
IDGi DISCONNECTED
GPCU
Check Class 3 Fault messages.
740121A
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.
740121B
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
767584J
All P/N
Associated P/N : ----
Part A : page 11
TFU 244100002 / TSM ATA 24
No
TFU 24.21.00.039
No
----
Associated P/N : ---242255
Yes
----
Associated P/N : ---242151
No
EIS II Soft Std S5
(SB24-1077)
GCU
Filter
----
Associated P/N : ---242151
Doc X Ref
---Yes
N/A
----
Revision 29
SIL 00-028 PART A : Failure Messages ATA 242300
Failure message CHECK GCU APU PIN C1, C5 GEN APU PIN A9, A10
Remark
Part
P/Ns Affected
Corrective P/N
Doc X Ref
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
TFU 244100008
No
TFU 315500003
Yes
(SB 24-1074)
Associated P/N : ---243251
SDACi: NO TR1 CURRENT 1PU1
SDAC
At APU start NO MAINT. ACTION
35-0E5-1510-22 35-0E5-1611-22
---35-0E5-1513-31
Associated P/N : ---243834
SDACi : NO DATA FROM BCLi
NO MAINT. ACTION if no Log Book complaint.
SDAC
No maintenance action required.
CIDS DIR
35-0E5-1510-22 35-0E5-1611-22
----
SLIDE BTL XY/ DEU B (300RHZ) with X=1, 3 or 4 and Y=R or L and Z=1, 6 or 8.
Z064H000030F
----
WRG: CAN BUS A (or B)
NO MAINT. ACTION if fault message displayed after a reset of CIDS or CIDS-SDF
CIDS DIR
Z064H000031B
Z064H000030D Z064H000030E Z064H000030F
Associated P/N : ----
Part A : page 12
No
Z064H000031A
Associated P/N : ---261000
Yes
35-0E5-1513-31
Associated P/N : ---256200
Filter
---SIL 23-039
TBD
----
Revision 29
No
SIL 00-028 PART A : Failure Messages ATA 261200
Failure message CHECK FDU ENGi SUPPLY
Remark
Part
P/Ns Affected
Corrective P/N
Doc X Ref
NO MAINT. ACTION if no log book complaint
FDU
730400-01
730401-02
TFU 261234020
No
TFU 26 13 00 001
No
TFU 26 13 00 001
No
TFU 26 17 34 012
No
OIT 999.0047/05
No
Associated P/N : ---261300
CHECK FDU APU LOOP A WARN CKT
No MAINT. ACTION if APU FDU test does not confirm the fault message
FDU
3720-00-00
---TBD
Associated P/N : ---261300
CHECK FDU APU LOOP B WARN CKT
No MAINT. ACTION if APU FDU test does not confirm the fault message
FDU
NO MAINT. ACTION if reset of the SDCU clears the message
SDCU
3720-00-00
Associated P/N : ---261734
SDCU CHANNEL 2 (10WQ)
RAI-2800-M0706
Associated P/N : ---275100
SFCC1(2) or FLP 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
Part A : page 13
---TBD
---SB 92-1021
----
49-170-11 From S/N 5813 To S/N 5956
Associated P/N : ----
Filter
----
Revision 29
SIL 00-028 PART A : Failure Messages ATA 275100
Failure message SFCCi or FLAP PPU POWER
Remark
Part
SFCC - 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.
P/Ns Affected
Corrective P/N
Doc X Ref
49117-10 (S/N 1732 to 1934) 49170-07 (S/N 1743 to 1904)
49-170-11
TFU 275134025
No
TFU 27 51 00 004
No
Associated P/N : ---275100
SLT/FLT CSU 51CV OR WIRING TO SLT1(2)/FLP1(2)
If recorded in PFR without warning No MAINT. ACTION SFCC required. If Warning refer to TFU 27 51 00 004
49170-11
---49170-11 Amdt. A
Associated P/N : ---275134
SDACi: NO DATA FROM SFCC
NO MAINT ACTION if no log book complaint
SDAC
If associated with failure message SFCC1(2) or FLP PPU POWER. Corrective action: replace SFCC at the origin of the fault.
SFCC
35-0E5-1510-22 35-0E5-1611-22
----
FLP1(2) PCU VALVEBLOCK 23(24) CV
----
49-170-11 From S/N 5813 To S/N 5956
Associated P/N : ---278100
SFCCi or SLAT PPU POWER
If recorded in PFR without warning: NO MAINTENANCE SFCC 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.
49117-10 49170-07 (S/N 1727 to 1906)
Associated P/N : ----
Part A : page 14
Yes
35-0E5-1513-31
Associated P/N : ---275453
Filter
OIT 999.0047/05
No
TFU 275134025
No
---49-170-11
----
Revision 29
SIL 00-028 PART A : Failure Messages ATA 2800
Failure message FUEL L(R) XFR VALVE OPEN
Remark
Part
P/Ns Affected
Corrective P/N
FQIC If this ECAM message is reported, perform functional BITE test of the ICTVs - FLSS Status (AMM 28-15-00-740002) 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. Associated P/N : ----
284234
FUEL QUANTITY FQIC 3QT
FQIC NO MAINT. ACTION if FQIC grades remains at 1 after FQIC test through CFDS. associated with ECAM warning : 28-00 FQI CH1(2) FAULT
SIC5059-xx-xx05 SIC5059-xx-xx06
FUEL LEVEL SENSING L (or R) UNFULL SENSOR 25QJ1 (or 25QJ2 or 26QJ1 or 26QJ2)
NO MAINT. ACTION if triggered in flight phase 02
FLSCU
NO MAINT. ACTION if not associated with ECAM warning.
ZC
ALL P/N
Associated P/N : ---301151
R(L) WAI FILTER OR VALVE 10DL (9DL)
775A0000-07
Associated P/N : ---307151
DRAINMAST HEATER FWD AFT
NO MAINT. ACTION if no blockage or system malfunction reported.
DMCU
4-60000H800 4-60000H840
Associated P/N : ----
Part A : page 15
Filter
TFU 281500003
No
TFU 284234030
No
---SIC5059-xx-xx07
Associated P/N : ---284634
Doc X Ref
---No
TBD
---775A0000-08
TFU 301100014 / TSM ATA30
Yes
TFU 307100002
No
---4-60000H882 SB 30-1030
----
Revision 29
SIL 00-028 PART A : Failure Messages ATA 307151
Failure message DRAINMAST HEATER FWD/AFT
Remark
Part
P/Ns Affected
Corrective P/N
Doc X Ref
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
DRAIN MAST
4-60000H880
4-60000H882
TFU 307100003
DRAINMAST HEATER MID
Valid only if Mod. 21598 embodied. NO MAINT. ACTION DMCU if no blockage or system malfunction reported.
4-60000H800 4-60000H840
----
DRAINMAST HEATER MID
Valid only if Mod 21598 embodied. Replace the drainmast DRAIN MAST even if the fault is not confirmed on ground. This anomaly has been identified. A correction will be incorporated in the next Drainmast.
4-60000H880
SB 30-1030
----
313234
BAD DATA FROM CFDIU
NO MAINT. ACTION
CFDIU(1TW)/HF(i) (3REi)
No maintenance action if no logbook complaint.
622-9738-020 622-9738-041
HF 964-0452-001 Transcei ver
Associated P/N : ----
Part A : page 16
No
SB 30-1030
---VSB ILS-720-34-01
No
AI S/B: 34-1093
Associated P/N : CFDIU 313234
TFU 307100003
4-60000H882
Associated P/N : ---ILS
TFU No 307100002/30710000 3
4-60000H882
Associated P/N : ---307151
No
SB 30-1030
Associated P/N : ---307151
Filter
B401ACM0404 No
TBD
----
Revision 29
SIL 00-028 PART A : Failure Messages ATA 313234
Failure message LGCIU: NO DATA FROM CFDS
Remark
Part
P/Ns Affected
Corrective P/N
Doc X Ref
Appears after a CFDIU power down, NO MAINTENANCE ACTION
LGCIU
664700500A4A
664700500A4B
TFU 323134043
No
TFU344100010
Yes
TFU 313300007
No
TFU 313300007
No
TFU 313300007
No
Associated P/N : ---313234
RADAR x: NO DATA FROM CFDIU
RADAR 204-1217-0418 204-1217-0421
NO MAINT. ACTION
Associated P/N : ---313352
QAR
NO MAINT. ACTION if mentioned in Phase 1 in last leg report
FDIU
NO MAINT. ACTION if mentioned in Phase 1 in last leg report
FDIU
9026-16079-01B2
Associated P/N : ---313352
QAR TAPE LOW
9026-16079-01B2
Associated P/N : ---313355
DFDR
NO MAINT. ACTION if mentioned in Phase 1 in last leg report
FDIU
9026-16079-01B2
Associated P/N : ----
Part A : page 17
Filter
---VSB RTA-4A-34-173
---9026-16079-02B3
---9026-16079-02B3
---9026-16079-02B3
----
Revision 29
SIL 00-028 PART A : Failure Messages ATA 313355
Failure message DFDR PLAYBACK
Remark
Part
P/Ns Affected
Corrective P/N
NO MAINTENANCE ACTION. RECOMMENDED STEP: EMBODY VSB SFIM FDIU/360-31-090
FDIU
ED43A1D3
ED43A1D4
Associated P/N : SSFDR 313634
NO DMU DATA (INTM)
DMU
No Maintenance Action required
DAR
No Maintenance Action required
DMU
No Maintenance Action required
DMU
795040-30-001
DAR TAPE LOW
----
795040-30-001
DU EWD(2WK1)/ECP(2WM)
No maintenance action required if no logbook complaint.
EIS II SXT3CE2SA0420 Software SXT4EE2SA050A
Associated P/N : ----
Part A : page 18
No
795040-31-002
---No
795040-30-002
Associated P/N : ---316322
---No
Associated P/N : ---313652
Filter No
795040-30-001
Associated P/N : ---313652
Doc X Ref
---Yes
TBD
----
Revision 29
SIL 00-028 PART A : Failure Messages ATA 316322
Failure message DU ND CAPT(3WK1)/ ND CAPT POT(8WK1)
Remark
Part
P/Ns Affected
No maintenance action required if no logbook complaint.
EIS II SXT3CE2SA0420 Software SXT4EE2SA050A
Corrective P/N
DU ND FO(3WK2)/ ND FO POT(8WK2)
No maintenance action required if no logbook complaint.
EIS II SXT3CE2SA0420 Software SXT4EE2SA050A
----
DU PFD CAPT(1WK1)/ PFD CAPT POT(7WK1)
No maintenance action required if no logbook complaint.
EIS II SXT3CE2SA0420 Software SXT4EE2SA050A
No maintenance action required if no logbook complaint.
EIS II SXT3CE2SA0420 Software SXT4EE2SA050A
----
DU PFD FO(1WK2)/ PFD FO POT(7WK2)
----
DU SD(2WK2)/ECP(2WM)
No maintenance action required if no logbook complaint.
EIS II SXT3CE2SA0420 Software SXT4EE2SA050A
Associated P/N : ----
Part A : page 19
Yes
TBD
Associated P/N : ---316322
Yes
TBD
Associated P/N : ---316322
Yes
TBD
Associated P/N : ---316322
Filter Yes
TBD
Associated P/N : ---316322
Doc X Ref
---Yes
TBD
----
Revision 29
SIL 00-028 PART A : Failure Messages ATA 316334
Failure message AFS:CHK DMCi-FMGCj CKT (i=1 or 2) (j=1 or 2)
Remark
Part
P/Ns Affected
Corrective P/N
NO MAINT. ACTION required if no log book complaint
FMGC
ALL P/N
TBD
Associated P/N : ---316334
HUDC : CHECK DMC1
HUDC
NO MAINT. ACTION
96154334-1
HUDC
HUDC : NO DMC1 DATA
NO MAINT. ACTION
CHECK LGCIU-PHC3
NO MAINT. ACTION if triggered in FWC flight phase 06 BSCU or 07 and if not associated with fault message "L/G EXT PROX SNSR 24GA(25GA) TGT POS"
96154334-1
E21327001 E21327003
Associated P/N : ---323171
LGCIUi 05GAi
LGCIU
NO MAINT. ACTION
664700500A4A
Associated P/N : ----
Part A : page 20
No
96154334-2
TFU 343500003
No
TFU 343500003
No
---96154334-2
Associated P/N : ---323171
Filter
----
Associated P/N : ---316334
Doc X Ref
---No
TBD
---664700500A4B
TFU 323134043
----
Revision 29
No
SIL 00-028 PART A : Failure Messages ATA 324224
Failure message SDACi:NO DATA FROM BSCU1+2
Remark
Part
P/Ns Affected
Corrective P/N
Wrong ATA REF. Should be 324234 instead. All FWC in BASIC configuration (Pre Mod 24159) are affected (E2, E3, E4, F2).
FWC
350E017271616 350E018301919 350E018312020 350E053020x0x
FWC STD H2F3
Doc X Ref
Filter No
(Target: Oct 2005)
(x=3, 4, 6) Associated P/N : ---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 350E018301919 350E018312020 350E053020x0x
---No
FWC STD H2F3 (Target: Oct 2005)
(x=3, 4, 6) Associated P/N : ---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
NO MAINT. ACTION if no Log Book complaint
SDAC
E21327003
---TBD
No
35-0E5-1513-31
No
Associated P/N : 324234
SDAC : NO DATA FROM BSCU
35-0E5-1510-22 35-0E5-1611-22
Associated P/N : ---324234
SDAC : NO DATA FROM TPIU
NO MAINT. ACTION if no Log Book complaint
SDAC
35-0E5-1510-22 35-0E5-1611-22
Associated P/N : ----
Part A : page 21
---No
35-0E5-1513-31
----
Revision 29
SIL 00-028 PART A : Failure Messages ATA 324334
Failure message ABCU(95GG)/ BRK SELECTOR VALVE(23GG)
Remark
Part
P/Ns Affected
Corrective P/N
NO MAINT. ACTION if triggered in flight phase 01 or 02 on A/C equipped with BSCS EMM (mod 26925)
BSCU
E21327003
TBD
Associated P/N : ---324418
SDACi: LH Y BRK PRESS XDCR 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)
SDACi:RH Y BRK PRESS XDCR 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
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
350E053020606 (FWC H2F2)
STEERING ELECTRO HYDRAULIC MODULE 6GC
C202163 SERIES C202452 SERIES
STEERING ELECTRO-HYD MODULE (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
Associated P/N : ----
Part A : page 22
Yes
P/N TBD
Post MOD 26925 Yes
FWC H2F3 P/N TBD
Post MOD 26925 No
N/A
Associated P/N : ---325151
No
FWC H2F3
Associated P/N : BSCU 325151
Filter
----
Associated P/N : BSCU 324418
Doc X Ref
PRE MOD 26925 No
N/A
PRE MOD 26925
Revision 29
SIL 00-028 PART A : Failure Messages ATA 341119
Failure message AOA SENSOR 3FP1(2,3)
Remark
Part
P/Ns Affected
Corrective P/N
Doc X Ref
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
TFU 341000017
No
Associated P/N : ---341119
AOA SNSRi (3FPi)/ ADIRUi(1FPi)
NO MAINTENANCE ACTION if appears after an AOA test.
ADIRU
465020-0303-0308
Associated P/N : ---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
No maintenance action required if no logbook complaint.
RADAR 822-1710-201 822-1710-202
Associated P/N : ---341234
ADIRUi+3(1FPi+3) ADRBUS /WXRi(1SQi) (i = 1 or 2)
Associated P/N : ---341234
AFS:ADIRU 1/2/3 DISAGREE
NO MAINT. ACTION if not associated to any Message in the ADIRU Bite
FAC
Part A : page 23
---465020-0303-0309
---No
066-50008-0409
---Yes
822-1710-203
----
B397AAM0507/0508 B397BAM0509 B397BAM0406/0407 B397AAM0509 B397CAM0101
Associated P/N : ----
Filter
TFU 229100009
----
Revision 29
Yes
SIL 00-028 PART A : Failure Messages ATA 341234
Failure message AFS:ADIRU 1/2/3 DISAGREE
Remark
Part
P/Ns Affected
Corrective P/N
Doc X Ref
NO MAINT.ACTION IF NO LOGBOOK COMPLAINT.
Pitot
Pre SB 34-1122
SB 34-1122
TFU220000012
No
TFU 220000012
Yes
TFU 275144003
No
Filter
(Pitot re-location)
Associated P/N : ---341234
AFS:ADIRU 1/2/3 DISAGREE
No maintenance action if no logbook complaint
FAC
B397AAM0507 B397AAM0508 B397BAM0406 B397BAM0407
---B397BAM0513
Associated P/N : ---341234
NO ADIRUi DATA CHECK WIRING TO SLT(FLP)i
When this message is followed by 27-51-34 SFCC1(2), 21(22)CV ignore this second message.
SFCC
No maintenance action if no logbook compaint.
RADAR 822-1710-201
49117-06
Associated P/N : ---341234
QUALIFIER Di/WXRj (1SQj) (i=1 or 2 and j= 1 or 2)
Associated P/N : ---341234
RADARi: NO DATA FROM ADIRU
The fault appears during ground test. Repeat test. If result OK no further MAINT ACTION required.
RADAR 204-1218-0418 204-1218-0421
Associated P/N : ----
Part A : page 24
---49117-07
---No
822-1710-202
---No
SIL 95-29 Rev.1
----
Revision 29
SIL 00-028 PART A : Failure Messages ATA 341234
Failure message RADARi:NO DATA FROM ADIRU
Remark
Part
P/Ns Affected
NO MAINT. ACTION if no log book complaint
RADAR 622-5132-020 622-5132-1120
HUD OHU
NO MAINT. ACTION if no log book complaint.
HUDC
96154334-1 96154334-2
VSB WRT-701X-34-77
---V65 SOFTWARE
Associated P/N : ---343631
FMGC
AFS : ILS i
NO MAINT. ACTION if occurs at the end of the flight
FWCi :NO DATA FROM ILSi
NO MAINT ACTION if occurs in flight phases 02 and 07. ILS
All P/N
Associated P/N : ---343631
622-9738-020
Associated P/N : ---343631
ILS i RECEIVER
NO MAINT. ACTION if no Log book complaint
ILS
204-1230-3518
TFU 343500003
Part A : page 25
Yes
---Yes
TBD
---Yes
622-9788-041
---204-1230-3521
TFU 343600004
204-1230-3532
Associated P/N : ----
Filter No
VSB WRT-701X-34-68
Associated P/N : ---343522
Doc X Ref
Corrective P/N
----
Revision 29
Yes
SIL 00-028 PART A : Failure Messages ATA 343631
Failure message ILSi
Remark
Part
P/Ns Affected
Corrective P/N
NO MAINT. ACTION if occurs in flight phase 02.
ILS
622-9738-020 622-9738-041
NONE
Associated P/N : ---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
MMR1 (40RT1)/GPWC (1WZ)
EGPWS 965-0976003-102-102
NO MAINT. ACTION required
343676
ILSi RECEIVER
Ref TSM task 34 36 00 810 801 "34 36 31 ILSi RECEIVER"
associated to ILS fault
622-9738-020
NO MLS (i) DATA
No maintenance action if no logbook complaint
AMU
3514xS01
Associated P/N : ----
Part A : page 26
No
ILS-720-34-11 ILS-900-34-6
---Yes
965-0976003-206-206
---No
622-9738-041
Associated P/N : ---343731
Yes
Collins VSB
Associated P/N : ---ILS
Filter
----
Associated P/N : ---343631
Doc X Ref
---Yes
TBD
----
Revision 29
SIL 00-028 PART A : Failure Messages ATA 344111
Failure message RADAR 1 ANTENNA
Remark
Part
P/Ns Affected
NO MAINT. ACTION if no log book complaint
RADAR 622-5132-020 622-5132-120
RADAR i ANTENNA
NO MAINT ACTION if nologbook complaint
RADAR 204-1217-0418 204-1217-0421
VSB WRT-701X-34-77
---VSB RTA-4A-34-160
RADAR i ANTENNA
NO MAINT ACTION if message recorded immediately after engine start (this item concerns only 2 airlines)
RADAR MI 585306-402
No maintenance action required if no logbook complaint.
RADAR 822-1710-201
Associated P/N : ---344111
WXR ANTENNA(11SQ)
Associated P/N : ---344112
RADAR 1 CONTROL UNIT
NO MAINT. ACTION if no log book complaint
RADAR 622-5132-020 622-5132-120
Associated P/N : ----
Part A : page 27
TFU 344100007
No
NONE
No
Rev.1
Associated P/N : ---344111
Filter No
VSB WRT-701X-34-68
Associated P/N : ---344111
Doc X Ref
Corrective P/N
---TBD
---No
822-1710-202
---VSB WRT-701X-34-68 VSB WRT-701X-34-77
----
Revision 29
No
SIL 00-028 PART A : Failure Messages ATA 344112
Failure message WXR CTL PNL(3SQ)/ WXRi(1SQi) (i = 1 or 2)
Remark
Part
P/Ns Affected
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
344133
DMCi: NO WXRj CHj DATA (i=1, 2 or 3; j=1 or 2)
RADAR 1 TRANSCEIVER
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
NO MAINT. ACTION if no log book complaint
RADAR 622-5132-020 622-5132-120
----
----
RADAR i TRANSCEIVER
NO MAINT ACTION if message recorded immediately after engine start (this item concerns only 2 airlines).
VSB WRT-701X-34-77
---TBD
Associated P/N : ---344133
RADARi TRANSCEIVER
NO MAINT. ACTION if no log book complaint
RADAR 204-1218-0418 204-1218-0421
Associated P/N : ----
Part A : page 28
No
VSB WRT-701X-34-68
Associated P/N : ---344133
No
TBD
Associated P/N : ----
RADAR MI 585306-402
Filter No
822-1710-202
Associated P/N : ---344133
Doc X Ref
Corrective P/N
NONE
Yes
TFU 344100007
No
---VSB RTA-4A-34-160 Rev.1
----
Revision 29
SIL 00-028 PART A : Failure Messages ATA 344133
Failure message WXRi(1SQi) (i=1 or 2)
Remark
Part
P/Ns Affected
Corrective P/N
No Maint. Action if fault msg recorded in the PFR without RADAR 066-50008-0405 cockpit effect and is associated with specific TSD (final 4 066-50008-0407 digits "0000"). The fault msg may be triggered if radar selected OFF and Pred Windshear scanning automatically activated during take-off or approach.
066-50008-0409
Associated P/N : ---344133
WXRi(1SQi) (i= 1 or 2)
No maintenance action if no logbook complaint.
RADAR 822-1710-201
Associated P/N : ---344137
WXR MOUNTING TRAY(5SQ)/ WXRi(1SQi) (i = 1 or 2)
No maintenance action required if no logbook complaint.
RADAR 822-1710-201
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
Associated P/N : ---344233
RA1 (2SA1) +RA2 (2SA2) / WXR1 (1SQ1)
Associated P/N : ---344233
RA1(2SA1)+RA2((2SA2)/ WXRi (1SQi) (I=1 or 2)
NO MAINT. ACTION if recorded during Engine Start (flight phase 02) or during switching from WXR1 to WXR2 and no associated cockpit effect.
RADAR 822-1710-201
Associated P/N : ----
Part A : page 29
Doc X Ref
Filter No
---No
822-1710-202
---No
822-1710-202
---No
066-50008-0409
---No
822-1710-202
----
Revision 29
SIL 00-028 PART A : Failure Messages ATA 344300
Failure message DMC(i): NO TCAS DATA (i = 1 or 2)
Remark
Part
P/Ns Affected
Corrective P/N
Doc X Ref
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
TFU 34.43.00.011
No
TFU 34.43.00.011
No
TFU 344300006
No
TFU 344300006
No
Associated P/N : ---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 066-50000-1x08 HONEY 066-50000-2x20 WELL 4066010-903/904 4066010-905
Filter
---TBD
940-300-001 Associated P/N : ---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 622-8971-320 ROCKW 622-8971-322 ELL 822-1293-322
NO MAINT ACTION if no logbook complaint. This deviation has been identified.
TCAS
Associated P/N : ---344300
TCAS ARINC 429
4066010-903
Associated P/N : ---344300
TCAS UNTRACEABLE
NO MAINT ACTION if no log book TCAS complaint.
TCAS
4066010-903
Associated P/N : ----
Part A : page 30
---TBD
---4066010-905
---4066010-905
----
Revision 29
SIL 00-028 PART A : Failure Messages ATA 344333
Failure message FWC(i): NO DATA FROM TCAS (i = 1 or 2)
Remark
Part
P/Ns Affected
No maintenance action required if no logbook complaint and if TCAS BITE is OK.
TCAS 066-50000-1x08 HONEY 066-50000-2x20 WELL 4066010-903/904 4066010-905
Corrective P/N
Doc X Ref
TBD
TFU 34.43.00.011
No
TFU 34.43.00.011
No
TFU 34.43.00.011
No
TFU 34.43.00.011
No
TFU 34.43.00.011
No
Filter
940-300-001 Associated P/N : ---344333
FWC(i): NO DATA FROM TCAS (i = 1 or 2)
No maintenance action required if no logbook complaint and if TCAS BITE is OK.
TCAS ACSS
7517900-10002 7517900-10003
---TBD
Associated P/N : ---344333
FWC(i): NO DATA FROM TCAS (i = 1 or 2)
No maintenance action required if no logbook complaint and if TCAS BITE is OK.
TCAS 622-8971-320 ROCKW 622-8971-322 ELL 822-1293-322
No maintenance action required if no logbook complaint and if TCAS BITE is OK.
TCAS 622-8971-320 ROCKW 622-8971-322 ELL 822-1293-322
---TBD
Associated P/N : ---344333
NO TCAS DATA
---TBD
Associated P/N : ---344333
NO TCAS DATA
No maintenance action required if no logbook complaint and if TCAS BITE is OK.
TCAS ACSS
7517900-10002 7517900-10003
Associated P/N : ----
Part A : page 31
---TBD
----
Revision 29
SIL 00-028 PART A : Failure Messages ATA 344333
Failure message NO TCAS DATA
Remark
Part
P/Ns Affected
No maintenance action required if no logbook complaint and if TCAS BITE is OK.
TCAS 622-8971-320 ROCKW 622-8971-322 ELL 822-1293-322
Corrective P/N
Doc X Ref
TBD
TFU 34.43.00.011
No
TFU 34.43.00.011
No
TFU 34.43.00.011
No
TFU 34.43.00.004
No
TFU 34.43.00.011
Yes
Associated P/N : ---344333
NO TCAS DATA
No maintenance action required if no logbook complaint and if TCAS BITE is OK.
TCAS 066-50000-1x08 HONEY 066-50000-2x20 WELL 4066010-903/904 4066010-905
Filter
---TBD
940-300-001 Associated P/N : ---344333
NO TCAS DATA
No maintenance action required if no logbook complaint and if TCAS BITE is OK.
TCAS ACSS
No maintenance action required if associated to the TCAS fault message "344334 TCAS (1SG)" and if TCAS BITE is OK.
TCAS
7517900-10002 7517900-10003
---TBD
Associated P/N : ---344334
ATC(i): NO DATA FROM TCAS (i = 1 or 2)
066-50000-0203 066-50000-0102 066-50000-0208 066-50000-0108
---TPA-81A-34-61 REV2 TPA-81A-34-72 TPA-81A-34-75 REV1
Associated P/N : ---344334
ATC(i): NO DATA FROM TCAS (i = 1 or 2)
No maintenance action if no logbook complaint and if TCAS BITE is OK.
TCAS 622-8971-320 ROCKW 622-8971-322 ELL 822-1293-322
Associated P/N : ----
Part A : page 32
---TBD
----
Revision 29
SIL 00-028 PART A : Failure Messages ATA 344334
Failure message ATC(i): NO DATA FROM TCAS (i = 1 or 2)
Remark
Part
P/Ns Affected
No maintenance action if no logbook complaint and if TCAS BITE is OK.
TCAS 066-50000-1x08 HONEY 066-50000-2x20 WELL 4066010-903/904 4066010-905
Corrective P/N
Doc X Ref
TBD
TFU 34.43.00.011
Yes
TFU 34.43.00.011
Yes
TFU 34.43.00.004
No
TFU 34.43.00.011
No
TFU 34.43.00.011
No
Filter
940-300-001 Associated P/N : ---344334
ATC(i): NO DATA FROM TCAS (i = 1 or 2)
No maintenance action if no logbook complaint and if TCAS BITE is OK.
TCAS ACSS
7517900-10002 7517900-10003
---TBD
Associated P/N : ---344334
TCAS (1SG)
No maintenance action required if no logbook complaint and if TCAS BITE is OK.
TCAS
No maintenance action required if no logbook complaint and if TCAS BITE is OK.
TCAS 066-50000-1x08 HONEY 066-50000-2x20 WELL 4066010-903/904 4066010-905
066-50000-0203 066-50000-0102 066-50000-0108 066-50000-0208
---TPA-81A-34-61-REV2 TPA-81A-34-72 TPA-81A-34-75 REV1
Associated P/N : ---344334
TCAS(1SG)
---TBD
940-300-001 Associated P/N : ---344334
TCAS(1SG)
No maintenance action required if no logbook complaint and if TCAS BITE is OK.
TCAS 622-8971-320 ROCKW 622-8971-322 ELL 822-1293-322
Associated P/N : ----
Part A : page 33
---TBD
----
Revision 29
SIL 00-028 PART A : Failure Messages ATA 344334
Failure message TCAS(1SG)
Remark
Part
P/Ns Affected
Corrective P/N
Doc X Ref
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
TFU 344300006
No
Associated P/N : ---345000
MODE S i
NO MAINT ACTION if no logbook complaint.
TCAS
4066010-903
---4066010-905
Associated P/N : ---345133
AFS:DMEi
NO MAINT ACTION if no log book complaint
FMGC C13042xA01 PEGASU S
Due to A/C out of emitter range. No Maint. Action if no Log Book complaint.
DME
Associated P/N : ---345133
AFS:DMEi
622-4540-023
Filter
---Yes
TBD
---VSB DME 700-34-33
TFU 345100008
Yes
VSB DME 700-34-27
Associated P/N : B398BxM0xxx FMGC LEGACY 345133
DME i TRANSCEIVER
NO MAINT. ACTION if no log book complaints
DME
622-4540-020 622-4540-021 622-4540-022 622-4540-023 Associated P/N : ----
Part A : page 34
VSB DME-700-34-27
TFU 345100008
----
Revision 29
No
SIL 00-028 PART A : Failure Messages ATA 345212
Failure message ATC CTL PNL(2SH)
Remark
Part
P/Ns Affected
Corrective P/N
This misbehavior will be corrected at the next standard of P/N 7517800-10005 and new ATC CTL PNL(3SH)
TCAS
7517800-10005
7517800-10005
Associated P/N : ---345233
ATCi (1SH1) / No maintenance action if not associated to ECAM TCAS (100SG) source TCAS (i = 1 or 2) 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
ATCi (1SH1) / TCAS (1SG) source TCAS (i = 1 or 2)
No Maint. Action if not associated to ECAM WARNING TCAS "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).
345233
NO ATC i DATA Source CFDS (i = 1 or 2)
No maintenance action is required if no logbook complaint.
Associated P/N : ---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
Associated P/N : ----
Part A : page 35
No
---TFU 34.43.00.011
7517900-10002 7517900-10003
751-7800-10002 751-7800-10005
No
TBD
Associated P/N : ---ATC
Filter
----
Associated P/N : ---345233
Doc X Ref
No
---Yes
TBD
---No
822-1710-202
----
Revision 29
SIL 00-028 PART A : Failure Messages ATA 345331
Failure message ADF i RECEIVER
Doc X Ref
Remark
Part
P/Ns Affected
Corrective P/N
NO MAINT. ACTION if no log book complaint.
ADF
622-5222-020
VSB ADF-700-34-20
Filter No
VSB ADF-700-34-21 VSB ADF-700-43-27
Associated P/N : ---345331
NO ADF(i) DATA
No maintenance action when ADF 1 or/and 2 not installed CFDIU on the aircraft.
----
Associated P/N : ---345531
AFS : VOR i
NO MAINT. ACTION if no logbook complaint
FMGC
NO MAINT ACTION if no logbook complaint
VOR
All P/N
Associated P/N : ---345531
VOR i : VOR RECEIVER
Yes
N/A
622-5220-020
---Yes
TBD
---VSB 700-34-10 Rev 1 VSB 700-34-19
Associated P/N : ---345572
VOR i RECEIVER
NO MAINT. ACTION if no log book complaint.
VOR
204-1231-3610
Associated P/N : ----
Part A : page 36
TFU 345500009 / TFU 345500013
No
TFU 345500010
No
---VSB RVA-36A-34-54
----
Revision 29
SIL 00-028 PART A : Failure Messages ATA 361134
Failure message SDAC:NO DATA FROM BMCi
Remark
Part
P/Ns Affected
Corrective P/N
NO MAINT. ACTION if no logbook complaint
SDAC
35-0E5-1510-22 35-0E5-1611-22
350E5-1513-31
Associated P/N : ---383100
CHECK LAV (X) OR CHECK VAC LINE LEAKAGE
Disconnect 42MG XDCR, then, the spurious message will VSC disappear
14404-001-1
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
NO MAINT. ACTION
VSC
Z064H000030D Z064H000030E Z064H000030F
Associated P/N : ---383134
VSC
14404-011A
Associated P/N : ---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
Associated P/N : ----
Part A : page 37
Filter No
---14404-011A SB 38-1027
Associated P/N : ----
Doc X Ref
TFU 383100003 / TSM ATA 38 / VSB 14404-38-01
No
TFU 38.31.00.026
Yes
TFU 38 31 00 022 SB 38-1044 REV2 VSB 14440403802
Yes
TFU 38.31.00.026
No
---Z064H000031A Z064H000031B
---14404-011B
---Z064H000031A Z064H000031B
----
Revision 29
SIL 00-028 PART A : Failure Messages ATA 383162
Failure message LIQD LVL XMTR (40MG)
Remark
Part
P/Ns Affected
Corrective P/N
Doc X Ref
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 Z064H000030F
Z064H000031A
TFU 38.31.00.026
Yes
TFU 383100003 / TSM ATA 38
No
AIRBUS SB: A32049-1061
Yes
S/B A320-49-1053
No
Z064H000031B
Associated P/N : ---383168
DIFF PRESS XDCR
NO MAINT. ACTION if 42MG XDCR has been disconnected.
VSC
14404-001-1
---14404-011A SB-38-1027
Associated P/N : ---492318
LCDT Sensor P29
No MAINT. ACTION
ECB
NO MAINT. ACTION if no logbook complaint
ECB
4500001 4500001A 4500001B 4500003G
---4500003H
Associated P/N : APU 493211
FUEL CTL UNIT P19
304817-1
SDAC : NO DATA FROM ECB
NO MAINT. ACTION if no Log Book complaint (GTCP36.300)
SDAC
35-0E5-1510-22 35-0E5-1611-22
Associated P/N : ----
Part A : page 38
APS 3200
304817-2
Associated P/N : GTCP 496134
Filter
36-300 No
35-0E5-1513-31
----
Revision 29
SIL 00-028 PART A : Failure Messages ATA 499414
Failure message OIL PRESS SW P14
Remark
Part
P/Ns Affected
Corrective P/N
NO MAINT. ACTION if no logbook complaint
ECB (GTCP 36-300)
304817-1
304817-2
Associated P/N : ---499651
APU OIL HEATER(8093KM)
APU 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
DOOR BTL XY/ DEU B (300RHZ) with X=1, 3 or 4 and Y=R or L and Z=1, 6 or 8.
CIDS DIR
No maintenance action required.
No
----
731150
FRV(CLOSED),J7(J8),ECU During FADEC motoring test
NO MAINTENANCE ACTION IF ECU 5.BE or 5.DE not fitted on A/C.
Z064H000031B
1820M89P02 1820M36P02 1820M88P02 1820M87P02
----
DMCi:NO ECUi A(B) DATA
No Maint. Action if it occurs in phase 02 at the end of an ECU engine run (80KTS not reached) or after any FADEC reset.
ALL P/N
Associated P/N : ----
Part A : page 39
TFU 732900033
SB 73-1034
No
SB 73-1037
Associated P/N : ---732160
No
Z064H000031A
Associated P/N : ---ECU
No
3800278-2 3800278-3 3800278-4
Z064H000030F
Filter
----
Associated P/N : ---520000
Doc X Ref
---Yes
N/A
DMC (EIS I)
Revision 29
SIL 00-028 PART A : Failure Messages ATA 732160
Failure message ECU(Ei-4000KS) (i=1 or 2)
Remark
Part
No Maint. Action if it occurs in phase 02 at the end of an DMC engine run (80KTS not reached) or after any FADEC reset. EIS II Soft
P/Ns Affected
Corrective P/N
SXT3F-E2SA-0410 SXT3C-E2SA-0420
TBD
Associated P/N : ---732234
DMCi: NO EECi A(B) DATA
No Maint. Action if it occurs in phase 02 at the end of an EEC engine run (80KTS not reached) or after any FADEC reset.
ALL P/N
EEC(Ei-4000KS) (i=1 or 2)
No Maint. Action if it occurs in phase 02 at the end of an DMC engine run (80KTS not reached) or after any FADEC reset. EIS II Soft
SXT3F-E2SA-0410 SXT3C-E2SA-0420
Associated P/N : ---752210
LPTC VLV,HMU During FADEC motoring test
No maintenance action if ECU 5.BE or 5.DE not fitted on A/C.
ECU
1820M89P02 1820M36P02 1820M88P02 1820M87P02 Associated P/N : ----
752420
ECU AIR,J7(8), ECU
Must be disregarded if CFMI S/B 72-436 AIRBUS S/B 71- ECU 1014 embodied on the aircraft.
1459M55P15 1459M55P16 1519M83P02 1519M83P03 Associated P/N : ----
Part A : page 40
Filter Yes
CFM ENGINE Yes
N/A
Associated P/N : ---732234
Doc X Ref
DMC (EIS I) Yes
TBD
IAE/PW ENGINE SB 73-1034
TFU 732900033
No
SB 73-1037
---No
1459M55P17 1519M83P04 1820M27P01
----
Revision 29
SIL 00-028 PART A : Failure Messages ATA 783100
Failure message HC/PROX SW/T/R UP ACT i
Remark
Part
EEC Associated with Maint. Status Eng I FADEC. No Maint. Action if recorded during phase 07 or 08 and if there is no crew report.
P/Ns Affected
Corrective P/N
Doc X Ref
SCN12C
SCN12D
TFU 783100080
Associated P/N : ---793311
QUALIFIER Bi/WXRj (1SQj) (i=1 or 2 and j= 1 or 2)
NO MAINT. ACTION if recorded during Engine Start (flight phase 02) or during switching from WXR1 to WXR2 and no associated cockpit effect.
RADAR 822-1710-201
SDACi:ENG2 OIL PRESS XMTR 4004EN (i=1 or 2), Source ECAM 1 or ECAM 2.
Wrong FIN number. Should be 4003EN instead. All FWC FWC in BASIC configuration (Pre Mod 24159) are affected (E2, E3, E4, F2).
ALL P/N
793316
CHECK N4 BRG SCAV PRESS XMTR CIRCUIT 4005 EN
NO MAINT. ACTION if EIU Ground Scanning result is RTOK
----
CHECK OIL PRESS SWITCH 3EN(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.
(Target: Oct 2005)
All P/N (IAE)
---3957905004
TFU 793316001
No
3957905005
TPIU
1058-34
Associated P/N : ----
Part A : page 41
No
FWC Std H2F3
Associated P/N : ---793415
No
822-1710-202
Associated P/N : ---EIU
No
----
Associated P/N : ---793315
Filter
---Yes
TBD
----
Revision 29
SIL 00-028 PART A : Failure Messages ATA
Failure message
XXXXXX ADF i : NO DATA FROM CONTROL SOURCE
Remark
Part
P/Ns Affected
Corrective P/N
Doc X Ref
NO MAINT. ACTION
ADF
622-5222-020 204-1168-7513
VSB ADF-700-34-21
TFU 345300006 / TFU 345300007
VSB DFA-75A-34-49 VSB ADF-700-34-27
Associated P/N : CFDIU XXXXXX DME : NO DATA FROM CONTROL SOURCE
DME
NO MAINT. ACTION
9599-614-03105
XXXXXX ILS i : NO DATA FROM CONTROL SOURCE
NO MAINT. ACTION
ILS
NO MAINT. ACTION
VHF
20412303518
622-5219-020
VSB RIA-35A-34-41
NO MAINT. ACTION (mainly due to FMS resets).
VOR
622-5220-020 20412313610
Part A : page 42
No
TFU 231200007
No
B401ACM0404
VSB VOR-700-34-10 VSB RVA-36A-34-54
Associated P/N : CFDIU
TFU 343600004
B401ACM0404
VSB VHF-700-23-30
Associated P/N : CFDIU XXXXXX VOR i : NO DATA FROM CONTROL SOURCE
Yes
----
Associated P/N : CFDIU XXXXXX VHFi:NO DATA FROM CONTROL SOURCE
Yes
B401ACM0404
VSB TDM-709-34-012
Associated P/N : ----
Filter
TFU 345500005 / TFU 345500008
B401ACM0404
Revision 29
Yes
SIL 00-028 PART B : PFR Warning Messages ATA
Warning message
Remark
Part
P/Ns Affected
Corrective P/N
Doc X Ref
2131
CAB PR LO DIFF PR
NO MAINT. ACTION if it occurs after a rapid flight profile change
CPC
902215702-7 902215702-8
9022-15702-10
TFU 213100005
Yes
TFU 213134005
No
TFU 215151004
No
Associated P/N : ---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
902215702-7
CPC
---902215702-8
Associated P/N : ---2151
PACKi (Maintenance Status)
751A0000-06
Associated to P1(2) FLOW CTL VALVE NO FCV MAINT. ACTION if Bite test OK
---751A0000-07
Associated P/N : ---2161
AIR PACK 1+2 FAULT
NO MAINT ACTION if it occurs at the flight beginning (PHASE 03 or 04).
ALL P/N
PC
Associated P/N : ---Part B : page
1
Filter
---N/A
Yes
---Revision 29
SIL 00-028 PART B : PFR Warning Messages ATA
Warning message
Remark
Part
P/Ns Affected
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
Corrective P/N
Associated P/N : Sensor 2161
TEMP CTL 1 (or 2) (Maintenance Status)
NO MAINT. ACTION if associated with fault message "237334 CIDS2(102RH) Source TEMP CTL". Status problem of a discrete label computed by the CIDS2 and used by ACSC 1 and 2.
1803A0000-03
ACSC
AFT(FWD) CAB DUCT OVHT
Check Temp. sensor output resistance
All P/N
ZC
1803B0000-01
CKPT DUCT OVHT
Check Temp. sensor output resistance
All P/N
ZC
Associated P/N : ---Part B : page
2
TFU 216134003 / SIL 21-049
No
SB A320-21-1149 / VSB 1803A-21-02
No
TFU 216318001 / SIL 21-049
No
TFU 216318001 / SIL 21-049
No
---N/A
Associated P/N : ---2163
Filter
----
Associated P/N : ---2163
Doc X Ref
---N/A
---Revision 29
SIL 00-028 PART B : PFR Warning Messages ATA
Warning message
Remark
Part
P/Ns Affected
Corrective P/N
Doc X Ref
2200
AUTO FLT A/THR OFF
Configuration Warning
FMGC
All P/N
N/A
N/A
Yes
N/A
Yes
TFU 226600004 / AMM ATA 34.13.00 pBlock 501
No
TFU 226300005
No
Associated P/N : ---2200
AUTO FLT AP OFF
Configuration Warning
FMGC
All P/N
Associated P/N : ---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
B397AAM0507/0508 B397BAM0406/0407
FAC
Associated P/N : ---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.
B397AAM0507/0508 B397BAM0406/0407 B397BAM0508/0509 B397CAM0101/0102 B397AAM0509/0510
FAC
Associated P/N : ---Part B : page
3
Filter
---N/A
---B397BAM0509
---B397BAM0510
---Revision 29
SIL 00-028 PART B : PFR Warning Messages ATA
Warning message
Remark
Part
P/Ns Affected
2300
COM SATCOM FAULT
No. Maint. Action if ECAM WARNING triggered when ADIRU 1+2+3 OFF
DMC EIS SXT3F-E2SA-0410 II Soft SXT3C-E2SA-0420
Associated P/N : ---2400
ELEC BCL i FAULT
NO MAINT. ACTION if no failure message in the PFR, and BCL test thru MCDU is OK.
35-0L5-1003-06 35-0L5-1004-07
BCL
Associated P/N : ---2600
SMOKE LAVATORY DET SMOKE
If associated with the SDCU fault message SMOKE "SMOKE DET LAV x" (x is the lavatory DET affected), ref the maintenance advice field of the TFU 261715003
GAI2800-02 PAI2830-00
Associated P/N : ---2615
AVIONICS SMOKE
If triggered on ground, associated with SMOKE amber memo LAND ASAP no evidence of DET 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 takeoff. Part B : page
4
CG7GO
Associated P/N : ----
Corrective P/N
Doc X Ref
EIS II STD S5
Filter No
---35-OL5-1005-08 (SB 24-1075)
TFU 243800007 / TFU 243800009/TFU 243800022
No
TFU 261715003
No
TFU 26 15 15 001
No
---TBD
---CGDU2000-00
---Revision 29
SIL 00-028 PART B : PFR Warning Messages ATA
Warning message
Remark
Part
P/Ns Affected
Corrective P/N
261600
SMOKE AFT CRG BTL1
Maintenance advise: Make sure that when AMM Task 26-16-00-710-001 "Operational test of the cargo-compartment Smokedetection system by PTT" is performed, the PTT button is hold 20 seconds as recommended and activated only one time.
CIDS DIR Z014H000030C
Z014H000131A Z014H000031A
Maintenance advise: Make sure that when AMM Task 26-16-00-710-001 "Operational test of the cargo-compartment Smokedetection system by PTT" is performed, the PTT button is hold 20 seconds as recommended and activated only one time.
CIDS DIR Z014H000030C
Maintenance advise: Make sure that when AMM Task 26-16-00-710-001 "Operational test of the cargo-compartment Smokedetection system by PTT" is performed, the PTT button is hold 20 seconds as recommended and activated only one time.
CIDS DIR Z014H000030C
Maintenance advise: Make sure that when AMM Task 26-16-00-710-001 "Operational test of the cargo-compartment Smokedetection system by PTT" is performed, the PTT button is hold 20 seconds as recommended and activated only one time.
CIDS DIR Z014H000030C
FAULT
261600
SMOKE AFT CRG BTL2 FAULT (if installed)
261600
SMOKE FWD CRG BTL1 FAULT
261600
SMOKE FWD CRG BTL2 FAULT (if installed)
Associated P/N : ----
Associated P/N : ----
Associated P/N : ----
Part B : page
Associated P/N : ---5
Doc X Ref
Filter No
---Z014H000131A Z014H000031A
No
---Z014H000131A Z014H000031A
No
---Z014H000131A Z014H000031A
No
---Revision 29
SIL 00-028 PART B : PFR Warning Messages ATA
Warning message
Remark
Part
2700
F/CTL ALT LAW
IF OCCURS AT ENGINE START,PERFORM ELAC ELACs RESET WITH ALL HYDRAULIC SYSTEMS DEPRESSURIZED.
P/Ns Affected
Corrective P/N
Doc X Ref
3945122502 STD L69
3945122505
TFU279300040/FC OM 3 02 27
No
TFU279000028
No
TFU 279500039
No
Associated P/N : ---2700
2700
F/CTL ELAC 2 PITCH FAULT
F/CTL ELAC1(2) FAULT
At engine start, if associated with "THS ELAC + ACTR SERVO MOT 1 9CE" maintenance THSA 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. Even if associated with "ELAC1(2)" maintenance message, failure of opposite ELAC may be suspected. Apply TSM procedure.
3945122502(ELAC) 3945122504(ELAC) 9231-4-600 (THSA)
---3945122505 (ELAC) 9231-5-600 (THSA)
Associated P/N : ----
---N/A
FCDC 115370-105 115370-1016
Associated P/N : ---2700
F/CTL SPD BRK DISAGREE
Configuration warning
Filter
All P/N
FCDC
Associated P/N : ---Part B : page
6
---N/A
Yes
---Revision 29
SIL 00-028 PART B : PFR Warning Messages ATA
Warning message
Remark
Part
P/Ns Affected
Corrective P/N
Doc X Ref
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
TFU 275134026
No
TFU 275134026
No
TFU 279300028
No
Associated P/N : ---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.
49117-10 49170-07
SFCC
Associated P/N : ---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
49117-10 49170-07
SFCC
Associated P/N : ---2793
ELAC i PITCH FAULT
IF NO MAINTENANCE MESSAGE associated : CHECK the PITCH CHANGE OVER DISCRETES LANE.
115370-0105
FCDC
Associated P/N : ---Part B : page
7
Filter
---Amdt A 49-170-11
---49-170-11 Amdt A 49-170-11
---115370-1016 115370-0106
---Revision 29
SIL 00-028 PART B : PFR Warning Messages ATA
Warning message
Remark
Part
2800
R(L) WING TK LO LVL
NO MAINT. ACTION if occurs at beginning of descent.
N/A
P/Ns Affected
Associated P/N : ---281500
FUEL INTERCELL TRANSFER XFR VALVE (29QM)/((72QM)/(10QP)
284634
FUEL LEVEL SENSING FLSCU1(2) 7QJ (9QJ)
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 28-46-00-740001). No further action is required, if both test of the FLSS status and FLSS BITE show NO FAULT.
FQIC
If this fault is reported in the PFR, perform the FLSCU BITE test (AMM 28-46-00-740001). If the test shows NO FAULT then no further action is required.
FQIC
Associated P/N : ----
Associated P/N : ----
Part B : page
8
Corrective P/N
Doc X Ref
Filter
SB 28-1029
TFU 284615003
No
TFU 281500009
No
TFU 284600009
No
----
----
----
Revision 29
SIL 00-028 PART B : PFR Warning Messages ATA
Warning message
Remark
Part
2900
BLUE RSVR
Should be a warning, as RAT operation can be affected. Will be re-classified.
N/A
P/Ns Affected
Associated P/N : ---3000
ANTI ICE CAPT (F/O) TAT
9599-607-14932 9599-607-12333
NO MAINT. ACTION if occurs on ground RA during wet / snowy / icy weather, or after deicing/high-press cleaning
Associated P/N : PHC 3000
ANTI ICE CAPT (F/O)PITOT
DISREGARD the message if occurs after LGCIU gear non-retraction. This deviation has been identified and will be cured at the next opportunaty of a new PHC std.
664700500A4B
Associated P/N : ---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
666 4202-2 666 4202-3 666 4202-4 666 4287-0
WHC
Associated P/N : ---Part B : page
9
Corrective P/N
Doc X Ref
Filter
SB 29-1055
TFU 293400002 / TSM ATA 29/SIL29050
No
TFU 303100017/3261000 03/344200003
No
TFU 323173001/3231710 43
No
TFU 304200004
No
---9599-607-14942 9599-607-12352
1663214-200 66400500A4D
---416-00318-001 416-00318-003
---Revision 29
SIL 00-028 PART B : PFR Warning Messages ATA
Warning message
Remark
Part
P/Ns Affected
Corrective P/N
Doc X Ref
3100
CFDIU
NO MAINT. ACTION if CFDIU power up test result is : CFDIU BITE MEMORY
CFDIU
B401ACM0404
Amdt A
TFU 313234031 / TSM ATA31
No
TFU 313600013 / TSM ATA 31
No
TFU 32 42 34 041 / FCOM 3.04.32
No
N/A
Yes
(Maintenance Status)
Associated P/N : ---3100
DMU (Maintenance Status)
Associated with the message : CAGA MEMORY FAIL.
DMU
903116243BOBOG0 903116243BODOJ0 903116243B0B0G1 903116243B0D0J1
---903116243B3B3G4 903116243B3B2G3 903116243B3D2J3 and subsequent std
Associated P/N : ---3200
BRAKES BSCU CH(i) FAULT
If occurs at engine shutdown, reset the BSCU (FCOM 3.04.32)
BSCU
All P/N
---N/A
Associated P/N : ---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
Associated P/N : ---Part B : page
10
Filter
---N/A
---Revision 29
SIL 00-028 PART B : PFR Warning Messages ATA
Warning message
Remark
Part
3200
L/G SHOCK ABSORBER FAULT
NO MAINT. ACTION if occurs on ground RA during wet / snowy / icy weather, or after deicing/high-press cleaning
P/Ns Affected
Corrective P/N
Doc X Ref
9599-607-14932 9599-607-12333
9599-607-14942 9599-607-12352
TFU 326100003/3442000 03/344200005
Yes
TFU 323134043
No
Associated P/N : ---3200
LGCIU i FAULT
NO MAINT. ACTION if BITE test OK
LGCIU
664700500A4A
Associated P/N : ---3200
LGCIU i FAULT
If not LGCIU faut message available in the PFR, refer to the Last Leg Report of the LGCIU
LGCIU
664700500A4C
Associated P/N : ---3400
NAV GPWS FAULT
NO MAINT. ACTION if occurs on ground during taxiing or lining-up
622-9738-020
ILS
Associated P/N : ---Part B : page
11
Filter
---664700500A4B
---664700500A4D
No
---622-9738-041
TFU 344800002
---Revision 29
Yes
SIL 00-028 PART B : PFR Warning Messages ATA
Warning message
Remark
Part
P/Ns Affected
Corrective P/N
Doc X Ref
3400
NAV GPWS FAULT
NO MAINT. ACTION if occurs on ground during Taxiing or Lining-up
ILS
20412303518
20412303521 20412303532
TFU 344800002
Yes
TFU 34.43.00.004 & 34.43.00.007
No
TFU 344300006
No
TFU 341000017
No
Associated P/N : ---3400
NAV TCAS FAULT
NO MAINT ACTION if TCAS BITE test is OK. If not OK ref TSM.
TCAS
066-50000-0203 066-50000-0102 066-50000-0208 066-50000-0108 Associated P/N : ----
3400
NAV TCAS FAULT
NO MAINT ACTION if TCAS BITE test is OK. If not OK ref to TSM.
TCAS
4066010-903
Associated P/N : ---3410
ADRi (Maintenance Status)
The MAINTENANCE STATUS may appear ADIRU after performing the AOA SENSOR test. See maintenance advice given in TFU 34 10 00 017
465020-0303-0308
Associated P/N : ---Part B : page
12
Filter
---TPA-81A-3461 REV 2 TPA-81A-34-72 TPA-81A-34-75 REV1
---4066010-905
---465020-0303-0309
---Revision 29
SIL 00-028 PART B : PFR Warning Messages ATA
Warning message
Remark
Part
P/Ns Affected
Corrective P/N
Doc X Ref
3410
ALTITUDE/AIRSPEED FLAGS
SEE MAINTENANCE ACTIONS I N TFU 341000012
ADIRU
HG1150AC05
HG1150AC06
TFU341000012
No
TFU 341000021
No
TFU 341000016
No
TFU 341000012/SB341084
No
ON PFD WITHOUT ECAM WARNING "NAV ADRi FAULT".
Associated P/N : ---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
Associated P/N : ---3410
NAV ADRx FAULT
Associated to ADM fault messages. NO MAINTENANCE ACTION if AIR DATA parameters are valid on ground
ADIRU
HG1150AC05
Associated P/N : ---3410
NAV ADRx FAULT
No associated maintenance message(source ADIRU ADR).Follow advice given in TFU341000012.
HG1150AC05
Associated P/N : ---Part B : page
13
Filter
---PG1152AC05
---MOD 25882
---HG1150AC06
---Revision 29
SIL 00-028 PART B : PFR Warning Messages ATA
Warning message
Remark
3441
NAV PRED W/S DET FAULT
3441
RED WXR FLAG ON PFD DURING ON/OFF SEQUENCE
Part
P/Ns Affected
Corrective P/N
If associated with fault message "DMCi: NO RADAR 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.
622-5132-622 622-5132-623
TBD
NO Maint. Action if WXR RADAR works correctly after power on.
204-1218-0418 204-1218-0421
RADAR
Associated P/N : ----
Associated P/N : ---3442
NAV RAi FAULT
622-8701-002 Apply Maintenance action described in RA TFU344200008 if correlated with both the ANTENN PFR fault messages "LRAi TRANSCEIVER" A and "LRAi ANTENNA" Associated P/N : ----
3442
NAV RAi FAULT
NO MAINT ACTION if event happens at high altitude (above 8192 ft).
9599-607-14942
RA
Associated P/N : ---Part B : page
14
Doc X Ref
Filter No
---TFU344100014
No
TFU344200008/ SIL 95-01/AOT 3403
No
TFU 344200007
No
---S/N > 2014
---ERT-530-34-34 ERT-530-34-35
---Revision 29
SIL 00-028 PART B : PFR Warning Messages ATA
Warning message
Remark
Part
P/Ns Affected
Corrective P/N
Doc X Ref
3443
NAV TCAS FAULT
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
7517900-10002 7517900-10003
TBD
TFU 34.43.00.011
No
TFU 34.43.00.011
No
without associated Maintenance Fault message.
3443
NAV TCAS FAULT without associated Maintenance Fault message.
3600
AIR BLEED (Maintenance Status)
Associated P/N : ----
If CFDS PFR filter Database contains fault TCAS 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.
066-50000-1X08 066-50000-2X20 622-8971-320/322 822-1293-322 940-300-001
NO MAINT. ACTION if the AIR BLEED MAINTENANCE STATUS is recorded in the PFR in phase 2, without any associated Fault Message.
785-002-61 785-002-7
BMC
3800
VSC
NO MAINT ACTION
14404-011A
VSC
---TBD
Associated P/N : ----
Associated P/N : ----
---N/A
No
---14404-011B
(Maintenance Status)
Associated P/N : ---Part B : page
15
Filter
TFU 38 31 00 022 SB 38-1044 REV2 VSB 14440403802
---Revision 29
Yes
SIL 00-028 PART B : PFR Warning Messages ATA
Warning message
Remark
7700
DUAL ENGINE FAILURE
NO MAINT. ACTION if occurs on ground RA during wet / snowy / icy weather, or after deicing/high press. cleaning.
7700
7700
ENG BLEED STATUS FAULT
ENG i EIU (Maintenance Status)
Part
NO MAINTENANCE ACTION if occurs at ECU power up
ECU
DISREGARD THE MESSAGE if occurs after LGCIU gear non retraction.
P/Ns Affected
Corrective P/N
Doc X Ref
9599-607-14932 9599-607-12333 9599-607-14942 9599-607-12552
9599-607-12352
TFU 326100003/3442000 03/344200005/3442 00013
Associated P/N : ----
----
1459M55P15 P16/P17/P18/P19 1519M83P02 P03/P04/P05/P06 1820M27P01/P02/P03
1459M55P21 1519M83P08 1820M27P05
Associated P/N : ----
----
664700500A4B
Associated P/N : ---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
Associated P/N : SDCU Part B : page
16
664700500A4C
Filter Yes
No
TFU 323173001/3234710 43
No
TFU 315300048/TFU 313600041
No
---VSB/RAI2800-26-005 for the SDCU VSB 795020-31-019 for the DMU post SB 26-005 Revision 29
SIL 00-028 PART B : PFR Warning Messages ATA
Warning message
Remark
Part
P/Ns Affected
Corrective P/N
Doc X Ref
7700
ENG i REVERSER FAULT
No maintenance action is required when occurs during engine shut off phase (Engine master switch off)
ECU
1820M36P07 1820M89P07
N/A
OIT/FOT 999.0111/99 TFU 78 31 00 098
No
TFU 732000004
No
Associated P/N : ---7700
ENG OVSPD PROT FAULT
Ref to FCOM 3.02.70.
All P/N
EEC
Associated P/N : ---7700
ENG TYPE DISAGREE
No Maint. Action if A/C is in ECU intermix configuration.
Associated P/N : ---7700
ENG X RESERVER FAULT
1820M36P06 1820M89P06 1820M87P07 1820M88P07
if associated to the following fault message ECU "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.
Associated P/N : ---Part B : page
---Partially corrected in: - SCN12C(A1) - SCN10A(A5)
----
ECU std 5AI ECU std 5AI+ ECU std 5AH ECU std 5AH+
ECU
17
Filter
No
---1820M87P09 1820M88P09
TFU 783100085
---Revision 29
No
SIL 00-028 PART B : PFR Warning Messages ATA
Warning message
Remark
Part
P/Ns Affected
Corrective P/N
Doc X Ref
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
1459M55Pxx 1519M83Pxx 1820M27Pxx 1820M36P06 1820M89P06
1820M87P09 1820M88P09 1820M36P07 1820M88P07
TFU 783100078/7831001 00
No
NO MAINT. ACTION if displayed before Engine start when ING/START selected. Disappear after a FADEC reset (>30 sec.)
ECU
TFU 752400002 / FCOM 3.02.18
No
7700
ENGi FADEC HI TEMP
Associated P/N : ---1459M55P15 1519M83P02
Associated P/N : ---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)
Associated P/N : ---7700
ENGi OVSPD PROT FAULT
Refer to FCOM 3.02.70 if it occurs at Engine start-up.
1459M55P15 P16/P17 1519M83P02 P03/P04 1820M27P01
ECU
Associated P/N : ---Part B : page
18
Filter
---1459M55P17 1519M83P04
---FWC H2F3
No
---1459M55P19 1519M83P06 1820M27P03
TFU 732110004
---Revision 29
No
SIL 00-028 PART B : PFR Warning Messages ATA
Warning message
Remark
Part
P/Ns Affected
Corrective P/N
Doc X Ref
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
3957900611 3957900612 39579050-03
Amdt C
TFU 743000082 / TFU 743000083
Associated P/N : ---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
SCN 15 SCN 16
EEC
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
SCN 15 SCN 16
EEC
Associated P/N : ----
Part B : page
19
No
---N/A
Associated P/N : ---7711
Filter
No
---N/A
No
----
Revision 29
SIL 00-028 PART C : Anomalies related to Class 3 Failure Messages ATA
Failure message
Remark
Part
P/Ns Affected
Corrective P/N
PARAMETER 26.1.320.10 not 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
90311624B3D2J3
Associated Part : FWC PARAMETER 26.1.320.01 not 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
Associated Part : FWC 212151
RECIRC FAN i OR SPLY
NO MAINT. ACTION
ZC
775A0000-05
Associated Part : ---212152
MIXER FLAP DRIVE
NO MAINT. ACTION
ZC
775A0000-05
Associated Part : ---215100
FLOW SEL
NO MAINT. ACTION
ZC
775A0000-05
Associated Part : ----
Part C : page
1
Doc X Ref
35-0E0-1618-7070/71 90311624B3D2J3
35-0E0-1618-7070/71 775A0000-06
TFU 216334044
---775A0000-06
TFU 216000003
---775A0000-06
----
Revision 29
SIL 00-028 PART C : Anomalies related to Class 3 Failure Messages ATA
Failure message
Remark
Part
P/Ns Affected
Corrective P/N
Doc X Ref
215218
Pi BLEED TEMP SENSOR
NO MAINT. ACTION
ZC
775A0000-05
775A0000-06
TFU 216334044
Associated Part : ---216111
Pi COMP TEMP SENSOR
NO MAINT. ACTION
ZC
775A0000-05
Associated Part : ---216112
Pi COMP OVHT SENSOR
NO MAINT. ACTION
ZC
775A0000-05
Associated Part : ---216115
Pi OUTLET TEMP SENSOR
NO MAINT. ACTION
ZC
775A0000-05
Associated Part : ---216134
PACKi CONT
NO MAINT. ACTION
ZC
775A0000-05
Associated Part : PC
Part C : page
2
---775A0000-06
TFU 216334044
---775A0000-06
TFU 216334044
---775A0000-06
TFU 216334044
---775A0000-06 759A0000-08
TFU 216134001 / TFU 216334044
759A0000-06/-07
Revision 29
SIL 00-028 PART C : Anomalies related to Class 3 Failure Messages ATA
Failure message
Remark
Part
P/Ns Affected
Corrective P/N
Doc X Ref
216151
Pi RAM AIR IN ACTUATOR
NO MAINT. ACTION
ZC
775A0000-05
775A0000-06
TFU 216334044
Associated Part : ---216152
PiRAM AIR OUT ACTUATOR
NO MAINT. ACTION
ZC
775A0000-05/-06/-07
Associated Part : ---216153
TURBINE BYPASS VALVE
NO MAINT. ACTION
ZC
775A0000-05
Associated Part : ---216315
TEMP SENSOR FWD (AFT) CAB DUCT I
NO MAINT. ACTION
ZC
775A0000-05
Associated Part : ---216315
TEMP SENSOR COCKPIT DUCT I
NO MAINT. ACTION
ZC
775A0000-05
Associated Part : ----
Part C : page
3
---775A0000-08
TFU 216334044
---775A0000-06
TFU 216334044
---775A0000-06
TFU 216334044
---775A0000-06
TFU 216334044
----
Revision 29
SIL 00-028 PART C : Anomalies related to Class 3 Failure Messages ATA
Failure message
Remark
Part
P/Ns Affected
Corrective P/N
Doc X Ref
216316
TEMP SENSOR R/H (L/H) MIXER I
NO MAINT. ACTION
ZC
775A0000-05
775A0000-06
TFU 216334044
Associated Part : ---216317
TEMP SENSOR FWD (AFT) CAB I
NO MAINT. ACTION
ZC
775A0000-05
Associated Part : ---216317
TEMP SENSOR COCKPIT I
NO MAINT. ACTION
ZC
775A0000-05
Associated Part : ---216318
FWD (AFT) CAB DUCT OVHT SENSOR I
NO MAINT. ACTION
ZC
775A0000-05
Associated Part : ---216318
COCKPIT DUCT OVHT SENSOR I
NO MAINT. ACTION
ZC
775A0000-05
Associated Part : ----
Part C : page
4
---775A0000-06
TFU 216334044
---775A0000-06
TFU 216334044
---775A0000-06
TFU 216334044
---775A0000-06
TFU 216334044
----
Revision 29
SIL 00-028 PART C : Anomalies related to Class 3 Failure Messages ATA
Failure message
Remark
Part
P/Ns Affected
Corrective P/N
216334
NO PACK DATA FROM ECS
NO MAINT. ACTION if zone cont. -5 fitted on A/C
ZC
775A0000-05
775A0000-06
Associated Part : ECB 216334
ZONE CONT
NO MAINT. ACTION
ZC
775A0000-05
Associated Part : ---216351
TRIM AIR VALVE COCKPIT
NO MAINT. ACTION
ZC
775A0000-05/-06/-07
Associated Part : ---216351
TRIM VALVE FWD (AFT) CAB
NO MAINT. ACTION
ZC
775A0000-05/-06/-07
Associated Part : ---216352
TRIM AIR PRESS VALVE I
NO MAINT. ACTION
ZC
775A0000-05
Associated Part : ----
Part C : page
5
Doc X Ref
304640-2 775A0000-06
TFU 216334044
---775A0000-08
TFU 216000004
---775A0000-08
TFU 216000004
---775A0000-07
TFU 216000003
----
Revision 29
SIL 00-028 PART C : Anomalies related to Class 3 Failure Messages ATA
Failure message
Remark
Part
P/Ns Affected
Corrective P/N
223334
NO PES MUX DATA
No MAINT. ACTION if no cabin crew complaint. This spurious PES Bite message is recorded when PES Bite is disabled in the CAM
CIDS
Z010H0005119 Z010H000520A
Z010H000521A
Associated Part : ---228334
FMGCx(1CAx) BUS FM ACARS/ATSU1(1TX1)
ATSU/ FMGCx protocol deviation when ATSU host LA2T0S162C0C0F1 ATSU does receive answer from FMGCx platform LA2T0S111C1B0F1 (when in slave condition). No S/W maintenance action required.
Associated Part : ---231233
VDR3(1RC3)/ATSU1(1TX1)
NO MAINT. ACTION.
ATSU
LA2T0J13000C0F1
Associated Part : VDR 233346
SEB 42LFT, 42RGT
REF SIL HUGHES 1142000-130-03 NO MAINT. ACTION
PES
1142300-131-xx
Associated Part : ---233346
SEB 41LFT, 41RGT
REF SIL HUGHES 1142000-130-03 NO MAINT. ACTION
PES
1142300-131-xx
Associated Part : ----
Part C : page
6
Doc X Ref
---LA2T0J13000C0F1
TFU 46 00 00 002
---TBD
TFU 46.00.00.002
064-50000-2051 VSB AVI-93-32
TFU 233300009
---VSB AVI-93-32
TFU 233300009
----
Revision 29
SIL 00-028 PART C : Anomalies related to Class 3 Failure Messages ATA
Failure message
Remark
233600
NO SCU DATA
No maintenance action if no cabin crew CIDS 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, 74303xx-xxx, RD-AV3001-33, 610860-xxxx.
Part
P/Ns Affected
Corrective P/N
Doc X Ref
Z01H0005119
Z010H000520A
TFU 233300009
Associated Part : ---242100
CHECK GCUi PIN A8A,A9B IDGi PIN B7,B8 WIRING
GPCU
740121A
Associated Part : ---242200
CHECK FIRE HANDLE i ; RESET GEN i
NO MAINT. ACTION if Fire handle switches actuation not mentionned in the Log Book.
GPCU
740121A
Associated Part : ---242218
TDC AC SENSOR 50 XU i
After a GPCU test, Generator 1& 2 P/B GPCU switches in the cockpit must be reset. Otherwise, this message will appear after the 2nd GPCU test
740121A 740121B
Associated Part : ---244134
GPCU
NO MAINT. ACTION
GPCU
740121A
Associated Part : ----
Part C : page
7
---740121B (S/B 24-1077)
TFU 244100002 / TSM ATA 24 pB 401
---740121B (SB 24-1077)
TFU 244100004
---Vdr SIL 229
TFU 244100003
---740121B (SB-24-1077)
----
Revision 29
SIL 00-028 PART C : Anomalies related to Class 3 Failure Messages ATA
Failure message
Remark
Part
284216
CTR CADENSICON 20 QT
NO MAINT. ACTION
Cadensicon 796-809-5
P/Ns Affected
Associated Part : ---284216
L(R) CADENSICON 19QTi
NO MAINT. ACTION
Cadensicon 796-809-5
Associated Part : ---301151
R(L) WAI FILTER OR VALVE 10DL(9DL)
NO MAINT. ACTION
ZC
775A0000-05
Associated Part : ---303134
PHC 6 DA 1(2,3)
PHC
1663214-200
Associated Part : ---313234
CFDIU(1TW1)/ATSU1(1TX1)
Protocol problem between ATSU and CFDIU. No maintenace action required.
ATSU host LA2T0S162C0C0F1 platform LA2T0S11C1B0F1 S/W
Associated Part : ----
Part C : page
8
Corrective P/N
Doc X Ref
796-809-6
TFU 284234029
---796-809-6
TFU 284234029 / TFU 284234016
---775A0000-07
TFU 216000003
---1663214-301
TFU 303134006 / TSM ATA 30
---LA2T0J13000C0F1
TFU 46 00 00 002
----
Revision 29
SIL 00-028 PART C : Anomalies related to Class 3 Failure Messages ATA
Failure message
Remark
Part
P/Ns Affected
Corrective P/N
313234
CFDIU(1TW)/ WXRi (i = 1 or 2)
No maintenance action required if no logbook complaint.
RADAR
822-1710-201
822-1710-202
Associated Part : ---313334
NO CLOCK DATA
NO MAINT. ACTION
FDIU
9026-16079-01B2
Associated Part : ---313334
NO DMC1 DATA
NO MAINT. ACTION
FDIU
9026-16079-01B2
Associated Part : ---313334
NO FWCi DATA
NO MAINT. ACTION
FDIU
9026-16079-01B2
Associated Part : ---313334
NO CFDS DATA
NO MAINT. ACTION
FDIU
9026-16079-01B2
Associated Part : ----
Part C : page
9
Doc X Ref
---9026-16079-02B3
---9026-16079-02B3
---9026-16079-02B3
---9026-16079-02B3
----
Revision 29
SIL 00-028 PART C : Anomalies related to Class 3 Failure Messages ATA
Failure message
Remark
Part
P/Ns Affected
Corrective P/N
313334
NO SDAC 1 DATA
NO MAINT. ACTION
FDIU
9026-16079-01B2
9026-16079-02B3
Associated Part : ---313355
DFDR PLAY BACK
NO MAINT. ACTION
FDIU
9026-16079-01B2
Associated Part : ---313355
DFDR PLAYBACK
Switch the recorder ground control P/B ON, then enter in the FDIU TEST MENU, check the DFDR status. NO MAINT. ACTION if associated with DFDR OPERATIVE NO PLAY BACK.
FDIU
9026-16079-01B2 9026-16079-01B3
Associated Part : ---315534
SDAC i
NO MAINT. ACTION if associated with SDAC codes 2000 to 2005
Doc X Ref
---9026-16079-02B3
TFU 313300007
---9026-16079-02B4
TFU 3133000015
---35-0E5-1513-31
TFU 315500002
35-0E5-1510-22 35-0E5-1611-22
Associated Part : ---315534
SDACx(1WVx)/ATSU1(1TX1)
ATSU host LA2T0S111C1B0F1 platform S/W
Associated Part : ----
Part C : page
10
---LA2T0J13000C0F1
TFU 46 00 00 002
----
Revision 29
SIL 00-028 PART C : Anomalies related to Class 3 Failure Messages ATA
Failure message
Remark
Part
316234
DMC(1WT2/3)/ATSU(1TX1)
Label 316 (wind direction) not properly received by the ATSU. Item under investigation. This deviation has no operational impact as data only needed for ADS applications.
ATSU host LA2T0S162C0C0F1 platform S/W
P/Ns Affected
Associated Part : ---316234
DMC(1WT1/3)/ATSU(1TX1)
Label 316 (wind direction) not properly received by the ATSU. Item under investigation. This deviation has no operational impact as data only needed for ADS applications. No maint. Action required.
ATSU host LA2T0S162C0C0F1 platform LA2T0S111C1B0F1 S/W
Associated Part : ---341034
NO DATA FROM ADIRS
NO MAINT. ACTION if appears in Phase 1,2 or 10 .
ZC
775A0000-05
Associated Part : ---341200
No access to ZONT PHC1(2,3) INTERFACE
NO MAINT. ACTION
PHC
1663214-200
Associated Part : ---341200
CHECK ADIRU1 (2,3) R STA PHC1(2,3) INTERFACE
NO MAINT. ACTION
PHC
1663214-200
Associated Part : ----
Part C : page
11
Corrective P/N
Doc X Ref
LA2T0J13000C0F1
---LA2T0J13000C0F1
TFU 46 00 00 002
---775A0000-06
TSM ATA 21
---1663214-301
TFU 303100013
---1663214-301
TFU 303100013
----
Revision 29
SIL 00-028 PART C : Anomalies related to Class 3 Failure Messages ATA
Failure message
Remark
Part
P/Ns Affected
Corrective P/N
Doc X Ref
341200
CHECK ADIRU1 (2,3) L STA PHC1(2,3) INTERFACE
NO MAINT. ACTION
PHC
1663214-200
1663214-301
TFU 303100013
Associated Part : ---341200
CHECK ADIRU 1 (2,3) AOA PHC1(2,3) INTERFACE
NO MAINT. ACTION
PHC
1663214-200
Associated Part : ---341200
CHECK ADIRU 1 (2,3) PITO PHC1(2,3) INTERFACE
NO MAINT. ACTION
PHC
1663214-200
Associated Part : ---341234
ADIRU3(1FP3) ADR BUS/ WXRi(1SQi) (i = 1 or 2)
No maintenance action required if no logbook complaint.
RADAR
622-5132-623
Associated Part : ---341234
ADIRU3(1FP3) ADR BUS/ WXRi(1SQi) (i = 1 or 2)
No maintenance action required if no logbook complaint.
RADAR
822-1710-201 822-1710-202
Associated Part : ----
Part C : page
12
---1663214-301
TFU 303100013
---1663214-301
TFU 303100013
---TBD
---822-1710-203
----
Revision 29
SIL 00-028 PART C : Anomalies related to Class 3 Failure Messages ATA
Failure message
Remark
Part
P/Ns Affected
Corrective P/N
341234
ADIRUi(1FPi) IR BUS/ WXRj(1SQj) (i = 1, 2 or 3 and j = 1 or 2)
No maintenance action required if no logbook complaint.
RADAR
822-1710-201 822-1710-202
822-1710-203
Associated Part : ---344233
RAi(2SAi)/WXRj (i = 1, 2 or 3 and j = 1 or 2)
No maintenance action required if no logbook complaint.
RADAR
822-1710-201
Associated Part : ---345233
ATCi (1SH1) / TCAS (1SG) (i = 1 or 2)
No Maint. Action. CLASS 3 fault TCAS message is triggered if ATC transponder in standby.
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
Associated Part : ---462134
ATSU1(1TX1)
No maintenance action required.
ATSU host LA2T0S162C0C0F1 platform LA2T0S111C1B0F1 S/W
Associated Part : ----
Part C : page
---822-1710-202
----
7517900-10002 7517900-10003
Associated Part : ---462134
Doc X Ref
13
---TBD
---LA2T0J13000C0F1
TFU 46 00 00 002
----
Revision 29
SIL 00-028 PART C : Anomalies related to Class 3 Failure Messages ATA
Failure message
Remark
Part
P/Ns Affected
Corrective P/N
Doc X Ref
710000
BALANCE ENGi N1-NB-VIB
NO MAINT. ACTION if no log book entry concerning Engin vibrations.
EVMU
241-211-000-021
241-211-000-031
TFU 773234005
Associated Part : ---710000
CHECK ENG i N2-NB-VIB
NO MAINT. ACTION if no log book entry concerning Engin vibrations.
EVMU
241-211-000-021
Associated Part : ---715100
J3, ADC1
NO MAINT. ACTION
ECU
---241-211-000-031
TFU 773234005
----
1459M55P15 1519M83P02
1459M55P17 1519M83P04
1459M55P16
1820M27P01
TFU 732900012
1519M83P03 Associated Part : ---715100
J4, ADC2
NO MAINT. ACTION
ECU
----
1459M55P15 1519M83P02
1459M55P17 1519M83P04
1459M55P16
1820M27P01
TFU 732900012
1519M83P03 Associated Part : ---732500
CHECK EIU WHC INTERFACE
Check/Confirm that EIU/WHC interface is defective
WHC
6664-202-3
Associated Part : ----
Part C : page
14
---6664-287-0
TFU 304034002
----
Revision 29
SIL 00-028 PART C : Anomalies related to Class 3 Failure Messages ATA
Failure message
Remark
Part
P/Ns Affected
Corrective P/N
Doc X Ref
753100
BLD SNSR,J15,ECU
NO MAINT.ACTION IF SB 72-1005 NOT EMBODIED ON THE A/C
ECU
1459M55P17 1519M83P04
SB 72-1005
TFU 732900025
1820M27P01
Associated Part : ---753100
VTURI,BLD SNSR,ECU
NO MAINT. ACTION IF SB 72-1005 NOT EMBODIED ON THE A/C.
ECU
1459M55P17 1519M83P04
---SB 72-1005
TFU 722900025
1820M27P01
Associated Part : ---753100
CWB3 SENS, J15 ECU
NO MAINT. ACTION if SB 72-1005 not embodied on the A/C
ECU
1459M55P15 1519M83P02
---SB : 72-1005
TFU 732900025
1459M55P16 1519M83P03 Associated Part : ---753100
WB3 SENS, J15 ECU
NO MAINT. ACTION if SB 72-1005 not embodied on the A/C
ECU
1459M55P15 1519M83P02
---SB : 72-1005
TFU 732900025
1459M55P16 1519M83P03 Associated Part : ----
Part C : page
15
----
Revision 29
SIL 00-028 PART D : Anomalies related to general use of CFDS ATA
Description of anomaly
Remark
Part
P/Ns Affected
Corrective P/N
Sel. valve and LGCIU faults are covered by the fault message: "LGCIU i 05GAi". With the LGCIU std 4D, the following message "LGCIU i 05GAi / L/G SEL VALVE 40G0A" will be triggered in case of valve or LGCIU failure.
LGCIU
664700500A4B 664700500A4C
664700500A4D
Associated Part : ---Recording in the PFR of "empty" DMU messages in flight phase 2 or 5. No Maintenance Action required.
DMU
795040-31-002
70
NVM FAULT DATA
ECU
NOT RETRIEVABLE
----
TBD
Associated Part : ---1459M55P15 1519M83P02
1459M55P17 1519M83P04
1459M55P16
1820M27P01
Doc X Ref
TFU 313600063
---TFU 732900031
1519M83P03 Associated Part : ---21
GND failures report
ZC
775A0000-05 775A0000-06
in last leg report,
775A0000-07
Associated Part : ----
Part D : page
1
----
----
Revision 29
SIL 00-028 PART D : Anomalies related to general use of CFDS ATA
Description of anomaly
Remark
Part
P/Ns Affected
Corrective P/N
21
No A/C ident in the
NO MAINT. ACTION
ZC
775A0000-05
775A0000-07
Doc X Ref
previous leg report
Associated Part : ---21
NO ACCEPTABLE FAILURE IN 26
NO MAINT. ACTION if no log book complaint.
ZC
775A0000-05
775A0000-06
Associated Part : ---21
No access to ZONE CONT
Make sure all C/B are pushed
ZC
775A0000-05
---TFU 216334047
----
775A0000-06
menu when PACK C/B is pulled.
Associated Part : ---21
No software number
NO MAINT. ACTION
ZC
775A0000-05
----
775A0000-07
in P/N of Zone Cont.
Associated Part : ----
Part D : page
2
----
Revision 29
SIL 00-028 PART D : Anomalies related to general use of CFDS ATA
Description of anomaly
Remark
Part
P/Ns Affected
Corrective P/N
Doc X Ref
21
OUTFLOW VALVE ELEK i
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
(04)
Associated Part : ---21
P.L.R. : Leg counting
ZC
775A0000-05
----
775A0000-07
deviation at leg 99
Associated Part : ---21
Test results
ZC
775A0000-07
----
775A0000-07
TFU 216134002 / TFU 216334004 / TSM ATA 21
in coded form
Associated Part : ---21
VENT AVNCS SYS FAULT during Ditching test procedure.
Reset AEVC C/B at the end of the Ditching test procedure.
AEVC
All P/N
NONE
Associated Part : ----
Part D : page
3
---TFU 212600010 / FCOM chapter 3.04.91 rev.20/AMM 212600 PB 527
----
Revision 29
SIL 00-028 PART D : Anomalies related to general use of CFDS ATA
Description of anomaly
Remark
Part
P/Ns Affected
Corrective P/N
Doc X Ref
216351
FAILURE NOT CLEARLY
NO MAINT. ACTION if no log book complaint.
ZC
775A0000-06 775A0000-05
775A0000-06
TFU 216334047
IDENTIFIED
Associated Part : ---22
22-83-34 FMGC (1CA1) / GPWC (1WZ)
NO MAINT. ACTION if appears after a GPWC test via the CFDS
GPWC
965-0676-020
S/W Mod 1
Associated Part : ---22
Disregard the indication
NO MAINT. ACTION
FAC
All P/N
---TFU 344800003
----
N/A
RTOK in the AFS Bite report
Associated Part : ---22
ELAC 1 & ELAC 2 messages displayed in the ground scan if no hydraulic pressure
NO MAINT. ACTION if no Hydraulic pressure on the A/C
FAC
All P/N
N/A
Associated Part : ----
Part D : page
4
---TSM ATA 22
----
Revision 29
SIL 00-028 PART D : Anomalies related to general use of CFDS ATA
Description of anomaly
Remark
Part
P/Ns Affected
Corrective P/N
Doc X Ref
22
FMGC MAG TRK on MCDU
NO MAINT. ACTION if appears after a GPWC ground scan. via the CFDS
GPWC
965-0676-020
S/W Mod 1
TFU 344800003
Associated Part : ---22
The message THR LK no more displayed on the PFD at the step 7 of the land test.
If DMC Mark II is installed, Ignore the DMC land test step7 question, and answer YES even if nothing is displayed on the PFD.
ALL P/N
FAC ---> B397BAM0508
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
FMGCi
Class 2 Fault message without associated Maintenance status. Apply TSM procedure
FCDC
B398AAM0409 B398BAM0206
B398BCM0104
B398BCM0106
115370-0105
5
TFU 227000014
----
115370-1016 115370-0106
Associated Part : ----
Part D : page
----
B398AAM0408 B398BAM0205
Associated Part : ---228334
TFU 229700004
B397BAM0509
Associated Part : ---22
----
MPD Task : 313000-03-1
----
Revision 29
SIL 00-028 PART D : Anomalies related to general use of CFDS ATA
Description of anomaly
Remark
Part
P/Ns Affected
Corrective P/N
228334
RMP1(2,3) : NO DATA FROM
Class 2 Fault message to be considered as a Class 3 message.
RMP
899-0850-002 899-0850-003
NONE
FMGCi
Doc X Ref
899-0850-004
Associated Part : ---23
Faults missing in Audio
Refer to messages in the PFR.
AMU
Previous and last leg reports
2790(*)A03 2790(*)A03
VSB 2790-23-006 VSB 2790-23-007
2790(*)A03
P/N: 2790(*)B06
* = C or D or E (3 or 4 or 5 boards) Associated Part : ---23
Wrong P/N of AMU and ACP
NO MAINT. ACTION
AMU
in the audio LRU identification
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
VSB 2790-23-006 VSB 2790-23-007
2790(*)A03
P/N: 2790(*)B06
CIDS DIR Z064H000030F
Part D : page
6
TFU 235100009/TFU 235100013
----
Z064H000031A Z064H000031B
Associated Part : ----
TFU 235100009/TFU 235100013
----
2790(*)A03 2790(*)A03
* = C or D or E (3 or 4 or 5 boards) Associated Part : ---230000
----
SB 23-1278
----
Revision 29
SIL 00-028 PART D : Anomalies related to general use of CFDS ATA
Description of anomaly
Remark
Part
230000
No date indication in
It may happen that further to a software loading a failure message is displayed without any date indication in the ground report of the CIDS1 or CIDS2 or the CIDS1 or 2 Toilet system.
CIDS DIR Z064H000030F Z064H000031A
the ground report of the CIDS or toilet system further to software loading.
P/Ns Affected
Corrective P/N TBD (end 2005)
Z064H000031B
Associated Part : ---230000
No date indication in the Last Leg Report of the CIDS Toilet system.
It may happen that a failure message is displayed without any date indication in the Last Leg Report of the CIDS1 or 2 Toilet system.
CIDS DIR Z064H000030F Z064H000031A
The Lavatory Smoke detection test can not be performed if the CIDS is in a "crossconfiguration" (AMM Task 26-1700-710-001) as it follows: Switchover of CIDS (CIDS1 passive, CIDS2 active, CIDS-SDF1
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: 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).
Z064H000031B
CIDS DIR Z064H000030F Z014H000030C
Z014H000131A Z014H000031A
CIDS DIR Z064H000031A Z064H000031B
7
----
TBD (end 2005)
Associated Part : ----
Part D : page
----
Z064H000031A Z064H000031B
Associated Part : ---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
----
TBD (end 2005)
Associated Part : ---230000
Doc X Ref
----
Revision 29
SIL 00-028 PART D : Anomalies related to general use of CFDS ATA
Description of anomaly
Remark
Part
P/Ns Affected
Corrective P/N
Doc X Ref
2311
IMPOSSIBILITY TO USE
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
VHF3 IN VOICE MODE
Associated Part : ---237334
BITE Test of CIDS The maintenance message "DIR2 (102RH) -SDF" is spuriously triggered during a system test of the smoke system through the MCDU with the following configuration: both CIDS directors
24
After a GPCU test, NO
Maintenance advise: Subject configuration may be reproduced for trouble shooting purpose. Therefore, the validity of the failure message must be checked through a CIDS-SDF ground scanning.
CIDS DIR Z014H000030C Z064H000030F
Z064H000031A Z064H000031B Z014H000131A Z014H000031A
Associated Part : ---Reinitialize GPCU test
GPCU
RESPONSE.
740121A 740121B
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
8
TFU 244100006
----
35-0L5-1005-08 (S/B 24-1075)
Associated Part : ----
Part D : page
----
Vdr SIL 229 SB 740121-24-7
Associated Part : ---24
----
TFU 243800007 / TFU 243800009
----
Revision 29
SIL 00-028 PART D : Anomalies related to general use of CFDS ATA
Description of anomaly
Remark
Part
P/Ns Affected
Corrective P/N
Doc X Ref
24
GCUi TEST NOT DONE
NO MAINT. ACTION if appears after a GPCU test. Reinitialize the GPCU test.
GPCU
740121A 740121B
Vdr SIL 229
TFU 244100005
or IDGi RUNNING
Associated Part : ---242334
GCU EMERG IN AVIONIC STATUS
If test result is OK, no maintenance action Could be corrected in a next CFDIU std
GCU
520915 amdt 4
TBD
Associated Part : ---261700
Operational check
CIDS DIR Z064H000030D Z064H000030E
of the Lavatory Smoke detection function as per AMM task 26-17-00710-001 not possible in case DIR1 and DIR-SDF2 or DIR2 and DIRSDF1 are active simultaneously (CIDS cross configuration). 27
Interruption of SFCC-
---TFU 313234035
----
TBD
Z064H000030F
Associated Part : ---reenter the SFCC MENU
SFCC
49117-06/07
----
N/A
TFU 275151047
CFDS communication when selecting the print option in the SFCC "SYSTEM DATA" pages. Associated Part : ----
Part D : page
9
----
Revision 29
SIL 00-028 PART D : Anomalies related to general use of CFDS ATA
Description of anomaly
Remark
Part
P/Ns Affected
Corrective P/N
Doc X Ref
2700
During Ground Scanning,
TSM procedure should be followed using the MAINT STATUS as entry point.
FCDC
115370-0106 115370-105
115370-1118
TFU 27 95 00 033
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. 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.
279300
115370-1016
Associated Part : ---TSM procedure should be followed using the ECAM WARNING as entry point.
FCDC
115370-0106 115370-105
115370-1118
FCDC
115370-0105
AIL SERVO FAULT in case of ELAC 1 (or 2) fault during GROUND SCANNING
AFS:ELACi
NO MAINT. ACTION if associated to B SYS LO PRESS (respectively Y SYS LO PRESS).
FAC
All P/N
10
----
N/A
Associated Part : ----
Part D : page
----
115370-1016 115370-0106
Associated Part : ---279334
TFU 279500033
115370-1016
Associated Part : ----
Ultimely flash of
----
----
Revision 29
SIL 00-028 PART D : Anomalies related to general use of CFDS ATA
Description of anomaly
Remark
Part
P/Ns Affected
Corrective P/N
Doc X Ref
279334
ELACi COM (MON) OR
Class 2 Fault message without associated Maintenance status. Apply TSM procedure
FCDC
115370-0105
115370-1016 115370-0106
MPD Task : 313000-03-1
BUS FROM FMGCi
Associated Part : ---279334
SEC3 OR BUS2 FROM ADR2 (ADR3 / IR2 / IR3)
Class 2 Fault message without associated Maintenance status. Apply TSM procedure
FCDC
115370-0105
115370-1016 115370-0106
Associated Part : ---279434
SEC2 OR INPUT OF L(R) THROTTLE CTL UNIT 8KSi
Class 2 Fault message without associated Maintenance status. Apply TSM procedure
FCDC
115370-0105
SEC3 OR WIRING FROM SFCC i
Class 2 Fault message without associated Maintenance status. Apply TSM procedure
FCDC
115370-0105
11
---MPD Task : 313000-03-1
----
115370-1016 115370-0106
Associated Part : ----
Part D : page
MPD Task : 313000-03-1
115370-1016 115370-0106
Associated Part : ---279434
----
MPD Task : 313000-03-1
----
Revision 29
SIL 00-028 PART D : Anomalies related to general use of CFDS ATA
Description of anomaly
Remark
Part
P/Ns Affected
Corrective P/N
Doc X Ref
279534
OP FCDC FAIL DISCR
Class 2 Fault message without associated Maintenance status. Apply TSM procedure
FCDC
115370-0105
115370-1016 115370-0106
MPD Task : 313000-03-1
Associated Part : ---301151
L(R) WAI FILTER OR VALVE9(10) Associated with E/Ws 30.00 WING ANTI ICE SYS FAULT
Do not forget to use the Zone Cont. Class 3 report upon wing anti ice Ecam Warnings.
ZC
775A0000-05
775A0000-07
Associated Part : ---31
BACK UP MODE DEVIATIONS
DO NOT CHOOSE ECAM1/2,FDIU,SFCC1 WHEN DOING STEP 6 OF AMM TASK 31 32 00 710 002
CFDIU
B401ACM0506
Bad counting of the
NO MAINT. ACTION
DMU
flight legs in the Class 3 Fault memory.
12
---TFU313234035
----
903116243BOBOG0 903116243BODOJ0
903116243B3B3G4 9031116243B3B2G3
903116243B0B0G1
903116243B3D2J3
903116243B0D0J1
and subsequent std
Associated Part : ----
Part D : page
TFU 216334046 / 216334046/TSM ATA 30
TBD
Associated Part : ---31
----
TFU 313600017
----
Revision 29
SIL 00-028 PART D : Anomalies related to general use of CFDS ATA
Description of anomaly
Remark
Part
P/Ns Affected
Corrective P/N
Doc X Ref
31
Bad PRINT OUT FORMAT.
NO MAINT. ACTION
Printer
805515-4501
805515-4501 VSB M3367
TFU 313522001
Associated Part : ---31
DIFFICULTIES FOR FILTER LOADING
SOME DIFFICULTIES MAY BE ENCOUNTERED WHEN USING ANY OUT OF THE PDL IN SERVICE BUT THE SFIM.
CFDIU
B401ACM0505 B401ACM0506
N/A
Associated Part : ---31
Duplication of Fault
CFDIU
B401ACM0404
---TFU313234038
----
B401ACM0606
TFU 313234029
message in PFR.
Associated Part : ---31
GR-OU-ND or GN-D - messages in phase 8/9
Generated by type 2 system. No maintenance Action.
CFDIU
B401ACM0506 B401ACM0507
C12860AA02
Associated Part : ----
Part D : page
13
----
----
Revision 29
SIL 00-028 PART D : Anomalies related to general use of CFDS ATA
Description of anomaly
Remark
Part
P/Ns Affected
Corrective P/N
Doc X Ref
31
Incoherent PFR Fault
Check EIU Previous Leg reports.
EIU
3957900611
3957900612
TFU 313234029
messages sent by the EIU.
Associated Part : ---31
Incoherent PFR recording time in the PFR header.
Due to Flight phases transitions anomalies.
CFDIU
B401ACM0404
B401ACM0506
Associated Part : ---31
Incomplete PFR Fault
Due to power transients.
CFDIU
B401ACM0404
---TFU 313234029
----
B401ACM0506
TFU 313234029
messages.
Associated Part : ---31
Message NO RESPONSE, PRESS RETURN after the start of DMC test.
To get the results, reenter DMC menu and access the "Test Result" item
DMC
All P/N
None
Associated Part : ----
Part D : page
14
----
----
Revision 29
SIL 00-028 PART D : Anomalies related to general use of CFDS ATA
Description of anomaly
Remark
Part
P/Ns Affected
Corrective P/N
Doc X Ref
31
Mixed GMT in PFR
Due to power transients.
CFDIU
B401ACM0404
B401ACM0506
TFU 313234029
Associated Part : ---31
NO "SYST" DATA (INTM)
If no logbook complaint, NO MAINT ACTION. This message is generated by the CFDIU (Source : CFDS).
CFDIU
B401ACM0506
TBD
Associated Part : ---31
NO DMC1 DATA recorded in
NO MAINT. ACTION
CFDIU
B401ACM0404
----
----
B401ACM0506
TFU 313234030
CFDIU ground scanning
Associated Part : ---31
NO FWC DATA recorded in CFDIU last leg report.
NO MAINT. ACTION if no log book complaint.
CFDIU
B401ACM0404
B401ACM0506
Associated Part : ----
Part D : page
15
---TFU 313234030
----
Revision 29
SIL 00-028 PART D : Anomalies related to general use of CFDS ATA
Description of anomaly
Remark
Part
P/Ns Affected
Corrective P/N
Doc X Ref
31
P/N read through LRU
NO MAINT. ACTION
FDIU
9026-16079-01B2
9026-16079-02B3
TFU 313300011
IDENT. Menu not in accordance with the actual P/N.
Associated Part : ---31
PFR with NO FAULT / NO WARNING.
Due to Flight phases transitions anomalies.
CFDIU
B401ACM0404
B401ACM0506
Associated Part : ---31
System source without
Under investigation. No Maint. Action.
CFDIU
B401ACM0404
---TFU 313234029
----
B401ACM0506
TFU 313234029
Fault message.
Associated Part : ---31
Untimely print out of
In flight pull, PRINTER C/B.
CFDIU
B401ACM0404
----
Amdt A
TFU 313234026
real time failure and warning.
Associated Part : ----
Part D : page
16
----
Revision 29
SIL 00-028 PART D : Anomalies related to general use of CFDS ATA
Description of anomaly
Remark
Part
P/Ns Affected
Corrective P/N
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
TBD
Doc X Ref
49-170-11
Associated Part : ---313234
ADFi : NO DATA FROM CFDIU
Class 2 Fault message to be considered as a Class 3 message.
ADF
204-1168-7513 622-5222-020
NONE
Associated Part : ---313234
AUDIO NO DATA FROM CFDIU
Class 2 Fault message to be considered as a Class 3 message.
AMU
2790CA03
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
17
----
N/A
Associated Part : ----
Part D : page
----
NONE
Associated Part : ---313234
----
----
Revision 29
SIL 00-028 PART D : Anomalies related to general use of CFDS ATA
Description of anomaly
Remark
Part
P/Ns Affected
Corrective P/N
313234
DME1(2,3) : NO DATA FROM
Class 2 Fault message to be considered as a Class 3 message.
DME
622-4540-023 9599-614-03105
NONE
CFDIU
Associated Part : ---313234
HFi : NO DATA FROM CFDIU
Class 2 Fault message to be considered as a Class 3 message.
HF
622-5272-020
NO DATA FROM CFDIU
Class 2 Fault message to be considered as a Class 3 message.
ILS
204-1230-3518 622-5222-020
RMP1(2,3) : NO DATA FROM CFDIU
Class 2 Fault message to be considered as a Class 3 message.
RMP
899-0850-002 899-0850-003
----
204-1230-3521 622-5222-041
Associated Part : ---313234
----
NONE
Associated Part : ---313234
Doc X Ref
----
NONE
899-0850-004
Associated Part : ----
Part D : page
18
----
Revision 29
SIL 00-028 PART D : Anomalies related to general use of CFDS ATA
Description of anomaly
Remark
Part
P/Ns Affected
Corrective P/N
313234
VHF1(2,3) : NO DATA FROM
Class 2 Fault message to be considered as a Class 3 message.
VHF
204-1237-4417
NONE
CFDIU
Associated Part : ---313234
VOR 1(2,3) :NO DATA FROM CFDIU
Class 2 Fault message to be considered as a Class 3 message.
VOR
204-1231-3610 622-5220-020
Doc X Ref
----
NONE
204-1231-3623 204-1231-3613 204-1231-3622 Associated Part : ---313234
WRX i : NO DATA FROM CFDIU
Class 2 Fault message to be considered as a Class 3 message.
WRX
204-1217-0418 204-1217-0421
VSB RTA-4A-34-173
Associated Part : ---313316
ACCELEROMETER
Class 2 Fault message without associated Maintenance Status. Apply TSM procedure.
FDIU
ED43A1D2 ED43A1D3
----
ED43A1D5
MPD 313000-04-01
90261607902B3
Associated Part : ----
Part D : page
----
19
----
Revision 29
SIL 00-028 PART D : Anomalies related to general use of CFDS ATA
Description of anomaly
32
Remark
Part
P/Ns Affected
Corrective P/N
Faults on the LGCIU ARINC OUTPUT BUS are reported "LGCIU i 05GAi". With the LGCIU std 4D, the following message will be triggered: " LGCIU/WRG: BUS i FEEDBACK".
LGCIU
664700500A4B 664700500A4C
664700500A4D
Associated Part : ---32
If a power interrupt of 10 ms or greater occurs after the transition from flight phase 1 to 2 with shock absorbers compressed any subsequent faults detected by the LGCIU will be logged in ground memory and not flight memory.
LGCIU
664700500A4B 664700500A4C
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
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 BSCU "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.
E21327001 E21327003
20
----
TBD
Associated Part : ----
Part D : page
----
664700500A4D
Associated Part : ---32
----
664700500A4D
Associated Part : ---32
Doc X Ref
----
Revision 29
SIL 00-028 PART D : Anomalies related to general use of CFDS ATA
Description of anomaly
Remark
Part
P/Ns Affected
Corrective P/N
32
During TPIU Bite test
Restart the TPIU Bite test
TPIU
1058-34
TBD
Doc X Ref
"NO RESPONSE" message may appears on the MCDU
Associated Part : ---32
Menu Mode access
LGCIU
664700500A4A
----
664700500A4B
TFU 323134043
possible during flight
Associated Part : ---32
No LGCIU fault message in the PFR.
The first failure logged in an empty LGCIU memory is not transmitted to the CFDIU for PFR recording.
LGCIU
66700500A4C
664700500A4D
Associated Part : ---32
Nothing in the LGCIU
LGCIU
664700500A4A
----
----
664700500A4B
TFU 323134043
Last Leg report instead of "NO FAILURE"
Associated Part : ----
Part D : page
21
----
Revision 29
SIL 00-028 PART D : Anomalies related to general use of CFDS ATA
Description of anomaly
Remark
Part
P/Ns Affected
Corrective P/N
Doc X Ref
32
Spurious NO DATA FROM
NO MAINT. ACTION
LGCIU
664700500A4A
664700500A4B
TFU 323134041
CFDS in the LGCIU Ground scanning, with date ???31
Associated Part : ---335100
EPSUs Battery Capacity test not possible through the MCDU
AMM task 33-51-00-710-011 to be updated accordingly.
CIDS DIR Z064H000030D Z064H000030E
TBD
Z064H000030F
Associated Part : ---335100
The Battery Capacity test of the EPSUs through the MCDU is not possible.
Maintenance advise: Pending availability CIDS DIR Z064H000030F of the MCDU test, the alternate AMM Task 33-51-00-710-011-01 "Remove Batteries for capacity check" should be applied.
Bad leg incrementation
NO MAINT. ACTION
GPWC
of GPWS Previous Leg Reports.
965-0676-020
22
----
9650676-020 S/W MOD 1
Associated Part : ----
Part D : page
----
Z064H000031A Z064H000031B
Associated Part : ---34
----
TFU 344800004
----
Revision 29
SIL 00-028 PART D : Anomalies related to general use of CFDS ATA
Description of anomaly
Remark
Part
P/Ns Affected
Corrective P/N
34
Bad LRU identification.
NO MAINT. ACTION
RADAR
204-1217-0418 204-1217-0421
VSB RTA-4A-34-161 TFU 344100007
Associated Part : ---34
Blank pages or erratic
NO MAINT. ACTION
RADAR
Data in Previous Leg Report.
204-1217-0418 204-1217-0421
FMGC (1CA1) / GPWC (1WZ) FMGC1 MAG TRK
Messages in the Ground Scanning and in GPWC the test result of the GPWC : NO MAINT. ACTION.
965-0676-020
Loss of fault messages
NO MAINT. ACTION
GPWC
in the GPWC Previous Leg Reports.
965-0676-020
23
TFU 344800003
----
9650676-020 S/W MOD 1
Associated Part : ----
Part D : page
----
9650676-020 S/W MOD 1
Associated Part : ---34
----
VSB RTA-4A-34-161 TFU 344100007
Associated Part : ---34
Doc X Ref
TFU 344800004
----
Revision 29
SIL 00-028 PART D : Anomalies related to general use of CFDS ATA
Description of anomaly
Remark
Part
P/Ns Affected
Corrective P/N
34
NO access to the ADF
NO MAINT ACTION
ADF
622-5222-020
VSB ADF-700-34-27
Doc X Ref
Last Leg Report after 64 legs flown without fault recorded in BITE
Associated Part : ---34
No access to the VOR
NO MAINTENANCE ACTION
VOR
622-5220-020
----
VSB-700-34-21
NONE
Last Leg Report after 64 legs flown without fault recorded in BITE.
Associated Part : ---34
No transmission of
NO MAINT. ACTION
HUDC
96154334-1
----
96154334-2
external failure at detection but after power cut
Associated Part : ---34
Random and transient
NO MAINT ACTION
HUDC
9615433402
----
V65
pattern (2sec) during aproach, instead of the wanted symbology display. Associated Part : ----
Part D : page
24
----
Revision 29
SIL 00-028 PART D : Anomalies related to general use of CFDS ATA
Description of anomaly
Remark
Part
P/Ns Affected
Corrective P/N
Doc X Ref
34
same message with same
NO MAINT. ACTION
GPWC
965-0676-020
965-0676-020 S/W MOD 1
TFU 344800004
date and GMT but different leg numbers in the Previous Leg Reports.
Associated Part : ---34
Wrong identification of
DME
622-4540-022
----
622-4540-023
TFU 345100009
DME : Message : DME-0 TRANSCEIVER
Associated Part : ---34 36
All ILS failures are coded as MMR failures in the following case:
When the CFDIU is swapped from an CFDIU 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.
B401ACM0507
TBD
Associated Part : ---345831
"GPSSU(1SNi)
when MMR installed on the A/C, GPSSU means GPS part of the MMR.
ADIRU
25
----
All P/N
Associated Part : ----
Part D : page
----
Ref TSM task: 34 58 00 810 805
----
Revision 29
SIL 00-028 PART D : Anomalies related to general use of CFDS ATA
Description of anomaly
Remark
Part
P/Ns Affected
Corrective P/N
Doc X Ref
361100
WAI NO BLEED AIR ENG i
Do not forget to use the Zone Cont. Class 3 report upon wing anti ice Ecam Warnings.
ZC
All P/N
775A0000-08
TFU 301100014
Associated with E/Ws 30.00 WING ANTI ICE L(R) VALVE OPEN
Associated Part : ---45
CFDIU BUS
The ATA chapter of this message should be 313234 instead of 45.
TCAS
4066010-904
TBD
Associated Part : ---451334
CFDS1(1TM)/ CIDS(10yRH)-SDFy (with (y=1 or 2)
The correct FIN of the CFDIU is 1TW instead of 1TM. Additionally, the ATA chapter and wording shall be 313234 CFDIU(1TW)/CIDS(10yRH)-SDFy (with y=1 or 2) instead of 451334 CFDS1(1TM)/CIDS(10yRH)-SDFy.
CIDS DIR Z014H000030C
GROUND SCANNING ATSU failures may be missing in ground scanning report.
Always reset the ATSU before ATSU performing the ground scanning function. host platform S/W
LA2T0S162C0C0F1
26
----
LA2T0S111C1B0F1
Associated Part : ----
Part D : page
----
Z014H000031A Z014H000131A
Associated Part : ---4621
----
----
Revision 29
SIL 00-028 PART D : Anomalies related to general use of CFDS ATA
Description of anomaly
Remark
Part
P/Ns Affected
Corrective P/N
Doc X Ref
4621
LINK TEST
Before activating the link test function, select the VHF3 in DATA mode (if VHF3 in VOICE mode, the test fails).
ATSU host platform S/W
LA2T0S162C0C0F1 LA2T0S111C1B0F1
LA2T0J13000C0F1
AMM task : 46 21 00 710 00200
Associated Part : ---4621
LRU identification
ATSU host platform S/W
A/C interfacce P/N displayed on LRU ident page is software P/N (LA2T0S162C0C000) and not disk P/N (LA2T0S162C0C0F1)
LA2T0S162C0C0F1 LA2T0S111C1B0F1
LA2T0J13000C0F1
Associated Part : ---4621
LRU identification AOC database not displayed on LRU ident MCDU page.
AOC database P/N is accessible on AOC menu (MISC menu for Allied Signal AOC, and CONFIG menu for Rockwell Collins AOC).
ATSU host platform S/W
LA2T0S162C0C0F1
MCDU dual access
AOC (Collins) simultaneously displayed and used on both MCDU, may induce to a MCDU protocol interuption leading to an ATSU time out. MCDU menu key has to be selected to recover ATSU normal mode. Only 1 MCDU must be used.
ATSU host platform S/W
LA2T0S162C0C0F1
27
AMM tasks : 46 21 00 610 00300/320
----
LA2T0S111C1B0F1
Associated Part : ----
Part D : page
AMM tasks : 46 21 00 610 00100/120
----
LA2T0S111C1B0F1
Associated Part : ---4621
----
----
Revision 29
SIL 00-028 PART D : Anomalies related to general use of CFDS ATA
Description of anomaly
Remark
Part
P/Ns Affected
4621
PRINT FAILED
A "PRINT FAILED" message can be displayed on MCDU, even if the print is successful.
ATSU LA2T0S162C0C0F1 host plateform S/W
Corrective P/N LA2T0S111C1B0F1
Associated Part : ---4621
PRINT FUNCTION
The "*" indicating the possibility to print is not always displayed. The "*" is systematicaly displayed after activating the PRINT function.
ATSU host platform S/W
LA2T0S162C0C0F1
SYSTEM REPORT TEST When the ATSU system test function is activated, the prompt "
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