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SUBJECT:
ATA CHAPTER:
AIRCRAFT TYPE:
APPLICABILITY:
1.
PURPOSE:
Centralized Fault Display System (CFDS) Anomalies
A318, A319, A320, A321
All Aircraft
The present SIL identifies all the known CFDS anomalies/BITE deviations. It is intended to be 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.
00
0.
REASON FOR REVISION:
Update of data. See Section 5 for detailed list of evolutions.
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2.
RECOMMENDATIONS
The appendix is divided into five parts, which are:
A. The list of PFR failure messages (internal and external) which request specific maintenance action.
B. The list of ECAM WARNINGS and MAINTENANCE STATUS shown on the PFR, which
request 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.
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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
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5.
LIST OF EVOLUTIONS
PART ATA
ITEMS
TYPE
REMARK
A
228334 FMGCi (1CAj)/RMPi (1RGi)/ILSi (1RTi)
Revised
Wording
A
231133
HF1 COUPLER (4RE1)/FEEDER HF1 (6RE1)/ANTENNA
(5RE1)
New
A
316322 DU ND CAPT(3WK1)/ND CAPT POT(8WK1)
New
A
316322 DU ND FO(3WK2)/ND FO POT(8WK2)
New
A
316322 DU PFD CAPT(1WK1)/PFD CAPT POT(7WK1)
New
A
316322 DU PFD FO(1WK2)/PFD FO POT(7WK2)
New
A
316322 DU EWD(2WK1)/ECP(6WM)
New
A
316322 DU SD(2WK2)/ECP(6WM)
New
A
341234 QUALIFIER Di/WXRj (1SQj) (i = 1 or 2 and j = 1 or 2)
New
A
341234
ADIRUi+3(1FPi+3) ADRBUS/WXRj(1SQj)
(i = 1 or 2 and j = 1 or 2)
Revised
Wording + P/N
A
344133 WXRi (1SQi) (i = 1 or 2)
New
A
344133
DMCi: NO WXRj CHj DATA
(i = 1, 2 or 3 and j = 1 or 2)
Revised
Wording
A
344300 DMC(i): NO TCAS DATA (i = 1 or 2)
Revised
Wording + P/N
A
344333 FWC(i): NO DATA FROM TCAS (i = 1 or 2)
Revised
Wording + P/N
A
344333 NO TCAS DATA
Revised
Wording + P/N
A
344334 ATC(i): NO DATA FROM TCAS (i = 1 or 2)
Revised
Wording + P/N
A
344334 TCAS (1SG)
Revised
Wording + P/N
A
345233 QUALIFIER Ci/WXRj (1SQj) (i = 1 or 2 and j = 1 or 2)
New
A
345233 ATCi (1SHi)/TCAS (100SG) source TCAS (i = 1 ou 2)
New
A
345233 NO ATCi DATA source CFDS (i = 1 or 2)
Revised
Wording + P/N
A
345233 ATCi (1SHi)/TCAS (1SG) source TCAS (i = 1 ou 2)
Revised
Add TFU ref.
B
2161
AIR:PACK i REGUL FAULT
Revised
Wording
B
3443
NAV TCAS FAULT
Revised
Add TFU ref.
C
313234 CFDIU (1TW)/WXRi (i = 1 or 2)
New
C
341234 ADIRU3 (1FP3) ADR BUS/WXRi (1SQi) (i = 1 or 2)
New
E
2161
AIR_PACK_1$2_FAULT
Revised
Wording
E
316322
DU_ND_CAPT(3WK1)/_______
ND_CAPT_POT(8WK1)
New
E
316322
DU_ND_FO(3WK2)/__________
ND_FO_POT(8WK2)
New
E
316322
DU_PFD_CAPT(1WK1)/_______
PFD_CAPT_POT(7WK1)
New
E
316322
DU_PFD_FO(1WK2)/________
PFD_FO_POT(7WK2)
New
E
316322
DU_EWD(2WK1)/__________
ECP(6WM)
New
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E
316322
DU_SD(2WK2)/____________
ECP(6WM)
New
E
341234
ADIRU$($FP$)_IR_BUS/____
WXR$($SQ$)
New
E
341234
ADIRU$$$($FP$$$)_ADRBUS/
WXR$($SQ$)
New
E
345233 NO_ATC_$_DATA__
Revised
Wording + P/N
6.
PROCEDURE TO DOWNLOAD FILES ATTACHED TO SIL ON AOLS
1/ Procedure to download SIL .pdf files:
- under Technical Publication select Engineering Technical Documentation,
- select Document Type and SIL Number then click on the SEARCH button,
- once selected SIL is opened, it is possible either to print or to save on disk.
2/ Procedure to download attached files to SIL 00-028:
Following files can be downloaded through the Airbus OnLine Services (AOLS) FTP:
- AIRBUS Filter Envelop (FILENVxx.320 [xx=REV]),
- AIRBUS FILTER DATABASE label to be stuck onto the floppy.
Procedure to download:
- select FTP Site under General Services menu,
- click on ASSOCIATED DOCUMENTS for SIL under the main ROOT,
- select the SIL 00-028 folder to access the package content.
Note that Filter Envelop used for A320, A330 and A340 require the Maintenance Filter Tool (MFT).
Please refer to SIL 00-088 which explains how to install MFT.
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LIST OF ABREVIATIONS
SIGLUM
TITLE
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
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
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SIGLUM
TITLE
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
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
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SIGLUM
TITLE
HUDC
ILS
ISIS
LGCIU
LOP
LRU
L/G
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
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
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
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SIGLUM
TITLE
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
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
000000 NO DATA NO MAINT. ACTION CFDIU B401ACM0505
----B401ACM0506
Associated P/N :
----No
212853 FWD CARGO FAN OR SPLY 6H NO MAINT. ACTION if power supply between FAN and
CVC is OK, 115 V 3 phases. (Minimum value : 110 V)
CVC 600615-01-500 600615-00-502 ----600615-01-502 600615-00-503 TFU 212854002 Associated P/N : ----No
212854 AFT CARGO FAN OR SPLY 35 NO MAINT. ACTION if power supply between FAN and
CVC is OK, 115 V 3 phases. (Minimum value : 110 V)
CVC 600615-01-500 600615-00-502 ----600615-01-502 600615-00-503 TFU 212854002 Associated P/N : ----No
215151 Pi FLOW CONTROL VALVE Associated to Maintenance Status PACK 1(2) , NO
MAINT. ACTION if Bite test OK
FCV 751A0000-06
----751A0000-07 TFU 215151004
Associated P/N :
----No
216334 EIUi : NO ZONE CONT
P(S) DATA
Associated with ECAM warning : ENG1(2) BLEED STATUS FAULT. NO MAINT. ACTION
ZC 775A0000-06 775A0000-07 TFU 216334051/
TFU 732900029 / TSM ATA 75
216334 EIUi NO ZONE CONT P(S) DATA
NO MAINT. ACTION If not associated to Maintenance Status : ENG1(2)EIU EIU 3957900609 3957900610 3957900611 3957905003 ----3957900612 3957905004 TFU 732534005 / TFU 732534042 / TSM ATA 71 Associated P/N : ----No
216334 NO ZONE CTL DATA NO MAINT. ACTION, Could be intermittent (INTM). ZC 775A0000-06
B401ACM0404
775A0000-07 TFU 216334051
Associated P/N : CFDIU
No
216334 SDACi: NO DATA FROM
ECS i
NO MAINT. ACTION if occurs in phase 6 ZC 775A0000-06
----775A0000-07 TFU 216334051
Associated P/N :
----No
226634 DMCi : No FACj DATA No Maintenance action DMC ALL P/N
----9615325050 (Soft std DMC V50)
Associated P/N :
----Yes
228112 FCU (2CA) BUS CP-L/
WRX 1 (1SQ1)
If no logbook associated logbook complaint, No maintenance action is required.
RADAR 066-50008-301 066-50008-405
Soft 05
228112 FCU(2CA)CP-L BUS/ WXRi(1SQi) (i = 1 or 2)
No maintenance action required if no logbook complaint. RADAR 822-1710-201
----822-1710-202 Associated P/N : ----No 228112 FCU(2CA)CP-R BUS/ WXRi(1SQi) (i = 1 or 2)
No maintenance action required if no logbook complaint. RADAR 822-1710-201
----822-1710-202
Associated P/N :
----No
228112 FCU(3CA)CP-L BUS/
WXRi 1SQi (I=1 or 2)
NO MAINT. ACTION if recorded during Engine Start (flight phase 02) or during switching from WXR1 to WXR2 and no associated cockpit effect.
RADAR 822-1710-201 ----822-1710-202 Associated P/N : ----No 228112 FCU(3CA)CP-R BUS/
WXRi 1SQi (I=1 or 2)
NO MAINT. ACTION if recorded during Engine Start (flight phase 02) or during switching from WXR1 to WXR2 and no associated cockpit effect.
RADAR 822-1710-201
----822-1710-202
Associated P/N :
----No
228112 RADARi:NO DATA FROM
EFIS i PANEL
NO MAINT. ACTION if no log book complaint RADAR 622-5132-020
622-5132-120
VSB WRT-701X-34-68 VSB WRT-701X-34-77
228212 AFS:MCDUi NO MAINT. ACTION if no log book complaint FMGC ALL P/N
----NONE TFU 229100011
Associated P/N :
----Yes
228212 MDCU3(3CA3)/ATSU1(1TX1) No maintenance action if MCDU 3 not installed. Can be filtered if MCDU 3 not installed
ATSU host platform S/W LA2T0S111C1B0F1 ----LA2T0J13000C0F1 TFU 46 00 00 002 Associated P/N : ----Yes
228334 AFS:FMGC$(DO NOT REMOVE)
NO MAINT. ACTION
FAC FAC pre Std
B397BAM0617
C13042xA01 B397BAM0617
Associated P/N : FMGC PEGA
Yes
228334 AFS:FMGCi NO MAINT ACTION IF MESSAGE NOT ASSOCIATED
WITH ANY ECAM WARNING AND COCPIT EFFECT
FMGC B546BAM0203 B546CCM0101 B546CAM0101 B398AAM0410 B398BAM0207 ----B546BAM0206 B546CAM0102 B546CCM0104 TFU229100055 Associated P/N : ----Yes B546BCM0205 C13042AA01
228334 AFS:FMGCi (FMi) NO MAINT. ACTION if no log book complaint FMGC B398AAM0408
B398BAM0205 B398BCM0104 B398AAM0409 B398BAM0206 B398BCM0106 TFU 229100010 Yes
228334 AFS:FMGCi/ATHR ENGD FDBK
NO MAINT. ACTION if not associated with ECAM WARNING : AUTO FLT A/THR OFF.
FMGC (LEGAC Y) B398AAM0xxx B398BAM0xxx B398BCM0xxx ----TBD Associated P/N : ----Yes 228334 FMGCi (1CAi)/ RMPi(1RGi)/ILSi(2RTi)
No maintenance action if not logbook complaint ILS 066-50006-X202
(Allied) 622-9738-041 (Collins) ----TBD (Allied) 822-0298-020 Associated P/N : ----No (Collins) 228334 FMGCi(1CAi) BUS MMR/ MMRi (40RTi)
Reset MMR1 when I equal 1 (Reset MMR2 when i equal 2). If in the Ground Scanning "FMGC BUS ILS/MMR" or in the TSD "PORT B RX FAIL" are visible carry out associated TSM task. MMR 822-1152-121 ----VSB Collins GLU 920-34-19 TSM task 34 36 00 810 870/871 Associated P/N : ----No 228334 FMGCi(1CAj)/ RMPi(1RGi)/ILSi(1RTi)
No maintenance action if no FM auto reset reported in the logbook.
FMGC All P/N
----N/A SIL 037 & SIL
22-038
Associated P/N :
----No
228334 FMGECi(1CAi)/
RMPi(1RGi)/ILSi(1RTi)
No maintenance action if no logbook entry ILS 622-9738-041
(Collins)
230000 DIR1 (101RH)/OBRM Maintenance advise: A CIDS interface and power-up test must be performed to confirm validity of the failure and to clear the failure message from the ground report.
CIDS DIR Z064H000030F Z064H000031A Z064H000031B ----TBD (end 2005) Associated P/N : ----No
231100 CHECK HF (i) ANTENNA
CIRCUIT
NO MAINT ACTION if no log book entry HF
TRANSC EIVER 622-5272-020 ----VSB HFS-700-36 TFU 231100002 Associated P/N : ----No
231100 ICAO ADDRESS/HFi(3REi) NO MAINT. ACTION. This message is triggered if
Datalink not activated (MOD 31286) and CFDIU Label 157 not received within 30s after HFDR power-up. This message is associated with CLASS3 Fault message "462134 ATSU(1TX1)/ HFi(3Ri)" HFDR 822-0990-003 Collins HFS900D ----TBD Associated P/N : ----Yes 231133 HF1 COUPLER(4RE1)/ FEEDER HF1(6RE1)/ANTENNA(5RE)
No maintenance action if no logbook compaint. COUPLE
R 792-6140-001 Associated P/N : ----No 231133 HFDRi(3REi)/ATSU1(1TX1) Source ACARS MU
NO MAINT. ACTION when HFDR not activated and CFDIU PRE STD 9B (Source name "ACARS MU" in the PFR) ATSU HOST Platform LA2T0J13000C0F1 LA2T0J13002C0F1
231133 NO HF 1 DATA Source CFDS
No Maint. Action if triggered in phase 02. HF
Transcei ver 964-0452-001 964-0452-012 ----TBD Associated P/N : ----No 231211 CHECK VHF 1 ANTENNA CIRCUIT
NO MAINT. ACTION if VSB mentioned in Corrective P/N not incorporated. VHF 622-5219-020 ----VSB VHF-700-23-36 VSB VHF-700-23-30 TFU 231200011 Associated P/N : ----No
231233 NO VHF3 DATA NO MAINT. ACTION when VHF3 not installed CFDS C12860AA02
(STD 9B)
----CFDIU STD 10 TBC
Associated P/N :
----Yes
231233 VHF 3 TRANSCEIVER NO MAINT. ACTION if no log book complaint VHF 622-5219-020
----VSB VHF-700-23-38
Associated P/N :
----No
231313 RMPi(1RGi)/RMPj(1RGj) NO MAINT. ACTION required RMP C12848AA01 C12848CA01 ----TBD Associated P/N : ----Yes
232834 SDU1(5RV1)/ATSU1(1TX1) Generated by ATSU when SATCOM not installed.
Disregard when SATCOM not installed (This message may be displayed on PFR, System Test and Ground scanning). ATSU host platform S/W LA2T0S162C0C0F1 LA2T0S111C1B0F1 TFU 46 00 00 002 Associated P/N : ----Yes 237300 FAP1 (120RH)/ DIR2/CAM
Maintenance advise: A CIDS interface and power-up test should be performed to confirm validity of the failure message. The associated time may be completely erroneous. CIDS SDF Z064H000030F Z064H000031A Z064H000031B ----TBD (end 2005) Associated P/N : ----No
237300 FAP1 (120RH)/DIR1/CAM Maintenance advise: To check the validity of the FAP
failure message, please select the FAP status page. Should any anomaly is visible on subject page, please refer to the corresponding trouble shooting task.
CIDS DIR Z064H000030F Z064H000031A Z064H000031B ----TBD (end 2005) Associated P/N : ----No
237300 FAP1 (120RH)/DIR2/CAM Maintenance advise: To check the validity of the FAP
failure message, please select the FAP status page. Should any anomaly is visible on subject page, please
CIDS DIR Z064H000030F Z064H000031A Z064H000031B TBD (end 2005) No
237313 AAP (126RH) ATT 4L Maintenance advise: If an AAP failure message is recorded into the PFR, perform a visual check of the AAP¨operation to determine the validity of the fault message. CIDS DIR Z064H000030F ----Z064H000031A Z064H000031B Associated P/N : ----No 237313 AAP (126RH) ATT 4L/ DEU B (300RH7)
Maintenance advise: If an AAP failure message is recorded into the PFR, perform a visual check of the AAP¨operation to determine the validity of the fault message. CIDS DIR Z064H000030F ----Z064H000031A Z064H000031B Associated P/N : ----No
237322 AIP (320RH1) ATT 1L Maintenance advise: A CIDS interface and power-up test
should be performed to confirm validity of the failure message. The associated time may be completely erroneous. CIDS SDF Z064H000030F Z064H000031A Z064H000031B ----TBD (end 2005) Associated P/N : ----No
237322 AIP (320RH9) ATT 4L Maintenance advise: A CIDS interface and power-up test
should be performed to confirm validity of the failure message. The associated time may be completely erroneous. CIDS SDF Z064H000030F Z064H000031A Z064H000031B ----TBD (end 2005) Associated P/N : ----No
237334 CIDS2(102RH) NO MAINT. ACTION. Associated with MAINT
STATUS TEMP CTL 1 and TEMP CTL 2. problem of a discrete label status computed by the CIDS2 and used by ACSC 1 and 2.
ACSC 1803A0000-03 TBD EYDCC Technical
note
P2161ME0308866-V1
237334 DIR1 (101RH) -SDF Maintenance advise: A CIDS interface and power-up test should be performed to confirm validity of the failure message. The associated time may be completely erroneous. CIDS SDF Z064H000030F Z064H000031A Z064H000031B ----TBD (end 2005) Associated P/N : ----No 237334 DIR1 (101RH) BUS/ DIR2 (102RH)
Maintenance advise: A CIDS interface and power-up test should be performed to confirm validity of the failure message. The associated time may be completely erroneous. CIDS SDF Z064H000030F Z064H000031A Z064H000031B ----TBD (end 2005) Associated P/N : ----No
237334 NO CIDS 1(2) DATA Please refer to TFU 23 73 00 083 CIDS Z010H000abcd
abcd=3113 or 3117 or 5115 or 5117 or 5118 or 5119 or 520A or 521A CFDS TBD TFU 23 73 00 083 Associated P/N : ALL P/N Yes
237334 NO CIDS 1(2) DATA (INTM) Please refer to TFU 23 73 00 083 CIDS Z010H000abcd
abcd= 3113 or 3117 or 5115 or 5117 or 5118 or 5119 or 520A or 521A CFDS TBD TFU 23 73 00 083 Associated P/N : ALL P/N No
240000 POWER SUPPLY INTERRUPT NO MAINTENANCE ACTION ILS 066-50008-0301
----066-50008-0405
Associated P/N :
----No
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 ----EIS II Soft Std S5 Associated P/N : ----Yes
242151 IDGi DISCONNECTED Check Class 3 Fault messages. GPCU 740121A
----740121B (SB24-1077) TFU 244100002 / TSM ATA 24 Associated P/N : ----No
242151 IDGi OIL LEVEL SENSOR/
GCUi - Source EPGS
Quality issue affecting component inside the GCU. Ony GCUs manufactured before Nov 2002 are affected. When message is triggered, the GCU should be removed and sent to vendor Hamilton Sundstrand for repair.
GCU 767584J
----TFU 24.21.00.039
Associated P/N :
----No
242255 AFS:28V PWR 11XU1 No MAINT. ACTION if occurs during PWR transfer:
Phase 02 (Engine start-up), Phase 09 and 10 (Engine Shut Down)
242300 CHECK GCU APU PIN C1, C5 GEN APU PIN A9, A10
1.If associated with a generator trip : remove the APU generator, otherwise, NO MAINT.ACTION. 2.If APU GEN FAULT imediately after APU start,reset APU GEN P/B SW. on OVHD panel. GCU 740120A 740120B ----740120C (SB 24-1074) TFU 244100008 Associated P/N : ----No 243251 SDACi: NO TR1 CURRENT 1PU1
At APU start NO MAINT. ACTION SDAC 35-0E5-1510-22
35-0E5-1611-22
----35-0E5-1513-31 TFU 315500003
Associated P/N :
----Yes
243834 SDACi : NO DATA FROM
BCLi
NO MAINT. ACTION if no Log Book complaint. SDAC 35-0E5-1510-22
35-0E5-1611-22 ----35-0E5-1513-31 Associated P/N : ----Yes 256200 SLIDE BTL XY/
DEU B (300RHZ) with X=1, 3 or 4 and Y=R or L and Z=1, 6 or 8.
No maintenance action required. CIDS
DIR Z064H000030F ----Z064H000031A Z064H000031B Associated P/N : ----No
261000 WRG: CAN BUS A (or B) NO MAINT. ACTION if fault message displayed after a
reset of CIDS or CIDS-SDF
CIDS DIR Z064H000030D Z064H000030E Z064H000030F TBD SIL 23-039 No
261200 CHECK FDU ENGi SUPPLY NO MAINT. ACTION if no log book complaint FDU 730400-01
----730401-02 TFU 261234020
Associated P/N :
----No
261300 CHECK FDU APU
LOOP A WARN CKT
No MAINT. ACTION if APU FDU test does not confirm the fault message
FDU 3720-00-00
----TBD TFU 26 13 00 001
Associated P/N :
----No
261300 CHECK FDU APU
LOOP B WARN CKT
No MAINT. ACTION if APU FDU test does not confirm the fault message
FDU 3720-00-00
----TBD TFU 26 13 00 001
Associated P/N :
----No
261734 SDCU CHANNEL 2 (10WQ) NO MAINT. ACTION if reset of the SDCU clears the
message SDCU RAI-2800-M0706 ----SB 92-1021 TFU 26 17 34 012 Associated P/N : ----No 275100 SFCC1(2) 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 49-170-11
From S/N 5813 To S/N 5956
275100 SFCCi or FLAP PPU POWER - If recorded in PFR without associated warning, NO MAINTENANCE ACTION required. If recorded in the PFR with the associated Ecam Warning: "F/CTL FLAP SYSi FAULT" or "F/CTL FLAP LOCKED" performed a manual reset of the SFCC through the SFCC MCDU BITE menu: SFCC/WTB RESET. SFCC 49117-10 (S/N 1732 to 1934) 49170-07 (S/N 1743 to 1904) ----49-170-11 TFU 275134025 Associated P/N : ----No 275100 SLT/FLT CSU 51CV OR WIRING TO SLT1(2)/FLP1(2)
If recorded in PFR without warning No MAINT. ACTION required. If Warning refer to TFU 27 51 00 004
SFCC 49170-11
----49170-11 Amdt. A TFU 27 51 00 004
Associated P/N :
----No
275134 SDACi: NO DATA FROM SFCC NO MAINT ACTION if no log book complaint SDAC 35-0E5-1510-22
35-0E5-1611-22 ----35-0E5-1513-31 Associated P/N : ----Yes 275453 FLP1(2) PCU VALVEBLOCK 23(24) CV
If associated with failure message SFCC1(2) or FLP PPU POWER. Corrective action: replace SFCC at the origin of the fault. SFCC 49-170-11 From S/N 5813 To S/N 5956 ----OIT 999.0047/05 Associated P/N : ----No
278100 SFCCi or SLAT PPU POWER If recorded in PFR without warning: NO MAINTENANCE
ACTION required. If associated with Ecam Warning: "F/CTL SLAT SYSi FAULT" or "F/CTL SLAT LOCKED"
SFCC 49117-10
49170-07
(S/N 1727 to 1906)
2800 FUEL L(R) XFR VALVE OPEN If this ECAM message is reported, perform functional BITE test of the ICTVs - FLSS Status (AMM 28-15-00-740-002) and a functional BITE test of the low-level sensors - FLSS BITE (AMM 28-46-00-740-001). No further action is required, if both test of the FLSS status and FLSS BITE show NO FAULT. FQIC ----TFU 281500003 Associated P/N : ----No
284234 FUEL QUANTITY FQIC 3QT NO MAINT. ACTION if FQIC grades remains at 1 after
FQIC test through CFDS. associated with ECAM warning : 28-00 FQI CH1(2) FAULT FQIC SIC5059-xx-xx05 SIC5059-xx-xx06 ----SIC5059-xx-xx07 TFU 284234030 Associated P/N : ----No
284634 FUEL LEVEL SENSING
L (or R) UNFULL SENSOR 25QJ1 (or 25QJ2 or 26QJ1 or 26QJ2)
NO MAINT. ACTION if triggered in flight phase 02 FLSCU ALL P/N
----TBD
Associated P/N :
----No
301151 R(L) WAI FILTER OR VALVE
10DL (9DL)
NO MAINT. ACTION if not associated with ECAM warning. ZC 775A0000-07 ----775A0000-08 TFU 301100014 / TSM ATA30 Associated P/N : ----Yes
307151 DRAINMAST HEATER FWD AFT NO MAINT. ACTION if no blockage or system
malfunction reported. DMCU 4-60000H800 4-60000H840 4-60000H882 SB 30-1030 TFU 307100002 No
307151 DRAINMAST HEATER FWD/AFT Replace the drainmast even if the fault is not confirmed on ground. This deviation has been identified. A correction will be incorporated in the next Drainmast
DRAIN MAST 4-60000H880 ----4-60000H882 SB 30-1030 TFU 307100003 Associated P/N : ----No
307151 DRAINMAST HEATER MID Valid only if Mod. 21598 embodied. NO MAINT. ACTION
if no blockage or system malfunction reported.
DMCU 4-60000H800 4-60000H840 ----4-60000H882 SB 30-1030 TFU 307100002/30710000 3 Associated P/N : ----No
307151 DRAINMAST HEATER MID Valid only if Mod 21598 embodied. Replace the drainmast
even if the fault is not confirmed on ground. This anomaly has been identified. A correction will be incorporated in the next Drainmast.
DRAIN MAST 4-60000H880 ----4-60000H882 SB 30-1030 TFU 307100003 Associated P/N : ----No
313234 BAD DATA FROM CFDIU NO MAINT. ACTION ILS 622-9738-020
622-9738-041 B401ACM0404 VSB ILS-720-34-01 AI S/B: 34-1093 Associated P/N : CFDIU No
313234 CFDIU(1TW)/HF(i) (3REi) No maintenance action if no logbook complaint. HF
Transcei ver
313234 LGCIU: NO DATA FROM CFDS Appears after a CFDIU power down, NO MAINTENANCE ACTION LGCIU 664700500A4A ----664700500A4B TFU 323134043 Associated P/N : ----No
313234 RADAR x: NO DATA FROM
CFDIU
NO MAINT. ACTION RADAR 204-1217-0418
204-1217-0421
----VSB RTA-4A-34-173 TFU344100010
Associated P/N :
----Yes
313352 QAR NO MAINT. ACTION if mentioned in Phase 1 in last leg
report FDIU 9026-16079-01B2 ----9026-16079-02B3 TFU 313300007 Associated P/N : ----No
313352 QAR TAPE LOW NO MAINT. ACTION if mentioned in Phase 1 in last leg
report FDIU 9026-16079-01B2 ----9026-16079-02B3 TFU 313300007 Associated P/N : ----No
313355 DFDR NO MAINT. ACTION if mentioned in Phase 1 in last leg
report
313355 DFDR PLAYBACK NO MAINTENANCE ACTION. RECOMMENDED STEP: EMBODY VSB SFIM FDIU/360-31-090
FDIU ED43A1D3
----ED43A1D4
Associated P/N : SSFDR
No
313634 NO DMU DATA (INTM) No Maintenance Action required DMU 795040-30-001
Associated P/N :
----No
313652 DAR No Maintenance Action required DMU 795040-30-001
----795040-31-002
Associated P/N :
----No
313652 DAR TAPE LOW No Maintenance Action required DMU 795040-30-001
----795040-30-002
Associated P/N :
----No
316322 DU EWD(2WK1)/ECP(2WM) No maintenance action required if no logbook complaint. EIS II
Software
SXT3CE2SA0420 SXT4EE2SA050A
316322 DU ND CAPT(3WK1)/ ND CAPT POT(8WK1)
No maintenance action required if no logbook complaint. EIS II Software SXT3CE2SA0420 SXT4EE2SA050A ----TBD Associated P/N : ----Yes 316322 DU ND FO(3WK2)/ ND FO POT(8WK2)
No maintenance action required if no logbook complaint. EIS II Software SXT3CE2SA0420 SXT4EE2SA050A ----TBD Associated P/N : ----Yes 316322 DU PFD CAPT(1WK1)/ PFD CAPT POT(7WK1)
No maintenance action required if no logbook complaint. EIS II Software SXT3CE2SA0420 SXT4EE2SA050A ----TBD Associated P/N : ----Yes 316322 DU PFD FO(1WK2)/ PFD FO POT(7WK2)
No maintenance action required if no logbook complaint. EIS II Software SXT3CE2SA0420 SXT4EE2SA050A ----TBD Associated P/N : ----Yes
316322 DU SD(2WK2)/ECP(2WM) No maintenance action required if no logbook complaint. EIS II
Software
SXT3CE2SA0420 SXT4EE2SA050A
316334 AFS:CHK DMCi-FMGCj CKT (i=1 or 2) (j=1 or 2)
NO MAINT. ACTION required if no log book complaint FMGC ALL P/N
----TBD
Associated P/N :
----No
316334 HUDC : CHECK DMC1 NO MAINT. ACTION HUDC 96154334-1
----96154334-2 TFU 343500003
Associated P/N :
----No
316334 HUDC : NO DMC1 DATA NO MAINT. ACTION HUDC 96154334-1
----96154334-2 TFU 343500003
Associated P/N :
----No
323171 CHECK LGCIU-PHC3 NO MAINT. ACTION if triggered in FWC flight phase 06
or 07 and if not associated with fault message "L/G EXT PROX SNSR 24GA(25GA) TGT POS"
BSCU E21327001 E21327003 ----TBD Associated P/N : ----No
324224 SDACi:NO DATA FROM BSCU1+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 (x=3, 4, 6) ----FWC STD H2F3 (Target: Oct 2005) Associated P/N : ----No
324224 SDACi:NO DATA FROM BSCU1
(I=1 or 2)
Wrong ATA REF. Should be 324234 instead. All FWC in BASIC configuration (Pre Mod 24159) are affected (E2, E3, E4, F2). FWC 350E017271616 350E018301919 350E018312020 350E053020x0x (x=3, 4, 6) ----FWC STD H2F3 (Target: Oct 2005) Associated P/N : ----No
324234 BSCU(10GG) NO MAINT. ACTION if the associated TSD shows fault
code 530 AND if triggered on ground during Engine start or Engine shut-down AND A/C equipped with BSCS EMM (mod 26925).
BSCU E21327003 TBD
Associated P/N :
No
324234 SDAC : NO DATA FROM BSCU NO MAINT. ACTION if no Log Book complaint SDAC 35-0E5-1510-22
35-0E5-1611-22
----35-0E5-1513-31
Associated P/N :
----No
324234 SDAC : NO DATA FROM TPIU NO MAINT. ACTION if no Log Book complaint SDAC 35-0E5-1510-22
35-0E5-1611-22
324334 ABCU(95GG)/
BRK SELECTOR VALVE(23GG)
NO MAINT. ACTION if triggered in flight phase 01 or 02 on A/C equipped with BSCS EMM (mod 26925)
BSCU E21327003 ----TBD Associated P/N : ----No 324418 SDACi: LH Y BRK 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) Post MOD 26925 FWC H2F3 P/N TBD Associated P/N : BSCU Yes 324418 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 350E053020606 (FWC H2F2) Post MOD 26925 FWC H2F3 P/N TBD Associated P/N : BSCU Yes 325151 STEERING ELECTRO HYDRAULIC MODULE 6GC
No MAINT. ACTION if fault message triggered after Landing Gear free fall extension and code 58 (code 6A on A320 with BOGIE) has been recorded in BSCU BITE.
BSCU C202163 SERIES C202452 SERIES PRE MOD 26925 N/A Associated P/N : ----No 325151 STEERING ELECTRO-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.
341119 AOA SENSOR 3FP1(2,3) Associated with the ECAM warning ANTI ICE CAPT (F/O,STBY) AOA. PHC 1663214-200 ----1663214-301 TFU 303100016 / TFU 303134006 / TSM ATA 30 Associated P/N : ----No
341119 AOA SNSRi (3FPi)/
ADIRUi(1FPi)
NO MAINTENANCE ACTION if appears after an AOA test. ADIRU 465020-0303-0308 ----465020-0303-0309 TFU 341000017 Associated P/N : ----No 341234 ADIRU1+3 (1FP1+3) BUS IR/WXR1 (1SQ1)
If no logbook complaint, do not remove the RTA-4B from the aircraft. Power cycling the RTA-4B or executing the Radar Test on the MCDU will clear the nuisance fault if it continues to be displayed in Ground Scanning.
RTA-4B 066-50008-0405 066-50008-0407 ----066-50008-0409 Associated P/N : ----No 341234 ADIRUi+3(1FPi+3) ADRBUS /WXRi(1SQi) (i = 1 or 2)
No maintenance action required if no logbook complaint. RADAR 822-1710-201 822-1710-202
----822-1710-203
Associated P/N :
----Yes
341234 AFS:ADIRU 1/2/3 DISAGREE NO MAINT. ACTION if not associated to any Message
in the ADIRU Bite
FAC B397AAM0507/0508 B397BAM0406/0407 B397BAM0509 B397AAM0509 B397CAM0101 TFU 229100009 Yes
341234 AFS:ADIRU 1/2/3 DISAGREE NO MAINT.ACTION IF NO LOGBOOK COMPLAINT. Pitot Pre SB 34-1122 ----SB 34-1122 (Pitot re-location) TFU220000012 Associated P/N : ----No
341234 AFS:ADIRU 1/2/3 DISAGREE No maintenance action if no logbook complaint FAC B397AAM0507
B397AAM0508 B397BAM0406 B397BAM0407 ----B397BAM0513 TFU 220000012 Associated P/N : ----Yes
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 49117-06 ----49117-07 TFU 275144003 Associated P/N : ----No 341234 QUALIFIER Di/WXRj (1SQj) (i=1 or 2 and j= 1 or 2)
No maintenance action if no logbook compaint. RADAR 822-1710-201
----822-1710-202
Associated P/N :
----No
341234 RADARi: NO DATA 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
341234 RADARi:NO DATA FROM ADIRU
NO MAINT. ACTION if no log book complaint RADAR 622-5132-020
622-5132-1120 ----VSB WRT-701X-34-68 VSB WRT-701X-34-77 Associated P/N : ----No
343522 HUD OHU NO MAINT. ACTION if no log book complaint. HUDC 96154334-1
96154334-2
----V65 SOFTWARE TFU 343500003
Associated P/N :
----Yes
343631 AFS : ILS i NO MAINT. ACTION if occurs at the end of the flight FMGC All P/N
----TBD
Associated P/N :
----Yes
343631 FWCi :NO DATA FROM
ILSi
NO MAINT ACTION if occurs in flight phases 02 and 07. ILS 622-9738-020
----622-9788-041
Associated P/N :
----Yes
343631 ILS i RECEIVER NO MAINT. ACTION if no Log book complaint ILS 204-1230-3518 204-1230-3521
204-1230-3532
343631 ILSi NO MAINT. ACTION if occurs in flight phase 02. ILS 622-9738-020 622-9738-041 ----NONE Associated P/N : ----Yes
343631 ILSi (2RTi) NO MAINT. ACTION required if no logbook complaint.
When receiver not tuned to any station, a self test is performed and this spurious message may be triggered.
ILS 622-9738-041 622-9738-020 ----Collins VSB ILS-720-34-11 ILS-900-34-6 Associated P/N : ----No
343631 MMR1 (40RT1)/GPWC (1WZ) NO MAINT. ACTION required EGPWS
965-0976-003-102-102 ---- 965-0976-003-206-206 Associated P/N : ----Yes
343676 ILSi RECEIVER Ref TSM task 34 36 00 810 801 associated to ILS fault
"34 36 31 ILSi RECEIVER" ILS 622-9738-020 ----622-9738-041 Associated P/N : ----No
344111 RADAR 1 ANTENNA NO MAINT. ACTION if no log book complaint RADAR 622-5132-020 622-5132-120 ----VSB WRT-701X-34-68 VSB WRT-701X-34-77 Associated P/N : ----No
344111 RADAR i ANTENNA NO MAINT ACTION if nologbook complaint RADAR 204-1217-0418
204-1217-0421 ----VSB RTA-4A-34-160 Rev.1 TFU 344100007 Associated P/N : ----No
344111 RADAR i ANTENNA NO MAINT ACTION if message recorded immediately
after engine start (this item concerns only 2 airlines)
RADAR MI 585306-402
----TBD NONE
Associated P/N :
----No
344111 WXR ANTENNA(11SQ) No maintenance action required if no logbook complaint. RADAR 822-1710-201
----822-1710-202
Associated P/N :
----No
344112 RADAR 1 CONTROL UNIT NO MAINT. ACTION if no log book complaint RADAR 622-5132-020
622-5132-120
VSB WRT-701X-34-68 VSB WRT-701X-34-77
344112 WXR CTL PNL(3SQ)/ WXRi(1SQi) (i = 1 or 2)
NO MAINT. ACTION if recorded during Engine Start (flight phase 02) or during switching from WXR1 to WXR2 and no associated cockpit effect.
RADAR 822-1710-201 ----822-1710-202 Associated P/N : ----No 344133 DMCi: NO WXRj CHj DATA (i=1, 2 or 3; j=1 or 2)
Associated to ECAM warning "NAV PRED W/S DET FAULT". Perform AMM Task 31-60-00-740-002 "EIS Input TEST". If test ok, the WXR/DMC interface works properly and the WXR transceiver units should not be removed. If the test fails, apply corresponding TSM procedure 34-41-00-810-8x "Loss of Weather Radar Channel j bus identified by the EIS i".
RADAR 622-5132-622 622-5132-623 ----TBD Associated P/N : ----No
344133 RADAR 1 TRANSCEIVER NO MAINT. ACTION if no log book complaint RADAR 622-5132-020
622-5132-120 ----VSB WRT-701X-34-68 VSB WRT-701X-34-77 Associated P/N : ----No
344133 RADAR i TRANSCEIVER NO MAINT ACTION if message recorded immediately
after engine start (this item concerns only 2 airlines).
RADAR MI 585306-402
----TBD NONE
Associated P/N :
----Yes
344133 RADARi TRANSCEIVER NO MAINT. ACTION if no log book complaint RADAR 204-1218-0418
204-1218-0421
VSB RTA-4A-34-160 Rev.1
344133 WXRi(1SQi) (i=1 or 2)
No Maint. Action if fault msg recorded in the PFR without cockpit effect and is associated with specific TSD (final 4 digits "0000"). The fault msg may be triggered if radar selected OFF and Pred Windshear scanning automatically activated during take-off or approach.
RADAR 066-50008-0405 066-50008-0407 ----066-50008-0409 Associated P/N : ----No 344133 WXRi(1SQi) (i= 1 or 2)
No maintenance action if no logbook complaint. RADAR 822-1710-201
----822-1710-202 Associated P/N : ----No 344137 WXR MOUNTING TRAY(5SQ)/ WXRi(1SQi) (i = 1 or 2)
No maintenance action required if no logbook complaint. RADAR 822-1710-201
----822-1710-202
Associated P/N :
----No
344233 RA1 (2SA1) +RA2 (2SA2) / WXR1 (1SQ1)
If no logbook complaint, do not remove the RTA-4B from the aircraft. Power cycling the RTA-4B or executing the Radar Test on the MCDU will clear the nuisance fault if it continues to be displayed in Ground Scanning.
RADAR 066-50008-0405 066-50008-0407 ----066-50008-0409 Associated P/N : ----No 344233 RA1(2SA1)+RA2((2SA2)/
WXRi (1SQi) (I=1 or 2)
NO MAINT. ACTION if recorded during Engine Start (flight phase 02) or during switching from WXR1 to WXR2 and no associated cockpit effect.
344300 DMC(i): NO TCAS DATA (i = 1 or 2)
No maintenance action required if no logbook complaint and if TCAS BITE is OK.
TCAS ACSS 7517900-10002 7517900-10003 ----TBD TFU 34.43.00.011 Associated P/N : ----No
344300 DMC(i): NO TCAS DATA
(i = 1 or 2)
No maintenance action required if no logbook complaint and if TCAS BITE is OK.
TCAS HONEY WELL 066-50000-1x08 066-50000-2x20 4066010-903/904 4066010-905 940-300-001 ----TBD TFU 34.43.00.011 Associated P/N : ----No
344300 DMC(i): NO TCAS DATA
(i = 1 or 2)
No maintenance action required if no logbook complaint and if TCAS BITE is OK.
TCAS ROCKW ELL 622-8971-320 622-8971-322 822-1293-322 ----TBD TFU 34.43.00.011 Associated P/N : ----No
344300 TCAS ARINC 429 NO MAINT ACTION if no logbook complaint. This
deviation has been identified.
TCAS 4066010-903
----4066010-905 TFU 344300006
Associated P/N :
----No
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 HONEY WELL 066-50000-1x08 066-50000-2x20 4066010-903/904 4066010-905 940-300-001 ----TBD TFU 34.43.00.011 Associated P/N : ----No 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 TFU 34.43.00.011 Associated P/N : ----No 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 ROCKW ELL 622-8971-320 622-8971-322 822-1293-322 ----TBD TFU 34.43.00.011 Associated P/N : ----No
344333 NO TCAS DATA No maintenance action required if no logbook complaint
and if TCAS BITE is OK.
TCAS ROCKW ELL 622-8971-320 622-8971-322 822-1293-322 ----TBD TFU 34.43.00.011 Associated P/N : ----No
344333 NO TCAS DATA No maintenance action required if no logbook complaint
and if TCAS BITE is OK.
TCAS ACSS
7517900-10002 7517900-10003
344333 NO TCAS DATA No maintenance action required if no logbook complaint and if TCAS BITE is OK.
TCAS ROCKW ELL 622-8971-320 622-8971-322 822-1293-322 ----TBD TFU 34.43.00.011 Associated P/N : ----No
344333 NO TCAS DATA No maintenance action required if no logbook complaint
and if TCAS BITE is OK.
TCAS HONEY WELL 066-50000-1x08 066-50000-2x20 4066010-903/904 4066010-905 940-300-001 ----TBD TFU 34.43.00.011 Associated P/N : ----No
344333 NO TCAS DATA No maintenance action required if no logbook complaint
and if TCAS BITE is OK.
TCAS ACSS 7517900-10002 7517900-10003 ----TBD TFU 34.43.00.011 Associated P/N : ----No 344334 ATC(i): NO DATA FROM TCAS (i = 1 or 2)
No maintenance action required if associated to the TCAS fault message "344334 TCAS (1SG)" and if TCAS BITE is OK. TCAS 066-50000-0203 066-50000-0102 066-50000-0208 066-50000-0108 ----TPA-81A-34-61 REV2 TPA-81A-34-72 TPA-81A-34-75 REV1 TFU 34.43.00.004 Associated P/N : ----No 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 ROCKW ELL 622-8971-320 622-8971-322 822-1293-322 TBD TFU 34.43.00.011 Yes
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 HONEY WELL 066-50000-1x08 066-50000-2x20 4066010-903/904 4066010-905 940-300-001 ----TBD TFU 34.43.00.011 Associated P/N : ----Yes 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 TFU 34.43.00.011 Associated P/N : ----Yes
344334 TCAS (1SG) No maintenance action required if no logbook complaint
and if TCAS BITE is OK.
TCAS 066-50000-0203 066-50000-0102 066-50000-0108 066-50000-0208 ----TPA-81A-34-61-REV2 TPA-81A-34-72 TPA-81A-34-75 REV1 TFU 34.43.00.004 Associated P/N : ----No
344334 TCAS(1SG) No maintenance action required if no logbook complaint
and if TCAS BITE is OK.
TCAS HONEY WELL 066-50000-1x08 066-50000-2x20 4066010-903/904 4066010-905 940-300-001 ----TBD TFU 34.43.00.011 Associated P/N : ----No
344334 TCAS(1SG) No maintenance action required if no logbook complaint
and if TCAS BITE is OK.
TCAS ROCKW ELL 622-8971-320 622-8971-322 822-1293-322 TBD TFU 34.43.00.011 No
344334 TCAS(1SG) No maintenance action required if no logbook complaint and if TCAS BITE is OK.
TCAS ACSS 7517900-10002 7517900-10003 ----TBD TFU 34.43.00.011 Associated P/N : ----No
345000 MODE S i NO MAINT ACTION if no logbook complaint. TCAS 4066010-903
----4066010-905 TFU 344300006
Associated P/N :
----No
345133 AFS:DMEi NO MAINT ACTION if no log book complaint FMGC
PEGASU S C13042xA01 ----TBD Associated P/N : ----Yes
345133 AFS:DMEi Due to A/C out of emitter range. No Maint. Action if no
Log Book complaint.
DME 622-4540-023 FMGC LEGACY VSB DME 700-34-33 VSB DME 700-34-27 TFU 345100008 Associated P/N : B398BxM0xxx Yes
345133 DME i TRANSCEIVER NO MAINT. ACTION if no log book complaints DME 622-4540-020
622-4540-021 622-4540-022
345212 ATC CTL PNL(2SH) This misbehavior will be corrected at the next standard of P/N 7517800-10005 and new ATC CTL PNL(3SH)
TCAS 7517800-10005 ----7517800-10005 Associated P/N : ----No 345233 ATCi (1SH1) /
TCAS (100SG) source TCAS (i = 1 or 2)
No maintenance action if not associated to ECAM WARNING "NAV TCAS FAULT". CLASS 1 fault message when ATC transponder is the active one. CLASS 3 fault message if the ATC transponder is in standby (See PART C).
T2CAS 9000000-10110 ----TBD Associated P/N : ----No 345233 ATCi (1SH1) / TCAS (1SG) source TCAS (i = 1 or 2)
No Maint. Action if not associated to ECAM WARNING "NAV TCAS FAULT". CLASS 1 fault message when ATC transponder is the active one. CLASS 3 fault message if the ATC transponder is in standby (See PART C). TCAS 7517900-10002 7517900-10003 ----TFU 34.43.00.011 Associated P/N : ----No 345233 NO ATC i DATA Source CFDS (i = 1 or 2)
No maintenance action is required if no logbook complaint. ATC 751-7800-10002 751-7800-10005 ----TBD Associated P/N : ----Yes 345233 QUALIFIER Ci/WXRj (1SQj) (i = 1 or 2 and j = 1 or 2)
345331 ADF i RECEIVER NO MAINT. ACTION if no log book complaint. ADF 622-5222-020 ----VSB ADF-700-34-20 VSB ADF-700-34-21 VSB ADF-700-43-27 Associated P/N : ----No
345331 NO ADF(i) DATA No maintenance action when ADF 1 or/and 2 not installed
on the aircraft. CFDIU ----N/A Associated P/N : ----Yes
345531 AFS : VOR i NO MAINT. ACTION if no logbook complaint FMGC All P/N
----TBD
Associated P/N :
----Yes
345531 VOR i : VOR RECEIVER NO MAINT ACTION if no logbook complaint VOR 622-5220-020
----VSB 700-34-10 Rev 1 VSB 700-34-19 TFU 345500009 / TFU 345500013 Associated P/N : ----No
361134 SDAC:NO DATA FROM BMCi NO MAINT. ACTION if no logbook complaint SDAC 35-0E5-1510-22 35-0E5-1611-22 ----350E5-1513-31 Associated P/N : ----No
383100 CHECK LAV (X) OR CHECK
VAC LINE LEAKAGE
Disconnect 42MG XDCR, then, the spurious message will disappear VSC 14404-001-1 ----14404-011A SB 38-1027 TFU 383100003 / TSM ATA 38 / VSB 14404-38-01 Associated P/N : ----No 383100 LIQD LVL XMTR (40MG) AND LIQD LVL SNSR (41MG)
The system operation can be checked on ground by using the MCDU toilet ground report or by checking the FAP Water/Waste page.
CIDS DIR Z064H000030D Z064H000030E Z064H000030F ----Z064H000031A Z064H000031B TFU 38.31.00.026 Associated P/N : ----Yes
383134 VSC NO MAINT. ACTION VSC 14404-011A
----14404-011B TFU 38 31 00 022 SB 38-1044 REV2 VSB 14440403802 Associated P/N : ----Yes
383141 TOILET ASSY LAV i
(with i = A, D, E, or F)
The system operation can be checked on ground by using the MCDU toilet ground report or by checking the FAP Water/Waste page.
CIDS DIR Z064H000030D Z064H000030E Z064H000031A Z064H000031B TFU 38.31.00.026 No
383162 LIQD LVL XMTR (40MG) The system operation can be checked on ground by using the MCDU toilet ground report or by checking the FAP Water/Waste page.
CIDS DIR Z064H000030D Z064H000030E Z064H000030F ----Z064H000031A Z064H000031B TFU 38.31.00.026 Associated P/N : ----Yes
383168 DIFF PRESS XDCR NO MAINT. ACTION if 42MG XDCR has been
disconnected. VSC 14404-001-1 ----14404-011A SB-38-1027 TFU 383100003 / TSM ATA 38 Associated P/N : ----No
492318 LCDT Sensor P29 No MAINT. ACTION ECB 4500001
4500001A 4500001B 4500003G APS 3200 4500003H AIRBUS SB: A320-49-1061 Associated P/N : APU Yes
493211 FUEL CTL UNIT P19 NO MAINT. ACTION if no logbook complaint ECB 304817-1
36-300
304817-2 S/B A320-49-1053
Associated P/N : GTCP
No
496134 SDAC : NO DATA FROM ECB NO MAINT. ACTION if no Log Book complaint
(GTCP36.300)
SDAC 35-0E5-1510-22
35-0E5-1611-22
499414 OIL PRESS SW P14 NO MAINT. ACTION if no logbook complaint ECB (GTCP 36-300) 304817-1 ----304817-2 Associated P/N : ----No
499651 APU OIL HEATER(8093KM) NO MAINT. ACTION required on A/C post SB 49-1026
and APU 36-300 pre Honeywell VSB 49-6702 and ECB P/N 3888394-230300 or ECB P/N 304817-1 or ECB P/N 304817-2 APU 3800278-2 3800278-3 3800278-4 Associated P/N : ----No 520000 DOOR BTL XY/
DEU B (300RHZ) with X=1, 3 or 4 and Y=R or L and Z=1, 6 or 8.
No maintenance action required. CIDS
DIR Z064H000030F ----Z064H000031A Z064H000031B Associated P/N : ----No 731150 FRV(CLOSED),J7(J8),ECU
During FADEC motoring test
NO MAINTENANCE ACTION IF ECU 5.BE or 5.DE not fitted on A/C. ECU 1820M89P02 1820M36P02 1820M88P02 1820M87P02 ----SB 73-1034 SB 73-1037 TFU 732900033 Associated P/N : ----No
732160 DMCi:NO ECUi A(B) DATA No Maint. Action if it occurs in phase 02 at the end of an engine run (80KTS not reached) or after any FADEC reset.
732160 ECU(Ei-4000KS) (i=1 or 2)
No Maint. Action if it occurs in phase 02 at the end of an engine run (80KTS not reached) or after any FADEC reset.
DMC EIS II Soft SXT3F-E2SA-0410 SXT3C-E2SA-0420 CFM ENGINE TBD Associated P/N : ----Yes
732234 DMCi: NO EECi A(B) DATA No Maint. Action if it occurs in phase 02 at the end of an engine run (80KTS not reached) or after any FADEC reset.
EEC ALL P/N DMC (EIS I) N/A Associated P/N : ----Yes 732234 EEC(Ei-4000KS) (i=1 or 2)
No Maint. Action if it occurs in phase 02 at the end of an engine run (80KTS not reached) or after any FADEC reset.
DMC EIS II Soft SXT3F-E2SA-0410 SXT3C-E2SA-0420 IAE/PW ENGINE TBD Associated P/N : ----Yes 752210 LPTC VLV,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 ----SB 73-1034 SB 73-1037 TFU 732900033 Associated P/N : ----No
752420 ECU AIR,J7(8), ECU Must be disregarded if CFMI S/B 72-436 AIRBUS S/B
71-1014 embodied on the aircraft.
ECU 1459M55P15 1459M55P16 1519M83P02 1459M55P17 1519M83P04 1820M27P01 No
783100 HC/PROX SW/T/R UP ACT i Associated with Maint. Status Eng I FADEC. No Maint. Action if recorded during phase 07 or 08 and if there is no crew report. EEC SCN12C ----SCN12D TFU 783100080 Associated P/N : ----No 793311 QUALIFIER Bi/WXRj (1SQj) (i=1 or 2 and j= 1 or 2)
NO MAINT. ACTION if recorded during Engine Start (flight phase 02) or during switching from WXR1 to WXR2 and no associated cockpit effect.
RADAR 822-1710-201
----822-1710-202
Associated P/N :
----No
793315 SDACi:ENG2 OIL PRESS
XMTR 4004EN (i=1 or 2), Source ECAM 1 or ECAM 2.
Wrong FIN number. Should be 4003EN instead. All FWC in BASIC configuration (Pre Mod 24159) are affected (E2, E3, E4, F2). FWC ALL P/N ----FWC Std H2F3 (Target: Oct 2005) Associated P/N : ----No
793316 CHECK N4 BRG SCAV PRESS
XMTR CIRCUIT 4005 EN
NO MAINT. ACTION if EIU Ground Scanning result is RTOK
EIU All P/N (IAE)
----3957905004 3957905005 TFU 793316001 Associated P/N : ----No
793415 CHECK OIL PRESS 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.
XXXXXX ADF i : NO DATA
FROM CONTROL SOURCE
NO MAINT. ACTION ADF 622-5222-020
204-1168-7513 B401ACM0404 VSB ADF-700-34-21 VSB DFA-75A-34-49 VSB ADF-700-34-27 TFU 345300006 / TFU 345300007 Associated P/N : CFDIU Yes
XXXXXX DME : NO DATA FROM
CONTROL SOURCE
NO MAINT. ACTION DME 9599-614-03105
----VSB TDM-709-34-012
Associated P/N :
----Yes
XXXXXX ILS i : NO DATA FROM
CONTROL SOURCE
NO MAINT. ACTION ILS 20412303518
B401ACM0404
VSB RIA-35A-34-41 TFU 343600004
Associated P/N : CFDIU
No
XXXXXX VHFi:NO DATA FROM
CONTROL SOURCE NO MAINT. ACTION VHF 622-5219-020 B401ACM0404 VSB VHF-700-23-30 TFU 231200007 Associated P/N : CFDIU No XXXXXX VOR i : NO DATA
FROM CONTROL SOURCE
NO MAINT. ACTION (mainly due to FMS resets). VOR 622-5220-020
20412313610 VSB VOR-700-34-10 VSB RVA-36A-34-54 TFU 345500005 / TFU 345500008 Yes
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 Associated P/N : ----Yes
2131 CAB PRESS SYST i FAULT If this warning occurs on ground with
ADIRS "OFF", Select ADIRS "ON". If the warning still present, ref TSM
CPC 902215702-7 ----902215702-8 TFU 213134005 Associated P/N : ----No 2151 PACKi (Maintenance Status)
Associated to P1(2) FLOW CTL VALVE NO MAINT. ACTION if Bite test OK
FCV 751A0000-06
----751A0000-07 TFU 215151004
Associated P/N :
----No
2161 AIR PACK 1+2 FAULT NO MAINT ACTION if it occurs at the
flight beginning (PHASE 03 or 04).
PC ALL P/N ----N/A Associated P/N : ----Yes 1
2161 AIR:PACK i REGUL FAULT When not associated with any maintenance message, check all sensors peripheral to the pack controler. PC All P/N ----TFU 216134003 / SIL 21-049 Associated P/N : Sensor No 2161 TEMP CTL 1 (or 2) (Maintenance Status)
NO MAINT. ACTION if associated with fault message "237334 CIDS2(102RH) Source TEMP CTL". Status problem of a discrete label computed by the CIDS2 and used by ACSC 1 and 2.
ACSC 1803A0000-03 ----1803B0000-01 SB A320-21-1149 / VSB 1803A-21-02 Associated P/N : ----No
2163 AFT(FWD) CAB DUCT OVHT Check Temp. sensor output resistance ZC All P/N
----N/A TFU 216318001 /
SIL 21-049
Associated P/N :
----No
2163 CKPT DUCT OVHT Check Temp. sensor output resistance ZC All P/N
----N/A TFU 216318001 / SIL 21-049 Associated P/N : ----No 2
2200 AUTO FLT A/THR OFF Configuration Warning FMGC All P/N
----N/A N/A
Associated P/N :
----Yes
2200 AUTO FLT AP OFF Configuration Warning FMGC All P/N
----N/A N/A
Associated P/N :
----Yes
2200 WINDSHEAR DET FAULT Appears at Slat extension if an ADR test
has been performed on ground. Pull the FAC C/B during the ADR test to avoid the message FAC B397AAM0507/0508 B397BAM0406/0407 ----B397BAM0509 TFU 226600004 / AMM ATA 34.13.00 pBlock 501 Associated P/N : ----No
2200 YAW DAMPER SYS NO MAINT. ACTION if occurs at Engine
start during strong wind conditions. Recentering the Yaw damper before Engine start with Electric Pump will avoid the message. FAC B397AAM0507/0508 B397BAM0406/0407 B397BAM0508/0509 B397CAM0101/0102 B397AAM0509/0510 ----B397BAM0510 TFU 226300005 Associated P/N : ----No 3
2300 COM SATCOM FAULT No. Maint. Action if ECAM WARNING triggered when ADIRU 1+2+3 OFF
DMC EIS II Soft SXT3F-E2SA-0410 SXT3C-E2SA-0420 ----EIS II STD S5 Associated P/N : ----No
2400 ELEC BCL i FAULT NO MAINT. ACTION if no failure message
in the PFR, and BCL test thru MCDU is OK.
BCL 35-0L5-1003-06 35-0L5-1004-07 ----35-OL5-1005-08 (SB 24-1075) TFU 243800007 / TFU 243800009/TFU 243800022 Associated P/N : ----No
2600 SMOKE LAVATORY DET SMOKE If associated with the SDCU fault message
"SMOKE DET LAV x" (x is the lavatory affected), ref the maintenance advice field of the TFU 261715003 SMOKE DET GAI2800-02 PAI2830-00 ----TBD TFU 261715003 Associated P/N : ----No
2615 AVIONICS SMOKE If triggered on ground, associated with
amber memo LAND ASAP no evidence of smoke, then FWC1 & FWC2 should be reset in order to clear the latch condition of the warning. This allows to prevent spurious LAND ASAP memo to be triggered at take-off. SMOKE DET CG7GO ----CGDU2000-00 TFU 26 15 15 001 Associated P/N : ----No 4
261600 SMOKE AFT CRG BTL1 FAULT
Maintenance advise: Make sure that when AMM Task 26-16-00-710-001 "Operational test of the cargo-compartment Smoke-detection system by PTT" is performed, the PTT button is hold 20 seconds as
recommended and activated only one time.
CIDS DIR Z014H000030C ----Z014H000131A Z014H000031A Associated P/N : ----No 261600 SMOKE AFT CRG BTL2
FAULT (if installed)
Maintenance advise: Make sure that when AMM Task 26-16-00-710-001 "Operational test of the cargo-compartment Smoke-detection system by PTT" is performed, the PTT button is hold 20 seconds as
recommended and activated only one time.
CIDS DIR Z014H000030C ----Z014H000131A Z014H000031A Associated P/N : ----No 261600 SMOKE FWD CRG BTL1 FAULT
Maintenance advise: Make sure that when AMM Task 26-16-00-710-001 "Operational test of the cargo-compartment Smoke-detection system by PTT" is performed, the PTT button is hold 20 seconds as
recommended and activated only one time.
CIDS DIR Z014H000030C ----Z014H000131A Z014H000031A Associated P/N : ----No 261600 SMOKE FWD CRG BTL2
FAULT (if installed)
Maintenance advise: Make sure that when AMM Task 26-16-00-710-001 "Operational test of the cargo-compartment Smoke-detection system by PTT" is performed, the PTT button is hold 20 seconds as
recommended and activated only one time.
CIDS DIR Z014H000030C ----Z014H000131A Z014H000031A Associated P/N : ----No 5
2700 F/CTL ALT LAW IF OCCURS AT ENGINE START,PERFORM ELACs RESET WITH ALL HYDRAULIC SYSTEMS DEPRESSURIZED. ELAC 3945122502 STD L69 ----3945122505 TFU279300040/FC OM 3 02 27 Associated P/N : ----No
2700 F/CTL ELAC 2 PITCH FAULT At engine start, if associated with "THS ACTR SERVO MOT 1 9CE" maintenance message refer to TFU 27 90 00 028. NO MAINTENANCE ACTION required if warning "F/CTL ELAC 2 PITCH FAULT" can be cleared through ELAC 2 push button reset. ELAC + THSA 3945122502(ELAC) 3945122504(ELAC) 9231-4-600 (THSA) ----3945122505 (ELAC) 9231-5-600 (THSA) TFU279000028 Associated P/N : ----No
2700 F/CTL ELAC1(2) FAULT Even if associated with "ELAC1(2)"
maintenance message, failure of opposite ELAC may be suspected. Apply TSM procedure. FCDC 115370-105 115370-1016 ----N/A TFU 279500039 Associated P/N : ----No
2700 F/CTL SPD BRK DISAGREE Configuration warning FCDC All P/N
----N/A
Associated P/N :
----Yes
6
2751 F/CTL If associated with the PFR message "SFCC1(2) FLAP(SLAT)", reset the SFCC.
SFCC 49-170-07 ----AMDT C 49-170-11 TFU 27 51 34 027 Associated P/N : ----No
275100 F/CTL FLAPS LOCKED If experienced at first A/C power-up when
electrical power is powered from batteries ref TFU 275134026 MAINTENANCE ADVICE field. SFCC 49117-10 49170-07 ----Amdt A 49-170-11 TFU 275134026 Associated P/N : ----No
278100 F/CTL SLATS LOCKED If experienced at first A/C power-up, when
electrical power is supplied from batteries ref TFU 27134026 MAINTENANCE ADVICE field SFCC 49117-10 49170-07 ----49-170-11 Amdt A 49-170-11 TFU 275134026 Associated P/N : ----No
2793 ELAC i PITCH FAULT IF NO MAINTENANCE MESSAGE
associated : CHECK the PITCH CHANGE OVER DISCRETES LANE.
FCDC 115370-0105 ----115370-1016 115370-0106 TFU 279300028 Associated P/N : ----No 7
