NO MAINT. ACTION if occurs after alpha-call-up programmation of this parameter when A/C equipped with FWC C4/C5 and IAE engines.
DMU All P/N
35-0E0-1618-7070/71 90311624B3D2J3
FWC Associated Part : 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
35-0E0-1618-7070/71 90311624B3D2J3
FWC Associated Part :
212151 RECIRC FAN i OR SPLY NO MAINT. ACTION ZC 775A0000-05
----775A0000-06 TFU 216334044
----Associated Part :
212152 MIXER FLAP DRIVE NO MAINT. ACTION ZC 775A0000-05
----775A0000-06 TFU 216000003
----Associated Part :
215100 FLOW SEL NO MAINT. ACTION ZC 775A0000-05 775A0000-06
215218 Pi BLEED TEMP SENSOR NO MAINT. ACTION ZC 775A0000-05
----775A0000-06 TFU 216334044
----Associated Part :
216111 Pi COMP TEMP SENSOR NO MAINT. ACTION ZC 775A0000-05
----775A0000-06 TFU 216334044
----Associated Part :
216112 Pi COMP OVHT SENSOR NO MAINT. ACTION ZC 775A0000-05
----775A0000-06 TFU 216334044
----Associated Part :
216115 Pi OUTLET TEMP SENSOR NO MAINT. ACTION ZC 775A0000-05
----775A0000-06 TFU 216334044
----Associated Part :
216134 PACKi CONT NO MAINT. ACTION ZC 775A0000-05 775A0000-06
759A0000-08
TFU 216134001 / TFU 216334044
216151 Pi RAM AIR IN ACTUATOR NO MAINT. ACTION ZC 775A0000-05
----775A0000-06 TFU 216334044
----Associated Part :
216152 PiRAM AIR OUT ACTUATOR NO MAINT. ACTION ZC 775A0000-05/-06/-07
----775A0000-08 TFU 216334044
----Associated Part :
216153 TURBINE BYPASS VALVE NO MAINT. ACTION ZC 775A0000-05
----775A0000-06 TFU 216334044
----Associated Part : 216315 TEMP SENSOR FWD (AFT)
CAB DUCT I
NO MAINT. ACTION ZC 775A0000-05
----775A0000-06 TFU 216334044
----Associated Part : 216315 TEMP SENSOR COCKPIT
DUCT I
NO MAINT. ACTION ZC 775A0000-05 775A0000-06 TFU 216334044
216316 TEMP SENSOR R/H (L/H) MIXER I
NO MAINT. ACTION ZC 775A0000-05
----775A0000-06 TFU 216334044
----Associated Part : 216317 TEMP SENSOR FWD (AFT)
CAB I
NO MAINT. ACTION ZC 775A0000-05
----775A0000-06 TFU 216334044
----Associated Part :
216317 TEMP SENSOR COCKPIT I NO MAINT. ACTION ZC 775A0000-05
----775A0000-06 TFU 216334044
----Associated Part : 216318 FWD (AFT) CAB DUCT
OVHT SENSOR I
NO MAINT. ACTION ZC 775A0000-05
----775A0000-06 TFU 216334044
----Associated Part : 216318 COCKPIT DUCT
OVHT SENSOR I
NO MAINT. ACTION ZC 775A0000-05 775A0000-06 TFU 216334044
216334 NO PACK DATA FROM ECS NO MAINT. ACTION if zone cont. -5 fitted on A/C
ZC 775A0000-05
304640-2 775A0000-06
ECB Associated Part :
216334 ZONE CONT NO MAINT. ACTION ZC 775A0000-05
----775A0000-06 TFU 216334044
----Associated Part :
216351 TRIM AIR VALVE COCKPIT NO MAINT. ACTION ZC 775A0000-05/-06/-07
----775A0000-08 TFU 216000004
----Associated Part :
216351 TRIM VALVE FWD (AFT) CAB NO MAINT. ACTION ZC 775A0000-05/-06/-07
----775A0000-08 TFU 216000004
----Associated Part :
216352 TRIM AIR PRESS VALVE I NO MAINT. ACTION ZC 775A0000-05 775A0000-07 TFU 216000003
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 does receive answer from FMGCx (when in slave condition). No
maintenance action required.
ATSU host platform S/W
LA2T0S162C0C0F1 LA2T0S111C1B0F1
----LA2T0J13000C0F1 TFU 46 00 00 002
----Associated Part :
231233 VDR3(1RC3)/ATSU1(1TX1) NO MAINT. ACTION. ATSU LA2T0J13000C0F1
064-50000-2051
TBD TFU 46.00.00.002
VDR Associated Part : 233346 SEB 42LFT, 42RGT REF SIL HUGHES 1142000-130-03 NO
MAINT. ACTION
PES 1142300-131-xx
----VSB AVI-93-32 TFU 233300009
----Associated Part : 233346 SEB 41LFT, 41RGT REF SIL HUGHES 1142000-130-03 NO
MAINT. ACTION
PES 1142300-131-xx VSB AVI-93-32 TFU 233300009
233600 NO SCU DATA No maintenance action if no cabin crew complaint. This message is recorded when the SCU pin prog is activated with the SCU not installed, and with the following SCU P/N: 0215-030, 743-03xx-xxx, RD-AV3001-33, 610860-xxxx.
CIDS Z01H0005119
----Z010H000520A TFU 233300009
----Associated Part : 242100 CHECK GCUi PIN A8A,A9B
IDGi PIN B7,B8 WIRING
GPCU 740121A
----740121B (S/B 24-1077)
TFU 244100002 / TSM ATA 24 pB 401
----Associated Part : 242200 CHECK FIRE HANDLE i ;
RESET GEN i
NO MAINT. ACTION if Fire handle switches actuation not mentionned in the Log Book.
GPCU 740121A
----740121B (SB 24-1077)
TFU 244100004
----Associated Part : 242218 TDC AC SENSOR 50 XU i After a GPCU test, Generator 1& 2 P/B
switches in the cockpit must be reset.
Otherwise, this message will appear after the 2nd GPCU test
GPCU 740121A 740121B
----Vdr SIL 229 TFU 244100003
----Associated Part :
244134 GPCU NO MAINT. ACTION GPCU 740121A 740121B
(SB-24-1077)
284216 CTR CADENSICON 20 QT NO MAINT. ACTION Cadensicon 796-809-5
----796-809-6 TFU 284234029
----Associated Part :
284216 L(R) CADENSICON 19QTi NO MAINT. ACTION Cadensicon 796-809-5
----796-809-6 TFU 284234029 / TFU 284234016
----Associated Part : 301151 R(L) WAI FILTER OR VALVE
10DL(9DL)
NO MAINT. ACTION ZC 775A0000-05
----775A0000-07 TFU 216000003
----Associated Part :
303134 PHC 6 DA 1(2,3) PHC 1663214-200
----1663214-301 TFU 303134006 / TSM ATA 30
----Associated Part : 313234 CFDIU(1TW1)/ATSU1(1TX1) Protocol problem between ATSU and
CFDIU. No maintenace action required.
ATSU host platform S/W
LA2T0S162C0C0F1 LA2T0S11C1B0F1
LA2T0J13000C0F1 TFU 46 00 00 002
313234 CFDIU(1TW)/
WXRi (i = 1 or 2)
No maintenance action required if no logbook complaint.
RADAR 822-1710-201
----822-1710-202
----Associated Part :
313334 NO CLOCK DATA NO MAINT. ACTION FDIU 9026-16079-01B2
----9026-16079-02B3
----Associated Part :
313334 NO DMC1 DATA NO MAINT. ACTION FDIU 9026-16079-01B2
----9026-16079-02B3
----Associated Part :
313334 NO FWCi DATA NO MAINT. ACTION FDIU 9026-16079-01B2
----9026-16079-02B3
----Associated Part :
313334 NO CFDS DATA NO MAINT. ACTION FDIU 9026-16079-01B2 9026-16079-02B3
313334 NO SDAC 1 DATA NO MAINT. ACTION FDIU 9026-16079-01B2
----9026-16079-02B3
----Associated Part :
313355 DFDR PLAY BACK NO MAINT. ACTION FDIU 9026-16079-01B2
----9026-16079-02B3 TFU 313300007
----Associated Part : 313355 DFDR PLAYBACK Switch the recorder ground control P/B
ON, then enter in the FDIU TEST MENU, check the DFDR status. NO MAINT. ACTION if associated with DFDR OPERATIVE NO PLAY BACK.
FDIU 9026-16079-01B2 9026-16079-01B3
----9026-16079-02B4 TFU 3133000015
----Associated Part :
315534 SDAC i NO MAINT. ACTION if associated with
codes 2000 to 2005
SDAC
35-0E5-1510-22 35-0E5-1611-22
----35-0E5-1513-31 TFU 315500002
----Associated Part :
315534 SDACx(1WVx)/ATSU1(1TX1) ATSU host
platform S/W
LA2T0S111C1B0F1 LA2T0J13000C0F1 TFU 46 00 00 002
316234 DMC(1WT2/3)/ATSU(1TX1) Label 316 (wind direction) not properly received by the ATSU. Item under investigation. This deviation has no operational impact as data only needed for ADS applications.
ATSU host platform S/W
LA2T0S162C0C0F1
----LA2T0J13000C0F1
----Associated Part : 316234 DMC(1WT1/3)/ATSU(1TX1) Label 316 (wind direction) not properly
received by the ATSU. Item under investigation. This deviation has no operational impact as data only needed for ADS applications. No maint. Action required.
ATSU host platform S/W
LA2T0S162C0C0F1 LA2T0S111C1B0F1
----LA2T0J13000C0F1 TFU 46 00 00 002
----Associated Part : 341034 NO DATA FROM ADIRS NO MAINT. ACTION if appears in
Phase 1,2 or 10 .
ZC 775A0000-05
----775A0000-06 TSM ATA 21
----Associated Part : 341200 No access to ZONT
PHC1(2,3) INTERFACE
NO MAINT. ACTION PHC 1663214-200
----1663214-301 TFU 303100013
----Associated Part : 341200 CHECK ADIRU1 (2,3) R STA
PHC1(2,3) INTERFACE
NO MAINT. ACTION PHC 1663214-200 1663214-301 TFU 303100013
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
----1663214-301 TFU 303100013
----Associated Part : 341200 CHECK ADIRU 1 (2,3) PITO
PHC1(2,3) INTERFACE
NO MAINT. ACTION PHC 1663214-200
----1663214-301 TFU 303100013
----Associated Part : 341234 ADIRU3(1FP3) ADR BUS/
WXRi(1SQi) (i = 1 or 2)
No maintenance action required if no logbook complaint.
RADAR 622-5132-623
----TBD
----Associated Part : 341234 ADIRU3(1FP3) ADR BUS/
WXRi(1SQi) (i = 1 or 2)
No maintenance action required if no logbook complaint.
RADAR 822-1710-201 822-1710-202
822-1710-203
341234 ADIRUi(1FPi) IR BUS/
WXRj(1SQj) (i = 1, 2 or 3 and j = 1 or 2)
No maintenance action required if no logbook complaint.
RADAR 822-1710-201 822-1710-202
----822-1710-203
----Associated Part : 344233 RAi(2SAi)/WXRj
(i = 1, 2 or 3 and j = 1 or 2)
No maintenance action required if no logbook complaint.
RADAR 822-1710-201
----822-1710-202
----Associated Part : 345233 ATCi (1SH1) / TCAS (1SG)
(i = 1 or 2)
No Maint. Action. CLASS 3 fault message is triggered if ATC transponder in standby.
TCAS 7517900-10002 7517900-10003
---- ----Associated Part : 462134 ATSU(1TX1)/HFi(3Ri) NO MAINT. ACTION. This message is
triggered if there is no ATSU link with HFDR, i.e. (MOD 30625/30331 not installed).
HFDR 822-0990-003 COLLINS HFS900D
----TBD
----Associated Part :
462134 ATSU1(1TX1) No maintenance action required. ATSU host
platform
LA2T0S162C0C0F1 LA2T0S111C1B0F1
LA2T0J13000C0F1 TFU 46 00 00 002
710000 BALANCE ENGi N1-NB-VIB NO MAINT. ACTION if no log book entry concerning Engin vibrations.
EVMU 241-211-000-021
----241-211-000-031 TFU 773234005
----Associated Part : 710000 CHECK ENG i N2-NB-VIB NO MAINT. ACTION if no log book
entry concerning Engin vibrations.
EVMU 241-211-000-021
----241-211-000-031 TFU 773234005
----Associated Part :
715100 J3, ADC1 NO MAINT. ACTION ECU 1459M55P15
1519M83P02 1459M55P16 1519M83P03
----1459M55P17 1519M83P04 1820M27P01
TFU 732900012
----Associated Part :
715100 J4, ADC2 NO MAINT. ACTION ECU 1459M55P15
1519M83P02 1459M55P16 1519M83P03
----1459M55P17 1519M83P04 1820M27P01
TFU 732900012
----Associated Part : 732500 CHECK EIU WHC INTERFACE Check/Confirm that EIU/WHC interface
is defective
WHC 6664-202-3 6664-287-0 TFU 304034002
753100 BLD SNSR,J15,ECU NO MAINT.ACTION IF SB 72-1005 NOT EMBODIED ON THE A/C
ECU 1459M55P17
1519M83P04 1820M27P01
----SB 72-1005 TFU 732900025
----Associated Part : 753100 VTURI,BLD SNSR,ECU NO MAINT. ACTION IF SB 72-1005
NOT EMBODIED ON THE A/C.
ECU 1459M55P17
1519M83P04 1820M27P01
----SB 72-1005 TFU 722900025
----Associated Part : 753100 CWB3 SENS, J15 ECU NO MAINT. ACTION if SB 72-1005 not
embodied on the A/C
ECU 1459M55P15
1519M83P02 1459M55P16 1519M83P03
----SB : 72-1005 TFU 732900025
----Associated Part : 753100 WB3 SENS, J15 ECU NO MAINT. ACTION if SB 72-1005 not
embodied on the A/C
ECU 1459M55P15
1519M83P02 1459M55P16 1519M83P03
----SB : 72-1005 TFU 732900025
----Associated Part :
Sel. valve and LGCIU faults are covered by the fault message: "LGCIU i 05GAi".
With the LGCIU std 4D, the following message "LGCIU i 05GAi / L/G SEL VALVE 40G0A" will be triggered in case of valve or LGCIU failure.
LGCIU 664700500A4B 664700500A4C
----664700500A4D
----Associated Part : Recording in the PFR of "empty" DMU
messages in flight phase 2 or 5. No Maintenance Action required.
DMU 795040-31-002
----TBD TFU 313600063
----Associated Part :
70 NVM FAULT DATA
NOT RETRIEVABLE
ECU 1459M55P15 1519M83P02 1459M55P16 1519M83P03
----1459M55P17 1519M83P04 1820M27P01
TFU 732900031
----Associated Part :
21 GND failures report in last leg report,
ZC 775A0000-05 775A0000-06
----775A0000-07
----Associated Part :
21 No A/C ident in the previous leg report
NO MAINT. ACTION ZC 775A0000-05
----775A0000-07
----Associated Part :
21 NO ACCEPTABLE FAILURE IN
26
NO MAINT. ACTION if no log book complaint.
ZC 775A0000-05
----775A0000-06 TFU 216334047
----Associated Part :
21 No access to ZONE CONT menu when PACK C/B is pulled.
Make sure all C/B are pushed ZC 775A0000-05
----775A0000-06
----Associated Part :
21 No software number in P/N of Zone Cont.
NO MAINT. ACTION ZC 775A0000-05
----775A0000-07
----Associated Part :
21 OUTFLOW VALVE ELEK i (04)
If it occurs during system calibration test in MAN MODE, repeat test in AUTO MODE.
CPC 902215702-7
----902215702-8 TFU 213134006 / TSM ATA 21
----Associated Part :
21 P.L.R. : Leg counting deviation at leg 99
ZC 775A0000-05
----775A0000-07
----Associated Part :
21 Test results in coded form
ZC 775A0000-07
----775A0000-07 TFU 216134002 / TFU 216334004 / TSM ATA 21
----Associated Part :
21 VENT AVNCS SYS FAULT
during Ditching test procedure.
Reset AEVC C/B at the end of the Ditching test procedure.
AEVC All P/N
----NONE TFU 212600010 / FCOM
chapter 3.04.91
rev.20/AMM 212600 PB 527
----Associated Part :
216351 FAILURE NOT CLEARLY IDENTIFIED
NO MAINT. ACTION if no log book complaint.
ZC 775A0000-06 775A0000-05
----775A0000-06 TFU 216334047
----Associated Part :
22 22-83-34 FMGC (1CA1) / GPWC (1WZ)
NO MAINT. ACTION if appears after a GPWC test via the CFDS
GPWC 965-0676-020
----S/W Mod 1 TFU 344800003
----Associated Part :
22 Disregard the indication RTOK in the AFS Bite report
NO MAINT. ACTION FAC All P/N
----N/A
----Associated Part :
22 ELAC 1 & ELAC 2 messages displayed in the ground scan if no hydraulic pressure
NO MAINT. ACTION if no Hydraulic pressure on the A/C
FAC All P/N
----N/A TSM ATA 22
----Associated Part :
22 FMGC MAG TRK on MCDU NO MAINT. ACTION if appears after a GPWC ground scan. via the CFDS
GPWC 965-0676-020
----S/W Mod 1 TFU 344800003
----Associated Part :
22 The message THR LK no
more displayed on the PFD at the step 7 of the land test.
If DMC Mark II is installed, Ignore the land test step7 question, and answer YES even if nothing is displayed on the PFD.
DMC ALL P/N
----FAC --->
B397BAM0508 B397BAM0509
TFU 229700004
----Associated Part :
22 Wrong (Alternate) City Pair on the PFR.
If Lateral revision at destination is used for inserting/changing Altn destination.
Inserting/Modifying via init A page in pre-flight or via secondary flight plan will avoid this anomaly.
FMGC B398AAM0408 B398BAM0205
TFU 227000014
----Associated Part :
228334 FMGCi Class 2 Fault message without
associated Maintenance status. Apply TSM procedure
FCDC 115370-0105
----115370-1016 115370-0106
MPD Task : 313000-03-1
----Associated Part :
228334 RMP1(2,3) : NO DATA FROM FMGCi
Class 2 Fault message to be considered as a Class 3 message.
RMP 899-0850-002 899-0850-003 899-0850-004
----NONE
----Associated Part :
23 Faults missing in Audio Previous and last leg reports
Refer to messages in the PFR. AMU 2790(*)A03 2790(*)A03 2790(*)A03
* = C or D or E (3 or 4 or 5 boards)
----VSB 2790-23-006 VSB 2790-23-007 P/N: 2790(*)B06
TFU 235100009/TFU 235100013
----Associated Part :
23 Wrong P/N of AMU and ACP in the audio LRU identification
NO MAINT. ACTION AMU 2790(*)A03
2790(*)A03 2790(*)A03
* = C or D or E (3 or 4 or 5 boards)
----VSB 2790-23-006 VSB 2790-23-007 P/N: 2790(*)B06
TFU 235100009/TFU 235100013
----Associated Part : 230000 BITE Test of the PES Maintenance advise: To determine the
status of the PES video system, it is recommended to check, after aircraft is energized, the ground report of CIDS1/CIDS2 menu through the MCDU
CIDS DIR Z064H000030F
----Z064H000031A Z064H000031B
SB 23-1278
----Associated Part :
230000 No date indication in
the ground report of the CIDS or toilet system further to software loading.
It may happen that further to a software loading a failure message is displayed without any date indication in the ground report of the CIDS1 or CIDS2 or the CIDS1 or 2 Toilet system.
CIDS DIR Z064H000030F Z064H000031A Z064H000031B
----TBD (end 2005)
----Associated Part :
230000 No date indication in
the Last Leg Report of the CIDS Toilet system.
It may happen that a failure message is displayed without any date indication in the Last Leg Report of the CIDS1 or 2 Toilet system.
CIDS DIR Z064H000030F Z064H000031A Z064H000031B
----TBD (end 2005)
----Associated Part :
230000 The Lavatory Smoke
detection test can not be performed if the CIDS is in a
"cross-configuration" (AMM Task 26-17-00-710-001) as it follows:
Switchover of CIDS (CIDS1 passive, CIDS2 active, CIDS-SDF1
Maintenance advise: Perform a CIDS reset as described in Appendix 1 to recover the usual CIDS configuration (CIDS part and CIDS-SDF part from the same unit active at the same time).
CIDS DIR Z064H000030F Z014H000030C
Associated Part :
230000 Video BITE Test
The test of the Video System through MCDU provides unreliable result. Only simultaneous CIDS and PES power-up initiate the PES BITE to be correctly reported (normal mode)
Maintenance advise: To determine the status of the PES video system, it is recommended to check, after aircraft is energized, the ground report of CIDS1/CIDS2 menu through the MCDU
CIDS DIR Z064H000031A Z064H000031B
----TBD (end 2005)
----Associated Part :
2311 IMPOSSIBILITY TO USE VHF3 IN VOICE MODE
NO MAINT.ACTION. IF AMU AMDT A , APPLY VSB 23-007.
AMU ALL P/N WITH AMDT A
----VSB 23-007 P/N: 2790(*)B06
TFU 235100013
----Associated Part :
237334 BITE Test of CIDS
The maintenance message "DIR2 (102RH) -SDF" is spuriously triggered during a system test of the smoke system through the MCDU with the following
configuration: both CIDS directors
Maintenance advise: Subject configuration may be reproduced for trouble shooting purpose. Therefore, the validity of the failure message must be checked through a CIDS-SDF ground scanning.
CIDS DIR Z014H000030C Z064H000030F
Associated Part :
24 After a GPCU test, NO RESPONSE.
Reinitialize GPCU test GPCU 740121A
740121B
----Vdr SIL 229 SB 740121-24-7
TFU 244100006
----Associated Part :
24 BCL messages in the PFR, without anything in the BCL Bite.
(Bite memory erased after a reset)
Perform the Maint. actions
corresponding to the PFR messages
BCL All P/N
----35-0L5-1005-08 (S/B 24-1075)
TFU 243800007 / TFU 243800009
----Associated Part :
24 GCUi TEST NOT DONE or IDGi RUNNING
NO MAINT. ACTION if appears after a GPCU test. Reinitialize the GPCU test.
GPCU 740121A 740121B
----Vdr SIL 229 TFU 244100005
----Associated Part :
242334 GCU EMERG IN AVIONIC STATUS
If test result is OK, no maintenance action Could be corrected in a next CFDIU std
GCU 520915 amdt 4
----TBD TFU 313234035
----Associated Part :
261700 Operational check
of the Lavatory Smoke detection function as per AMM task 26-17-00-710-001 not possible in case DIR1 and SDF2 or DIR2 and DIR-SDF1 are active simultaneously (CIDS cross configuration).
CIDS DIR Z064H000030D Z064H000030E Z064H000030F
----TBD
----Associated Part :
27 Interruption of SFCC-CFDS communication when selecting the print option in the SFCC "SYSTEM DATA" pages.
reenter the SFCC MENU SFCC 49117-06/07
----N/A TFU 275151047
----Associated Part :
2700 During Ground Scanning, MAINT STATUS F/CTL may be triggered without associated fault message if the failure affects the servovalve or the POS XDCR or the SOLENOID valve signal.
TSM procedure should be followed using the MAINT STATUS as entry point.
FCDC 115370-0106 115370-105 115370-1016
----115370-1118 TFU 27 95 00 033
----Associated Part :
2700 During Ground Scanning, ECAM WARNING F/CTL AILERON SERVO FAULT may be triggered without associated fault message if the failure affects the servovalve or the POS XDCR or the SOLENOID valve signal.
TSM procedure should be followed using the ECAM WARNING as entry point.
FCDC 115370-0106 115370-105 115370-1016
----115370-1118 TFU 279500033
----Associated Part :
279300 Ultimely flash of
AIL SERVO FAULT in case of ELAC 1 (or 2) fault during GROUND SCANNING
FCDC 115370-0105
----115370-1016 115370-0106
----Associated Part :
279334 AFS:ELACi NO MAINT. ACTION if associated to B
SYS LO PRESS (respectively Y SYS LO PRESS).
FAC All P/N
----N/A
----Associated Part :
279334 ELACi COM (MON) OR BUS FROM FMGCi
Class 2 Fault message without
associated Maintenance status. Apply TSM procedure
FCDC 115370-0105
----115370-1016 115370-0106
MPD Task : 313000-03-1
----Associated Part :
279334 SEC3 OR BUS2 FROM ADR2 (ADR3 / IR2 / IR3)
Class 2 Fault message without
associated Maintenance status. Apply TSM procedure
FCDC 115370-0105
----115370-1016 115370-0106
MPD Task : 313000-03-1
----Associated Part :
279434 SEC2 OR INPUT OF L(R) THROTTLE CTL UNIT 8KSi
Class 2 Fault message without
associated Maintenance status. Apply TSM procedure
FCDC 115370-0105
----115370-1016 115370-0106
MPD Task : 313000-03-1
----Associated Part :
279434 SEC3 OR WIRING FROM SFCC i
Class 2 Fault message without
associated Maintenance status. Apply TSM procedure
FCDC 115370-0105
----115370-1016 115370-0106
MPD Task : 313000-03-1
----Associated Part :
279534 OP FCDC FAIL DISCR Class 2 Fault message without
associated Maintenance status. Apply TSM procedure
FCDC 115370-0105
----115370-1016 115370-0106
MPD Task : 313000-03-1
----Associated Part :
301151 L(R) WAI FILTER OR
VALVE9(10) Associated with E/Ws 30.00 WING ANTI ICE SYS FAULT
Do not forget to use the Zone Cont.
Class 3 report upon wing anti ice Ecam Warnings.
ZC 775A0000-05
----775A0000-07 TFU 216334046 / 216334046/TSM ATA 30
----Associated Part :
31 BACK UP MODE DEVIATIONS DO NOT CHOOSE
ECAM1/2,FDIU,SFCC1 WHEN DOING STEP 6 OF AMM TASK 31 32 00 710 002
CFDIU B401ACM0506
----TBD TFU313234035
----Associated Part :
31 Bad counting of the
flight legs in the Class 3 Fault memory.
NO MAINT. ACTION DMU 903116243BOBOG0
903116243BODOJ0 903116243B0B0G1 903116243B0D0J1
----903116243B3B3G4 9031116243B3B2G3 903116243B3D2J3
TFU 313600017
----and subsequent std
Associated Part :
31 Bad PRINT OUT FORMAT. NO MAINT. ACTION Printer 805515-4501
----805515-4501 VSB M3367
TFU 313522001
----Associated Part :
31 DIFFICULTIES FOR FILTER LOADING
SOME DIFFICULTIES MAY BE ENCOUNTERED WHEN USING ANY OUT OF THE PDL IN SERVICE BUT THE SFIM.
CFDIU B401ACM0505 B401ACM0506
----N/A TFU313234038
----Associated Part :
31 Duplication of Fault message in PFR.
CFDIU B401ACM0404
----B401ACM0606 TFU 313234029
----Associated Part :
31 GROUND or GND -messages in phase 8/9
Generated by type 2 system. No maintenance Action.
CFDIU B401ACM0506 B401ACM0507
----C12860AA02
----Associated Part :
31 Incoherent PFR Fault messages sent by the EIU.
Check EIU Previous Leg reports. EIU 3957900611
----3957900612 TFU 313234029
----Associated Part :
31 Incoherent PFR recording time in the PFR header.
Due to Flight phases transitions anomalies.
CFDIU B401ACM0404
----B401ACM0506 TFU 313234029
----Associated Part :
31 Incomplete PFR Fault messages.
Due to power transients. CFDIU B401ACM0404
----B401ACM0506 TFU 313234029
----Associated Part :
31 Message NO RESPONSE,
PRESS RETURN after the start of DMC test.
To get the results, reenter DMC menu and access the "Test Result" item
DMC All P/N
----None
----Associated Part :
31 Mixed GMT in PFR Due to power transients. CFDIU B401ACM0404
----B401ACM0506 TFU 313234029
----Associated Part : 31 NO "SYST" DATA (INTM) If no logbook complaint, NO MAINT
ACTION. This message is generated by the CFDIU (Source : CFDS).
CFDIU B401ACM0506
----TBD
----Associated Part :
31 NO DMC1 DATA recorded in CFDIU ground scanning
NO MAINT. ACTION CFDIU B401ACM0404
----B401ACM0506 TFU 313234030
----Associated Part :
31 NO FWC DATA recorded in CFDIU last leg report.
NO MAINT. ACTION if no log book complaint.
CFDIU B401ACM0404
----B401ACM0506 TFU 313234030
----Associated Part :
31 P/N read through LRU
IDENT. Menu not in accordance with the actual P/N.
NO MAINT. ACTION FDIU 9026-16079-01B2
----9026-16079-02B3 TFU 313300011
----Associated Part :
31 PFR with NO FAULT / NO WARNING.
Due to Flight phases transitions anomalies.
CFDIU B401ACM0404
----B401ACM0506 TFU 313234029
----Associated Part :
31 System source without Fault message.
Under investigation. No Maint. Action. CFDIU B401ACM0404
----B401ACM0506 TFU 313234029
----Associated Part :
31 Untimely print out of real time failure and warning.
In flight pull, PRINTER C/B. CFDIU B401ACM0404
----Amdt A TFU 313234026
----Associated Part :
31 12 34 FLPi NO CFDIU DATA The ATA chapter of this message should be 313234 instead of 311234.
SFCC 49-117-09 49-117-10 49-170-11
----TBD
----Associated Part :
313234 ADFi : NO DATA FROM CFDIU
Class 2 Fault message to be considered as a Class 3 message.
ADF 204-1168-7513 622-5222-020
----NONE
----Associated Part :
313234 AUDIO NO DATA FROM CFDIU
Class 2 Fault message to be considered as a Class 3 message.
AMU 2790CA03
----NONE
----Associated Part :
313234 CFDS prompt not
available on MCDU at CFDIU power up.
Wait 1 minute after CFDIU power up to get the CFDS prompt on the MCDU.
CFDIU B401ACM0507 C12860AA02
----N/A
----Associated Part :
313234 DME1(2,3) : NO DATA FROM CFDIU
Class 2 Fault message to be considered as a Class 3 message.
DME 622-4540-023 9599-614-03105
----NONE
----Associated Part :
313234 HFi : NO DATA FROM CFDIU
Class 2 Fault message to be considered as a Class 3 message.
HF 622-5272-020
----NONE
----Associated Part : 313234 NO DATA FROM CFDIU Class 2 Fault message to be considered
as a Class 3 message.
ILS 204-1230-3518 622-5222-020
----204-1230-3521 622-5222-041
----Associated Part :
313234 RMP1(2,3) : NO DATA FROM CFDIU
Class 2 Fault message to be considered as a Class 3 message.
RMP 899-0850-002 899-0850-003 899-0850-004
----NONE
----Associated Part :
313234 VHF1(2,3) : NO DATA FROM CFDIU
Class 2 Fault message to be considered as a Class 3 message.
VHF 204-1237-4417
----NONE
----Associated Part :
313234 VOR 1(2,3) :NO DATA FROM CFDIU
Class 2 Fault message to be considered as a Class 3 message.
VOR 204-1231-3610 622-5220-020 204-1231-3623 204-1231-3613 204-1231-3622
----NONE
----Associated Part :
313234 WRX i : NO DATA FROM CFDIU
Class 2 Fault message to be considered as a Class 3 message.
WRX 204-1217-0418 204-1217-0421
----VSB RTA-4A-34-173
----Associated Part : 313316 ACCELEROMETER Class 2 Fault message without
associated Maintenance Status. Apply TSM procedure.
FDIU ED43A1D2 ED43A1D3 90261607902B3
----ED43A1D5 MPD 313000-04-01
----Associated Part :
32 Faults on the LGCIU ARINC OUTPUT BUS are reported "LGCIU i 05GAi". With the LGCIU std 4D, the following message will be triggered: " LGCIU/WRG: BUS i FEEDBACK".
LGCIU 664700500A4B 664700500A4C
----664700500A4D
----Associated Part :
32 If a power interrupt of 10 ms or greater
occurs after the transition from flight phase 1 to 2 with shock absorbers compressed any subsequent faults detected by the LGCIU will be logged in ground memory and not flight memory.
LGCIU 664700500A4B 664700500A4C
----664700500A4D
----Associated Part :
32 For all fault messages " PROX SNSR
xxGA TGT POS" related to the nose L/G doors sensor (mechanical failure) the "S"
of POS is missing.
LGCIU 664700500A4B 664700500A4C
----664700500A4D
----Associated Part :
32 BSCU BITE report
Wrong DATE, TIME and FLIGHT PHASE due to lack of
communciation with CFDIU at the time fault msg is recorded. CLASS 3
communciation with CFDIU at the time fault msg is recorded. CLASS 3