B. If the colors displayed on the lower ECAM display unit are not correct:
- replace the DU-ECAM, LOWER (4WT2) (Ref. AMM TASK 31-63-22-000-001) and (Ref. AMM TASK 31-63-22-400-001).
C. If the colors displayed on the CAPT ND are not correct:
- replace the ND-CAPT (3WT1) (Ref. AMM TASK 31-63-22-000-001) and (Ref. AMM TASK 31-63-22-400-001).
D. If the colors displayed on the F/O ND are not correct:
- replace the ND-F/O (3WT2) (Ref. AMM TASK 31-63-22-000-001) and (Ref. AMM TASK 31-63-22-400-001).
E. If the colors displayed on the CAPT PFD are not correct:
- replace the PFD-CAPT (2WT1) (Ref. AMM TASK 31-63-22-000-001) and (Ref. AMM TASK 31-63-22-400-001).
F. If the colors displayed on the F/O PFD are not correct:
- replace the PFD-F/O (2WT2) (Ref. AMM TASK 31-63-22-000-001) and (Ref. AMM TASK 31-63-22-400-001).
5. Close-up
________
A. Put the aircraft back to its initial configuration.
(1) Do the EIS stop procedure
(Ref. AMM TASK 31-60-00-860-002).
(2) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 001-049, 051-099, 101-149, 151-199, ∞∞31-63-00∞∞∞∞∞∞∞∞∞∞Page C203
201-299, 301-399, Aug 01/05 CES
R **ON A/C 401-499,
TASK 31-63-00-810-972
Failure of the FWC1 Detected by the DMC
1. Possible Causes
_______________
- FWC-1 (1WW1)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
31-53-00-810-810 Loss of the ARINC 429 Data between the FWC 1 and the DMC 1 31-53-00-810-811 Loss of the ARINC 429 Data between the FWC 1 and the DMC 2 31-53-00-810-813 Loss of the ARINC 429 Data between the FWC 1 and the DMC 3 AMM 31-53-34-000-001 Removal of the Flight Warning Computer (FWC) (1WW1,1WW2) AMM 31-53-34-400-001 Installation of the Flight Warning Computer (FWC) (1WW1,1WW2) AMM 31-60-00-740-007 GROUND SCANNING Test of the DMC
3. Fault Confirmation
__________________
A. Test Do the Ground Scanning Test of the DMC (Ref. AMM TASK 31-60-00-740-007).
4. Fault Isolation
_______________
A. If the test gives the maintenance message: FWC1(1WW1)
- Do the fault isolation (Para. 4. A.) of the following procedures (Ref. TASK 31-53-00-810-810), (Ref. TASK 31-53-00-810-811) and (Ref. TASK 31-53-00-810-813).
(1) if the fault continues:
- replace the FWC-1 (1WW1), (Ref. AMM TASK 31-53-34-000-001) and (Ref. AMM TASK 31-53-34-400-001).
5. Close-up
________
A. Do the test given in Para. 3.B.
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 401-499, ∞∞31-63-00∞∞∞∞∞∞∞∞∞∞Page C204
Aug 01/05 CES
Failure of the FWC2 Detected by the DMC
1. Possible Causes
_______________
- FWC-2 (1WW2)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
31-63-00-810-962 Loss of the ARINC 429 Link between the FWC2 and the
DMC2 31-63-00-810-963 Loss of the ARINC 429 FWC2 Input of the DMC1 31-63-00-810-966 Loss of the ARINC 429 Link from the FWC2 to the DMC3 AMM 31-53-34-000-001 Removal of the Flight Warning Computer (FWC)
(1WW1,1WW2) AMM 31-53-34-400-001 Installation of the Flight Warning Computer (FWC) (1WW1,1WW2) AMM 31-60-00-740-007 GROUND SCANNING Test of the DMC
3. Fault Confirmation
__________________
A. Test Do the Ground Scanning Test of the DMC (Ref. AMM TASK 31-60-00-740-007).
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊(cè) 指示和記錄系統(tǒng) 2(110)
