3. Fault Confirmation
__________________
A. Test Do the operational test of the DMC/DU Data Bus (Ref. AMM TASK 31-60-00-720-002)
4. Fault Isolation
_______________
A. If the test gives:
(1) the maintenance message DU SD (4WT2)/WRG: DMC2 (1WT2)
- check the wiring between the DMC2 and the Lower ECAM DU (4WT2) (Ref. ASM 31-61/00)
(a) if the wiring is correct:
- replace the DU-ECAM, LOWER (4WT2) (Ref. AMM TASK 31-63-22-000-001)and (Ref. AMM TASK 31-63-22-400-001)
(b) If the fault continues:
- replace the DMC-2 (1WT2) (Ref. AMM TASK 31-63-34-000-001) and (Ref. AMM TASK 31-63-34-400-001)
B. Do the test given in Para. 3.
「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, ∞∞31-63-81∞∞∞∞∞∞∞∞∞∞Page C210
Aug 01/05 CES Failure of the A629 BUS from the CAPT PFD DU to the DMC3
1. Possible Causes
_______________
- PFD-CAPT (2WT1)
- DMC-3 (1WT3)
- wiring
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
31-63-81-810-960 Failure of the A629 BUS from the CAPT PFD DU to the
DMC1 AMM 31-60-00-720-002 Operational Test of the DMC/DU data bus AMM 31-63-22-000-001 Removal of the Display Unit
(2WT1,2WT2,3WT1,3WT2,4WT1,4WT2) AMM 31-63-22-400-001 Installation of the Display Unit
(2WT1,2WT2,3WT1,3WT2,4WT1,4WT2) AMM 31-63-34-000-001 Removal of the DMC (1WT1,1WT2,1WT3) AMM 31-63-34-400-001 Installation of the DMC (1WT1,1WT2,1WT3) ASM 31-61/00
3. Fault Confirmation
__________________
A. Test
(1) Make sure that the DMC1 is correctly installed (Ref. AMM TASK 31-63-34-400-001)
(2) Do the operational test of the DMC/DU Data Bus (Ref. AMM TASK 31-60-00-720-002)
4. Fault Isolation
_______________
A. If the test gives:
(1) the maintenance message DU PFD CAPT(2WT1)/WRG: DMC1(1WT1)
- do the relative fault isolation procedure (Ref. TASK 31-63-81-810-960)
(2) the maintenance message DU PFD CAPT(2WT1)/WRG: DMC3(1WT3)
- check the wiring between the DMC3 and the CAPT PFD DU (2WT1) (Ref. ASM 31-61/00)
(a) if the wiring is correct:
- replace the PFD-CAPT (2WT1) (Ref. AMM TASK 31-63-22-000-001) and (Ref. AMM TASK 31-63-22-400-001)
(b) If the fault continues:
- replace the DMC-3 (1WT3) (Ref. AMM TASK 31-63-34-000-001) and (Ref. AMM TASK 31-63-34-400-001)
B. Do the test given in Para. 3.
Failure of the A629 BUS from the CAPT ND DU to the DMC3
1. Possible Causes
_______________
- ND-CAPT (3WT1)
- DMC-3 (1WT3)
- wiring
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
31-63-81-810-961 Failure of the A629 BUS from the ND CAPT DU to the
DMC1 AMM 31-60-00-720-002 Operational Test of the DMC/DU data bus AMM 31-63-22-000-001 Removal of the Display Unit
(2WT1,2WT2,3WT1,3WT2,4WT1,4WT2) AMM 31-63-22-400-001 Installation of the Display Unit
(2WT1,2WT2,3WT1,3WT2,4WT1,4WT2) AMM 31-63-34-000-001 Removal of the DMC (1WT1,1WT2,1WT3) AMM 31-63-34-400-001 Installation of the DMC (1WT1,1WT2,1WT3) ASM 31-61/00
3. Fault Confirmation
__________________
A. Test
(1) Make sure that the DMC1 is correctly installed (Ref. AMM TASK 31-63-34-400-001)
(2) Do the operational test of the DMC/DU Data Bus (Ref. AMM TASK 31-60-00-720-002)
4. Fault Isolation
_______________
A. If the test gives:
(1) the maintenance message DU ND CAPT(3WT1)/WRG: DMC1(1WT1)
- do the relative fault isolation procedure (Ref. TASK 31-63-81-810-961)
(2) the maintenance message DU ND CAPT(3WT1)/WRG: DMC3(1WT3)
- check the wiring between the DMC3 and the CAPT ND DU (3WT1) (Ref. ASM 31-61/00)
(a) if the wiring is correct:
- replace the ND-CAPT (3WT1) (Ref. AMM TASK 31-63-22-000-001) and (Ref. AMM TASK 31-63-22-400-001)
(b) If the fault continues: 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：A320 Trouble Shooting Manual 排故手册 指示和记录系统 3(87)
