61/04).
B. Do the test given in Para. 3.
Failure of the DMC1 Pin Programming
1. Possible Causes
_______________
- DMC-1 (1WT1)
- ground signals at DMC1 (1WT1) connector AB
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
AMM 31-60-00-740-002 EIS Input Test
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)
R AWM 31-61-28
3. Fault Confirmation
__________________
A. Test
Do the EIS input test (Ref. AMM TASK 31-60-00-740-002).
4. Fault Isolation
_______________
A. If the test gives the maintenance message:
DMC1: PROGRAM PIN
or
DMC1: POSITION PIN
R - do a check for ground signals at DMC1 (1WT1) connector AB (Ref. AWM 31-R 61-28).
(1) If the wiring is incorrect:
- repair the wiring.
(2) If the wiring is correct:
- replace the DMC-1 (1WT1) (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.
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞31-63-81∞∞∞∞∞∞∞∞∞∞Page 230
May 01/01 CES Loss of CAPT PFD or CAPT ND or Upper ECAM DU Image
1. Possible Causes
_______________
- PFD-CAPT (2WT1)
- DMC-1 (1WT1)
- ND-CAPT (3WT1)
- DU-ECAM, UPPER (4WT1)
- wiring
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 31-60-00-740-002 EIS Input Test
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 31-61/04
3. Fault Confirmation
__________________
A. Test
Do the EIS input test (Ref. AMM TASK 31-60-00-740-002).
4. Fault Isolation
_______________
A. If the test gives the maintenance message DMC1 : RECONF WIRING and there is no CAPT PFD image:
- replace the PFD-CAPT (2WT1) (Ref. AMM TASK 31-63-22-000-001) and (Ref. AMM TASK 31-63-22-400-001).
(1) If the fault continues:
- do a check of the wiring from CAPT PFD (2WT1) pins AA/35, 36 to DMC1 (1WT1) pins AB/9B, 9C (Ref. ASM 31-61/04).
(a) If there is no continuity:
- repair the wiring.
(b) If there is continuity:
- do a check and repair the wiring from CAPT PFD (2WT1) pins AA/38, 39 to DMC1 (1WT1) pins AB/9D, 9E (Ref. ASM 31-61/04).
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞31-63-81∞∞∞∞∞∞∞∞∞∞Page 231
Feb 01/98 CES 1 If the fault continues:
_
- replace the DMC-1 (1WT1) (Ref. AMM TASK 31-63-34-000-001) and (Ref. AMM TASK 31-63-34-400-001).
B. If the test gives the maintenance message DMC1 : RECONF WIRING and there is no CAPT ND image:
- replace the ND-CAPT (3WT1) (Ref. AMM TASK 31-63-22-000-001) and (Ref. AMM TASK 31-63-22-400-001).
(1) If the fault continues:
- do a check of the wiring from CAPT ND (3WT1) pins AA/35, 36 to DMC1 (1WT1) pins AB/10B, 10C (Ref. ASM 31-61/04).
(a) If there is no continuity:
- repair the wiring.
(b) If there is continuity:
- do a check and repair the wiring from CAPT ND (3WT1) pins AA/38, 39 to DMC1 (1WT1) pins AB/10D, 10E (Ref. ASM 31-61/04).
1 If the fault continues:
_
- replace the DMC-1 (1WT1) (Ref. AMM TASK 31-63-34-000-001) and (Ref. AMM TASK 31-63-34-400-001).
C. If the test gives the maintenance message DMC1 : RECONF WIRING and there is no upper ECAM DU image:
- replace the DU-ECAM, UPPER (4WT1) (Ref. AMM TASK 31-63-22-000-001) and (Ref. AMM TASK 31-63-22-400-001).
中國航空網(wǎng) m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320 Trouble Shooting Manual 排故手冊(cè) 指示和記錄系統(tǒng) 3(6)
