W DOC AIRBUS | TSM A320F

Failure of the CAPT ND Detected by the DMC1


TASK 31-63-81-810-842-A
Failure of the CAPT ND Detected by the DMC1


1. Possible Causes
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
AMM 31-60-00-740-002
Perform Electronic Instrument System (EIS) Input Test
AMM 31-60-00-740-004
EIS System Test
ASM 316104
AMM 31-63-22-000-001
Removal of the Display Unit
AMM 31-63-22-400-001
Installation of the Display Unit
AMM 31-63-34-000-001
Removal of the DMC
AMM 31-63-34-400-001
Installation of the DMC
3. Fault Confirmation
Subtask 31-63-81-740-132-A ** ON A/C NOT FOR ALL
A. Test
Do the EIS input test AMM 31-60-00-740-002.
Subtask 31-63-81-740-132-B ** ON A/C NOT FOR ALL
A. Test
Do the EIS system test AMM 31-60-00-740-004.
4. Fault Isolation
Subtask 31-63-81-810-099-A
A. If the test gives the maintenance message DMC1-DU ND1 LINK:
  • on the panel 301VU, push the CAPT PFD/ND XFR pushbutton switch (9WT1)
  • do the test given in Para. 3.
   (1) If this test gives the maintenance message DMC1-DU ND1 LINK:
     (a) If the fault continues:
  • do a check of the wiring from the DMC1 (1WT1) pins AB/10B, 10C to the first terminal block ASM 316104.
       1 If there is no continuity:
  • repair the wiring.
       2 If there is continuity:
  • do a check and repair the wiring from the DMC1 (1WT1) pins AB/10D, 10E to the first terminal block ASM 316104.
   (2) If this test gives no maintenance message:
     (a) If the fault continues:
  • do a check of the wiring from the CAPT ND (3WT1) pins AA/35, 36 to the first terminal block ASM 316104.
       1 If there is no continuity:
  • repair the wiring.
       2 If there is continuity:
  • do a check and repair the wiring from the CAPT-ND (3WT1) pins AA/38, 39 to the first terminal block ASM 316104.
Subtask 31-63-81-740-133-A
B. Do the test given in Para. 3.
[Rev.8 from Aug 2018] 2026.04.04 04:30:57 UTC