W DOC AIRBUS | TSM A320F

Loss of the ECU 1 Channel A Output Bus by the DMC 2


TASK 31-63-00-810-878-A
Loss of the ECU 1 Channel A Output Bus by the DMC 2


1. Possible Causes
  • DMC-2 [1WT2]
  • wiring
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
AMM 31-60-00-740-002
Perform Electronic Instrument System (EIS) Input Test
AMM 31-60-00-740-007
GROUND SCANNING Test of the DMC
ASM 316201
AMM 31-63-34-000-001
Removal of the DMC
AMM 31-63-34-400-001
Installation of the DMC
3. Fault Confirmation
Subtask 31-63-00-865-110-A
A. Make sure that this(these) circuit breaker(s) is(are) closed:
PANELDESIGNATIONFINLOCATION
** ON A/C ALL
49VUENGINE/1/FADEC A/AND EIU 12KS1A04
Subtask 31-63-00-740-166-A ** ON A/C NOT FOR ALL
B. Test
Do the EIS input test AMM 31-60-00-740-002.
Subtask 31-63-00-740-166-B ** ON A/C NOT FOR ALL
B. Test
Do the Ground Scanning Test of the DMC AMM 31-60-00-740-007.
4. Fault Isolation
Subtask 31-63-00-810-126-A ** ON A/C NOT FOR ALL
A. If the test gives the maintenance message DMC 2 : NO ECU 1A DATA:
   (1) If the fault continues:
  • do a check and repair the wiring from the DMC 2 (1WT2) pins AA/1A, 1B to the first terminal block ASM 316201.
Subtask 31-63-00-810-126-B ** ON A/C NOT FOR ALL
A. If the test gives the maintenance message ECU(E1-4000KS)BUS ECU1A/DMC2(1WT2):
   (1) If the fault continues:
  • do a check and repair the wiring from the DMC 2 (1WT2) pins AE/1J, 1K to the first terminal block ASM 316201.
Subtask 31-63-00-740-167-A
B. Do the test given in Para. 3.B.
[Rev.8 from Aug 2018] 2026.04.04 04:30:43 UTC