W DOC AIRBUS | TSM A320F

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


TASK 31-63-00-810-873-A
Loss of the ECU 2 Channel B Output Bus by the DMC 1


1. Possible Causes
  • DMC-1 [1WT1]
  • 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 31-63-00-865-105-A
A. Make sure that this(these) circuit breaker(s) is(are) closed:
PANELDESIGNATIONFINLOCATION
** ON A/C ALL
121VUENGINE/ENG2/FADEC B/AND EIU 24KS2Q40
Subtask 31-63-00-740-156-A ** ON A/C NOT FOR ALL
B. Test
Do the EIS input test AMM 31-60-00-740-002.
Subtask 31-63-00-740-156-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 31-63-00-810-121-A ** ON A/C NOT FOR ALL
A. If the test gives the maintenance message DMC 1 : NO ECU 2B DATA:
   (1) If the fault continues:
  • do a check and repair the wiring from the DMC 1 (1WT1) pins AA/15J, 15K to the first terminal block ASM 316201.
Subtask 31-63-00-810-121-B ** ON A/C NOT FOR ALL
A. If the test gives the maintenance message ECU(E2-4000KS)BUS ECU2B/DMC1(1WT1):
   (1) If the fault continues:
  • do a check and repair the wiring from the DMC 1 (1WT1) pins AE/15A, 15B to the first terminal block ASM 316201.
Subtask 31-63-00-740-157-A
B. Do the test given in Para. 3.B.
[Rev.8 from Aug 2018] 2026.04.04 04:30:43 UTC