W DOC AIRBUS | TSM A320F

Loss of the TCAS Input Bus by the DMC 2


TASK 31-63-00-810-912-A
Loss of the TCAS Input 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 31-63-00-865-144-A
A. Make sure that this(these) circuit breaker(s) is(are) closed:
PANELDESIGNATIONFINLOCATION
** ON A/C ALL
121VUCOM NAV/TCAS4SGK10
Subtask 31-63-00-740-234-A ** ON A/C NOT FOR ALL
B. Test
Do the EIS input test AMM 31-60-00-740-002.
Subtask 31-63-00-740-234-C ** 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 31-63-00-810-160-A ** ON A/C NOT FOR ALL
A. If the test gives the maintenance message DMC 2 : NO TCAS DATA:
   (1) If the fault continues:
  • do a check and repair the wiring from the DMC 2 (1WT2) pins AA/5E, 5F to the first terminal block ASM 316201.
Subtask 31-63-00-810-160-C ** ON A/C NOT FOR ALL
A. If the test gives the maintenance message TCAS(1SG)/DMC2(1WT2):
   (1) If the fault continues:
  • do a check and repair the wiring from the DMC 2 (1WT2) pins AA/10E, 10F to the first terminal block ASM 316201.
Subtask 31-63-00-740-235-A
B. Do the test given in Para. 3.B.
[Rev.8 from Aug 2018] 2026.04.04 04:30:45 UTC