W DOC AIRBUS | TSM A320F

Loss of the ARINC 429 Link between the FWC2 and the DMC2


TASK 31-63-00-810-962-A
Loss of the ARINC 429 Link between the FWC2 and the DMC2


1. Possible Causes
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
ASM 315205
AMM 31-53-34-000-001
Removal of the Flight Warning Computer (FWC)
AMM 31-53-34-400-001
Installation of the Flight Warning Computer (FWC)
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
AMM 31-63-34-000-001
Removal of the DMC
AMM 31-63-34-400-001
Installation of the DMC
3. Fault Confirmation
Subtask 31-63-00-865-191-A
A. Make sure that this(these) circuit breaker(s) is(are) closed:
PANELDESIGNATIONFINLOCATION
** ON A/C ALL
121VUEIS/FWC2/SPLY2WWQ07
Subtask 31-63-00-740-334-A ** ON A/C NOT FOR ALL
B. Test
Do the EIS input test (system 2) AMM 31-60-00-740-002.
Subtask 31-63-00-740-334-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 31-63-00-810-210-A ** ON A/C NOT FOR ALL
A. If the test gives the maintenance message:
DMC2: NO FWC2 DATA
   (1) If the fault continues:
     (a) If the fault continues:
  • do a check and repair the wiring from DMC2 (1WT2) pins AA/10J, 10K to the FWC2 (1WW2) ASM 315205.
Subtask 31-63-00-810-210-B ** ON A/C NOT FOR ALL
A. If the test gives the maintenance message:
FWC2(1WW2) BUSX DATA/DMC2(1WT2)
   (1) If the fault continues:
     (a) If the fault continues:
  • do a check and repair the wiring from DMC2 (1WT2) pins AD/8C, 8D to the FWC2 (1WW2) ASM 315205.
Subtask 31-63-00-740-335-A
B. Do the test given in Para. 3.B.
[Rev.8 from Aug 2018] 2026.04.04 04:40:06 UTC