Loss of Data Communication to Lav
TASK 38-31-00-810-836-A
Loss of Data Communication to Lav
1. Possible Causes
A. Referenced Information
3. Fault Confirmation
Subtask 38-31-00-710-117-A ** ON A/C NOT FOR ALL Subtask 38-31-00-740-071-A ** ON A/C NOT FOR ALL 4. Fault Isolation
Subtask 38-31-00-810-134-C ** ON A/C NOT FOR ALL
[Rev.8 from Aug 2018]
2026.04.04 04:34:15 UTC
Loss of Data Communication to Lav
1. Possible Causes
- Aircraft Wiring
- Circuit Breaker 32MG
- Circuit Breaker 34MG
- Circuit Breaker 39MG
- Circuit Breaker 45MG
- DEU-B 300RH
- Flush Valve
A. Referenced Information
| REFERENCE | DESIGNATION |
|---|---|
| AMM 23-73-47-000-001 | Removal of the Decoder/Encoder Unit B (300RH) |
| AMM 23-73-47-400-001 | Installation of the Decoder/Encoder Unit B (300RH) |
| AMM 38-31-00-710-009 | Operational Test of the Toilet Unit |
| AMM 38-31-00-740-001 | BITE Test of the Vacuum Toilet System |
| ASM 383111 | |
| AMM 38-31-57-000-001 | Removal of the Flush Valve |
| AMM 38-31-57-400-001 | Installation of the Flush Valve |
Subtask 38-31-00-710-117-A ** ON A/C NOT FOR ALL Subtask 38-31-00-740-071-A ** ON A/C NOT FOR ALL 4. Fault Isolation
Subtask 38-31-00-810-134-C ** ON A/C NOT FOR ALL
A. If the LAST/PREVIOUS LEGS Report gives the maintenance message
TOILET ASSY LAV X
FCU / DEU-B (FIN)
and
the FAP gives the maintenance message CHECK LAVATORY - POWER SUPPLY LAV XX:
Subtask 38-31-00-710-120-A ** ON A/C NOT FOR ALL TOILET ASSY LAV X
FCU / DEU-B (FIN)
and
the FAP gives the maintenance message CHECK LAVATORY - POWER SUPPLY LAV XX:
- do a check of the Aircraft Wiring between the DEU-B and the related lavatory and repair if necessary ASM 383111.
- Open and close the related Circuit Breaker 32MG or Circuit Breaker 34MG or Circuit Breaker 39MG or Circuit Breaker 45MG .
- Replace the related DEU-B 300RH , AMM 23-73-47-000-001 and AMM 23-73-47-400-001.
- Replace the related Flush Valve , AMM 38-31-57-000-001 and AMM 38-31-57-400-001.
B. Test
(1) Do the test as given in paragraph 3. A. to check the correct operation.
(2) After the subsequent flight, make sure that the fault does not continue.
(1) Do the test as given in paragraph 3. A. to check the correct operation.
(2) After the subsequent flight, make sure that the fault does not continue.
MCDU Display