Loss of the ECU 1 Bus A of the FWC 1
TASK 31-53-00-810-852-A
Loss of the ECU 1 Bus A of the FWC 1
1. Possible Causes
A. Referenced Information
3. Fault Confirmation
Subtask 31-53-00-710-138-A ** ON A/C NOT FOR ALL
Subtask 31-53-00-810-101-A ** ON A/C NOT FOR ALL
[Rev.8 from Aug 2018]
2026.04.04 04:30:15 UTC
Loss of the ECU 1 Bus A of the FWC 1
1. Possible Causes
- FWC-1 [1WW1]
- wiring
A. Referenced Information
| REFERENCE | DESIGNATION |
|---|---|
| AMM 31-50-00-710-001 | Ground Scanning of the Central Warning System |
| ASM 315203 | |
| 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) |
Subtask 31-53-00-710-138-A ** ON A/C NOT FOR ALL
A. Test
4. Fault IsolationNOTE: This troubleshooting task is not necessary for operators who do the "one engine taxi" procedure according to FCOM, and get the maintenance message from the engine that was not in operation.
(1) Do the ground scanning of the central warning systems (FWC) AMM 31-50-00-710-001. Subtask 31-53-00-810-101-A ** ON A/C NOT FOR ALL
A. If the test gives the maintenance message FWC1 : NO DATA FROM ECU1-A:
Subtask 31-53-00-710-139-A ** ON A/C NOT FOR ALL - replace the FWC-1 [1WW1] , AMM 31-53-34-000-001 and AMM 31-53-34-400-001.
- do a check and repair the wiring from FWC 1 (1WW1) pins AB/4A, 4B to the first terminal block , ASM 315203.
B. Do the test given in Para. 3.