Failure of the Electrical Wiring between the BCL 1 and Bus 3PP
TASK 24-38-00-810-809-A
Failure of the Electrical Wiring between the BCL 1 and Bus 3PP
1. Possible Causes
A. Referenced Information
3. Fault Confirmation
Subtask 24-38-00-710-066-A 4. Fault Isolation
Subtask 24-38-00-810-058-B
[Rev.8 from Aug 2018]
2026.04.04 04:26:47 UTC
Failure of the Electrical Wiring between the BCL 1 and Bus 3PP
1. Possible Causes
P/BSW-ELEC/BAT1 - aircraft wiring
A. Referenced Information
| REFERENCE | DESIGNATION |
|---|---|
| AMM 24-38-00-710-001 | Operational Test of the Battery Charge Limiter (BCL), (with the CFDS) |
| ASM 243801 |
Subtask 24-38-00-710-066-A 4. Fault Isolation
Subtask 24-38-00-810-058-B
A. If the test gives the maintenance message CHECK DC BAT BUS 3PP/BCL 1 CIRCUIT:
Subtask 24-38-00-710-067-A - do a check of the status of the circuit breaker 8PB1.
- replace the
P/BSW-ELEC/BAT1 ASM 243801.
- do a check and repair the aircraft wiring from the battery 1 line contactor pin A/F to the BCL 1 pin A/A, ELEC/BAT 1 pushbutton switch and circuit breaker (8PB1) included, ASM 243801.
- close it.
B. Do the test given in Para. 3.