BAT1 and BAT2 disconnected some seconds after the BAT1 and BAT2 Pushbutton Switches are pushed
TASK 24-38-00-810-845-A
BAT1 and BAT2 disconnected some seconds after the BAT1 and BAT2 Pushbutton Switches are pushed
1. Possible Causes
2. Job Set-up Information
A. Referenced Information
3. Fault Confirmation
Subtask 24-38-00-710-126-A
Subtask 24-38-00-810-095-A
Subtask 24-38-00-860-064-A
[Rev.8 from Aug 2018]
2026.04.04 04:26:51 UTC
BAT1 and BAT2 disconnected some seconds after the BAT1 and BAT2 Pushbutton Switches are pushed
1. Possible Causes
2. Job Set-up Information
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 24-38-00-710-126-A
A. Test
Not applicable.
4. Fault IsolationNot applicable.
Subtask 24-38-00-810-095-A
A. If the FAULT legend of the BAT1 and BAT2 pushbutton switches does not come on when:
. the aircraft electrical circuits are energized by the batteries only,
. the voltage of the batteries is more than 25V.
Subtask 24-38-00-710-127-A 5. Close-up. the aircraft electrical circuits are energized by the batteries only,
. the voltage of the batteries is more than 25V.
- do a check for a ground signal at pin A/Y of the BCL1 (2) ASM 243801.
- replace the RELAY-BUS 1XP CTL [15XC] .
- replace the RELAY-BUS 2XP CTL [16XC] .
- do a check and repair the wiring between:
. pin A2 of BUS 2XP control relay (16XC) and the ground,
. pin A3 of BUS 2XP control relay (16XC) and pin A2 of BUS 1XP control relay (15XC),
. pin A3 of BUS 1XP control relay (15XC) and pin A/Y of the BCL1 (2).
Subtask 24-38-00-860-064-A
A. Put the aircraft back to its initial configuration.