APU Generator Overload
TASK 24-20-00-810-944-A
APU Generator Overload
1. Possible Causes
A. Referenced Information
3. Fault Confirmation
Subtask 24-20-00-700-123-A ** ON A/C NOT FOR ALL
Subtask 24-20-00-810-221-A ** ON A/C NOT FOR ALL
[Rev.8 from Aug 2018]
2026.04.04 04:26:26 UTC
APU Generator Overload
1. Possible Causes
- wiring
- feeders
- GAPCU [24XG]
A. Referenced Information
| REFERENCE | DESIGNATION |
|---|---|
| AMM 24-41-00-861-002 | Energize the Aircraft Electrical Circuits from the External Power |
| AMM 24-41-00-862-002 | De-energize the Aircraft Electrical Circuits Supplied from the External Power |
| AMM 24-41-34-000-001 | Removal of the Ground Power Control Unit (GPCU) |
| AMM 24-41-34-400-001 | Installation of the Ground Power Control Unit (GPCU) |
Subtask 24-20-00-700-123-A ** ON A/C NOT FOR ALL
A. Test
(a) On the upper ECAM DU, the warning GEN APU OVERLOAD is shown and the APU generator or the external power trips.
4. Fault IsolationNOTE: Make sure that the cause of the overload is not a load added to the normal load because then, the total load will be more than the maximum permitted load. If this occurs, no trouble shooting is necessary.
(1) Energize the aircraft electrical circuits from the APU AMM 24-41-00-861-002. (a) On the upper ECAM DU, the warning GEN APU OVERLOAD is shown and the APU generator or the external power trips.
Subtask 24-20-00-810-221-A ** ON A/C NOT FOR ALL
A. If the test confirms the fault:
Subtask 24-20-00-860-194-A ** ON A/C NOT FOR ALL - do a check of the circuit breakers related to the loads from the APU generator.
- do a check and repair the wiring and the related equipment for a short circuit or a short to ground.
- do a check and repair the feeders of the AC 1 (1XP) and AC 2 (2XP) bus bar for a short to ground, or a short circuit.
- replace the GAPCU [24XG] AMM 24-41-34-000-001 and AMM 24-41-34-400-001.
B. Do this procedure to make sure that the system operates correctly:
(1) Energize the aircraft electrical circuits from the APU AMM 24-41-00-861-002. On the upper ECAM DU, the warning APU GEN OVERLOAD is not shown and there is no trip.
(2) De-energize the aircraft electrical circuits from the APU AMM 24-41-00-862-002.
(1) Energize the aircraft electrical circuits from the APU AMM 24-41-00-861-002. On the upper ECAM DU, the warning APU GEN OVERLOAD is not shown and there is no trip.
(2) De-energize the aircraft electrical circuits from the APU AMM 24-41-00-862-002.