Failure of the APU Generator PMG-Stator
TASK 24-23-00-810-807-A
Failure of the APU Generator PMG-Stator
1. Possible Causes
2. Job Set-up Information
A. Referenced Information
3. Fault Confirmation
Subtask 24-23-00-869-059-A ** ON A/C NOT FOR ALL
Subtask 24-23-00-810-068-A ** ON A/C NOT FOR ALL
[Rev.8 from Aug 2018]
2026.04.04 04:26:39 UTC
Failure of the APU Generator PMG-Stator
1. Possible Causes
2. Job Set-up Information
A. Referenced Information
| REFERENCE | DESIGNATION |
|---|---|
| AMM 24-23-51-000-001 | Removal of the APU Generator |
| AMM 24-23-51-400-001 | Installation of the APU Generator |
| 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 24-23-00-869-059-A ** ON A/C NOT FOR ALL
A. Test
Not applicable.
4. Fault IsolationNot applicable.
NOTE: As the APU GEN was set to OFF because of a true failure, the fault confirmation is not necessary.
Subtask 24-23-00-810-068-A ** ON A/C NOT FOR ALL
A. If the fault symptom is identified by the CFDS message GAPCU (24XG)/ GEN APU (8XS) PMG and the upper ECAM-DU warning APU GEN FAULT:
Subtask 24-23-00-860-061-A ** ON A/C NOT FOR ALL - replace the GAPCU [24XG] AMM 24-41-34-000-001 and AMM 24-41-34-400-001.
- replace the GEN-APU [8XS] AMM 24-23-51-000-001 and AMM 24-23-51-400-001.
B. Make sure that the aircraft electrical circuits operate correctly in APU configuration.
(1) Energize the aircraft electrical circuits from the APU AMM 24-41-00-861-002.
(2) Let the APU generator operate for five minutes to make sure that it operates correctly.
(3) 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.
(2) Let the APU generator operate for five minutes to make sure that it operates correctly.
(3) De-energize the aircraft electrical circuits from the APU AMM 24-41-00-862-002.