Failure of the APU Availability Relay
TASK 24-20-00-810-836-A
Failure of the APU Availability Relay
1. Possible Causes
2. Job Set-up Information
A. Referenced Information
3. Fault Confirmation
Subtask 24-20-00-700-076-A ** ON A/C NOT FOR ALL
Subtask 24-20-00-810-075-A ** ON A/C NOT FOR ALL
[Rev.8 from Aug 2018]
2026.04.04 04:26:13 UTC
Failure of the APU Availability Relay
1. Possible Causes
2. Job Set-up Information
A. Referenced Information
| REFERENCE | DESIGNATION |
|---|---|
| ASM 242302 | |
| AMM 24-23-34-000-001 | Removal of the GCU-APU |
| AMM 24-23-34-400-001 | Installation of the GCU-APU |
| 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 |
| ASM 496101 | |
| AMM 49-61-34-000-001 | Removal of the Electronic Control Box (ECB) (GTCP 36-300) |
| AMM 49-61-34-400-001 | Installation of the Electronic Control Box (ECB) (GTCP 36-300) |
Subtask 24-20-00-700-076-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 24-20-00-810-075-A ** ON A/C NOT FOR ALL
A. If the fault symptom is identified by the CFDS message CHECK GCU APU PIN A6A APU CTL RLY 6KD CKT and the upper ECAM DU warning APU GEN FAULT:
Subtask 24-20-00-700-077-A ** ON A/C NOT FOR ALL - replace the RELAY-APU AVAIL [6KD] .
- do a check of the wiring for open circuit:
. between the APU generator pin B/2B and the APU availability relay pin A/2,
. then between the APU GCU pin A/6A and the APU availability relay pin A/1,
. then between the APU relay pin A/X1 and the ECB pin B/J6 ASM 242302 and ASM 496101.
- repair the above defective wiring.
- replace the GCU-APU [1XS] AMM 24-23-34-000-001 and AMM 24-23-34-400-001.
- replace the ELECTRONIC CONTROL BOX [59KD] AMM 49-61-34-000-001 and AMM 49-61-34-400-001.
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) 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) De-energize the aircraft electrical circuits from the APU AMM 24-41-00-862-002.