DOC AIRBUS | AMM A320FOperational Test of the Automatic Galley Shedding
TASK 24-27-00-710-002-A
Operational Test of the Automatic Galley Shedding
1. Reason for the Job
Make sure that the automatic galley shedding is operative when there are no more indications on the ECAM ELEC page.
2. Job Set-up Information
A. Referenced Information
3. Job Set-up
Subtask 24-27-00-860-051-A
Subtask 24-27-00-710-051-A
Subtask 24-27-00-865-052-A
[Rev.10 from 2021]
2026.03.31 23:22:57 UTC
Operational Test of the Automatic Galley Shedding
1. Reason for the Job
Make sure that the automatic galley shedding is operative when there are no more indications on the ECAM ELEC page.
2. Job Set-up Information
A. Referenced Information
| REFERENCE | DESIGNATION |
|---|---|
| TASK 24-41-00-861-002-A | Energize the Aircraft Electrical Circuits from the External Power |
| TASK 24-41-00-861-002-A-01 | Energize the Aircraft Electrical Circuits from the APU |
| TASK 24-41-00-861-002-A-02 | Energize the Aircraft Electrical Circuits from Engine 1(2) |
| TASK 24-41-00-862-002-A | De-energize the Aircraft Electrical Circuits Supplied from the External Power |
| TASK 24-41-00-862-002-A-01 | De-energize the Aircraft Electrical Circuits Supplied from the APU |
| TASK 24-41-00-862-002-A-02 | De-energize the Aircraft Electrical Circuits Supplied from the Engine 1(2) |
Subtask 24-27-00-860-051-A
A. Aircraft Maintenance Configuration
(1) Energize the aircraft electrical circuits from the APU (Ref. AMM TASK 24-41-00-861-002).
(2) In the cockpit, on the overhead panel 35VU, make sure that the GALLEY pushbutton switch is pushed (the OFF legend is off).
(3) In the forward and aft galleys, make sure that all the units operate.
Subtask 24-27-00-865-050-A (1) Energize the aircraft electrical circuits from the APU (Ref. AMM TASK 24-41-00-861-002).
(2) In the cockpit, on the overhead panel 35VU, make sure that the GALLEY pushbutton switch is pushed (the OFF legend is off).
(3) In the forward and aft galleys, make sure that all the units operate.
B. Make sure that this(these) circuit breaker(s) is(are) closed:
4. Procedure| PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C ALL | |||
| 122VU | ELEC/GALY & CAB/CTL | 1XA | S26 |
| 122VU | ELEC/GALY & CAB/FAULT/LT CTL | 8XA | S25 |
| 122VU | ELEC/GALY & CAB/GND/FLT/LOGIC | 7XA | S24 |
Subtask 24-27-00-710-051-A
A. Operational Test of the Automatic Galley Sheeding:
5. Close-up| ACTION | RESULT |
|---|---|
1.On the panel 122VU:
| In the forward and aft galleys:
|
Subtask 24-27-00-865-052-A
A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
Subtask 24-27-00-862-051-A | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C ALL | |||
| 122VU | ELEC/GALY & CAB/GND/FLT/LOGIC | 7XA | S24 |
B. De-energize the aircraft electrical circuits supplied from the APU. (Ref. AMM TASK 24-41-00-862-002).