Operational Test of the GEN FAULT Warning

TASK 24-27-00-710-001-A
Operational Test of the GEN FAULT Warning

1. Reason for the Job
Make sure that the GEN FAULT warning 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)

3. Job Set-up
Subtask 24-27-00-860-050-A

A. Aircraft Maintenance Configuration
(1) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
(2) In the cockpit, on the overhead panel 35VU, make sure that the GEN1 (2) pushbutton switch is released.

4. Procedure
Subtask 24-27-00-710-050-A

A. Operational Test of the GEN FAULT Warning:

ACTION	RESULT
1.On the panel 35VU: push the GEN1(2) pushbutton switch.	On the panel 35VU: the FAULT legend of the GEN1(2) pushbutton switch comes on.
2.On the panel 35VU: release the GEN1(2) pushbutton switch.	On the panel 35VU: the FAULT legend of the GEN1(2) pushbutton switch goes off, the OFF legend of the GEN1(2) pushbutton switch comes on.

5. Close-up
Subtask 24-27-00-862-050-A

A. De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).

[Rev.10 from 2021] 2026.03.31 23:22:56 UTC