Operational Check of EVMU through CFDS on ECAM A320
1. Reason for the Job
Self explanatory
2. Job Set-up Information
A. Referenced Information
| REFERENCE | DESIGNATION |
| Ref. 24-41-00-861-002-A | Energize the Aircraft Electrical Circuits from the External Power |
| Ref. 24-41-00-861-002-A01 | Energize the Aircraft Electrical Circuits from the APU |
| Ref. 24-41-00-861-002-A02 | Energize the Aircraft Electrical Circuits from Engine 1(2) |
| Ref. 24-41-00-862-002-A | De-energize the Aircraft Electrical Circuits Supplied from the External Power |
| Ref. 24-41-00-862-002-A01 | De-energize the Aircraft Electrical Circuits Supplied from the APU |
| Ref. 24-41-00-862-002-A02 | De-energize the Aircraft Electrical Circuits Supplied from the Engine 1(2) |
| Ref. 31-32-00-860-012-A | Procedure to Get Access to the SYSTEM REPORT/TEST/ENG Page |
3. Job Set-up
SUBTASK 77-32-34-861-062-A
A. Energize the aircraft electrical circuits Ref. AMM TASK 24-41-00-861-002.
SUBTASK 77-32-34-865-071-A
B. Make sure that this(these) circuit breaker(s) is(are) closed:
SUBTASK 77-32-34-869-090-A
C. Aircraft Maintenance Configuration
(1) On the MCDU 1(2), get the SYSTEM REPORT/TEST ENG page Ref. AMM TASK 31-32-00-860-012.
(2) Push the line key adjacent to the EVMU indication: the first EVMU page comes into view
4. Procedure
SUBTASK 77-32-34-710-055-A
A. Test of the EVMU:
5. Close-up
SUBTASK 77-32-34-862-062-A
A. De-energize the aircraft electrical circuits Ref. AMM TASK 24-41-00-862-002.
