DOC AIRBUS | AMM A320FInstallation of the ECAM Control Panel
TASK 31-61-12-400-001-A
Installation of the ECAM Control Panel
1. Reason for the Job
Self explanatory
2. Job Set-up Information
A. Work Zones and Access Panels
B. Referenced Information
3. Job Set-up
Subtask 31-61-12-865-051-A
Subtask 31-61-12-420-050-A
Subtask 31-61-12-860-051-A
[Rev.10 from 2021]
2026.04.01 00:38:12 UTC
Installation of the ECAM Control Panel
1. Reason for the Job
Self explanatory
2. Job Set-up Information
A. Work Zones and Access Panels
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 210 | CKPT,FWD COMPT BHD TO FLT COMPT BULKHEAD |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 31-50-00-710-001-A | Ground Scanning of the Central Warning System |
| TASK 31-50-00-710-004-A | Operational Test of the ECAM Control Panel |
ECAM Control PanelSubtask 31-61-12-865-051-A
A. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged:
Subtask 31-61-12-860-050-A | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 49VU | EIS/ECAM/CTL/PNL | 15WT | E12 |
| ** ON A/C NOT FOR ALL | |||
| 49VU | EIS/ECAM/CTL/PNL | 15WT | E11 |
B. Aircraft Maintenance Configuration
(1) Clean the component interfaces and the adjacent area.
(2) Do an inspection of the component interfaces and the adjacent area.
4. Procedure(1) Clean the component interfaces and the adjacent area.
(2) Do an inspection of the component interfaces and the adjacent area.
Subtask 31-61-12-420-050-A
A. Installation of the Control Panel ECAM
(1) Remove the blanking caps from the electrical connectors (3) and (4).
(2) Connect the electrical connectors (4) to the receptacles (3) of the ECAM control panel (2).
(3) Install the ECAM control panel (2) in its housing (5).
(4) Tighten the quarter-turn fasteners (1).
Subtask 31-61-12-865-052-A (1) Remove the blanking caps from the electrical connectors (3) and (4).
(2) Connect the electrical connectors (4) to the receptacles (3) of the ECAM control panel (2).
(3) Install the ECAM control panel (2) in its housing (5).
(4) Tighten the quarter-turn fasteners (1).
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
Subtask 31-61-12-710-051-A | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 49VU | EIS/ECAM/CTL/PNL | 15WT | E12 |
| ** ON A/C NOT FOR ALL | |||
| 49VU | EIS/ECAM/CTL/PNL | 15WT | E11 |
C. Do the operational test of the Central Warning Systems (Ref. AMM TASK 31-50-00-710-001)
5. Close-upNOTE: As an alternative procedure, you can do this operational test without the CFDS (Ref. AMM TASK 31-50-00-710-004)
Subtask 31-61-12-860-051-A
A. Put the aircraft back to its initial configuration.
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Put the system back to the serviceable condition.
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Put the system back to the serviceable condition.