DOC AIRBUS | AMM A320FInstallation of the Radio Management Panel (RMP)
TASK 23-13-13-400-001-A
Installation of the Radio Management Panel (RMP)
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 23-13-13-865-051-A
Subtask 23-13-13-420-050-A
Subtask 23-13-13-860-050-A
[Rev.10 from 2021]
2026.04.01 04:40:03 UTC
Installation of the Radio Management Panel (RMP)
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 23-13-00-710-001-A | Operational Test of the Radio Management Panel (RMP) |
| TASK 23-13-00-740-001-A | BITE Test of the Radio Management Panel (RMP) |
| 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) |
RMP1 and 2Subtask 23-13-13-865-051-A
A. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged:
4. Procedure| PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C ALL | |||
| FOR FIN: 1RG1 (RMPCOM/NAV FREQ SEL, 1) | |||
| 49VU | COM/RMP/1 | 2RG1 | G10 |
| FOR FIN: 1RG2 (RMPCOM/NAV FREQ SEL, 2) | |||
| 121VU | COM NAV/RMP/2 | 2RG2 | L02 |
| ** ON A/C NOT FOR ALL | |||
| FOR FIN: 1RG3 (RMPCOM FREQ SEL, 3) | |||
| 121VU | COM NAV/RMP/3 | 2RG3 | L03 |
Subtask 23-13-13-420-050-A
A. Installation of the RMP
(1) Clean the component interfaces and the adjacent area.
(2) Do an inspection of the component interfaces and the adjacent area.
(3) Remove the blanking caps from the plug (4) and the receptacle (3).
(4) Make sure that the plug (4) and the receptacle (3) are clean and in the correct condition.
(5) Connect the plug (4) to the receptacle (3).
(6) Install the RMP (2) in its housing.
(7) Tighten the fasteners (1) a quarter turn.
Subtask 23-13-13-865-056-A (1) Clean the component interfaces and the adjacent area.
(2) Do an inspection of the component interfaces and the adjacent area.
(3) Remove the blanking caps from the plug (4) and the receptacle (3).
(4) Make sure that the plug (4) and the receptacle (3) are clean and in the correct condition.
(5) Connect the plug (4) to the receptacle (3).
(6) Install the RMP (2) in its housing.
(7) Tighten the fasteners (1) a quarter turn.
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
Subtask 23-13-13-740-050-A | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C ALL | |||
| FOR FIN: 1RG1 (RMPCOM/NAV FREQ SEL, 1) | |||
| 49VU | COM/RMP/1 | 2RG1 | G10 |
| FOR FIN: 1RG2 (RMPCOM/NAV FREQ SEL, 2) | |||
| 121VU | COM NAV/RMP/2 | 2RG2 | L02 |
| ** ON A/C NOT FOR ALL | |||
| FOR FIN: 1RG3 (RMPCOM FREQ SEL, 3) | |||
| 121VU | COM NAV/RMP/3 | 2RG3 | L03 |
C. Do the BITE test of the RMP (Ref. AMM TASK 23-13-00-740-001).
5. Close-upNOTE: As an alternative procedure, you can do the operational test without the Centralized Fault Display System (CFDS) (Ref. AMM TASK 23-13-00-710-001).
Subtask 23-13-13-860-050-A
A. Make sure that the work area is clean and clear of tools and other items.
(1) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002)
(1) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002)