DOC AIRBUS | AMM A320FInstallation of the ILS Receiver
TASK 34-36-31-400-001-A
Installation of the ILS Receiver
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 34-36-31-010-051-A
Subtask 34-36-31-420-050-A
Subtask 34-36-31-410-050-A
[Rev.9 from 2019]
2026.04.02 06:23:18 UTC
Installation of the ILS Receiver
1. Reason for the Job
Self explanatory
2. Job Set-up Information
A. Work Zones and Access Panels
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 121 | AVIONICS COMPARTMENT |
| 122 | AVIONICS COMPARTMENT |
| 811 |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 22-97-00-710-001-A | Operational Test of the LAND CAT III Capability |
Subtask 34-36-31-010-051-A
A. Get Access
(1) Make sure that the access platform is in position at the access door 811 in zone 122.
(2) Make sure that the access door 811 is open.
Subtask 34-36-31-865-051-A (1) Make sure that the access platform is in position at the access door 811 in zone 122.
(2) Make sure that the access door 811 is open.
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged:
4. Procedure| PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| FOR FIN: 2RT1 (RECEIVERILS, 1) | |||
| 49VU | NAV/ILS/1 | 1RT1 | G12 |
| FOR FIN: 2RT2 (RECEIVERILS, 2) | |||
| 121VU | COM NAV/ILS/2 | 1RT2 | K09 |
Subtask 34-36-31-420-050-A
A. Installation of the ILS Receiver (2RT1, 2RT2)
(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 electrical connectors (2).
(4) Make sure that the electrical connectors (2) are clean and in the correct condition.
(5) Install the ILS receiver (1) on its rack (3).
(6) Push the ILS Receiver (1) on its rack (3) to connect the electrical connectors (2).
(7) Engage the nuts (4) on the lugs (5) and tighten.
Subtask 34-36-31-865-052-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 electrical connectors (2).
(4) Make sure that the electrical connectors (2) are clean and in the correct condition.
(5) Install the ILS receiver (1) on its rack (3).
(6) Push the ILS Receiver (1) on its rack (3) to connect the electrical connectors (2).
(7) Engage the nuts (4) on the lugs (5) and tighten.
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
Subtask 34-36-31-740-050-A | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| FOR FIN: 2RT1 (RECEIVERILS, 1) | |||
| 49VU | NAV/ILS/1 | 1RT1 | G12 |
| FOR FIN: 2RT2 (RECEIVERILS, 2) | |||
| 121VU | COM NAV/ILS/2 | 1RT2 | K09 |
C. BITE test of the ILS
(1) Do the BITE test of the ILS (Ref. AMM D/O 34-36-00-74)
5. Close-up(1) Do the BITE test of the ILS (Ref. AMM D/O 34-36-00-74)
NOTE: If the airline operates the aircraft in CAT 3 conditions, do the LAND CAT III capability test
(Ref. AMM TASK 22-97-00-710-001).
(2) As an alternative procedure, without the CFDS, you can do the operational test of the ILS (Ref. AMM D/O 34-36-00-71). (Ref. AMM TASK 22-97-00-710-001).
Subtask 34-36-31-410-050-A
A. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Close the access door 811.
(3) Remove the access platform(s).
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Close the access door 811.
(3) Remove the access platform(s).