W DOC AIRBUS | AMM A320F

Installation of the Landing Elevation Selector


TASK 21-31-15-400-801-A
Installation of the Landing Elevation Selector


ZONE: 210
FIN: 20HL
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
 B. Referenced Information
REFERENCE
DESIGNATION
TASK 21-31-00-710-002-A
Operational Test of the Pressure Control and Monitoring
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)
TASK 33-13-00-710-001-A
Operational Test of the Instrument and Panel Integral-Lighting
3. Job Set-up
Subtask 21-31-15-862-051-A
A. De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
Subtask 21-31-15-865-051-A
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged:
PANELDESIGNATIONFINLOCATION
** ON A/C ALL
122VULIGHTING/INSTL LT/OVHD/PNL3LFY03
4. Procedure
Subtask 21-31-15-420-050-A
A. Installation of the Landing Elevation Selector
   (1) Clean the component interfaces and the adjacent area.
   (2) Do an inspection of the component interfaces and the adjacent area.
   (3) Install the selector (9) and put the locating stud (10) at the top, opposite to the black mark (11).
NOTE: Make sure that the locating stud (10) is in position in the hole on the shaft below the black mark (11).
   (4) Install the washer (12) and the nut (13).
   (5) Installation of the intergrally-lighted identification Plate (11LF):
     (a) Put the intergrally-lighted identification plate (16) in position on overhead control and indicating panel 25VU (6).
     (b) Install and tighten the five screws (17).
   (6) Align the knob (14) with the flat of the shaft. Push the knob (14) until it is fully engaged.
   (7) Moderately tighten the two screws (15).
   (8) Remove the CAP-BLANKING from each electrical connector and receptacle.
   (9) Make sure that all the electrical connections are clean and in the correct condition.
   (10) Connect the electrical connector (8).
   (11) Install panel 25VU (6) in its housing.
   (12) Tighten the four quarter-turn fasteners (7).
Subtask 21-31-15-865-052-A
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C ALL
122VULIGHTING/INSTL LT/OVHD/PNL3LFY03
Subtask 21-31-15-861-050-A
C. Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
Subtask 21-31-15-710-050-A
D. Operational Test
   (1) Do the operational test of the instrument and panel integral lighting (Ref. AMM TASK 33-13-00-710-001).
   (2) Do the operational test of the pressure control and monitoring (Ref. AMM TASK 21-31-00-710-002).
5. Close-up
Subtask 21-31-15-942-050-A
A. Make sure that the work area is clean and clear of tools and other items.
[Rev.10 from 2021] 2026.04.02 06:11:14 UTC