W DOC AIRBUS | AMM A320F

Installation of the Proximity Switches of the Aft Emergency Exits


TASK 52-73-11-400-004-E
Installation of the Proximity Switches of the Aft Emergency Exits


ZONE: 835
ZONE: 845
FIN: 6WN1 ** ON A/C NOT FOR ALL
FIN: 6WN2 ** ON A/C NOT FOR ALL
1. Reason for the Job
Self explanatory
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
AR
ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE
No specific
Torque wrench: range to between 4 and 3 m.N (35.40 and 26.55 lbf.in ) T
 B. Consumable Materials
REFERENCE
DESIGNATION
(Material No.14QFB1)
Wire-Locking Dia: 0.8 mm CRES Nickel Alloy -
 C. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
835
MID PASSENGER/CREW DOOR
845
MID PASSENGER/CREW DOOR
835, 845
FOR [6WN1] (PROX SW-HANDLE, L AFT EMER EXIT ESC SLIDE)
835CZ
FOR [6WN2] (PROX SW-HANDLE, R AFT EMER EXIT ESC SLIDE)
845CZ
 D. Referenced Information
REFERENCE
DESIGNATION
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 25-23-47-400-802-A
Installation of the Door Linings of the Emergency Exit, zones 251/252
TASK 52-22-00-410-002-A
Closing of the Emergency Exit Doors from the Outside
TASK 52-22-00-860-004-A
Special Precaution after Maintenance on the Door Damper and Emergency Operation Cylinder
TASK 52-71-00-820-009-F
Adjustment of the Proximity Switches of the Emergency Exits with the Door Checking Tool
TASK 52-71-00-820-009-F-01
Adjustment of the Proximity Switches of the Aft Emergency-Exit Doors with the ECAM Display Unit (DU)
TASK 52-73-00-710-002-E
Operational Test of the Warning System Related to the Emergency Exit Doors
3. Job Set-up
Subtask 52-73-11-860-059-A ** ON A/C NOT FOR ALL
A. Aircraft Maintenance Configuration
   (1) Make sure that the ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE is in position at applicable emergency exits 835 or 845.
   (2) Make sure that the aircraft electrical circuits are energized.
(Ref. AMM TASK 24-41-00-861-002).
Subtask 52-73-11-865-081-A ** ON A/C NOT FOR ALL
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged:
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
121VUEIS/SLIDES/ARM AND WARN/FLT15WNP11
121VUEIS/SLIDES/ARM AND WARN/GND13WNP10
121VUEIS/SDAC1 AND 2/DOOR/DET/PAX48WVP05
4. Procedure
Subtask 52-73-11-420-071-A ** ON A/C NOT FOR ALL Subtask 52-73-11-865-082-A ** ON A/C NOT FOR ALL
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
121VUEIS/SLIDES/ARM AND WARN/FLT15WNP11
121VUEIS/SLIDES/ARM AND WARN/GND13WNP10
121VUEIS/SDAC1 AND 2/DOOR/DET/PAX48WVP05
Subtask 52-73-11-710-059-A ** ON A/C NOT FOR ALL
C. Operational Test
   (1) Do an operational test of the warning system related to the emergency exits (Ref. AMM TASK 52-73-00-710-002).
5. Close-up
Subtask 52-73-11-410-072-A ** ON A/C NOT FOR ALL
A. Installation of the Lining Panel
   (1) Install the insulation.
   (2) Install the removed lining panel (Ref. AMM TASK 25-23-47-400-802):
     (a) FOR [6WN1] (PROX SW-HANDLE, L AFT EMER EXIT ESC SLIDE)
     (b) FOR [6WN2] (PROX SW-HANDLE, R AFT EMER EXIT ESC SLIDE)
Subtask 52-73-11-410-073-A ** ON A/C NOT FOR ALL
B. Close Access
   (1) Make sure that the work area is clean and clear of tools and other items.
   (2) Obey the special precautions after you do work on the emergency exits (Ref. AMM TASK 52-22-00-860-004).
   (3) Close the applicable emergency exits door (Ref. AMM TASK 52-22-00-410-002).
   (4) Remove the access platform(s).
Subtask 52-73-11-862-062-A ** ON A/C NOT FOR ALL
C. De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
[Rev.10 from 2021] 2026.04.01 01:48:44 UTC