W DOC AIRBUS | AMM A320F

Adjustment of the Proximity Switches of the Emergency Exit Doors with the ECAM Display Unit (DU)


TASK 52-71-00-820-007-A-01
Adjustment of the Proximity Switches of the Emergency Exit Doors with the ECAM Display Unit (DU)


WARNING: STOP THE OPENING PROCEDURE IF THE RED WARNING LIGHT FLASHES. IF THE RED WARNING LIGHT FLASHES, REMAINING PRESSURE CAN CAUSE THE DOOR TO OPEN SUDDENLY AND CAN:
  • KILL OR CAUSE SERIOUS INJURY TO PERSONS
  • CAUSE DAMAGE TO THE AIRCRAFT.
1. Reason for the Job
There are two methods to do the adjustment of the proximity switches of the emergency exit doors:
  • Mechanically - with the doors checking tool
  • Electronically - with the ECAM DU.
This task gives the electronic method. For the other method, refer to the related task in this page block.
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
AR
ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
843EZ, 844EZ
835, 845
833, 833EZ, 834, 834EZ, 843, 844
 C. Expendable Parts
FIG.ITEM
DESIGNATION
IPC-CSN
5
LOCK WASHER
AIPC 52-22-21-09-218
5
LOCK WASHER
AIPC 52-22-21-09-615
5
LOCK WASHER
AIPC 52-22-21-24-430
5
LOCK WASHER
AIPC 52-22-21-24-690
 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 25-23-47-000-013-A
Removal of the Door Linings of the RH FWD Emergency Exit Door at zone 251 or RH AFT at zone 252 or LH AFT at zone 232.
TASK 25-23-47-000-802-A
Removal of the Door Linings of the Emergency Exit, zones 251/252
TASK 25-23-47-400-013-A
Installation of the Door Linings of the RH FWD Emergency Exit Door at zone 251, or RH AFT at zone 252, or LH AFT at zone 232.
TASK 25-23-47-400-802-A
Installation of the Door Linings of the Emergency Exit, zones 251/252
TASK 31-60-00-860-001-A
EIS Start Procedure
TASK 31-60-00-860-002-A
EIS Stop Procedure
TASK 52-22-00-010-002-A
Opening of the Emergency Exit Doors from the Outside
TASK 52-22-00-410-001-A
Closing of the Emergency Exit Doors from the Passenger Compartment
TASK 52-22-00-410-002-A
Closing of the Emergency Exit Doors from the Outside
TASK 52-22-00-860-003-A
Special Precaution before Maintenance on the Door Damper and Emergency Operation Cylinder
TASK 52-22-00-860-004-A
Special Precaution after Maintenance on the Door Damper and Emergency Operation Cylinder
TASK 52-73-00-710-002-B
Operational Test of the Warning System related to the Emergency Exits
TASK 52-73-00-710-002-E
Operational Test of the Warning System Related to the Emergency Exit Doors
3. Job Set-up
Subtask 52-71-00-861-058-A ** ON A/C NOT FOR ALL
A. Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
Subtask 52-71-00-010-067-A ** ON A/C NOT FOR ALL
B. Get Access
   (1) Put the ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at emergency exit door 834, 843, 833 or 844.
   (2) Open the applicable emergency exit door from the outside of the aircraft (Ref. AMM TASK 52-22-00-010-002).
   (3) Obey the special precautions before you start the work on the emergency exit door (Ref. AMM TASK 52-22-00-860-003).
   (4) Close emergency exit door 834, 843, 833 or 844 from the inside of the aircraft (Ref. AMM TASK 52-22-00-410-001).
Subtask 52-71-00-010-074-A ** ON A/C NOT FOR ALL
C. Removal of the Lining Panel
   (1) Remove the applicable lining panel (Ref. AMM TASK 25-23-47-000-013):
     (a) For 19WV1:
     (b) For 19WV2:
     (c) For 21WV1:
     (d) For 21WV2:
   (2) Remove the insulation.
Subtask 52-71-00-010-067-B ** ON A/C NOT FOR ALL
D. Get Access
   (1) Put the ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at emergency exit door 835 or 845.
   (2) Open the applicable emergency exit door from the outside of the aircraft (Ref. AMM TASK 52-22-00-010-002).
   (3) Obey the special precautions before you start the work on the emergency exit door (Ref. AMM TASK 52-22-00-860-003).
   (4) Close emergency exit door 835 or 845 from the inside of the aircraft (Ref. AMM TASK 52-22-00-410-002).
Subtask 52-71-00-010-074-B ** ON A/C NOT FOR ALL
E. Removal of the Lining Panel
   (1) Remove the applicable lining panel (Ref. AMM TASK 25-23-47-000-802):
     (a) For 21WV1:
     (b) For 21WV2:
   (2) Remove the insulation.
Subtask 52-71-00-860-058-A ** ON A/C NOT FOR ALL
F. Aircraft Maintenance Configuration
   (1) Make sure that the emergency exit doors are closed.
   (2) Do the EIS start procedure (Ref. AMM TASK 31-60-00-860-001).
   (3) On the ECAM control panel, push the DOOR key (on the lower ECAM DU, the "DOOR/OXY" page comes into view).
4. Procedure
Subtask 52-71-00-820-064-A ** ON A/C NOT FOR ALL Subtask 52-71-00-820-064-B ** ON A/C NOT FOR ALL Subtask 52-71-00-710-054-A ** ON A/C NOT FOR ALL 5. Close-up
Subtask 52-71-00-860-059-A ** ON A/C NOT FOR ALL
A. Aircraft Maintenance Configuration
   (1) Do the EIS stop procedure (Ref. AMM TASK 31-60-00-860-002).
Subtask 52-71-00-410-078-A ** ON A/C NOT FOR ALL
B. Installation of the Lining Panel
   (1) Install the insulation.
   (2) Install the removed lining panel (Ref. AMM TASK 25-23-47-400-013):
     (a) For 19WV1:
     (b) For 19WV2:
     (c) For 21WV1:
     (d) For 21WV2:
Subtask 52-71-00-410-070-A ** ON A/C NOT FOR ALL
C. Close Access
   (1) Obey the special precautions after the work on the emergency exit door (Ref. AMM TASK 52-22-00-860-004).
   (2) Make sure that the work area is clean and clear of tools and other items.
   (3) Close emergency exit door 833, 843, 843 or 844 (Ref. AMM TASK 52-22-00-410-002).
   (4) Remove the access platform(s).
Subtask 52-71-00-410-078-B ** ON A/C NOT FOR ALL
D. 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 21WV1:
     (b) For 21WV2:
Subtask 52-71-00-410-070-B ** ON A/C NOT FOR ALL
E. Close Access
   (1) Obey the special precautions after the work on the emergency exit door (Ref. AMM TASK 52-22-00-860-004).
   (2) Make sure that the work area is clean and clear of tools and other items.
   (3) Close emergency exit door 835 or 845 (Ref. AMM TASK 52-22-00-410-002).
   (4) Remove the access platform(s).
Subtask 52-71-00-862-060-A ** ON A/C NOT FOR ALL
F. De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
[Rev.10 from 2021] 2026.04.02 06:28:30 UTC