WARNING : BEFORE YOU START WORK ON THE DOOR, MAKE SURE THAT:
_______
 -
THE EMERGENCY CONTROL HANDLE IS IN THE DISARMED POSITION WITH THE SAFETY PIN INSTALLED.

 -
THE PERCUSSION LEVER OF THE DOOR-DAMPER AND EMERGENCY-OPERATION CYLINDER IS IN THE DISARMED POSITION WITH THE SAFETY PIN INSTALLED.

 WARNING : STOP THE OPENING PROCEDURE IF THE RED WARNING LIGHT FLASHES.
_______ RESIDUAL PRESSURE COULD CAUSE THE DOOR TO OPEN WITH A SUDDEN FORCE AND INJURE PERSONS AND/OR DAMAGE THE AIRCRAFT.
 (1)
 Put the access platform in position in front of the passenger/crew door 831 or 841 or 832 or 842.

 (2)
 Open the applicable passenger/crew door (Ref. TASK 52-10-00-010-001).

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 (3) Obey the special precautions before you start work on the door (Ref. TASK 52-10-00-860-001).
 Subtask 52-71-00-010-053-A
 C. Removal of the Lining Panel
 (1) Remove the lining panel:
 FOR 11WV1
 221JW 221HW (Ref. TASK 25-23-45-000-005).
 FOR 11WV2
 222JW 222HW (Ref. TASK 25-23-45-000-002).
 FOR 15WV1
 261UW 261VW (Ref. TASK 25-23-45-000-003).
 FOR 15WV2
 262UW 262VW (Ref. TASK 25-23-45-000-004).

 (2) Remove the insulation blanket. Subtask 52-71-00-860-050
 D. Aircraft Maintenance Configuration
 (1)
 Make sure that the doors are closed.

 (2)
 Do the EIS start procedure (Ref. 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 52-71-00-820-052
 A. Adjustment of the Proximity Switch
 (Ref. Fig. 504/TASK 52-71-00-991-004)

 WARNING : DO NOT OPEN THE DOOR DURING THE ADJUSTMENT.
_______
 (1) Turn the screw (2) until the symbol of the passenger/crew door is green on the lower ECAM DU.
 NOTE : The target (3) and the proximity switch (1) must not be in
____
 contact.

 (2) Turn the screw (2) in the opposite direction until the symbol of the passenger/crew door is amber on the lower ECAM DU.
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 Adjustment of the Proximity Switches (11WV1, 11WV2, 15WV1, 15WV2) of the
 Locking Hook - Passenger/Crew Doors
 Figure 504/TASK 52-71-00-991-004

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 (3) From this position, turn the screw (2) by two turns to two turns and a half. The flats of the screw (2) must be in the same position as shown on the figure.
 Subtask 52-71-00-710-056
 B. Operational Test
 (1) Do an operational test of the warning system related to the passenger/crew doors (Ref. TASK 52-71-00-710-001).
 5. Close-up
________ Subtask 52-71-00-860-063
 A. Put the aircraft back to its initial configuration.
 (1) Do an EIS stop procedure (Ref. TASK 31-60-00-860-002). Subtask 52-71-00-410-054-A
 B. Installation of the Lining Panel
 (1)
 Install the insulation blanket.

 (2)
 Install the lining panel:
 FOR 11WV1
 221JW 221HW (Ref. TASK 25-23-45-400-006).
 FOR 11WV2
 222JW 222HW (Ref. TASK 25-23-45-400-007).
 FOR 15WV1
 261UW 261VW (Ref. TASK 25-23-45-400-008).
 FOR 15WV2
 262UW 262VW (Ref. TASK 25-23-45-400-005).

 Subtask 52-71-00-410-053
 C. Close Access
 (1)
 Obey the special precautions after the work on the door (Ref. TASK 52-10-00-860-002).

 (2)
 Remove all the ground support equipment, the maintenance equipment, the standard and special tools and all other items.

 (3)
 Close the applicable passenger/crew door 831 or 841 or 832 or 842 (Ref. TASK 52-10-00-410-001).

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 (4)
 Remove the access platform(s).

 (5)
 Make sure that the work area is clean and clear of tool(s) and other items.

 Subtask 52-71-00-862-051
 D. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
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 TASK 52-71-00-820-002
 Adjustment of the Proximity Switches (4WN1, 4WN2, 7WN1, 7WN2, 13WV1, 13WV2, 17WV1, 17WV2) of the Passenger/Crew Doors with the CHECKING TOOL-DOORS
　
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