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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