(6)
 From this position turn the screw (3) by two turns to two turns and a half. The flats of the screw (3) must be in the same position as shown on the figure.

 (7)
 Disconnect the CHECKING TOOL-DOORS (355M03210000) from the proximity switch (1).

 (8)
 Connect the electrical connector (2) of the proximity switch (1) to its related connector.

 Subtask 52-71-00-865-074
 B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 15WN, 13WN, 48WV
 Subtask 52-71-00-710-055
 C. Operational Test
 (1) Do an operational test of the door warning system related to the passenger/crew door (Ref. TASK 52-71-00-710-001).
 5. Close-up
________ Subtask 52-71-00-410-066-A
 A. 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

 1EFF : ALL 1 52-71-00Page 528 1 1 May 01/04R 1 1 1CES 1

 262UW 262VW (Ref. TASK 25-23-45-400-005). Subtask 52-71-00-410-072
 B. Close Access
 (1)
 Obey the special precautions after the work on the door (Ref. TASK 52-10-00-860-002).

 (2)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (3)
 Remove all the ground support equipment, the maintenance equipment, the standard and special tools and all other items.

 (4)
 Close the applicable passenger/crew door 831 or 841 or 832 or 842 (Ref. TASK 52-10-00-410-001).

 (5) Remove the access platform(s). Subtask 52-71-00-862-070
 C. De-energize the ground service network
 (Ref. TASK 24-42-00-862-001)

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 TASK 52-71-00-820-001- 01
 Adjustment of the Proximity Switches (11WV1, 11WV2, 15WV1, 15WV2) of the Locking Hook of the Passenger/Crew Doors with the ECAM DU
 1. Reason for the Job
__________________
 Self Explanatory
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific access platform 3.5 m (11 ft. 6 in.)
 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied
 from the External Power 31-60-00-860-001 EIS Start Procedure 31-60-00-860-002 EIS Stop Procedure 52-10-00-010-001 Opening of the Passenger/Crew Door 52-10-00-410-001 Closing of the Passenger/Crew Door 52-10-00-860-001 Special Precautions before Work on the Passenger/Crew
 Door 52-10-00-860-002 Special Precautions after Work on the Passenger/Crew
 Door 52-71-00-710-001 Operational Test of the Door Warning System 52-71-00-991-004 Fig. 504 FOR FIN 11WV1 25-23-45-000-005 Removal of the Door Frame Linings at the Left FWD
 Passenger/Crew Door 25-23-45-400-006 Installation of the Door Frame Linings at the Left
 FWD Passenger/Crew Door FOR FIN 11WV2 25-23-45-000-002 Removal of the Door Frame Linings at the Right FWD
 Passenger/Crew Door
R 1EFF : ALL 1 52-71-00Page 530 1 1 May 01/04 1 1 1CES 1 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------

25-23-45-400-007 Installation of the Door Frame Linings at the Right
 FWD Passenger/Crew Door FOR FIN 15WV1 25-23-45-000-003 Removal of the Door Frame Linings at the Left AFT
 Passenger/Crew Door 25-23-45-400-008 Installation of the Door Frame Linings at the Left
 AFT Passenger/Crew Door FOR FIN 15WV2 25-23-45-000-004 Removal of the Door Frame Linings at the Right AFT
 Passenger/Crew Door 25-23-45-400-005 Installation of the Door Frame Linings at the Right AFT Passenger/Crew Door
 3. Job Set-up
__________
 Subtask 52-71-00-861-051
 A. Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).
　
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