(6)
 TORQUE the nut (1) to between 0.6 and 0.7 m.daN (53.09 and 61.94 lbf.in).

 (7) Safety the nut (1) with MISCELLANEOUS (Material No. 19-010). Subtask 52-71-00-710-064
 B. Operational Test
 (1) Do an operational test of the door warning system related to the avionics compartment doors (Ref. TASK 52-71-00-710-001).
 5. Close-up
________ Subtask 52-71-00-860-066
 A. Put the aircraft back to its initial configuration.
 (1) Do an EIS Stop Procedure (Ref. TASK 31-60-00-860-002). Subtask 52-71-00-410-080
 B. Close Access
 (1)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (2)
 Open the applicable avionics compartment door 811 or 812 or 824 (Ref. TASK 52-41-00-010-002).

 (3)
 Get out of the avionics compartment.

 (4)
 Close the applicable avionics compartment door 811 or
 812 or
 824 (Ref. TASK 52-41-00-410-002).

R 1EFF : ALL 1 52-71-00Page A500 1 1 May 01/05 1 1 1CES 1

 (5) Remove the access platform(s). Subtask 52-71-00-862-064
 C. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
R 1EFF : ALL 1 52-71-00Page A501 1 1 May 01/05 1 1 1CES 1

R **ON A/C 001-049, 051-099, 101-149, 201-299,

 TASK 52-71-00-820-009
 Adjustment of the Proximity Switches (5WN1, 5WN2, 6WN1, 6WN2) of the Emergency Exits
 1. Reason for the Job
__________________
 Self Explanatory
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION
 -------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s)
 No specific hexagonal socket wrench
 No specific access platform 3.50 m (11 ft. 6 in.)

 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-42-00-861-001 Energize the Ground Service Network from the External Power 24-42-00-862-001 De-energize the Ground Service Network Supplied from
 the External Power 52-10-00-010-001 Opening of the Passenger/Crew Door 52-10-00-410-001 Closing of the Passenger/Crew Door 52-73-00-710-002 Operational Test of the Warning System related to the
 Emergency Exits 52-71-00-991-016 Fig. 515 FOR FIN 5WN1 25-23-47-000-002 Removal of the Upper Sidewall Panel Assy 241LW,
 (242LW), 241CW, (242CW) and 241FW, (242FW) 25-23-47-400-002 Installation of the Upper Sidewall Panel Assy 241LW,
 (242LW), 241CW, (242CW) and 241FW, (242FW) FOR FIN 5WN2 25-23-47-000-002 Removal of the Upper Sidewall Panel Assy 241LW,
 (242LW), 241CW, (242CW) and 241FW, (242FW)
R 1EFF : 001-049, 051-099, 101-149, 201-299, 1 52-71-00Page A502 1 1 May 01/05 1 1 1CES 1 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------

25-23-47-400-002 Installation of the Upper Sidewall Panel Assy 241LW,
 (242LW), 241CW, (242CW) and 241FW, (242FW) FOR FIN 6WN1 25-23-47-000-002 Removal of the Upper Sidewall Panel Assy 241LW,
 (242LW), 241CW, (242CW) and 241FW, (242FW) 25-23-47-400-002 Installation of the Upper Sidewall Panel Assy 241LW,
 (242LW), 241CW, (242CW) and 241FW, (242FW) FOR FIN 6WN2 25-23-47-000-002 Removal of the Upper Sidewall Panel Assy 241LW,
 (242LW), 241CW, (242CW) and 241FW, (242FW) 25-23-47-400-002 Installation of the Upper Sidewall Panel Assy 241LW, (242LW), 241CW, (242CW) and 241FW, (242FW)
 3. Job Set-up
__________
 Subtask 52-71-00-861-064
 A. Energize the ground service network
 (Ref. TASK 24-42-00-861-001).

 Subtask 52-71-00-010-077
 B. Get Access
 WARNING : DO NOT OPEN THE PASSENGER/CREW DOOR IF THE WIND SPEED IS MORE
_______
 THAN 65 KNOTS.

 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 an access platform in position in front of the passenger/crew door 831.

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

 (3)
 Disarm the escape slide of the applicable emergency exit as follows: (Ref. Fig. 515/TASK 52-71-00-991-016)