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(b) For the right door: 842GZ, 842FZ, 842EZ, 842CZ, 842BZ, 842AZ
(4) Install the frame lining panels:
(a)
For the left door (Ref. TASK 25-23-45-400-008): 261TW, 261UW, 261VW, 261WW.
(b)
For the right door (Ref. TASK 25-23-45-400-005): 262TW, 262UW, 262VW, 262WW.
(5) Install the escape slide on the door (Ref. TASK 25-62-44-400-001) R **ON A/C 003-049, 051-099, 101-149, 151-199, 201-299, 301-399, 401-499,
Subtask 52-13-11-410-050-C
B. Installation of the Component
(1)
Remove the BALLAST WEIGHT - PASSENGER CREW DOOR (98D52103501000) (Ref. TASK 52-10-00-080-001) or the escape slide/raft (Ref. TASK 25-62-44-400-001) if previously kept in position (as an alternative to the ballast weight).
(2)
Install the door insulation blankets.
(3)
Install the door lining panels (Ref. TASK 25-23-46-400-002)
(a)
For the left door: 832GZ, 832FZ, 832EZ, 832CZ, 832BZ, 832AZ.
(b)
For the right door: 842GZ, 842FZ, 842EZ, 842CZ, 842BZ, 842AZ.
(4)
Install the frame lining panels:
(a)
For the left door (Ref. TASK 25-23-45-400-008): 261TW, 261UW, 261VW, 261WW.
(b)
For the right door (Ref. TASK 25-23-45-400-005): 262TW, 262UW, 262VW, 262WW.
(5)
Install the emergency escape slide/raft on the door (Ref. TASK 25-62-44-400-001).
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Subtask 52-13-11-410-054
C. Close Access
(1)
Obey the special precautions after the work on the door (Ref. TASK 52-10-00-860-002).
(2)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
(3)
Close the aft passenger/crew door 832 (842) (Ref. TASK 52-10-00-410-001).
(4) Remove the access platform(s). Subtask 52-13-11-862-051
D. Aircraft Maintenance Configuration
(1) De-energize the ground service network
(Ref. TASK 24-42-00-862-001).
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________________________________________
TASK 52-13-12-000-001
Removal of the Support Arm, Door Buffer, Door Pushbutton Switch and Door Stay Mechanism
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 3.50 m (11 ft. 6 in.)
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
52-10-00-010-001 Opening of the Passenger/Crew Door 52-13-11-000-001 Removal of the Aft Passenger/Crew Door 52-13-14-000-001 Removal of the Door-Damper and Emergency-Operation
Cylinder 52-13-12-991-001 Fig. 401 52-13-12-991-002 Fig. 402 52-13-12-991-003 Fig. 403
3. Job Set-up
__________
WARNING : DO NOT OPEN THE PASSENGER/CREW DOOR IF THE WIND SPEED IS MORE THAN
_______
65 KNOTS.
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.
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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.
Subtask 52-13-12-010-053
A. Get Access
(1)
Put an access platform in position in front of the applicable passenger/crew door.
(2)
Open the Aft passenger/crew door 832 (842) (Ref. TASK 52-10-00-010-001).
Subtask 52-13-12-020-052
B. Removal of the Component
(1)
Remove the aft passenger/crew door (Ref. TASK 52-13-11-000-001).
(2)
Remove the door-damper and emergency-operation cylinder (Ref. TASK 52-13-14-000-001).
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