__________________
Self Explanatory
2.
Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
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REFERENCE QTY DESIGNATION
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No specific circuit breaker(s) safety clip(s)
No specific two shims 0.2 mm (0.0078 in.)
No specific access platform 3.50 m (11 ft. 6 in.)
R No specific Torque Wrench : range 0.00 to 1.20 m.daN
R (0.00 to 9.00 lbf.ft)
B. Consumable Materials
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REFERENCE DESIGNATION
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Material No. 08-007A
SEALANT, HIGH TEMP. (Ref. 20-31-00)
Material No. 19-010 USA AMS 5687
LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA
(Ref. 20-31-00)
C. Expendable Parts
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FIG.ITEM |DESIGNATION |IPC-CSN
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cotter pin 53-46-04 80B-060
1EFF : ALL 1 52-13-21Page 501 1 1 May 01/05 1 1 1CES 1 D. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
25-23-46-000-002 Removal of the Door Linings at the AFT Passenger/Crew Doors
25-23-46-400-001 52-10-00-010-001 52-10-00-410-001 52-10-00-860-001 Installation of the Door Linings at the FWD Passenger/Crew DoorsOpening of the Passenger/Crew DoorClosing of the Passenger/Crew DoorSpecial Precautions before Work on the Passenger/Crew Door
52-10-00-860-002 Special Precautions after Work on the Passenger/Crew Door
52-11-31-400-001 52-13-31-000-001 52-71-00-820-001 Installation of the Lining FlapRemoval of the Lining FlapAdjustment of the Proximity Switches (11WV1, 11WV2, 15WV1, 15WV2) of the Locking Hook of the Pax/Crew Doors with the CHECKING TOOL-DOOR
52-13-21-991-001 Fig. 501
**ON A/C 001-049, 051-099, 101-105, 151-154, 201-207, 52-13-21-991-031 Fig. 502
R **ON A/C 106-149, 155-199, 208-299, 301-399, 401-499,
52-13-21-991-031-A Fig. 502A
**ON A/C ALL
52-13-21-991-002 Fig. 503
1EFF : ALL 1 52-13-21Page 502 1 1 Aug 01/05 1 1 1CES 1
3. Job Set-up
__________
Subtask 52-13-21-010-050
A. Get Access
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.
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 the zone 831 (841).
(2)
Open the aft passenger/crew door 832 842 (Ref. TASK 52-10-00-010-001).
(3)
Obey the special precautions before you start work on the door (Ref. TASK 52-10-00-860-001).
Subtask 52-13-21-865-050
B. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------121VU EIS/SLIDES/ARM AND WARN/FLT 15WN P11 121VU EIS/SLIDES/ARM AND WARN/GND 13WN P10 121VU EIS/SDAC1 AND 2/DOOR/DET/PAX 48WV P05
1EFF : ALL 1 52-13-21Page 503 1 1 Feb 01/01R 1 1 1CES 1
Subtask 52-13-21-010-051
C. Removal of Components
(1)
Remove the lining flap (Ref. TASK 52-13-31-000-001).
(2)
Remove the door lining panels (Ref. TASK 25-23-46-000-002).
(a)
For the left passenger/crew door 832EZ.
(b)
For the right passenger/crew door 842EZ.
(3)
Remove the door insulation.
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