1EFF : ALL 1 52-13-18Page 814 1 1 Aug 01/00 1 1 1CES 1 MECHANISM - DOOR LOCKING - REMOVAL/INSTALLATION
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TASK 52-13-21-000-001
Removal of the Door Locking Mechanism
1. Reason for the Job
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Self Explanatory
2. Job Set-up Information
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A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s) No specific lint free cloth No specific lint-free cloth No specific access platform 3.5 m (11 ft. 6 in.) 98D52103501000 1 BALLAST WEIGHT - PASSENGER CREW DOOR
B. Consumable Materials
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Material No. 11-004 USA MIL-T-81533 1.1.1TRICHLOROETHANE (METHYL CHLOROFORM) (Ref. 20-31-00)
Material No. 19-003 USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
1EFF : ALL 1 52-13-21Page 401 1 1 Feb 01/98 1 1 1CES 1 C. Referenced Information
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20-22-00-000-001 Removal of STA-LOK Nuts and Lockwashers 25-23-46-000-002 Removal of the Door Linings at the AFT Passenger/Crew Doors
R 25-62-44-000-002 Removal of the Escape-Slide Pack-Assembly 52-10-00-010-001 Opening of the Passenger/Crew Door 52-10-00-480-001 Installation of the Passenger/Crew Door Ballast
Weight (98D52103501000) for Escape Slide 52-10-00-480-001 Installation of the Passenger/Crew Door Ballast Weight (98D52103501000) for Escape Slide/Raft 52-10-00-860-001 Special Precautions before Work on the Passenger/Crew
Door 52-11-31-000-001 Removal of the Lining Flap 52-13-31-000-001 Removal of the Lining Flap 56-31-13-000-001 Removal of the Window of the AFT Passenger/Crew Door 52-13-21-991-007 Fig. 401 52-13-21-991-010 Fig. 402 52-13-21-991-006 Fig. 403 52-13-21-991-008 Fig. 404 52-13-21-991-005 Fig. 405 52-13-21-991-012 Fig. 406 52-13-21-991-014 Fig. 407 52-13-21-991-015 Fig. 408 52-13-21-991-016 Fig. 409 52-13-21-991-018 Fig. 410 52-13-21-991-020 Fig. 411
3. Job Set-up
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Subtask 52-13-21-010-059
A. Get Access
WARNING : DO NOT OPEN THE PASSENGER/CREW DOOR IF THE WIND SPEED IS MORE
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THAN 65 KNOTS.
WARNING : BEFORE YOU START WORK ON THE DOOR, MAKE SURE THAT:
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THE EMERGENCY CONTROL HANDLE IS IN THE DISARMED POSITION WITH THE SAFETY PIN INSTALLED.
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THE PERCUSSION LEVER OF THE DOOR-DAMPER AND EMERGENCY-OPERATION CYLINDER IS IN THE DISARMED POSITION WITH THE SAFETY PIN INSTALLED.
1EFF : ALL 1 52-13-21Page 402 1 1 Feb 01/04 1 1 1CES 1 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 or 841.
(2)
Open the passenger/crew door (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 52-13-21-865-057
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
**ON A/C 001-002,
Subtask 52-13-21-010-060
C. Removal of Components
(1) Remove the escape slide (Ref. TASK 25-62-44-000-002).
R (2) Install the BALLAST WEIGHT - PASSENGER CREW DOOR (98D52103501000) R (Ref. TASK 52-10-00-480-001).
(3)
Remove the door lining panels (Ref. TASK 25-23-46-000-002).
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