B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
25-23-46-000-001 Removal of the Door Linings at the FWD Passenger/Crew Doors R 25-62-44-000-002 Removal of the Escape-Slide Pack-Assembly 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 52-11-31-991-001 Fig. 401
1EFF : ALL 1 52-11-31Page 401 1 1 Feb 01/04 1 1 1CES 1
3. Job Set-up
__________ Subtask 52-11-31-010-050
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 front of the passenger/crew door 831(841).
(2)
Open the passenger/crew door 831 (841).
(3)
Obey the special precautions before you start work on the door (Ref. TASK 52-10-00-860-001).
Subtask 52-11-31-865-050
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 52-11-31Page 402 1 1 May 01/98R 1 1 1CES 1
**ON A/C 001-002,
Subtask 52-11-31-010-051
C. Removal of Components
(1)
Remove the escape slide (Ref. TASK 25-62-44-000-002).
(2)
Remove the door lining panels (Ref. TASK 25-23-46-000-001).
(3)
Install the BALLAST WEIGHT - PASSENGER CREW DOOR (98D52103501000) (Ref. TASK 52-10-00-480-001).
(4) Remove the door insulation. R **ON A/C 003-049, 051-099, 101-149, 151-199, 201-299, 301-399, 401-499,
Subtask 52-11-31-010-051-A
C. Removal of Components
(1)
Remove the escape slide/raft (Ref. TASK 25-62-44-000-002).
(2)
Remove the door lining panels (Ref. TASK 25-23-46-000-001).
(3)
Install the BALLAST WEIGHT - PASSENGER CREW DOOR (98D52103501000) (Ref. TASK 52-10-00-480-001).
(4) Remove the door insulation.
**ON A/C ALL
4. Procedure
_________
Subtask 52-11-31-020-050
A. Removal of the Lining Flap
(Ref. Fig. 401/TASK 52-11-31-991-001)
(1) Disengage the rods (1) as follows:
(a)
Remove the cotter pins (2) and discard them.
(b)
Remove the pins (3) and the washers (4).
1EFF : ALL 1 52-11-31Page 403 1 1 Aug 01/05 1 1 1CES 1
Lining Flap Figure 401/TASK 52-11-31-991-001
1EFF : 1 1R 1CES ALL 1 11 1 52-11-31 Page 404 May 01/04
(2)
Disengage the lining flap (5) from the bellcrank assy (6) as follows:
(a)
Remove the cotter pins (7) and discard them.
(b)
Remove the pins (8) and the washers (9).
(3)
Disengage the lining flap (5) from the rods (1) and from the bellcrank assy (6).
1EFF : ALL 1 52-11-31Page 405 1 1 May 01/04R 1 1 1CES 1
TASK 52-11-31-400-001
Installation of the Lining Flap
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM DOORS 艙門2(35)
