R Location of the Slide Release Components
R Figure 503/TASK 52-22-00-991-028
1EFF : 301-399, 1 52-22-00 Page 517
1 1 May 01/04
1 1
1CES 1
R **ON A/C 102-149, 201-207, 211-299, 301-399, 401-499,
5. Close-up
________
**ON A/C 301-399,
Subtask 52-22-00-860-073
A. Put the aircraft back to its initial configuration.
(Ref. Fig. 502/TASK 52-22-00-991-025)
(1)
Pull up the slide control handle in the disarmed position and install the PIN - SAFETY SLIDE (98A52107632000).
(2)
Remove the dynamometer and the nylon strip from the release lever.
(3)
Connect the release lever assembly with the inflation reservoir as follows:
(a)
Put the release cable in position to the release lever.
(b)
Close the safety clamp and safety it with the lockwire, corrosion-resistance steel, dia 0.8 mm (0.032 in.).
(4)
Remove the lock pin from the operation valve of the inflation reservoir and put it into the related stowage pocket.
Subtask 52-22-00-410-062
B. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Install the rear inside fairing in the applicable overhead stowage compartment.
(3)
If removed, install the overhead stowage compartment (Ref. TASK 25-24-41-400-001) and/or the related door frame lining (Ref. TASK 25-23-47-400-004), (Ref. TASK 25-23-47-400-009) and (Ref. TASK 25-23-47-400-010).
(4)
Close the access door of the applicable overhead stowage compartment.
R 1EFF : 102-149, 201-207, 211-299, 301-399, 1 52-22-00Page 518 1401-499, 1Aug 01/05 1 1 1CES 1R (5) Do the special precaution on the door damper and emergency operation R cylinder (Ref. TASK 52-22-00-860-004).
R (6) Close the applicable door (Ref. TASK 52-22-00-410-001) and remove the R RIGGING PIN - SLIDE RELEASE MECHANISM.
1EFF : 301-399, 1 52-22-00Page 519 1 1 May 01/04 1 1 1CES 1 1EFF : 301-399, 1 52-22-00Page 520 1 1 May 01/04 1 1 1CES 1R C. Referenced Information
R TASK 52-22-00-820-002
R Adjustment of the Emergency Exit Door
R 1. Reason for the Job__________________
R To adjust the emergency exit doors (referred to as door) to the correct
R position on the aircraft (lateral gaps, skin offset and parallel motion)
R 2. Job Set-up Information______________________
R A. Fixtures, Tools, Test and Support Equipment
R -------------------------------------------------------------------------------
R REFERENCE QTY DESIGNATION
R -------------------------------------------------------------------------------
R No specific tape
R No specific Torque Wrench : range 0.20 to 3.60 m.daN
R (2.00 to 26.00 lbf.ft)
R 98D52207557000 1 BALLAST WEIGHT - EMERGENCY EXIT
R B. Expendable Parts
R -------------------------------------------------------------------------------
R FIG.ITEM |DESIGNATION |IPC-CSN
R -------------------------------------------------------------------------------
R 12 cotter pin 52-22-02 04A-330
R 32 lock plates 52-22-31 02 -040
R 50 cotter pin 52-22-04 06 -070A
R 60 cotter pin 52-22-04 06 -070A
R -------------------------------------------------------------------------------R REFERENCE DESIGNATION R -------------------------------------------------------------------------------
R 25-23-47-000-004
R
R 25-23-47-000-010
R
R 25-23-47-000-012
R
R 25-23-47-000-013
R
R
R 25-23-47-400-004
R
R 25-23-47-400-009
R
R 25-23-47-400-012
R
R 25-23-47-400-013
R
R
R 52-22-00-010-001
R
R 52-22-00-410-001
R
R 52-22-00-820-005
R 52-22-00-860-003
R
R 52-22-00-860-004
R
R 52-22-31-820-001
R 52-22-00-991-006
R 52-22-00-991-007
R 52-22-00-991-008
R 52-22-00-991-009
R 52-22-00-991-010
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：A320飞机维护手册 AMM DOORS 舱门3(66)
