(9)
Remove the nuts (201), the bolts (203) and the flange bearing (202) from the door structure.
(10) Move the locking shaft (176) in the rear direction so that the shaft end comes free from the door structure.
1EFF : 301-399, 1 52-22-21Page 434 1 1 May 01/04 1 1 1CES 1
(11)
Loosen the attachment screw and remove the target lever (173) from
the locking shaft (176).
(12)
Remove the locking shaft (176) from the door struture.
(13)
If required, remove the nuts (206), the screws (204) and the stop fitting (205) from the door structure.
1EFF : 301-399, 1 52-22-21Page 435 1 1 May 01/04 1 1 1CES 1 TASK 52-22-21-400-003
Installation of the Locking Shaft Mechanism (60" Door)
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 3.2 m (10 ft. 6 in.)
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 04-004 USA MIL-PRF-23827 TYPE I
SYNTH.ESTER BASED GREASE HIGH PRESSURE
(Ref. 20-31-00)
C. Expendable Parts
-------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
110 cotter pin 52-22-21 06 -120 113 tie-wrap 52-22-21 06 -160 115 tie-wrap 52-22-21 06 -170 124 cotter pin 52-22-21 06 -210 136 cotter pin 52-22-21 04A-120 141 cotter pin 52-22-21 04A-120 149 cotter pin 52-22-21 04A-120 158 cotter pin 52-22-21 04A-240 164 cotter pin 52-22-21 09A-370 181 cotter pin 52-22-21 09A-400 186 cotter pin 52-22-11 04 -070 187 cotter pin 52-22-21 09A-400
1EFF : 301-399, 1 52-22-21Page 436 1 1 May 01/04 1 1 1CES 1 D. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
25-23-47-000-012 Removal of the Door Linings of the LH FWD Emergency Exit Door, zone 231
25-23-47-000-013 Removal of the Door Linings of the RH FWD Emergency Exit Door at zone 251 or RH AFT at zone 252 or LH AFT at zone 232.
25-23-47-400-013 Installation of the Door Linings of the RH FWD Emergency Exit Door at zone 251, or RH AFT at zone 252, or LH AFT at zone 232.
52-22-00-010-001 Opening of the Emergency Exit Doors from the Passenger Compartment 52-22-00-410-001 Closing of the Emergency Exit Doors from the
Passenger Compartment 52-22-00-820-003 Adjustment of the Locking Mechanism 52-22-00-860-003 Special Precaution before Maintenance on the Door
Damper and Emergency Operation Cylinder 52-22-00-860-004 Special Precaution after Maintenance on the Door
Damper and Emergency Operation Cylinder 52-22-21-991-003 Fig. 404 52-22-21-991-004 Fig. 405
3. Job Set-up
__________
Subtask 52-22-21-865-057
A. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
-------------------------------------------------------------------------------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 : 301-399, 1 52-22-21Page 437 1 1 May 01/04 1 1 1CES 1 Subtask 52-22-21-860-052
B. Aircraft Maintenance Configuration
(1)
Make sure that emergency exit door (referred to as door) is opened as required (Ref. TASK 52-22-00-010-001).
(2)
Make sure that the special precaution procedure for the door damper and emergency operation cylinder are done (Ref. TASK 52-22-00-860-003).
(3)
Make sure that the access platform is in position below the partly opened door.
(4)
Make sure that the door lining is removed (Ref. TASK 25-23-47-000-012) or (Ref. TASK 25-23-47-000-013).
4. Procedure
_________ Subtask 52-22-21-910-052
A. Preparation for Installation
(1)
Make sure that the parts retained from the removed component are clean and in the correct condition.
(2) 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(120)
