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时间:2011-03-26 23:52来源:蓝天飞行翻译 作者:admin
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 (c)
 Remove the eye-end of the link rod (15) from the fork-end of the intermediate shaft lever (21).

 (d)
 If necssary, remove the bush (20) from the intermediate shaft lever (21).


 (5)
 Remove the nuts (43), the washers (44), the screws (9) and the indicator plate (10) from the door structure.

 (6)
 Remove the bolts (8), the washers (7) and the arm/disarm unit (11) from the door structure.

 (7)
 If necessary, remove the spring unit (33) from the arm/disarm unit

 (11)
 as follows:

 (a)
 Remove and discard the cotter pin (38) from the pin (36).

 (b)
 Remove the washer (37) and the pin (36) and remove the spring unit (33) from the lever of the arm/disarm unit (11).

 

 (8)
 If necessary, remove the link rod (15) from the arm/disarm unit (11) as follows:

 (a)
 Remove and discard the cotter pin (13) from the nut (12).

 (b)
 Remove the nut (12), the washers (14), the bush (18) and the bolt (16).

 (c)
 Remove the fork-end of the link rod (15) from the lever of the arm/disarm unit (11).

 (d)
 If necessary, remove the bush (17) from the link rod (15).

 

 (9)
 Remove the PIN - SAFETY SLIDE (98A52107632000) from the arm/disarm unit (11) only when you replace the arm/disarm unit (11).


 1EFF : 301-399, 1 52-22-22Page 405 1 1 May 01/04 1 1 1CES 1 TASK 52-22-22-400-001


 Installation of the Arm/Disarm Unit
 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.) 98A52107632000 1 PIN - SAFETY SLIDE
 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 -------------------------------------------------------------------------------
4 cotter pin 52-22-22 03 -100 13 cotter pin 52-22-22 04 -100 31 cotter pin 52-22-22 04 -100 38 cotter pin 52-22-22 04 -100 41 cotter pin 52-22-22 03 -100
 1EFF : 301-399, 1 52-22-22Page 406 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.
 25-23-47-400-012  Installation of the Door Linings of the LH FWD Emergency Exit Door, zone 231
 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
 52-22-00-720-001  Check of Door Unlocking from Inside/Outside in Armed Position and of Slide Release Mechanism Arming/Disarming, Functional Check ofSlide Cable Movement
 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 52-22-22-991-001 Fig. 401
 3. Job Set-up
__________
 Subtask 52-22-22-865-051
 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 52-22-22Page 407 1 1 May 01/04 1 1 1CES 1 Subtask 52-22-22-860-050


 B. Aircraft Maintenance Configuration
 
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