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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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__________________
 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 -------------------------------------------------------------------------------
50 cotter pin 52-22-21 11 -080 57 lockwasher 52-22-21 11 -160 65 cotter pin 52-22-21 11 -270
 1EFF : 301-399, 1 52-22-22Page 415 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 52-22-22-991-002 Fig. 402
 3. Job Set-up
__________
 Subtask 52-22-22-865-054
 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 416 1 1 May 01/04 1 1 1CES 1 Subtask 52-22-22-860-051


 B. Aircraft Maintenance Configuration
 (1)
 Make sure that the applicable emergency exit door (referred to as door) is opened as required (Ref. TASK 52-22-00-010-001).

 (2)
 Make sure that the access platform is in position below the partly opened door.

 (3)
 Make sure that the special precaution on the door damper and emergency operation cylinder is completed (Ref. TASK 52-22-00-860-003).

 (4)
 Make sure that the door linings are removed (Ref. TASK 25-23-47-000-012) and (Ref. TASK 25-23-47-000-013).


 4. Procedure
_________ Subtask 52-22-22-910-051
 A. Preparation for Installation
 (1)
 Make sure that the parts retained from the removed component are clean and in the correct condition.

 (2)
 Do an inspection of the component interface and/or the adjacent area.

 (3)
 Make sure that the bushes (69) and (70) are in the correct condition.

 (4)
 Apply COMMON GREASE (Material No. 04-004) to all surfaces of parts which move.


 Subtask 52-22-22-420-051
 B. Installation of the Transmission Shaft
 (Ref. Fig. 402/TASK 52-22-22-991-002)

 (1) Install the transmission shaft (60) and the shaft levers (59) and
 (61)
 as follows:

 (a)
 Partly insert the transmission shaft (60) into the related structure bearing.

 (b)
 Assemble the shaft levers (59) and (61) on their splines of the transmission shaft (60) and put the washers (56) and (55) in position.


 1EFF : 301-399, 1 52-22-22Page 417 1 1 May 01/04 1 1 1CES 1


 (c)
 Fully insert the transmission shaft (60) into the opposite structure bearing.
 
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