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时间:2011-03-26 23:52来源:蓝天飞行翻译 作者:admin
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

 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 52-22-00-820-002 Adjustment of the Emergency Exit Door 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 52-22-31-991-001 Fig. 401 52-22-31-991-006 Fig. 402
 3. Job Set-up
__________
 Subtask 52-22-31-860-050
 A. 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 special precaution on the door damper and emergency operation cylinder is completed (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 applicable door linnings are removed as required (Ref. TASK 25-23-47-000-012) or (Ref. TASK 25-23-47-000-013).


 1EFF : 301-399, 1 52-22-31Page 406 1 1 May 01/04 1 1 1CES 1


 (5) Make sure that the insulation mat is removed from the inner side of the door.
 4. Procedure
_________ Subtask 52-22-31-910-050
 A. Preparation for Installation
 (Ref. Fig. 401/TASK 52-22-31-991-001)

 (1) Remove the old sealant from the door frame , the stop fittings (5), the guide rollers (8) and the roller guides (11).
 NOTE : Use a wooden or plastic scraper.
____
 (2)
 Clean the component interface and/or the adjacent area.

 (3)
 Do an inspection of the component interface and/or the adjacent area.

 (4)
 Apply a layer of SEALANTS (Material No. 09-016) to the mating surface of the stop fittings (5), the guide rollers (8) and the roller guides (11).

 (5)
 Apply a layer of SEALANTS (Material No. 09-016) to the mating surface of the bolts (1), (7) and (10) and the nuts (2), (9) and (12).


 Subtask 52-22-31-420-050
 B. Installation of the Adjustable Stops and the Roller Guides
 (Ref. Fig. 401/TASK 52-22-31-991-001)

 (1) Install the adjustable stops (5) as follows:
 (a)
 Put the stop fitting (5) in position at the door member and attach it with the bolts (1) and the nuts (2).

 (b)
 Apply SEALANTS (Material No. 09-013) around the edges of the stop fitting (5).

 (c)
 If removed, install the stop bolt (6), the new lock plate (4) and the nut (3).


 NOTE : Safety the nut (3) when the skin offset between the door
____ and fuselage is correct adjusted.
 1EFF : 301-399, 1 52-22-31Page 407 1 1 May 01/04 1 1 1CES 1


 (2)
 Install the guide rollers (8) as follows:

 (a)
 Put the guide roller (8) in position at the door member and attach it with the bolts (7) and the nuts (9).

 (b)
 Apply SEALANTS (Material No. 09-013) around the edges of the guide roller (8).

 

 (3)
 Install the roller guides (11) as follows:

 (a)
 Put the roller guide (11) in position at the door member and attach it with the bolts (10) and the nuts (12).

 (b)
 Apply SEALANTS (Material No. 09-013) around the edges of the roller guide (11).

 


 Subtask 52-22-31-820-050
 C. Adjustment Procedure
 (1) Pre-adjust the adjustable stops as follows:
 (Ref. Fig. 402/TASK 52-22-31-991-006)

 (a) Measure the distance "A" between the head of the stop bolts (6) and the surface of the stop fitting (5).
 NOTE : The distance "A" must be between the 4.0 mm (0.1574 in.)
____
 and 6.0 mm (0.2362 in.).

 (b) If the distance "A" is out of tolerance, loosen the nut (3) and turn the stop bolt (6) as required.
 (2)
 Make sure that the skin offset between the fuselage and the door is correctly adjusted (Ref. TASK 52-22-00-820-002).

 (3)
 TORQUE the nut (3) to between 2.0 m.daN (14.7492 lbf.ft) and 2.2 m.daN (16.2241 lbf.ft).


 
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