• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-26 23:42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

 (1) For the door equipped with the door damper and emergency-operation cylinder, serie P/N FE174 and FE196, connect the guide arms (132) and
 (133) on the door side (Ref. TASK 52-13-12-400-002).
 1EFF : ALL 1 52-13-11Page 452 1 1 Feb 01/04R 1 1 1CES 1


 Guide Arms - Installation Figure 414/TASK 52-13-11-991-022
 1EFF : 1 1R 1CES  ALL  1 11 1 52-13-11 Page 453 Feb 01/04

 

 (2) For the door equipped with door damper and emergency-operation cylinder, serie P/N FE240, connect the guide arms as follows:
 (a)
 Put the door in the up closed position in contact with the seal

 (134) at FR68.

 (b)
 Connect the guide arms (133) and (132) (Ref. TASK 52-13-12-400-002).


 1_ Do a check of the clearance L1 at FR66.
 NOTE : Measure the clearance at door stop level L5.____
 - the clearance L1 must be equal to the difference between the
 flushness D1 measured between the door and the door frame
 forward of the door, and the flushness D2 measured between
 the door and the door frame aft of the door.
 - the maximum clearance L1 must be of 5 mm (0.1968 in.).
 - if necessary, adjust the fittings (130) and (131) on the X
 axis.

 Subtask 52-13-11-420-052
 M. Connection of the Door-Damper and Emergency-Operation Cylinder (Ref. Fig. 402/TASK 52-13-11-991-004)
 (1)
 Put the telescopic rod (31) in position on the eyebolt (26).

 (2)
 Install the spacer (30) and the screw (33) with the lockwasher (32).

 (3)
 Install the washer (29) and the nut (28) and tighten it.


 (4) Install the new cotter pin (27). Subtask 52-13-11-020-052
 N. Removal of the Sling (Ref. Fig. 401/TASK 52-13-11-991-002)
 (1)
 Remove the sling (10) from the hoist fitting.

 (2)
 Remove the hoist fittings (2) from the door and attach them to the sling (10).

 (3)
 Install the blanking plugs (1) in the hoisting point holes.


 1EFF : ALL 1 52-13-11Page 454 1 1 Feb 01/04R 1 1 1CES 1


 (4)
 Install new self adhesive patches (3) on the door at the hoisting points.

 (5)
 If necessary, paint the self adhesive patches to the same color as the adjacent area (Ref. TASK 51-75-12-300-003).


 Subtask 52-13-11-820-057
 P. Check and Adjustment of the Escape Slide
 (Ref. Fig. 405/TASK 52-13-11-991-018, 410/TASK 52-13-11-991-012)

 (1)
 Close the door

 (2)
 Put the emergency control handle in the ARMED position.

 (3)
 Install the RIGGING PIN (98DNSA20206120) on the emergency control hanle (rigging point).

 (a)
 F1 is 0.2 mm (0.0078 in.) to 0.8 mm (0.0314 in.).

 (b)
 F2 is 0.5 mm (0.0196 in.) to 1.0 mm (0.0393 in.).

 

 (4)
 If the clearances F1 and F2 are not in the tolerances, adjust the girt bar fittings as follows:

 (a)
 Remove the RIGGING PIN (98DNSA20206120) from the emergency control handle.

 (b)
 Put the emergency control handle in the DISARMED position.

 (c)
 Open the door and identify the position of the serrations of the girt bar fittings.

 (d)
 Adjust the position of the girt bar fittings on the X axis and the Y axis to get correct clearances F1 and F2.

 (e)
 Tighten the screws (71), (76) on the girt bar fittings (72), (75). (Ref. Fig. 405/TASK 52-13-11-991-018)

 (f)
 Apply SEALANTS (Material No. 09-005) on the heads of the screws (71), (76) and on the periphery of the girt bar fittings (72), (75).

 

 (5)
 Take a dynamometer to measure the load and operate the emergency control handle several times and make sure that the load necessary to operate the handle is not more than 7 daN (15.7366 lbf).


 1EFF : ALL 1 52-13-11Page 455 1 1 Feb 01/04R 1 1 1CES 1


 Subtask 52-13-11-820-062
 Q. Check and Adjustment of the Door Damper and Emergency-Operation Cylinder (Ref. Fig. 415/TASK 52-13-11-991-015)
 (1)
 Put the door in the up closed position, in contact with the frame, with the seal compressed.

 (2)
 Make sure that the clearance K2, between the telescopic rod (41) and the fitting (42) is 1.5 mm (0.0590 in.).


 Subtask 52-13-11-820-058
 R. Check and Adjustment of the Compensation Mechanism
 (1) Do a check and adjustment of the compensation mechanism (Ref. TASK 52-11-00-820-002).
 Subtask 52-13-11-220-050
 
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2(87)