• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-26 23:57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

 0.2 mm (0.0078 in.) and 0.6 mm (0.0236 in.).

 (e)
 Tighten the jam nuts (186) and Safety them with the tab washers (187).


 (6) Push up the door handle until it is in the UNLOCKED position. position.
 1EFF : 001-049, 053-099, 101-149, 201-299, 1 52-32-11Page 576 1301-399, 1Aug 01/05 1 1 1CES 1

 **ON A/C 051-052,


 Subtask 52-32-11-820-061-B
 A. Adjustment of the Skin Offset
 (Ref. Fig. 509A/TASK 52-32-11-991-014-C)

 (1)
 Remove the vent door stop from the opened vent door as follows:

 (a)
 Release the tab washers (72) from the jam nuts (73).

 (b)
 Loosen the jam nuts (73) to release the adjustment bolts (74).

 (c)
 Remove the adjustment bolts (74) with the jam nuts (73) and the tab washers (72) from the hinge arms (71).

 (d)
 Remove and discard the tab washers (72).

 

 (2)
 Close the vent door as follows:

 (a)
 Press the roller lever of the interlock mechanism outboard to release the blockage of the locking shaft.

 (b)
 Turn the locking handle up to the locked position and push it into the recess of the handle flap.

 

 (3)
 Measure the skin offset between the external contour of the vent door and the AFT cargo door as follows:


 NOTE : Make sure that the skin offset which must be out of wind is
____ between 0.5 mm (0.0196 in.) and 1.5 mm (0.0590 in.)
 (4) If the skin offset is not correct, adjust the length of the connecting rod (78) as follows:
 (a)
 Cut and remove the lockwire from the locking devices (75).

 (b)
 Loosen the jam nuts (76) to release the turnbuckle (77).

 (c)
 Turn the turnbuckle (77) to set the connection rod (78) to the correct length and to adjust the skin offset correctly.

 (d)
 Tighten the jam nuts (76).

 (e)
 Safety the jam nuts (76) with MISCELLANEOUS (Material No. 19-010) on the locking devices (75).


 1EFF : 051-052, 1 52-32-11Page 577 1 1 Aug 01/05 1 1 1CES 1 1EFF : 051-052, 151-199, 401-499, 1 52-32-11Page 578 1 1 Aug 01/05 1 1 1CES 1


 (5) Adjust the clearance between the vent door stop and the stop of the vent door frame as follows:
 (a) Pull the locking handle out of the recess and turn it down to the unlocked position to open the vent door.
 (b) Install the adjustment bolts (74) with the jam nuts (73) and new tab washers (72) in the hinge arms (71).
 NOTE : Make sure that the tab washers (72) are correctly attached____ on the hinge arms (71).
 (c) Close the vent door again (Refer to Para. A.2).
 (d) Turn the adjustment bolts (74) until the clearance is between 0.2 mm (0.0078 in.) and 0.6 mm (0.0236 in.).
 (e) Tighten the jam nuts (73) correctly.
 (f) Safety the jam nuts (73) with the tab washers (72).
 (6) Push the handle flap in and pull the locking handle out of the recess. Turn the locking handle to the opened position. 
R  **ON A/C 151-199, 401-499,
 Subtask 52-32-11-820-061-A
 A. Adjustent of the Skin Offset 
R  **ON A/C 151-199,
 (Ref. Fig. 509C/TASK 52-32-11-991-014-A) 
R  **ON A/C 401-499, 
R  (Ref. Fig. 509D/TASK 52-32-11-991-014-D)

 

 Adjustment of the Vent Door
 Figure 509C/TASK 52-32-11-991-014-A
 1EFF :  151-199,  1  52-32-11 Page 579 
1  1  Aug 01/05
 1  1
 1CES  1

 

R  Adjustment of the Vent Door 
R  Figure 509D/TASK 52-32-11-991-014-D
 1EFF :  401-499,  1  52-32-11 Page 580 
1  1  Aug 01/05
 1  1
 1CES  1

 

R **ON A/C 151-199, 401-499,
 (1)
 Remove the vent door stop from the opened vent door as follows:

 (a)
 Release the tab washers (187) from the jam nuts (186).

 (b)
 Loosen the jam nuts (186) to release the adjustment bolts (185).

 (c)
 Remove the adjustment bolts (185) with the jam nuts (186) and the tab washers (187) from the hinge arms (188).

 (d)
 Remove and discard the tab washers (187).

 

 (2)
 Close the vent door as follows:

 (a)
 Press the roller lever of the interlock mechanism outboard to release the blockage of the latching shaft.

 (b)
 Move the door handle down to the locked position and push it into the recess of the door structure.
 
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5(41)