• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-21 08:32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

_
 (22) and (23) of the flexible control-assembly. 3 Loosen the adjust nuts (22) and (23).
_
 4 Turn the adjust nuts (22) and (23) to adjust the cable-travel.

_
 5 Tighten the adjust nuts (22) and (23).

_

 (j)
 Do a check of the adjusted cable-travel and do the steps (a) thru

 (h) again

 (k)
 Safety the adjust nuts (22) and (23) with MISCELLANEOUS (Material No. 19-010) (Ref. TASK 20-11-11-911-001).

 (l)
 Remove the test tool from the flexible control-assembly.

 


 1  Loosen the knurled sleeve-nut fully and remove the two
_
 collets.

 2  Carefully remove the test tool from the related slot of the
_
 flexible control-cable (13).

 3  Put the two collets in position on the test tool, move the
_ knurled sleeve-nut up and install the plug.
R  **ON A/C 151-199, 401-499,
 Subtask 25-62-43-420-054-A
 B. Installation of the Emergency Escape-Slide Release-Mechanism
 WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK
_______ AREA WHEN YOU USE SPECIAL MATERIALS. IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH OR IN YOUR EYES : -FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 AND 15 MINUTES. -GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS. DO NOT BREATHE THE FUMES FROM THE MATERIAL. DO NOT SMOKE WHEN YOU USE THE MATERIAL. DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF HEAT. THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE AND SKIN IRRITANTS.
 WARNING : OBEY THE MANUFACTURER'S INSTRUCTIONS WHEN YOU USE THIS/THESE
_______ MATERIAL/S. USE PROTECTIVE CLOTHING, RUBBER GLOVES, GOGGLES AND A MASK.
 (Ref. Fig. 404A/TASK 25-62-43-991-003-A, 405A/TASK 25-62-43-991-004-A, 406A/TASK 25-62-43-991-005-A, 407A/TASK 25-62-43-991-006-A, 408A/TASK 25-62-43-991-007-A, 409A/TASK 25-62-43-991-008-A)
R  EFF : 001-049, 051-099, 101-149, 151-199, 25-62-43Page 480 201-299, 401-499, Aug 01/05
 CES


 (1) Install the release-mechanism camshaft assembly: (Ref. Fig. 408A/TASK 25-62-43-991-007-A)
 (a) Assemble the camshaft assembly: NOTE : You will find punch marks on the camshaft (135), on the
____ shaft (130) and on the lever (142) to make the assembly easier.
 1 Put the washers (133) and (136) in position on the shaft
_
 (135).

 2 Put the lever (132) and (137) together with the bush (134) in
_
 position on the shaft (135).

 3 Install the bolt (131) and the nut (138).
_
 4 Put the washers (139) in position on the shaft (135).

_
 5 Apply COMMON GREASE (Material No. 04-004) to the torsion

_
 spring (140).

 6 Put the torsion spring (140) in position on the camshaft (135)
_ 7 Make sure that the spring-end of the torsion spring (140) is
_ engaged in the related locating-hole of the lever (137).
 8 Install the lever (142):
_ WARNING : BE CAREFUL WHEN YOU INSTALL THE LEVER ON THE
_______ CAMSHAFT AND CONNECT IT TO THE TORSION-SPRING. THE TENSION OF THE TORSION-SPRING CAN CAUSE SUDDEN MOVEMENT OF THE LEVER. THIS CAN CAUSE INJURY TO PERSONNEL AND/OR DAMAGE TO EQUIPMENT.
 a Apply COMMON GREASE (Material No. 04-004) to the splines of
_ the camshaft (135) and the lever (142).
 b Apply a force on the spring-end of the torsion spring (140)
_ and adjust a pre-tension to between 0.875 and 1.049 m.daN
 (77.43 and 92.83 lbf.in). c Install the lever (142) on the camshaft (135).
_


 Adjustments Figure 409A/TASK 25-62-43-991-008-A14 (SHEET 1) 
R  EFF :  151-199, 401-499,  25-62-43 Page 482 Aug 01/05
 CES 

 

 Adjustments Figure 409A/TASK 25-62-43-991-008-A24 (SHEET 2) 
R  EFF :  151-199, 401-499,  25-62-43 Page 483 Aug 01/05
 CES 

 

 Adjustments Figure 409A/TASK 25-62-43-991-008-A34 (SHEET 3) 
R  EFF :  151-199, 401-499,  25-62-43 Page 484 Aug 01/05
 CES 

 

 Adjustments Figure 409A/TASK 25-62-43-991-008-A44 (SHEET 4) 
R  EFF :  151-199, 401-499,  25-62-43 Page 485 Aug 01/05
 CES 

 

 NOTE : The punch mark "G" on the lever (142) must align
____ with the punch mark "H" on the camshaft (135).
 d Make sure that the spring-end of the torsion spring (140)
_ is engaged in the related locating-hole of the lever (142).
 e If the pre-tension of the torsion spring (140) is not in
_ the limits to between 0.875 and 1.049 m.daN (77.43 and
 
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 EQUIPMENT/FURNISHINGS 设备4(104)