• 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

 -------------------------------------------------------------------------------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
 Subtask 52-11-22-110-050
 C. Cleaning
 WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL
_______ MATERIALS ONLY WITH A GOOD SUPPLY OF AIR. OBEY THE MANUFACTURERS INSTRUCTIONS. PUT ON PROTECTIVE CLOTHING. DO NOT GET THEM IN YOUR MOUTH. DO NOT SMOKE. DO NOT BREATHE THE GAS. THESE MATERIALS ARE POISONOUS, FLAMMABLE AND SKIN IRRITANT. GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED.
 WARNING : OBEY THE MANUFACTURER'S INSTRUCTIONS WHEN YOU USE THE SPECIAL
_______
 MATERIAL.
 THIS MATERIAL IS DANGEROUS.

 (1)
 Clean the component interface and/or the adjacent area.

 (2)
 Clean all the other components with CLEANING AGENTS (Material No. 11-004) and MISCELLANEOUS (Material No. 19-003).


 1EFF : ALL 1 52-11-22Page 425 1 1 May 01/05R 1 1 1CES 1


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

 (4)
 Make sure that the parts retained from the removed component are clean and in the correct condition. (Ref. TASK 52-11-22-220-001)


 4. Procedure
_________ Subtask 52-11-22-420-050
 A. Installation of the Girt Bar Control Shaft
 (Ref. Fig. 407/TASK 52-11-22-991-006)

 (1)
 Put the bellcrank (155) and the spacer (159) in position.

 (2)
 Install the shaft (167).

 (3)
 Install the taper pins (154), (160) with COMMON GREASE (Material No. 04-004).

 (4)
 Install the washers (156), (161), the nuts (157), (158) and tighten them.

 (5)
 Install the levers (145), (164) on the shaft (167).

 (6)
 Install the taper pins (144), (165) with COMMON GREASE (Material No. 04-004).

 (7)
 Install the washers (147), (163), the nuts (146), (162) and tighten them.

 (8)
 Put the flexible control (152) in position.

 (9)
 Install the washer (151), the bolt (153), the washer (150) and the nut (148).


 (10) TORQUE the nut (148) to between 0.3 and 0.35 m.daN (26.54 and 30.97 lbf.in).
 NOTE : If you install a new bolt (153) drill a hole of 1.9 mm (0.0748
____
 in.).

 (11)
 Install the cotter pin (149).

 (12)
 Install the telescopic forks (143), the bolts (140), the nuts (142).

 (13)
 TORQUE the nuts (142) to between 0.3 and 0.35 m.daN (26.54 and 30.97 lbf.in).


 1EFF : ALL 1 52-11-22Page 426 1 1 May 01/05R 1 1 1CES 1


 Subtask 52-11-22-420-051
 B. Installation of the Flexible Control Assembly (Ref. Fig. 405/TASK 52-11-22-991-004, 406/TASK 52-11-22-991-010)
 (1)
 Remove the grease nipple (99) from the new flexible control (108).

 (2)
 Assembly of the flexible control

 (a)
 Install the nut (109) on the flexible control (108).

 (b)
 Install the washer (110), the fitting (111), the washer (112) on the flexible control (108).

 (c)
 Install the nut (113) on the flexible control (108).

 (d)
 Put the nut (109) in position so that you get the dimension X3.

 (e)
 TORQUE the nuts (109), (113) to 1.2 m.daN (106.19 lbf.in).

 (f)
 Install the seal nut (114).

 


R  (g) TORQUE the seal nut (114) to between 0.35 and 0.45 m.daN (30.97 and 39.82 lbf.in).
 (h)
 Install the nut (115), the lockwasher (116) and the eye end assembly (117).

 (i)
 Put the nut (115) in position so that you get the dimension X4.

 (j)
 TORQUE the nut (115) to between 0.6 and 0.7 m.daN (53.09 and

 61.94 lbf.in).

 (k)
 Safety the nut (115) with the lockwasher (116).

 (l)
 Install the nut (107) on the flexible control (108).

 (m)
 Install the washer (104).


 (3) Installation of the flexible control.
 (a)
 Before installation, slightly bend the flexible control (115) to the final shape.

 (b)
 Push the flexible control (108) through the hole at the bottom of the door.


 1EFF : ALL 1 52-11-22Page 427 1 1 Nov 01/03 1 1 1CES 1


 (c)
 Install the grease nipple (99) on the new flexible control (108).
 
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(22)