• 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

121VU HYDRAULIC/HYD POWER/Y 3803GX N30 122VU DOORS/CARGO 1MJ T12 123VU Y HYD/ELEC/PUMP 3802GX AB06 123VU Y HYD/ELEC/ELEC PUMP/NORM 3801GX AB03
 4. Procedure
_________ R **ON A/C 001-049, 053-099, 101-149, 151-199, 201-299, 301-399, 401-499,
 (Ref. Fig. 408/TASK 52-32-21-991-008)
 **ON A/C 051-052,

 (Ref. Fig. 408A/TASK 52-32-21-991-008-A) R **ON A/C 001-049, 053-099, 101-149, 151-199, 201-299, 301-399, 401-499,
 Subtask 52-32-21-910-054-A
 A. Preparation for Installation
 (1)
 Make sure that the parts retained from the removed component are clean and in the correct condition.

 (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 COMMON GREASE (Material No. 04-004) to the sliding surfaces of the bushes (261),(264) and the and (270).


R 1EFF : ALL 1 52-32-21Page A400 1 1 Aug 01/05 1 1 1CES 1


 (5) Apply a layer of COMMON GREASE (Material No. 04-004) to the pins (271),(266), to the spring pin (268) and to the shaft of the bolts
 (265) and (268).
 -Make sure that the threads of the bolts (1),(18) remain free of grease.
 **ON A/C 051-052,
 Subtask 52-32-21-910-054
 A. Preparation for Installation
 (1)
 Make sure that the parts retained from the removed component are clean and in the correct condition.

 (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 COMMON GREASE (Material No. 04-004) to the sliding surfaces of the bushes (4),(14) and the flanged bushes (3),(6) and (13).

 (5)
 Apply a layer of COMMON GREASE (Material No. 04-004) to the pins (19),(2), to the spring pin (15) and to the shaft of the bolts (1),(18).


 -Make sure that the threads of the bolts (1),(18) remain free of grease.
 **ON A/C 001-049, 053-099, 101-149, 201-299, 301-399,
 Subtask 52-32-21-560-053-A
 B. Preparation for Replacement Component
 (1) Replace the tab washer (274) of the stop assy (277) as follows:
 (a)
 Bend the tab washer (274) to release the lock nut (275).

 (b)
 Remove the stop screw (276) together with the lock nut (275) and the tab washer (274) from the interlock lever (269).

 (c)
 Install the new tab washer (274) on the stop screw (276).


 1EFF : ALL 1 52-32-21Page A401 1 1 Aug 01/05R 1 1 1CES 1


 (d) Install the stop screw (276) together with the lock nut (275) and the new tab washer (274) in the interlock lever (269).
 Subtask 52-32-21-420-056-A
 C. Installation of the Interlock Mechanism
 (1)
 Install the spring sleeve (272) on the interlock fitting as follows:

 (a)
 Put the spring sleeve (272) in the installation position and attach it with the pin (266) and the related spacers (264).

 (b)
 Safety the pin (266) with the washer (256) and the new cotter pin (257).

 (c)
 Move the spring 273) over the spring sleeve (272).

 

 (2)
 Assemble the spring pin (272) into the spring sleeve (272).

 (3)
 Connect the interlock lever (269) with the interlock fitting as follows:

 (a)
 Put the interlock lever (269) and the sleeve (270) in position and attach them with the bolt (267), the washers (255) and the nut (254).

 (b)
 Tighten the nut (254) and safety it with the new cotter pin (253).

 

 (4)
 Connect the roller lever (263) to the interlock fitting as follows:

 (a)
 Put the roller lever (263) in position and install the bush (261) into the interlock fitting.

 (b)
 Install the bolt (265), the washers (260) and the nut (259) on the interlock fitting.

 (c)
 Tighten the nut (259) and safety it with the new cotter pin (258).

 

 (5)
 Install the pin (271) in the interlock fitting and safety it with the washer (251) and the new cotter pin (252).


R 1EFF : 001-049, 053-099, 101-149, 201-299, 1 52-32-21Page A402 1301-399, 1Aug 01/05 1 1 1CES 1

 **ON A/C 051-052,


 Subtask 52-32-21-560-053
 B. Preparation for Replacement Component
 (1)
 Replace the tab washer (28) of the stop (25) as follows:

 (a)
 Bend the tab washer (28) to release the lock nut (27).

 (b)
 Remove the adjusting screw (26) together with the lock nut (27) and the tab washer (28) from the interlock lever (16).
 
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(99)