• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-26 23:38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

 (b)
 For the right door: 222AW, 222BW, 222CW, 222EW, 222FW, 222GW, 222HW, 222JW, 222KW 222LW, 222MW, 222NW, 222PW, 222QW, 232AW, 232CW, 232BW. (Ref. TASK 25-23-45-000-002)

 


 Subtask 52-11-11-420-054
 G. Installation of the Sling
 (Ref. Fig. 401/TASK 52-11-11-991-001)

 (1)
 Remove the self-adhesive patches (3) from the hoisting points. Discard the patches.

 (2)
 Remove the blanking plugs (1) from the door hoisting points.

 (3)
 Remove the hoist fittings (2) from the tool and install it on the hoisting points of the door

 (4)
 Install the SLING - PASSENGER DOOR (98A52108004001) (10) on the hoist fittings (2).


 (5) Carefully move the door into the installation position. Subtask 52-11-11-420-058
 H. Loosening of the Girt Bar Fittings
 (Ref. Fig. 405/TASK 52-11-11-991-015)

 (1) Loosen the screws (91) and (96) from the girt bar fittings (92) and (95).
 1EFF : ALL 1 52-11-11Page 418 1 1 Feb 01/04R 1 1 1CES 1


 Girt Bar Fitting Figure 405/TASK 52-11-11-991-015
 1EFF : 1 1R 1CES  ALL  1 11 1 52-11-11 Page 419 May 01/98

 

 (2) Remove the sealant located on the periphery of the girt bar fittings (92), (95) and on the heads of the screws (91), (96) use a CLEANING AGENTS (Material No. 11-004) with a MISCELLANEOUS (Material No. 19-003).
 (3)
 Make sure that the girt bar fittings can move.
 Subtask 52-11-11-020-052


 J.
 Removal of the Washers of the Upper Guide Fittings
 **ON A/C 001-049, 051-056,

 

 (Ref. Fig. 406/TASK 52-11-11-991-011) R **ON A/C 057-099, 101-149, 151-199, 201-299, 301-399, 401-499,
 (Ref. Fig. 406A/TASK 52-11-11-991-011-A)
 **ON A/C ALL

 (1)
 Remove the nuts (104), the bolts (105) and the washers (103) from the upper guide fittings (102).

 (2)
 Install the bolts (105) and the nuts (104) and retain the washers (103).


 **ON A/C 001-002,
 Subtask 52-11-11-420-057
 K. Installation of the Ballast Weight
 (1) Install the BALLAST WEIGHT - PASSENGER CREW DOOR (98D52103501000) (Ref. TASK 52-10-00-480-001).
 NOTE : If no ballast weight is available, it is permitted to use the
____ escape slide on the door during the adjustment (as an alternative to BALLAST WEIGHT - PASSENGER CREW DOOR (98D52103501000)). If you do this, make sure that the escape slide lets you have access for the adjustment procedure.
 1EFF : ALL 1 52-11-11Page 420 1 1 Aug 01/05 1 1 1CES 1


 Guide Fittings - Clearance and Adjustment
 Figure 406/TASK 52-11-11-991-011

R 1EFF : 001-049, 051-056, 1 52-11-11Page 421 1 1 May 01/05 1 1 1CES 1


 Guide Fittings - Clearance and Adjustment Figure 406A/TASK 52-11-11-991-011-A
R 1EFF : 057-099, 101-149, 151-199, 201-299, 1 52-11-11Page 422 1301-399, 401-499, 1Aug 01/05 1 1 1CES 1R **ON A/C 003-049, 051-099, 101-149, 151-199, 201-299, 301-399, 401-499,


 Subtask 52-11-11-420-057-A
 K. Installation of the Ballast Weight
 (1) Install the BALLAST WEIGHT - PASSENGER CREW DOOR (98D52103501000) (Ref. TASK 52-10-00-480-001).
 NOTE : If no ballast weight is available, it is permitted to use the
____ escape slide/raft on the door during the adjustment (as an alternative to BALLAST WEIGHT - PASSENGER CREW DOOR (98D52103501000)). If you do this, make sure that the escape slide/raft lets you have access for the adjustment procedure.
 **ON A/C ALL
 4. Procedure
_________
 Subtask 52-11-11-420-055

 A. Temporary Installation of the Door on the Door Support Arm
 (Ref. Fig. 403/TASK 52-11-11-991-004)

 (1)
 Put the upper connection link (61) in position.

 (2)
 Install the washers (64) on each side of the yoke (65).

 (3)
 Install the bolt (63) with the washer (62).

 (4)
 Install the nut (70) with the washer (71).

 (5)
 Put the lower connection link (61) in position.

 (6)
 Install the washers (64) on each side of the yoke (65).

 (7)
 Install the bolt (63) with the washer (62).

 (8)
 Install the nut (70) with the washer (71)


 1EFF : ALL 1 52-11-11Page 423 1 1 Aug 01/05 1 1 1CES 1 Subtask 52-11-11-420-050


 B. Installation of the Door
 (Ref. Fig. 403/TASK 52-11-11-991-004)

 **ON A/C 001-049, 051-056,
 (Ref. Fig. 406/TASK 52-11-11-991-011) R **ON A/C 057-099, 101-149, 151-199, 201-299, 301-399, 401-499,
 
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1(134)