• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-25 17:53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

 (k)
 Remove the GUIDE CONE (J47554).

 (l)
 Install the ring (5), align the rigging bores with the pin (1).

 (m)
 Install the bolt (6), the washer (2) and the nut (3). TORQUE the nut (3) to between 1.7 and 2 m.daN (12.53 and 14.74 lbf.ft) and safety with the new cotter pin (4).


 (4)
 Install the lockstay assy (Ref. TASK 32-21-17-400-001).

 (5)
 Apply a layer of SEALANTS (Material No. 09-001) in the zones E.


 1EFF : ALL 1 32-21-16Page 417 1 1 Aug 01/05R 1 1 1CES 1


 Subtask 32-21-16-820-055
 C. Adjust the positions of the attachment roller as follows:
 (1)
 Make sure that the SAFETY PIN - NLG DOOR (98D32203502000) and the GROUND LOCK SLEEVE (460005835) are in position.

 (2)
 Make sure that the fork end (40) is in the correct position and that the bolt (35) is lightly tightened.


 NOTE : If possible, measure the dimension K on the old lockstay assy
____ and adjust the new lockstay to the same dimension with: shim (42), shim (43), shim (44), shim (45), shim (46) and shim (47).
 (3)
 Retract the landing gear (Ref. TASK 32-30-00-867-001).

 (4)
 On the left side, remove the cotter pins (60) and (64), the nuts (61) and (65) and the washers (62) and (66).

 (5)
 Remove the bolts (71) and (68), remove the rod (63).

 (6)
 Remove the SAFETY PIN - NLG DOOR (98D32203502000) from the left door (69). Manually close the left door (69) and put against the front stop (70).

 (7)
 Measure the clearance J3 and write it.
 (Ref. Fig. 404/TASK 32-21-16-991-006)


 (8)
 Release the left door (69) and install the SAFETY PIN - NLG DOOR (98D32203502000).

 (9)
 Measure the clearance J4 and write it.


 (10)
 Measure the clearance J1 and write it

 (11)
 Measure the clearance J2 and write it.

 (12)
 Extend the landing gear (Ref. TASK 32-30-00-867-002) NOTE : To help adjustment of the clearances J1 and J2, make a note of

____ the location of the support (48) on the lockstay.

 (13)
 Remove the cotter pin (37), the nut (38), the washer (39), the pin (30), the washer (31), the roller (33) and the washers (32).


 1EFF : ALL 1 32-21-16Page 418 1 1 Aug 01/05R 1 1 1CES 1


 (14)
 If necessary:

 -cut and discard the lockwire from the bolt (35),
 -release the tabs of the lock plate (34).

 (15)
 Remove the bolt (35), the lock plate (34) and the washer (36). Remove the fork end (40) and the serrated plate (41).

 (16)
 Choose between the six shim: shim (42), shim (43), shim (44), shim (45), shim (46), shim (47) to adjust the clearance K and get the clearances J3 = 20 mm (0.7874 in.) and J4 = 74 mm (2.9133 in.) min.

 (17)
 Apply some SPECIAL MATERIALS (Material No. 05-047) on the chosen shims and install them on the support (48).


 NOTE : Make sure that the stud (49) is installed.
____
 (18)
 Install the serrated plate (41) on the fork end (40).

 (19)
 Install the fork end (40) and the serrated plate.

 (20)
 Apply a thin layer of SPECIAL MATERIALS (Material No. 05-047) to the threaded and unthreaded part of the bolt (35) .

 (21)
 Install the washer (36), the new lock plate (34) and the bolt (35).

 (22)
 Adjust the clearances J1 and J2. NOTE : Move the support (48) on the drag strut assembly to get the

____
 adjustment


 (23)
 TORQUE the bolt (35) to between 3.3 and 3.9 m.daN (24.33 and 28.76 lbf.ft).

 (24)
 Install the pin (30), the washers (31), (32) and the roller (33). Install the washer (39) and the nut (38). TORQUE the nut (38) to between 1.7 and 2 m.daN (12.53 and 14.74 lbf.ft).

 (25)
 Retract the landing gear (Ref. TASK 32-30-00-867-001).

 (26)
 Measure the clearances J1,J2,J3,J4 and make sure that they are in the tolerance .


 NOTE : If the clearances are not in the tolerance, do the adjustment
____
 again.

 (27) Extend the landing gear (Ref. TASK 32-30-00-867-002).
 1EFF : ALL 1 32-21-16Page 419 1 1 Aug 01/05R 1 1 1CES 1


 (28)
 Safety the bolt (35) with the tabs of the lock plate (34) and with MISCELLANEOUS (Material No. 19-010).

 (29)
 Safety the nut (38) with the new cotter pin (37).

 (30)
 Install the rod (63), the bolt (71), the washer (62) and the nut (61).
 
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 LANDING GEAR 起落架3(95)