(c) Disconnect the spring element (192) from the lever (190) as follows:
1 Remove and discard the cotter pin (189) from the nut (188).
_
2 Remove the nut (188), the washers (185) and the bolt (184)
_ from the lever (190).
3 Remove the spring element (192) from the lever (190).
_
(d)
Move the locking shaft (183) laterally until the end of the joint assembly (163) comes free from the bulk door structure.
(e)
Remove the flange (164) and the flange bearing (151) from the joint assembly (163).
(f)
Remove the nuts (162), the washers (160) and the bolts (161) to remove the locking washer (159) from the joint assembly (163).
(g)
Pull the joint assembly (163) from the locking shaft (183) and remove it from the structure of the Bulk cargo door.
(3) Disassemble the main lever (122) from the locking shaft (183) as follows:
(a)
Remove the nut (176), the washers (175) and the bolt (174) from the main lever (122).
(b)
Move the main lever (122) from the tooth of the locking shaft (183).
R 1EFF : 004-049, 055-099, 101-149, 221-221, 1 52-33-21Page 422 1224-224, 228-228, 1May 01/05 1 1 1CES 1
(4)
Disassemble the lever (190) from the locking shaft as follows:
(a)
Remove the nut (191), the washers (187) and the bolt (186) from the lever (190).
(b)
Remove the lever (190) from the tooth of the locking shaft (183).
(5)
Disassemble the limit stop (173) from the locking shaft (183) as follows:
(a)
Remove the nut (182), the washers (172) and the bolt (171) from the limit stop (173).
(b)
Remove the limit stop (173) from the tooth of the locking shaft (183).
(6)
Move the locking shaft (183) through the flange bearings (179) and
(196) and remove it from the structure of the Bulk cargo door.
(7)
Remove the flange bearings (179) and (196) from the Bulk cargo door as follows:
(a)
Remove the nuts (177) and (197), the washers (178) and (194) and the bolts (181)and (193) from the flange bearings (179) and (196).
(b)
Carefully disconnect the flange bearings (179) and (196) from the door frame (180) and (195).
Subtask 52-33-21-020-052-A
C. Removal of the Latch Assembly
(Ref. Fig. 403A/TASK 52-33-21-991-003-A)
(1)
Remove the hook arrester (224) from the crossbeam of FR61 as follows:
(a)
Remove the nut (226) and the bolt (225) and disconnect the hook arrester (224) from the crossbeam (220).
(b)
If necessary, remove the nut (223), the bolt (221) and the roller
(222) from the hook arrester (224).
(2)
Remove the locking hook (209) from the spring element (192) as follows:
(a) Remove and discard the cotter pin (216) from the nut (215).
R 1EFF : 004-049, 055-099, 101-149, 221-221, 1 52-33-21Page 423 1224-224, 228-228, 1May 01/05 1 1 1CES 1
Latch Assembly with Hook Arrester Figure 403A/TASK 52-33-21-991-003-A
R 1EFF : 004-049, 055-099, 101-149, 221-221, 1 52-33-21Page 424 1224-224, 228-228, 1May 01/05 1 1 1CES 1
(b)
Remove the nut (215), the washers (212) and the bolt (211) from the locking hook (209).
(c)
Disconnect the locking hook (209) from the spring element (192).
(d)
if necessary, remove the bushes (213) and (214) from the fork-end of the locking hook (209).
(3)
Remove the locking hook (209) as follows:
(a)
Remove and discard the cotter pin (204) from the nut (205).
(b)
Remove the nut (205) from the hook axle (208).
(c)
Remove the nuts (201), the washers (202) and the bolts (203) from the hook bracket (206).
(d)
Disconnect the hook bracket (206) from the door fitting (207).
(e)
Remove the hook axle (208) together with the locking hook (209) from the door fitting (210).
(f)
Disassemble the hook axle (208) from the locking hook (209).
(4)
Remove the spring element (192) from the lever (190) as follows:
(a) 中國航空網 m.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：A320飛機維護手冊 AMM DOORS 艙門6(61)
