(145) to connect the barrel lock (141) with the tooth shaft (149).
(7)
Make sure that the locking shaft (183) is in the correct postion for the attachment of the subsequent componenents:
(a) Connect the spring element (192) to the lever (190) as follows:
1_ Put the spring element (192) to the lever (190) and attach it
with the bolt (184), the washers (185) and the nut (188).
2_ Tighten the nut (188) and safety it with the new cotter pin
(189).
1EFF : 004-049, 055-099, 101-149, 221-221, 1 52-33-21Page 441 1224-224, 228-228, 1May 01/05 1 1 1CES 1 (b) Connect the spring element (125) to the main lever (122) as follows:
1_ Put the spring element (125) to the main lever (122) and
attach it with the bolt(123), the washers (124) and the nut
(126).
2_ Tighten the nut (126) and safety it the new cotter pin (127).
(8) Safety the locking shaft (183) as follows:
(a)
Install the bolts (158), the washers (157) and the nuts (156) to connect the flange (164) with the joint assembly (163).
(b)
Install the bolts (161), the washers (160) and the nuts (162) to attach the locking washer (159) to the joint assembly (163).
Subtask 52-33-21-420-052-A
D. Installation of the Latch Assembly (Ref. Fig. 403A/TASK 52-33-21-991-003-A)
(1)
Install the hook arrester (224) on the crossbeam (220) as follows:
(a)
If removed, install the roller (222) on the hook arrester (224) and attach it with the bolt (221) and the nut (223).
(b)
Install the hook arrester (224) on the crossbeam (220) and attach it with the bolts (225) and the nuts (226).
(2)
Install the locking hook (209) as follows:
(a)
Put the locking hook (209) in position and move the hook axle
(208) into the door fitting (207) so that both parts engages.
(b)
Assemble the hook axle (208) into the door fitting (210).
(c)
Put the hook bracket (206) in position and attach it with the bolts (203), the washer (202) and the nut (201).
(d)
Install the nut (205) on the hook axle and safety it with the new cotter pin (204).
1EFF : 004-049, 055-099, 101-149, 221-221, 1 52-33-21Page 442 1224-224, 228-228, 1May 01/05 1 1 1CES 1
(e) Connect the spring element (192) to the locking hook (209) as follows:
1 If removed, install the bushes (213) and (214) into the
_ fork-end of the locking hook (209).
2 Put the spring element (192) to the locking hook (209) and
_ attach it with the bolt (211), the washers (212) and the nut (215).
3 Tighten the nut (215) and safety it the new cotter pin (216).
_
(3) Connect the spring element (192) to the lever (190) as follows:
(a)
Put the spring element (192) in position to the lever (190) and attach it with the bolt (184), the washers (185) and the nut (188).
(b)
Tighten the nut (188) and safety it with the new cotter pin (189).
R **ON A/C 001-049, 051-099, 101-149, 221-221, 224-224, 228-228,
5. Close-up
________
Subtask 52-33-21-820-050
A. Do an adjustment of the applicable components to get a satisfactory locking mechanism (Ref. TASK 52-33-11-820-002).
Subtask 52-33-21-910-051
B. Protective Treatment
(1)
Apply a bead of SEALANTS (Material No. 09-016) in the corners between all sealed components and the structure and let it dry.
(2)
Apply STRUCTURE PAINTS (Material No. 16-003) to the sealant and let it dry.
1EFF : 001-049, 051-099, 101-149, 221-221, 1 52-33-21Page 443 1224-224, 228-228, 1May 01/05 1 1 1CES 1R **ON A/C 001-049, 051-099, 101-105,
Subtask 52-33-21-410-050
C. Close Access
(1)
Make sure that the support device is removed.
(2)
Close the Bulk door (Ref. TASK 52-30-00-860-008).
(3)
Make sure that the work area is clean and clear of tool(s) and other items.
(4)
Install the insulation packs in the work area and the lining on the Bulk door (Ref. TASK 52-33-13-400-001).
(5)
Close the AFT cargo-compartment door (Ref. TASK 52-30-00-860-002).
(6) Remove the access platform(s). R **ON A/C 106-149, 221-221, 224-224, 228-228,
Subtask 52-33-21-410-050-A
C. Close Access
(1)
Make sure that the support device is removed.
(2)
Close the Bulk door (Ref. TASK 52-30-00-860-011).
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6(68)
