(12)
 Remove the spacer (520) and the washer (519).

 (13)
 Remove the nut (522), the bolt (524) and the bearing assy (523).

 (14)
 Remove the stalock nut (545) (Ref. TASK 20-22-00-000-001).

 (15)
 Remove the washer (544).

 (16)
 Remove the nuts (501) the bolt (502) and the bearing assy (535).

 (17)
 Pull the sleeve (537) towards the outer side of the door.

 (18)
 Remove the nuts (513) the bolt (503) and the bearing assy (542) and the spacer (543).

 (19)
 Push the sleeve (537) towards the inner side of the door.

 (20)
 Remove the sleeve (537) equipped with the cranck (539) and the spacer

 (538) and (541).

 (21)
 Remove the cranck (539) the spacer (538) and (541).

 (22)
 Remove the sealant from the bearing assy (517) (535) and (542) and the door structure with CLEANING AGENTS (Material No. 11-004) and MISCELLANEOUS (Material No. 19-003).

 1EFF : ALL 1 52-13-21Page 428 1 1 May 01/98R 1 1 1CES 1

 Subtask 52-13-21-020-060
 K. Removal of the Upper and Lower Connection Links
 (Ref. Fig. 411/TASK 52-13-21-991-020)

 (1)
 Remove the plate assembly.
 (Ref. Fig. 402/TASK 52-13-21-991-010)

 (a)
 Remove the screws (182) and (184) and the washers (183).

 (b)
 Remove the plate assy (181).

 (c)
 Clean the contact surface with CLEANING AGENTS (Material No. 11-004) and lint free cloth.

 (2)
 Remove the window to remove the upper connection link (Ref. TASK 56-31-13-000-001).

 (3)
 Make sure that the compensation mechanism is released.

 (4)
 Close and lock the door.

 (5)
 Disconnect the upper and lower connection links (423) and (461) from the support arm (410).

 (a)
 Remove the nuts (408) and (454) and disconnect the bonding leads

 (407) and (468).

 (b)
 Remove the bolts (424) and (469) and disconnect the bonding leads

 (424) and (464).

 (c)
 Remove the cotter pins (406) and (457) and discard them.

 (d)
 Remove the nuts (405) and (456), the washers (418) and (455) the bolts (403) and (451) the washers (404) and (452) and the set of washers (409) and (459).

 (e)
 Disconnect the support arm (410) from the upper and lower connection links (461) and (423).

 (6)
 Disconnect the upper connection link (461).

 (a)
 Remove the cotter pin (450) and discard it.

 (b)
 Remove the nut (467), the washer (466) the bushing (465).

 (c)
 Remove the bolt (459) and remove the upper connection link (461).

 1EFF : ALL 1 52-13-21Page 429 1 1 May 01/98R 1 1 1CES 1

 Upper and Lower Connection Links Figure 411/TASK 52-13-21-991-020- 12 (SHEET 1)
 1EFF : 1 1R 1CES  ALL  1 11 1 52-13-21 Page 430 May 01/98

 Upper and Lower Connection Links Figure 411/TASK 52-13-21-991-020- 22 (SHEET 2)
 1EFF : 1 1R 1CES  ALL  1 11 1 52-13-21 Page 431 May 01/98

 (d)
 Remove the washer (462) from the bolt (459).

 (e)
 Remove the bush (463) and the washer (464) and the bush (460) from the door structure.

 (7)
 Disconnect the rod (435).

 (a)
 Remove the cotter pin (420) and discard it.

 (b)
 Remove the nut (422), the washer (421).

 (c)
 Remove the bolt (431) and the washer (432) and the bushes (433) and (434).

 (d)
 Disconnect the rod (431).

 (8)
 Disconnect the rod (417).

 (a)
 Remove the cotter pin (416) and discard it.

 (b)
 Remove the nut (415) and the washer (437).

 (c)
 Remove the bolt (411), the washer (412) and the bushes (413) and (414).

 (9)
 Disconnect the lower connection link (423).

 (a)
 Remove the cotter pin (401) and discard it.

 (b)
 Remove the nut (402), the washer (430) and the bushing (429).

 (c)
 Remove the bolt (419) and the lower connection link (423).

 (d)
 Remove the washer (426) from the bolt (419).

 (e)
 Remove the bush (427) and the washer (429) and the bush (436) from the door structure.

 1EFF : ALL 1 52-13-21Page 432 1 1 May 01/98R 1 1 1CES 1
　
中國航空網 www.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2(117)