(b)
 Install the bushes (427) and (436) with COMMON GREASE (Material No. 04-004) on the door structure.

 (c)
 Install the adjustable washer (426) on the bolt (419).

 (d)
 Apply COMMON GREASE (Material No. 04-004) on the surface of the bolt (419) in contact with the bushes (427) and (436).

 (e)
 Put the lower connection link (423) in position and install the bolt (419).

 (f)
 Make sure that the clearance J17 is 0 +0 +0.1 mm (0.0000 +0.0000 +0.0039 in.).

 (g)
 If the clearance J17 is not in the tolerances, adjust the thickness of the adjustable washer (426).

 (h)
 Install the bushing (429) with COMMON GREASE (Material No. 04-004), the washer (430) and the nut (402).

 1EFF : ALL 1 52-13-21Page 483 1 1 Feb 01/01 1 1 1CES 1

 (i)
 TORQUE the nut (402) to between 1.2 and 1.35 m.daN (106.19 and

 119.46 lbf.in).

 (j)
 Install a new cotter pin (401). NOTE : If you install a new bolt (419), drill a hole of 2 mm

____ (0.0787 in.) for the cotter pin installation.
 (4) Connect the rod (435).
 (a)
 Install the bushes (433) and (434) with SPECIAL MATERIALS (Material No. 05-002).

 (b)
 Install the washer (432) and the bolt (431).

 (c)
 Install the washer (421) and the nut (422).

 (d)
 TORQUE the nut (422) to between 0.6 and 0.7 m.daN (53.09 and

 61.94 lbf.in).

 (e)
 Install a new cotter pin (420). NOTE : If you install a new bolt (431), drill a hole of 1.9 mm

____ (0.0748 in.) for the cotter pin installation.
 (5) Connect the rod (417).
 (a)
 Install the bushes (413) and (414) with SPECIAL MATERIALS (Material No. 05-002).

 (b)
 Install the washer (412) and the bolt (411).

 (c)
 Install the washer (437) and the nut (415).

 (d)
 TORQUE the nut (415) to between 0.3 and 0.35 m.daN (26.54 and

 30.97 lbf.in).

 (e)
 Install a new cotter pin (416). NOTE : If you install a new bolt (411), drill a hole of 1.9 mm

____ (0.0748 in.) for the cotter pin installation.
 1EFF : ALL 1 52-13-21Page 484 1 1 Feb 01/01 1 1 1CES 1

 (6) Connect the upper and lower connection links (423) and (461) on the support arm (410).
 (a)
 Install the washers (404) and (452), the bolts (403) and (451), the set of washers (409) and (458), the washers (418) and (455) and the nuts (405) and (456).

 (b)
 TORQUE the nuts (405) and (456) to between 1.2 and 1.35 m.daN

 (106.19 and 119.46 lbf.in).

 (c)
 Install a new cotter pin (401) and a new cotter pin (450).

 (d)
 Put the bonding leads (425) and (468) in position and install the bolt (429) and (469).

 (e)
 Install the bonding leads (407) and (453) and the nuts (408) and

 (454) and tighten them.
 NOTE : When you install the bonding leads (407) and (453), do an

____ electrical bonding (Ref. TASK 20-28-00-912-004).
 (7)
 Open the door.

 (8)
 With the door in the position, rig the bellcrank (472) with RIGGING PIN (98DNSA20206120).

 (9)
 If the rigging is not correct, adjust the length of the rod 417 as
 follows:

 (a)
 Remove and discard the lockwire from the nuts (470).

 (b)
 Loosen the nuts (470) and release the lockwashers (471).

 (c)
 Turn the barrel of the rod (417) until you get the correct rigging.

 (d)
 Tighten the nuts (470) and make sure that the lockwashers (471) are correctly positioned.

 (e)
 Remove the RIGGING PIN (98DNSA20206120).

 (10) Install the window (Ref. TASK 56-31-13-400-002).
 1EFF : ALL 1 52-13-21Page 485 1 1 Feb 01/01 1 1 1CES 1

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

 (a)
 Apply SEALANTS (Material No. 09-018) on the surface of the plate assembly (181) in contact with the door structure.

 (b)
 Put the plate assembly (181) in position.

 (c)
 Apply SEALANTS (Material No. 09-016) in the housing of the screws

 (182) and (184).

 (d)
 Install the washers (183) and the screws (182) and (184) and tighten them.

 (e)
 Remove the unwanted sealant with CLEANING AGENTS (Material No. 11-004) and MISCELLANEOUS (Material No. 19-003).
　
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(131)