(g)
Safety the nuts (279) and the lockwashers (278) with
MISCELLANEOUS (Material No. 19-010).
(h)
Install the bushes (233) and (232) with SPECIAL MATERIALS (Material No. 05-002).
(i)
Install the washer (209), the bolt (210), the washer (203) and the nut (204).
(j)
TORQUE the nut (204) to between 0.3 and 0.35 m.daN (26.54 and
30.97 lbf.in).
(k)
Install a new cotter pin (205). NOTE : If you install a new bolt (210), drill a hole of 1.9 mm
____ (0.0748 in.) for the cotter pin installation.
(l)
Remove the PIN - RIGGING (98D52103006000) from the bellcrank (280).
(17) Connect the rod (217). (Ref. Fig. 413/TASK 52-13-21-991-022)
(a)
Put the door in the up position.
(b)
Install the RIGGING PIN (98DNSA20206120) on the lowering shaft (293).
(c)
Put the hook (292) in contact with the inner control handle (238).
(d)
Make sure that the clearance J18 between the hook (292) and the inner control handle (238) is 0.2 mm (0.0078 in.) to 1 mm (0.0393 in.).
(e)
If the clearance J18 is not in the tolerances adjust the hook
(292) as follows.
1 Remove and discard the cotter pin (294).
_
2 Loosen the nut (295).
_
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Gearbox - Rod Connection Figure 413/TASK 52-13-21-991-022- 13 (SHEET 1)
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Gearbox - Rod Connection Figure 413/TASK 52-13-21-991-022- 23 (SHEET 2)
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Gearbox - Rod Connection Figure 413/TASK 52-13-21-991-022- 33 (SHEET 3)
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3_ Adjust the hook (292) to get the correct clearance.
4_ Tighten the nut (295).
5_ Install a new cotter pin (294).
NOTE : If you install a new bolt (293), drill a hole of 2 mm____
(0.0787 in.) for the cotter pin installation.
(f)
Remove and discard the lockwire from the nuts (291).
(g)
Loosen the nuts (291) and release the lockwashers (292).
(h)
Turn the barrel of the rod (217) to get the connection.
(i)
Tighten the nuts (291).
(j)
Make sure that the lockwashers (292) are correctly positioned.
(k)
Safety the nuts (291) and the lockwashers (290) with MISCELLANEOUS (Material No. 19-010).
(l)
Install the spacer (236).
(m)
Install the washer (218), the bolt (216) and the nut (219).
(n)
TORQUE the nut (219) to between 0.16 and 0.17 m.daN (14.15 and
15.04 lbf.in).
(o)
Install a new cotter pin (220). NOTE : If you install a new bolt (216), drill a hole of 1.8 mm
____ (0.0708 in.) for the cotter pin installation.
(p)
Remove the RIGGING PIN (98DNSA20206120) from the lowering shaft (293).
(18) Remove the unwanted sealant with CLEANING AGENTS (Material No. 11-004) and a MISCELLANEOUS (Material No. 19-003).
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Subtask 52-13-21-420-053
D. Installation of Lowering Shaft
(Ref. Fig. 405/TASK 52-13-21-991-005)
(1)
Put the lowering shaft (82) in position.
(2)
Apply SEALANTS (Material No. 09-018) on the surface of the door in contact with the plate (84).
(3)
Install the plate (84), the bolts (83) and the nuts (88).
(4)
TORQUE the nuts (88) to between 0.35 and 0.45 m.daN (30.97 and 39.82 lbf.in).
(5)
Apply COMMON GREASE (Material No. 04-004) on the surface in contact with the lever (86).
(6)
Install the lever (86). Make sure that the grooves are aligned. Install the bolt (87) and the nut (85). Tighten the nut.
(7)
Apply SEALANTS (Material No. 09-018) on the surface of the door in contact with the bearing (79).
(8)
Put the bearing (79) in position.
(9)
Install the bolt (80) and the nuts (78).
(10)
TORQUE the nuts (78) to between 0.35 and 0.45 m.daN (30.97 and 39.82 lbf.in).
(11)
Apply COMMON GREASE (Material No. 04-004) on the surface of the lowering shaft (82) in contact with the lever assy (75).
(12) 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2(122)
