____
(d)
Install the tapered pin (345), the spacer (346) and the nut (347) and tighten it.
(2) If necessary, assemble the housing assy (359) as follows:
(a) Put the shaft lever (314) in position and move the support shaft
(348) into the housing assy (359).
NOTE : Make sure that their attachment holes are align.
____
(b)
Install the tapered pin (352), the spacer (351) and the nut (350) and tighten it.
(c)
Assemble the shaft lever (327) and the spacer in position on the support shaft (348).
NOTE : Make sure that their attachment holes are align.
____
(d)
Install the tapered pin (354), the spacer (355) and the nut (356) and tighten it.
(e)
Put the housing assy (359) in position to the beam (349) and attach it with the screws (358) and the washers (357).
R 1EFF : 001-049, 053-099, 101-105, 151-199, 1 52-31-21Page A428 1201-220, 1May 01/05 1 1 1CES 1 (3) Install the horizontal connection rod (290) as follows:
(a) If required, disassemble the connection rod (290) for the
installation as follows:
1 Remove the nuts (295), the washers (294) and the bolts (293).
_
2 Remove the rod-end (281) and (292) from the center rod (291).
_
(b)
Put the rod-ends (281) and (292) and center rod (291) in position to the door structure.
(c)
Assemble the rod-ends (281) and (292) on the center rod (291) and attach them the bolts (293), the washers (294) and the nuts (295).
(d)
Install the rigging pin (311) into the bearing assy (329) and the shaft lever (332).
(e)
Connect the rod-end (281) to the drift pin (283) as follows: 1 If removed, install the bush (288) into the drift pin (283).
_ 2 Put the rod-end (281) in position and attach it with the bolt
_ (282), the washers (287) and (289) and the nut (286).
3 Safety the nut (286) with the new cotter pin (285).
_
(f) Connect the rod-end (292) to the bellcrank lever (299) as
follows:
1 Put the rod-end (292) in position to the bellcrank lever (299)
_ and attach it with the bolt (298), the washers (297) and the nut (300).
2 Safety the nut (300) with the new cotter pin (301).
_
(4)
Do the same steps to install the connection rod (296).
(5)
Install the vertical control rod (317) as follows:
(a) Connect the upper fork-end of the control rod (317) from the shaft lever (314) as follows:
1 Put the control rod (317) in position to the shaft lever (314)
_ and attach it with the bolt (315), the washers (316) and the nut (324).
R 1EFF : 001-049, 053-099, 101-105, 151-199, 1 52-31-21Page A429 1201-220, 1May 01/05 1 1 1CES 1 2 Safety the nut (324) with the new cotter pin (323).
_
(b) Connect the lower fork-end of the control rod (317) to the drift pin lever (321) as follows:
1_ Put the control rod (317) in position to the drift pin lever
(321) and attach it with the bolt (322), the washers (320) and
the nut (319).
2_ Safety the nut (319) with the new cotter pin (318).
(6) Install the vertical control rod (328) as follows:
(a)
Make sure that the rigging pin (311) is installed into the bearing assy (329) and the shaft lever (332).
(b)
Make sure that the length of the control rod (328) is between
592.0 mm (23.3070 in.) and 602.0 mm (23.7008 in.).
(c)
Connect the upper fork-end of the control rod (328) with the shaft lever (332) as follows:
1 Put the connection rod (328) in position to the shaft lever
_ (332) and attach it with the bolt (330), the washers (331) and the nut (333).
2 Safety the nut (333) with the new cotter pin (355).
_
(d) Connect the lower fork-end of the connection rod (328) to the shaft lever (327) as follows:
1_ If necessary, adjust the length of the connection rod (328) so
that its fork-end aligns with the shaft lever (327).
NOTE : Safety the connection rod (328) after the final____
adjustment with MISCELLANEOUS (Material No. 19-010).
2_ Put the control rod (328) into the position to the the shaft
lever (327) and attach it with the bolt (313), the washers
(312) and the nut (326).
3_ Safety the nut (326) with the new cotter pin (325).
(7) Remove the rigging pin (311) from the bearing assy (329).
R 1EFF : 001-049, 053-099, 101-105, 151-199, 1 52-31-21Page A430 1201-220, 1May 01/05 1 1 1CES 1 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4(121)
