(11)
Hold the movable fairing and remove the nut (49), the washer (48), the bush (47) and the bolt (58).
(12)
Lower the movable fairing sufficiently, to get access to the flap-track-beam attachment (32).
(13)
If you are to install a replacement fairing:
(a)
Measure the inner dimension of the flap-track-beam attachment (32), (dimension 'X').
(b)
Measure the outer dimension of the side-load stay (30), (dimension 'Y').
(c)
Calculate the difference between the dimensions.
(d)
Use the table that follows for the correct selection of shims. NOTE : All the dimensions in the table are in millimeters.
____
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 57-55-11Page 417 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1 -------------------------------------------------------------------------------| Column A | Column B | Column C | -------------------------------------------------------------------------------|If the difference| this is the total | Add these quantities of shim type | |between Dim. 'X' | thickness of the | together, to get the thickness | |and Dim. 'Y' is | shims necessary to | that is given in Column B. | |as given below, | get the correct fit. | 0.3 thick | 0.4 thick | 0.5 thick | -------------------------------------------------------------------------------| To 0.6 | 0.5 | -| -| 1 | -------------------------------------------------------------------------------| 0.61 to 0.7 | 0.6 | 2 | -| -| -------------------------------------------------------------------------------| 0.71 to 0.8 | 0.7 | 1 | 1 | -| -------------------------------------------------------------------------------| 0.81 to 0.9 | 0.8 | -| 2 | -| -------------------------------------------------------------------------------| 0.91 to 1.0 | 0.9 | -| 1 | 1 | -------------------------------------------------------------------------------| 1.01 to 1.1 | 1.0 | -| -| 2 | -------------------------------------------------------------------------------| 1.11 to 1.2 | 1.1 | 2 | -| 1 | -------------------------------------------------------------------------------| 1.21 to 1.3 | 1.2 | 1 | 1 | 1 | -------------------------------------------------------------------------------| 1.31 to 1.4 | 1.3 | 1 | -| 2 | -------------------------------------------------------------------------------| 1.41 to 1.5 | 1.4 | -| 1 | 2 | -------------------------------------------------------------------------------| 1.51 to 1.6 | 1.5 | 2 | 1 | 1 | -------------------------------------------------------------------------------| 1.61 to 1.7 | 1.6 | 1 | 2 | 1 | -------------------------------------------------------------------------------
(14) Install the side-load stay (30) as follows:
(a)
Align the side-load stay (30) and the flap-track-beam rear attachment (32).
(b)
Install the bolt (31), the shims (29), the washer (26) and the nut (27).
1 If you install the shims (29) that you removed, make sure that
_ they are in the same related positions.
2 If you install new shims (29), install them equally on each
_
side of the side-load stay (30).
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 57-55-11Page 418 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1
(c)
TORQUE the nut (27) to between 1.7 and 1.8 m.daN (12.53 and 13.27 lbf.ft).
(d)
Examine the related positions of the hole in the bolt (31) and the slot in the nut (27).
(e)
TORQUE the nut (27), until the next slot aligns with the hole, to
2.8 m.daN (20.64 lbf.ft) maximum.
(f)
Safety the nut (27) with a new cotter pin (28).
(15)
For the track 2, the track 3 and the track 4 positions:
(a)
Apply a thin layer of SEALANTS (Material No. 09-018) or SEALANTS (Material No. 09-019) to the interfaces of the sliding bush (47) and the bolt (58), but not to the threads.
(b)
Align the control rod (54) with the flap drive arm (46) and install the bolt (58), the bush (47), the washer (48) and the nut (49).
(c)
For the track 3 and the track 4 positions, torque the nut (49) to
1.0 m.daN (88.49 lbf.in).
(d)
For the track 2 position, torque the nut (49) to between 1.4 and
1.5 m.daN (10.32 and 11.06 lbf.ft).
(e) 中國(guó)航空網(wǎng) www.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：A320飛機(jī)維護(hù)手冊(cè) AMM WINGS 機(jī)翼5(56)
