-
DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE RACEWAYS.
-
DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE INSTALLATIONS.
-MAKE SURE THAT THE ELECTRICAL CABLES ARE INSTALLED CORRECTLY. INCORRECT INSTALLATION CAN CAUSE DAMAGE.
Subtask 27-51-44-420-057
A. Preparation for Installation
(1)
Clean the component interface and/or the adjacent area with a MISCELLANEOUS (Material No. 19-003) made moist with CLEANING AGENTS (Material No. 11-026).
(2)
Make sure that the parts retained from the removed component are clean and in the correct condition.
(3) Do an inspection of the component interface and/or the adjacent area. R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
Subtask 27-51-44-420-055
B. Installation of the Interconnecting Strut
(1)
Install the washer (3) and the bush (4).
(2)
Put the interconnecting strut (1) in the correct position for installation. Make sure that the position is correct as follows:
(a)
The TOP indication on the interconnecting strut (1) is at the top.
(b)
The flanged bush on the interconnecting strut (1) is at the top.
(c)
The inspection/setting hole/s is/are at the bottom. NOTE : The strut can have one or two inspection/setting holes.
(3)
Install the bolt (2), the washer (5) and the nut (6).
(4)
TORQUE the nut (6) to between 1.1 and 1.7 m.daN (97.34 and 150.44 lbf.in).
(5)
Install the new cotter pin (7).
____ Subtask 27-51-44-820-050
C. Adjustment of the Interconnecting Strut
(1) Install the PIN-SETTING (98D27504031000) in the inspection/setting hole in the interconnecting strut (1).
NOTE : The strut can have one or two inspection/setting holes. If
____ there are two, use the hole that is not blocked by the aircraft structure.
(2)
If necessary, adjust the actuating rod of the interconnecting strut
(1)
so that you can install the PIN-SETTING as follows:
(a)
Align the rod-end (16) with the flap until you can install the bolt (15).
(b)
If necessary, remove and discard the lockwire from the locknut (17).
(c)
Loosen the locknut (17) sufficiently to let you turn the nut (18).
(d)
Adjust the nut (18) until you can install the PIN-SETTING. Make sure that you can see the threads of the rod-end (16) through the check hole. If you cannot see the threads of the rod-end (16) through the check hole, check the flap rigging (Ref. TASK 27-51-00-820-003).
(e)
Tighten the locknut (17).
(f)
Do an operational test of the flap interconnecting strut and the flap-attachment failure-detection sensors (Ref. TASK 27-51-00-710-002).
(g)
Loosely install the washer (14) and the nut (13).
(3)
Remove the blanking caps and connect the electrical connectors (10) and (11) to their related connectors (9) and (8) on the inboard flap. (Ref. Fig. 402/TASK 27-51-44-991-004)
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 27-51-44Page 413 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1
Interconnecting Strut - Electrical Connections
Figure 402/TASK 27-51-44-991-004
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 27-51-44Page 414 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1
(4) Clean the electrical connectors (10) and (11) with a MISCELLANEOUS
(Material No. 19-003) made moist with CLEANING AGENTS (Material No.
11-026).
(5) Apply a continuous layer of STORAGE PRESERVATION (Material No. 15-
008) to the electrical connectors (10) and (11).
(6) Remove the PIN-SETTING from the inspection/setting hole in the
interconnecting strut (1).
R **ON A/C 301-399,
R Subtask 27-51-44-420-055-A
R B. Installation of the Interconnecting Strut
R (1) Install the bush (8).
R (2) Install the guide washer (7) on the dowel (23). Make sure that the
R guide washer (7) is in the correct position with the chamfer
R outboard.
R (3) Put the interconnecting strut (1) in the correct position for
R installation. Make sure that the position is correct as follows:
R (a) The TOP indication on the interconnecting strut (1) is at the
R top.
R (b) The flanged bush on the interconnecting strut (1) is at the top.
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 FLIGHT CONTROLS 飛行操縱4(108)
