R 1EFF : 001-003, 051-054, 1 27-21-41Page 436 1 1 May 01/05 1 1 1CES 1
(c) Do the steps written above again and connect the servo actuators 3025GM (35) at RIB4 and 1025GM (35) at RIB3.
(18)
Apply a thin layer of the SPECIAL MATERIALS (Material No. 05-005) (Ref. TASK 51-75-13-916-002) to all the cadmium-plated steel parts of the rudder hinges which you can see.
(19)
Connect the push-rod (10) from the transducer 42WV (13) to the bracket (11) of the rudder (2) (Ref. Fig. 403/TASK 27-21-41-991-003)
(a)
Install the flanged bushes (18),(19) in the attachment bracket (14).
(b)
Cut and remove the temporary tie wraps, and release the push-rod
(10)
from the hinge arm (12).
(c)
Put the eye-end of the push-rod (10) in position at the attachment bracket (14).
(d)
Install the sliding bush (17) in the attachment bracket (14).
(e)
Install the bolt (16), the washer (20) and the nut (21) at the connection of the attachment bracket (14) and the push-rod (10).
(f) Safety the nut (21) with a new cotter pin (22). R **ON A/C 004-049, 055-099, 101-149, 151-199, 201-299, 301-399, 401-499,
Subtask 27-21-41-420-051-A
D. Installation of the Rudder
(1)
Make sure that during the subsequent procedure, the correct identified components are installed at each connection.
(2)
Install the bushes (73),(74) in the hinge arm (63) at the location of the hinge No. 6 (RIB9 of the vertical stabilizer (1)). (Ref. Fig. 405/TASK 27-21-41-991-005)
(3)
Use the crane to lift the rudder (2) into position aft of the vertical stabilizer (1).
NOTE : There must be a mechanic at each of the hinges to align:
____
-
the axis of the hinge arms
-
the servo actuators 1025GM/2025GM/3025GM, with the hinge fittings on the rudder (2).
(4)
Move the rudder (2) to the left of the aircraft center line and then forward.
(5)
Prevent damage to the component interface and the adjacent area.
(a)
Make sure that there is sufficient clearance between the push-rod
(10)
of the transducer 42W, and the vertical stabilizer (1) and the rudder (2).
(b)
Make sure that there is sufficient clearance between the piston arms of the servo actuators 1025GM/2025GM/3025GM (35), and the vertical stabilizer (1) and the rudder (2).
(c)
Make sure that the edges of the support brackets are not damaged during the installation of the hinge arms.
(6)
Put the hinge arms (12),(50),(63),(90) in position at the brackets (11),(51),(64),(91) of the rudder (2).
(7)
Align the bolt holes in the hinge arms (12),(50),(63),(90) with their related bolt holes in the brackets (11),(51),(64),(91).
(8)
Connect the hinge No. 1 at RIB2 to the bracket (11) of the rudder (2). (Ref. Fig. 403/TASK 27-21-41-991-003)
(a)
Install the bush (25) in the bracket (11).
(b)
Install the locking plate (24) at the bracket (11).
(c)
Put the washer (15) on the bolt (23).
(d)
Install the bolt (23) through the connection of the bracket (11) and the hinge arm (12).
(e)
Install the bush (26) on the bolt (23) until the bush (26) goes into the bracket (11).
(f)
Install the slotted nut (27) on the bolt (23). Do not tighten the slotted nut (27) at this time.
(g)
Put the bonding jumper (31) in position and install the bolt (30) (Ref. TASK 20-28-00-912-004).
中國航空網 m.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2(10)
