TM 55-1520-240-23-9
11-225
INSTALL AFT LCT CONNECTING LINK
(Continued)
11-225
NOTE
Positive retention bolts are installed
in flight control connections. These
bolts are self-retaining and require a
special nut and torque (Task 1-13).
1.
Remove nut (1), washers (2 and 3), and bolt (4)
from yoke (5) and actuator bearing (6).
2.
Remove nut (7), washer (8), and bolt (9) from
swashplate (10).
3.
Position link (11) in lug (12) of swashplate (10).
Cable of link must face inboard and alignment
guide (13) of clip (14) must face forward.
4.
Apply antiseize compound (E75) to shrink
bushing (15) on bolt (9). Keep compound off
threads of bolt. Wear gloves (E184.1) and
goggles.
5.
Install bolt (9) head aft, through lug (12) of
swashplate (10) and connecting link rod end
bearing (16). Install washer (8) and nut (7).
Torque nut to 660 to 780 inch-pounds. Do
not exceed 1400 inch-pounds for cotter pin
alignment.
6.
Install cotter pin (17).
INSPECT
7.
Remove nut (18), washer (19 and 20), and bolt
(21) from yoke (5).
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