TM 1-1520-238-23
11-1216
11.286.
RIGGING LONGITUDINAL FLIGHT CONTROLS BETWEEN PILOT CYCLIC STICK AND
LONGITUDINAL SERVOCYLINDER – continued
i. Slowly move longitudinal servocylinder input
lever (2) to aline lower lever (18) with upper
edge of boss (19) on servocylinder body (20).
j. Check that holes (21) in input lever (2) aline
with F.S. 165 push-pull rod end (1).
(1) If holes in input lever (2) do not aline with rod
end (1), adjust upper end of F.S. 165 push-
pull rod (22) rod end (1) to aline holes (para
11.2).
(2) If holes in input lever (2) aline with rod end (1)
go to next step.
k. Install F.S. 165 rod end (1) on input lever (2).
Torque nut (4) 30 to 40 INCH-POUNDS.
(1) Install bolt (5) through washer (6), arm (2),
and rod end (1).
(2) Check fit of self-retaining bolt (5) (para 11.1).
(3) Install nut (4). Torque nut (4) to 30 INCH-
POUNDS. Use torque wrench.
(4) Increase torque to aline cotter pin hole, but do
not exceed 40 INCH-POUNDS.
(5) Install new cotter pin (3).
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M04-3017-3
13
19
2
1
22
15
20
18
21
M04-3017-8
1
2
3
4
5
6
