TM 1-1520-238-23
11-1256
11.293.
RIGGING DIRECTIONAL FLIGHT CONTROLS BETWEEN PILOT AND CPG PEDALS – continued
i. Remove -9 rig pin (13) from CPG SPAD (14).
j. Remove -9 rig pin (10) from directional F.S. 110
bellcrank (11).
k. Remove -9 rig pin (9) from SPAD (7).
l. Install F.S. 542 rod end (1) on directional ser-
vocylinder input linkage (2). Torque nut (4) 30
to 40 INCH-POUNDS.
(1) Install bolt (5) through washer (6), input link-
age (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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M04-3026-10
13
14
M04-3026-9
11
10
M04-3026-5
7
9
2
4
3
6
M04-3026-8
1
5
