TM 1-1520-238-23
Change 4
11-379
11.85.
CPG CYCLIC STICK FLIGHT CONTROL ARM ASSEMBLY DISASSEMBLY/ASSEMBLY
(AVIM) – continued
i. Allow adhesive to cure 12 HOURS at ambient
temperature or cure 1.5 HOURS at 135 F (57
C).
j. Install arm (1) on support (2). Torque nut (4) 65
to 85 INCH-POUNDS.
(1) Aline arm (1) with two retainers (8) and
spacers (7).
(2) Install bolt (6) through washer (5), support
(2), spacer (7), retainer (8), arm (1), retainer
(8), spacer (7), and support (2).
(3) Check fit of self-retaining bolt (6) (para 11.1).
(4) Install washer (5) and nut (4).
(5) Torque nut (4) to 65 INCH-POUNDS. Use
torque wrench.
(6) Increase torque to aline cotter pin hole, but do
not exceed 85 INCH-POUNDS.
(7) Install new cotter pin (3).
k. Inspect (QA).
END OF TASK
M04-4301-9
5
4
3
7
8
8
1
2
7
6
5
