TM 1-1520-238-23
11-1060
11.252.
DIRECTIONAL F.S. 216.25 PUSH–PULL ROD REMOVAL/INSTALLATION – continued
c. Install aft end of rod (4) on bellcrank (5).
Torque nut (7) 30 to 40 INCH-POUNDS.
(1) Aline rod (4) with bellcrank (5).
(2) Install bolt (8) through bushing (9), bellcrank
(5), and rod (4).
(3) Check fit of self-retaining bolt (8) (para 11.1).
(4) Install nut (7). Torque nut (7) to 30 INCH-
POUNDS. Use torque wrench.
(5) Increase torque to aline cotter pin hole, but do
not exceed 40 INCH-POUNDS.
(6) Install new cotter pin (6).
d. Remove -9 rig pin (1) from directional F.S. 348
bellcrank (2) and bracket (3).
e. Inspect (QA).
f. Install catwalk center section (para 2.84).
g. Install access panel L200 (para 2.2).
h. Remove external primary hydraulic power
(para 1.72).
i. Perform directional flight control rigging
maintenance
operational
check
(TM 1-1520-238-T).
END OF TASK
M04-1798-7
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5
9
6
4
7
3
2
M04-1798-8
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