TM 1-1520-238-23
11-423
11.96.
LATERAL F.S. 118.50 PUSH-PULL ROD ASSEMBLY REMOVAL/INSTALLATION – continued
11.96.6. Installation
CAUTION
To prevent damage to flight control sys-
tem components, do not use force to
aline bellcrank with bracket or to aline
push-pull rod with bellcrank.
a. Install rod (5) on bellcrank (12). Torque nut (14)
30 to 40 INCH-POUNDS.
(1) Aline rod end (5) with bellcrank (12).
(2) Install bolt (15) through washer (16), bushing
(17), bellcrank (12), and rod end (5).
(3) Check fit of self-retaining bolt (15) (para
11.1).
(4) Install nut (14). Torque nut (14) 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 (13).
b. Install rod (5) on bellcrank (6). Torque nut (8) 30
to 40 INCH-POUNDS.
(1) Aline rod end (5) with bellcrank (6).
(2) Install bolt (9) through washer (10), bushing
(11), bellcrank (6), and rod end (5).
(3) Check fit of self-retaining bolt (9) if required
(para 11.1).
(4) Install nut (8). Torque nut (8) 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 (7).
c. Inspect (QA).
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