TM 1-1520-238-23
11-523
11.119.
LONGITUDINAL F.S. 118.50 PUSH-PULL ROD ASSEMBLY REMOVAL/INSTALLATION – continued
11.119.5. Inspection
a. Check removed and attaching parts for dam-
age (para 11.5).
b. Check removed and attaching parts for corro-
sion (para 1.49).
c. Check all installed bushing(s) and/or bear-
ing(s) for wear (para 11.5).
d. Check all removed bushing(s) and/or bear-
ing(s) for wear (para 11.4).
11.119.6. 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 (1) on bellcrank (10). Torque nut (12)
30 to 40 INCH-POUNDS.
(1) Aline rod (2) with bellcrank (10).
(2) Install bolt (13) through washer (14), bushing
(15), bellcrank (10), and rod (2).
(3) Check fit of self-retaining bolt (13) (para
11.1).
(4) Install nut (12). Torque nut (12) 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 (11).
GO TO NEXT PAGE
M04-5088-4
10
2
15
12
11
14
13
