TM 1-1520-238-23
11-1141
11.270.
DIRECTIONAL F.S. 534 BELLCRANK REMOVAL/INSTALLATION
11.270.6. 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 bellcrank (5) on bracket (12). Torque nut
(10) 30 to 40 INCH-POUNDS.
(1) Aline bellcrank (5) with bracket (12).
(2) Install bolt (11) through bellcrank (5) and
bracket (12).
(3) Check fit of self-retaining bolt (11) (para 11.1).
(4) Install nut (10). Torque nut (10) to 30 INCH-
POUNDS. Use torque wrench.
(5) Increase torque to aline cotter pin hole, but do
not exceed 40 INCH-POUNDS.
(6) Install cotter pin (13).
(7) Apply sealing compound to head of bolt (11)
and nut (10). Use sealing compound
(item 178, App F).
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M04-1774-5
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