TM 1-1520-238-23
11-461
11.104. LATERAL F.S. 159.13 BELLCRANK BRACKET ASSEMBLY REMOVAL/INSTALLATION – continued
11.104.6. 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 bracket (20) on airframe (26).
(1) Aline bracket (20) with airframe (26).
(2) With one person holding bracket, install two
bolts (28) through washers (31), airframe
(26), and bracket (20).
(3) With one person holding bracket, install two
bolts (27) through washers (31), airframe
(26), and bracket (20).
(4) With one person holding bolts (27) and (28),
install four washers (30) and nuts (29).
b. Install bellcrank (14) on bracket (20). Torque
nut (22) 30 to 40 INCH-POUNDS.
(1) Aline bellcrank (14) with bracket (20).
(2) Install bolt (23) through washer (24), bushing
(25), bracket (20), and bellcrank (14).
(3) Check fit of self-retaining bolt (23) (para
11.1).
(4) Install nut (22). Torque nut (22) 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 (21).
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28
31
30
29
31
27
M04-4398-7
20
29
30
26
14
23
24
25
20
M04-4398-8
22
21
