TM 1-1520-238-23
11-1004
11.234.
PILOT DIRECTIONAL CONTROL PEDAL PIVOT SUPPORT ASSEMBLY
REMOVAL/INSTALLATION – continued
b. Install rod (7) on support (8). Torque nut (10) 30
to 40 INCH-POUNDS.
(1) Aline rod (7) with support (8).
(2) Install bolt (11) through bushing (12), support
(8), and rod (7).
(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 new cotter pin (9).
c. Inspect (QA).
d. Install covers (1) and (2) on airframe (3).
(1) Aline cover (2) with airframe (3).
(2) Install nine screws (4) and washers (5).
(3) Aline cover (1) with cover (2) and airframe
(3).
(4) Install bolt (6) and washer (5).
(5) Install 15 screws (4) and washers (5).
(6) Apply sealing compound to faying surface of
covers (1) and (2). Use sealing compound
(item 176, App F).
e. Inspect (QA).
f. Install pilot directional control pedal (para
11.233).
g. Install flex chute, turret, and area weapon
(TM 9-1090-208-23).
END OF TASK
VIEW ROTATED
8
12
11
7
9
10
M04-4425-7
2
1
4
5
5
6
5
4
3
M04-4425-8
