TM 1-1520-238-23
11-457
11.103.
LATERAL F.S. 159.13 PUSH-PULL ROD ASSEMBLY REMOVAL/INSTALLATION – continued
b. Install rod (13) on bellcrank (14). Torque nut
(16) 30 to 40 INCH-POUNDS.
(1) Aline rod (13) with bellcrank (14).
(2) Install bolt (17) through washer (18), bushing
(19), bellcrank (14), and rod (13).
(3) Check fit of self-retaining bolt (17) (para
11.1).
(4) Install nut (16). Torque nut (16) 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 (15).
c. Inspect (QA).
d. Install cover (1) on bulkhead (2).
(1) Aline holes in cover (1) with holes in bulkhead
(2).
(2) Install 19 screws (11) and washers (12).
(3) Secure insulation (10) on bulkhead (2) by fas-
tening pile tape (26) on hook tape (27).
(4) Install two clamps (5) and (7) on wire har-
nesses (8) and (9).
(5) Install screw (3) through washer (4), clamp
(5), spacer (6), clamp (7), and bulkhead (2).
e. Inspect (QA).
f. Perform lateral flight control rigging mainte-
nance operational check (TM 1-1520-238-T).
g. Install air duct No. 11 (para 13.27).
h. Install pilot seat (para 2.161).
i. Install access panel L200 (para 2.2).
END OF TASK
15
17
18
19
16
14
M04-4379-7
13
1
M04-4379-8
12
11
2
26
10
27
M04-4379-9
6
7
8
9
3
4
5
2
