TM 1-1520-238-23
11-550
11.125.
LONGITUDINAL F.S. 159.62 PUSH-PULL ROD ASSEMBLY REMOVAL/INSTALLATION – continued
b. Install rod (6) on bellcrank (7). Torque nut (9) 30
to 40 INCH-POUNDS.
(1) Aline rod (6) with bellcrank (7).
(2) Install bolt (10) through washer (11), bushing
(12), bellcrank (7), and rod (6).
(3) Check fit of self-retaining bolt (10) (para
11.1).
(4) Install nut (9). Torque nut (9) 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 (8).
c. Inspect (QA).
d. Install cover (1) on bulkhead (2).
(1) Aline holes in cover (1) with holes in bulkhead
(2).
(2) Install 17 screws (4) and washers (5).
(3) Secure insulation (3) on bulkhead (2) by fas-
tening pile tape (19) on hook tape (20).
e. Inspect (QA).
f. Install pilot seat (para 2.161).
g. Perform longitudinal flight control rigging
maintenance
operational
check
(TM 1-1520-238-T).
h. Install access panel R200 (para 2.2).
END OF TASK
10
11
12
8
7
9
M04-4384-8
6
4
5
2
1
3
M04-4384-9
19
20
