TM 1-1520-238-23
11-620
11.139.
COLLECTIVE F.S. 161.60 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 18 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 transformer-rectifier No. 2 (para 9.32).
g. Perform collective flight control rigging main-
tenance operational check (TM 1-1520-238-T).
h. Install pilot seat (para 2.161).
i. Install access panel R200 (para 2.2).
END OF TASK
9
M04-4388-8
6
7
1211
10
8
1
3
5
4
2
19
20
M04-4388-9
