TM 1-1520-238-23
11-762
Change 3
11.172.
PILOT LONGITUDINAL SHEAR PIN ACTIVATED DECOUPLER (SPAD)
REMOVAL/INSTALLATION – continued
c. Install rod (18) on SPAD (19). Torque nut (21) 30
to 40 INCH-POUNDS.
(1) Aline rod (18) with SPAD (19).
(2) Install bolt (22) through washer (23), bushing
(24), SPAD (19), and rod (18).
(3) Check fit of self-retaining bolt (22) (para
11.5).
(4) Install nut (21). Torque nut (21) 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 (20).
d. Attach connector (A334)P1 (16) to receptacle
J271 (17).
e. Inspect (QA).
f. Perform longitudinal flight control rigging
maintenance
operational
check
(TM 1-1520-238-T).
g. Perform DASE maintenance operational
check (TM 1-1520-238-T).
h. Install door (13) on floor (10).
(1) Install 28 screws (14) and washers (15).
i. Install door (9) on floor (10).
(1) Install 16 screws (11) and washers (12).
j. Install air duct No. 21 (para 13.28).
k. Install pilot seat (para 2.161).
l. Install access panel R200 (para 2.2).
END OF TASK
22
23
24
18
21
20
M04-1742-13
19
M04-1742-14
1716
M04-1742-15
11
12
14
15
13
10
9
