TM 1-1520-238-23
11-691
11.155.
PILOT DIRECTIONAL SHEAR PIN ACTIVATED DECOUPLER (SPAD) SHEAR PIN
REPLACEMENT – continued
CAUTION
To prevent damage to flight control sys-
tem components, do not use force to
aline push-pull rod with arm.
d. Install rod end (1) on arm (2). Torque nut (4) 30
to 40 INCH-POUNDS.
(1) Aline rod (1) with arm (2).
(2) Install bushing (7) in arm (2).
(3) Install bolt (5) through washer (6) (if re-
quired), arm (2), rod (1), and bushing (7).
(4) Install nut (4).
(5) Torque nut (4) to 30 INCH-POUNDS. Use
torque wrench.
(6) Increase torque to aline cotter pin hole, but do
not exceed 40 INCH-POUNDS.
(7) Install new cotter pin (3).
e. Inspect (QA).
f. Perform flight control system maintenance
operational check (TM 1-1520-238-T).
g. Perform DASE maintenance operational
check (TM 1-1520-238-T).
h. Install flex chute, turret, and area weapon
(TM 9-1090-208-23).
END OF TASK
M04-1810-8
UP
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