TM 1-1520-238-23
11-648
11.146. CPG DIRECTIONAL SHEAR PIN ACTIVATED DECOUPLER (SPAD) SHEAR PIN
REPLACEMENT – continued
d. Install rod (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), bushing
(7), arm (2), and rod (1).
(4) Check fit of self-retaining bolt (5) (para 11.1).
(5) Install nut (4). 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 access doors B60 and B65L; install
fairing L60 (para 2.2).
i. Inspect (QA).
END OF TASK
1
6
7
2
4
3
M04-1806-6
5
