TM 1-1520-238-23
11-674
11.152.
PILOT DIRECTIONAL SHEAR PIN ACTIVATED DECOUPLER (SPAD) REMOVAL – continued
CAUTION
To prevent damage to flight control sys-
tem components, do not use force if bind-
ing or roughness occurs while moving
controls.
l. Install -9 rig pin (44) through bracket (45) and
directional F.S. 110 bellcrank (46).
(1) Locate bracket (45) and bellcrank (46) in gun
turret bay.
(2) Install -9 rig pin (44) through bracket (45) and
bellcrank (46).
m. Install -9 rig pin (47) through directional F.S.
164 bellcrank (48) and bracket (49).
(1) Locate bellcrank (48) and bracket (49) on
main deck.
(2) Install -9 rig pin (47) through bellcrank (48)
and bracket (49).
11.152.4. Cleaning
a. Clean removed and attaching parts (para
1.47).
11.152.5. Inspection
a. Check removed and attaching parts for dam-
age (para 11.5).
b. Check removed and attaching parts for corro-
sion (para 1.49).
c. Check all installed bushing(s) and/or bear-
ing(s) for wear (para 11.5).
d. Check all removed bushing(s) and/or bear-
ing(s) for wear (para 11.4).
END OF TASK
M04-1808-12
45
44
46
47
48
49
