TM 1-1520-238-23
11-770
11.174.
PILOT LONGITUDINAL SHEAR PIN ACTIVATED DECOUPLER (SPAD) ASSEMBLY
DISASSEMBLY/ASSEMBLY (AVIM) – continued
11.174.4. Cleaning
a. Clean removed and attaching parts or surfaces (para 1.47).
11.174.5. Inspection
a. Check arms and lever for gouges.
(1) Maximum gouge depth is 0.025 INCH and is acceptable if no material is raised above surrounding surface.
b. Check cam for gouges.
(1) Maximum gouge depth is 0.025 INCH and is acceptable if no material is raised above surrounding surface.
c. Check removed and attaching parts for cracks. None allowed.
d. Check removed and attaching parts for damage (para 11.5).
e. Check removed and attaching parts for corrosion (para 1.49).
f. Check all installed bushing(s) and/or bearing(s) for wear (para 11.5).
g. Check all removed bushing(s) and/or bearing(s) for wear (para 11.4).
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