TM 55-1520-240-23-9
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INSPECT FOR DAMAGE AFTER REMOVAL OF BENT OR SHEARED RIGGING PIN
11-18
INITIAL SETUP
Applicable Configurations:
All
Tools:
As Required
Materials:
None
Personnel Required:
Inspector
References:
TM 1-1520-253-23
Equipment Condition:
As Required
1.
Inspect flight control system components for
damage as follows:
a.
Inspect rig pin hole for elongation.
b.
Inspect supports of bellcranks with rig pin
holes for cracks, bending, sheared, or
loose rivets. No cracks allowed. If a crack
in the support is suspected, refer to TM
1-1520-253-23.
c.
Inspect bellcranks with rig pin hole for
damage at pin hole and lug holes. No
cracks allowed. If a crack in the bellcrank is
suspected, refer to TM 1-1520-253-23.
d.
Inspect connecting links in system for bowing,
bent rod ends or loose rivets at rod ends.
FOLLOW-ON MAINTENANCE:
As Required
END OF TASK
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