INSPECT FOR DAMAGE AFTER REMOVAL OF BENT OR SHEARED RIGGING PIN
Inspect flight control system components for
damage as follows:
Inspect rig pin hole for elongation.
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
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.
Inspect connecting links in system for bowing,
bent rod ends or loose rivets at rod ends.
END OF TASK