51-10-06 CURTISS-WRIGHT Applies to all model C-46 Series aircraft.
Compliance required at next periodic inspection, not to exceed 100 hours, and each 200 hours or nearest regular inspection period thereafter.
Inspect all aileron, rudder and elevator hinge fittings and adjacent structure for cracks, loose rivets, worn bolts and condition of bearings. If defects are found, the part should be replaced by an undamaged part or repaired.
This supersedes AD 50-14-1.