As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RIGHT WING, OUTBOARD FLAP, INBOARD HINGE FITTING OUTBOARD MID BORE HOLE FOUND CORRODED. REMOVED AND REPLACED AS PER MM 27-50- 30-4 AND FLAP ADJUSTMENT CARRIED OUT AS PER MM 27-50-00-830-805. FLAP SYSTEM RANGE OF MOVEMENT TEST CARRIED OUT AS PER MM 27-50-00-710-801.