As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RT WING - OUTBOARD FLAP, INBOARD HINGE FITTING, INBOARD AFT BORE HOLE FOUND CORRODED. RIGHT WING OUTBOARD FLAP ASSEMBLY 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.