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 (WING SIDE) PIVOT BORE HOLE FOUND CORROSIONS. HINGE HOLE BORE (HOLE 4) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER CMM 57-44-08 AND EA 1-5750-T0343678 P1 STEP 2A AND STEP 2. INBD FWD HINGE (WING SIDE) CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.