As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RIGHT HAND WING INBOARD FLAP OUTBOARD AFT (FLAP SIDE) HINGE PIVOT INBOARD HOLE BORE CORROSION. HOLE BORE (HOLE G AND F) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03. BUSHING FABRICATED AND INSTALLED AS PER CMM 57-52-03 AND EA 1-5750-130949C PART5 STEP 2A AND STEP 2B. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.