As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT HAND WING INBOARD FLAP OUTBOARD AFT (FLAP SIDE) HINGE PIVOT OUTBOARD HOLE BORE CORROSION. HOLE BORE (HOLE B AND A) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03. OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER CMM 57-52-03 AND EA 1-5750-130946C PART5 STEP 2A AND 2B. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.