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 FORWARD (WING SIDE) HINGE PIVOT BORE HOLE CORROSION. HINGE PIVOT 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 1-5750-130944 A P3 STEP 1A AND STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.