As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RT WING O/B FLAP O/B FWD (WING SIDE) HINGE PIVOT HOLE BORE CORROSION. HINGE PIVOT HOLE BORE (NR 4 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09, OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER CMM 57-44-09 AND EA 1-5750-T0342163 P1 STEP 2B AND STEP 2. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.