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 I/B FWD HINGE (WING SIDE) LOWER MOUNT I/B BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08 EXISTING HOLE: 0.709", FINAL HOLE: 0.712", MAXIMUM ALLOWABLE HOLE: 0.709". SHOULDER BUSHING FABRICATED AND INSTALLED AS PER EO 1-5750-T0335622 PART 1 STEP 2C AND STEP 2. FLIGHT SURFACES EO 1-5750-7-5002-RT WING OUTBD FLAP INBD FWD HINGE (WING SIDE) CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.