As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LT WING O/B FLAP O/B FWD HINGE (WING SIDE) LOWER MOUNT O/B BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09 EXISTING HOLE: 0.586", FINAL HOLE: 0.597", MAXIMUM ALLOWABLE HOLE: 0.584". SHOULDER BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T0335621 PART 1 STEP 2A AND STEP 2. FLIGHT SURFACES EO 1-5750-7-5002-LT WING OUTBD FLAP OUTBD HINGE (WING SIDE) CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.