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 HINGE (WING SIDE) ACTUATOR ATTACH INBOARD BORE CORROSION. HINGE REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-08. EXISTING HOLE DIAMETER 1.220 INCH; FINAL HOLE DIAMETER 1.234 INCH; MAXIMUM ALLOWABLE DIAMETER 1.220 INCH. OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T0331719 PART 1 STEP 2A. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.