As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) ACTUATOR ATTACH INBOARD BORE CORROSION. HINGE REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-09 EXISTING HOLE DIA 1.218", FINAL HOLE DIA 1.226", MAXIMUM ALLOWABLE HOLE DIA 1.220". OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T0331716 PART 1 STEP 2C. REPAIR CLASSIFIED MINOR PER GMM 6-2-100.