As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) BARREL NUT UPPER BOLT HOLE CORROSION. HINGE REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44--09 EXISTING HOLE DIA 0.405", FINAL HOLE DIA 0.422", MAXIMUM ALLOWABLE HOLE DIA 0.391". OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T0331713 PART 1 STEP 2C. REPAIR CLASSIFIED MINOR PER GMM 6-2-100.