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 LOWER BOLT H0LE CORROSION. HINGE REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-09. EXISTING HOLE DIAMETER 0.406 INCH; FINAL HOLE DIAMETER 0.422 INCH; MAXIMUM ALLOWABLE DIAMETER 0.391 INCH. OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T0331713 PART 1 STEP 2C. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.