As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RIGHT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE) BARREL NUT HOLE SURFACE FOUND CORROSION. CORROSION REWORKED AND FOUND BEYOND REWORK LIMIT AS PER CMM57-44-09. NEW REPAIR SHIM FABRICATED AND INSTALLED PER CMM57-44-09 AND EA NR 1-5750-73336C PT 3 STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.