As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RIGHT WING OUTBD FLAP INBD (WING SIDE) CLEVIS FITTING HOLE BORE FOUND CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER CMM57-44-16. OVERSIZED BUSHING AND REPAIR WASHER FABRICATED AND INSTALLED PER CMM57-44-16 AND EA 1-5740-130969A PT 2 STEPS 2, 2A & 2B. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.