As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RIGHT WING OUTBD FLAP OUTBD HINGE (WING SIDE) LOWER MOUNT INBD HOLE BORE FOUND CORROSION. HOLE NR 3 CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER CMM57-44-09. SHOULDER BUSHING FABRICATED AND INSTALLED PER CMM57-44-09 AND EA 1-5750-73336C PT 3 STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.