As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
MECHANICALLY BLENDED FOUR AREAS OF CORROSION ON THE LT WING OTBD FLAP PUSHROD ATTACH FITTINGS, PERFORMED AN EDDY CURRENT INSPECTION AND AN ULTRASONIC THICKNESS INSPECTION. FOUND INBOARD FITTING BEYOND LIMITS. PROTECTED BARE METAL IAW SRM 51-10-02 TO AREAS WITHIN CORROSION LIMIT BLENDS. REPAIRED THE LT FLAP PUSHROD ATTACHMENT IAW ENGINEERING MEMO.