As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RIGHT WING, OTBD FLAP OTBD FWD HINGE UPPER BARREL NUT HOLE BORE CORROSION. CORROSION AT HOLE NR 7 REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING IS 0.387 INCH, FINAL IS 0.405 INCH, MAXIMUM ALLOWABLE IS 0.391 INCH. REPAIR BUSHING FABRICATED BY MACHINING & INSTALLED IAW EA 1-5750-T0318565 P 1 STEP 1B. REFER TO WRI 57502076 FOR WORK DETAILS. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.