As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RIGHT WING, OTBD FLAP INBD FWD HINGE LOWER MOUNT OTBD HOLE BORE CORROSION. CORROSION AT HOLE NR 7, REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING 0.0713 INCH, FINAL= 0.719 INCH & MAXIMUM ALLOWABLE= 0.709 INCH. SHOULDER BUSHING FABRICATED BY MACHINING & INSTALLED IAW EA 1-5750-T0318610 P1 STEP 1B. REFER TO WRI 57502078 FOR WORK DETAILS. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.