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 PIVOT HOLE BORE CORROSION. CORROSION AT HOLE NR 4 REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING DIAMETER 2.313 INCH, FINAL DIAMETER = 2.316 INCH & MAXIMUM ALLOWABLE DIAMETER = 2.3135 INCH. REPAIR BUSHING FABRICATED BY MACHINING & INSTALLED IAW EA 1-5750-T0318610 P 1 STEP 1A. REFER TO WRI 57502078 FOR WORK DETAILS. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.