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 ACTUATOR INBD HOLE BORE CORROSION. CORROSION AT HOLE NR 8 REWORKED & FOUND EXCEED LIMIT IAW CMM 57-44-08. EXISTING DIAMETER 1.218 INCH, FINAL DIAMETER = 1.247 INCH, MAXIMUM ALLOWABLE =1.220 INCH. REPAIR BUSHING FABRICATED BY MACHINING & INSTALLED IAW EA 1-5750-T0318610 P1 STEP 1C. REFER TO WRI 57502078 FOR WORK DETAILS. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.