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 SIDE LOAD FITTING BARREL NUT HOLE FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09 REVISION 78. NEW BUSHING FABRICATED AND INSTALLED IAW CMM 57-44-09 REVISION 78 AND EA 1-5750-T0306612 PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 120.