As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RT WING OTBD FLAP INBD HINGE (WING SIDE) PIVOT HOLE FOUND CORRODED. REPAIRED IAW EA1-5740-147656. EXISTING HOLE: 2.252" FINAL HOLE: 2.3185" MAX HOLE: 2.3135" . NEW BUSHING FABRICATED AND INSTALLED IAW EA 1-5740-147656. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.