As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RIGHT WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE) PIVOT INBOARD LUG HOLE BORE FOUND CORRODED. BORE REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-52-03. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-135692F, PART 5, STEP 2 AND 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.