As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT WING INBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) PIVOT INBOARD BORE FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-52-03. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-132244 H, PART 6, STEPS 2 AND 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.