As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT WING - FLAP SIDE OUTBOARD FLAP INBOARD HINGE INBOARD PIVOT BORE LUG HOLE FOUND WITH CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER MD-10 CMM 57-52-02. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-10 CMM 57-52- 02 AND E.A.#8-5750-T0362751 PART 1 STEP 1A AND STEP 1, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.