As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION AT WING, INBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) PIVOT HOLE BORE NR 3 HOLE. REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44- 07. OVERSIZED REPAIR BUSHING FABRICATED AND INSTALLED CMM 57-44-07 AND EA 1-5750-T0321647 F PART 3 STEP 1A AND STEP 1C. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.