As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION FOUND DURING FPI ON LT WING (FLAP SIDE) INBD FLAP, OTBD AFT HINGE BRACKET PIVOT OTBD LUG BORE. REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-03 REVISION 72. EXISTING DIAMETER 1.329",FINAL DIAMETER 1.335", MAXIMUM ALLOWABLE DIAMETER 1.220". BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-156845 PART 1 STEP 4 AND STEP 5. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REV .114.