As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RT WING O/B FLAP I/B AFT HINGE (FLAP SIDE) PIVOT I/B BORE CORROSION. RH WING O/B FLAP I/B AFT HINGE (FLAP SIDE) PIVOT I/B BORE CORROSION REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-04 EXISTING HOLE 1.195", FINAL HOLE 1.200", MAXIMUM ALLOWABLE HOLE 1.150" OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER EA # 1-5750-T0335652-PT1 STEP 1A. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.