What was found
RT WING O/B FLAP I/B AFT HINGE (FLAP SIDE) PIVOT I/B LUG SURFACE CORROSION. RH WING O/B FLAP I/B AFT HINGE (FLAP SIDE) PIVOT I/B BORE LUG SURFACE CORROSION REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-04 EXISTING THICKNESS 0.447", MATERIAL REMOVED: 0.003", REMAINING THICKNESS 0.444", MINIMUM ALLOWABLE THICKNESS: 0.450". REPAIR CARRIED OUT AS PER EA # 1-5750-T0335652-PT1 STEP 1A. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.