What was found
RIGHT WING, WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT HOLE SURFACE FOUND CORROSION. HOLE SURFACE REWORKED AS PER MD-11 CMM 57-44-09. REPAIR SHIM FABRICATED AND INSTALLED AS PER MD-11CMM 57-44-09 AND EA.# : 1-5750-132168 A P3 , STEP 1. REPAIR EVALUATED AND FOUND BARREL NUT MATING SURFACE REMAINING THICKNESS OF UPPER : 0.375" BEYOND REWORK LIMIT AND LOWER : 0.379" WITHIN REWORK LIMIT . MINIMUM THICKNESS LIMIT = 0.710" - (0.667" / 2 ) = 0.3765" ACCEPTED AS PER EA # : 1-5750-132168 A P3 , FIGURE 6. TITLE: WINGS-TRAILING EDGE & TRAILING EDGE DEVICES - EO 1-5750-7-5002- RH WING -OUTBD FLAP OUTBD HINGE ASSY (WING SIDE) CORROSION REPAIR.REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.