What was found
RIGHT WING OUTBOARD FLAP AFT INBOARD HINGE, FOUND INBOARD PIVOT HOLE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL THICKNESS OF LUG: 0.506, MATERIAL REMOVED : 0.007, REMAINING THICKNESS OF LUG: 0.506. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76713, TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.