What was found
LT WING - OUTBOARD FLAP AFT INBOARD HINGE, FOUND INBOARD PIVOT HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL THICKNESS= 0.507, MATERIAL REMOVED= 0.006, REMAINING THICKNESS= 0.501. COMPLIED WITH FEDEX EA 1-5750-76716, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.