What was found
LEFT WING - OUTBOARD FLAP AFT INBOARD HINGE, FOUND OUTBOARD HOLE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL THICKNESS= 0.512, MATERIAL REMOVED= 0.003, REMAINING THICKNESS= 0.409. COMPLIED WITH FEDEX EA 1-5750-76716, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.