What was found
LT WING, OB FLAP, IB AFT HINGE OB PIVOT HOLE FLANGE CORRODED. CORROSION REMOVED PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL THICKNESS = 0.502. MATERIAL REMOVED = 0.004 REMAINING THICKNESS = 0.498. COMPLIED WITH FEDEX EA 1-5750-76807, LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED