As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LT WING, OB FLAP IB AFT HINGE OB PIVOT HOLE FOUND CORRODED. CORROSION REMOVED PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER = 1.062 FINAL DIAMETER = 1.095. COMPLIED WITH FEDEX EA 1-5750-76807, LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED.