As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LT WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) HOLE NR 2 OUTBOARD SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS = 0.411, MATERIAL REMOVED = 0.005, REMAINING THICKNESS = 0.406 AND REPAIRED AS PER FEDEX EA 1-5750-80287, TITLE: WINGS - LT OUTBOARD FLAP - INBOARD FLAP SIDE HINGE BRACKET PIVOT AND ACTUATOR BORES - CORROSION REMOVAL AND REPAIR.