As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND RT WING LEADING EDGE UPPER AFT SKIN CORRODED WITH SEVERAL .125 INCH CRACKS AT FASTENERS. THE LEADING EDGE WAS REMOVED, REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 57-10-0. INSTALLED FLEX PANEL IAW MM 27-80-02 AND OPERATIONAL CHECK WAS GOOD.