As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND SCREW HOLE ON TOP OF LT WING FIXED LEADING EDGE CORRODED AT WS 250. THE CORROSION WAS REMOVED IAW SRM 57-20-1. THE CORRODED AREA OF SKIN WAS CUT OUT. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW AEROCORP ENGINEERING ORDER 04884.