What was found
RIGHT WING UPPER FIBERGLASS PANEL PUNCTURE ABOUT 4 FT FROM FUSELAGE. REPAIRED DAMAGED LEADING EDGE PANEL IAW SRM 51-40-09.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT WING UPPER FIBERGLASS PANEL PUNCTURE ABOUT 4 FT FROM FUSELAGE. REPAIRED DAMAGED LEADING EDGE PANEL IAW SRM 51-40-09.