As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LT WING STIFFENER GOUGED BEYOND LIMITS AT WS 825 REAR SPAR. THE LEFT WING STIFFENER, P/N 112T1237-1, WAS FOUND GOUGED BEYOND LIMITS AT WS 825 REAR SPAR. NO DAMAGE WAS REPORTED ON THE ADJACENT STRUCTURES. THEREFORE, THE GOUGED WAS LIKELY CAUSED BY FOD. REPLACED STIFFENER PER BAC DWG 112T1237 AND SRM 51-40-2.