What was found
RIGHT WING LEADING EDGE, INBOARD FSS 231, SPAR STIFFENER IS GOUGED. MAJOR REPAIR ACCOMPLISHED: REMOVED AND REPLACED THE STIFFENER PER SRM 51-40-2 AND BAC DWG 112N2002.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT WING LEADING EDGE, INBOARD FSS 231, SPAR STIFFENER IS GOUGED. MAJOR REPAIR ACCOMPLISHED: REMOVED AND REPLACED THE STIFFENER PER SRM 51-40-2 AND BAC DWG 112N2002.