What was found
AT C-CHECK, RT WING LEADING EDGE FRONT SPAR OUTBD VERTICAL STIFFENER CRACKED AT LOWER END, NR 6 SLAT OUTBD. REPLACED VERTICALS STIFFENER PER SRM 51-10-1. N/R 2065.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT C-CHECK, RT WING LEADING EDGE FRONT SPAR OUTBD VERTICAL STIFFENER CRACKED AT LOWER END, NR 6 SLAT OUTBD. REPLACED VERTICALS STIFFENER PER SRM 51-10-1. N/R 2065.