What was found
INSPECTION FOUND RT WING FRONT SPAR VERTICAL STIFFENER CORRODED AT STA 244. THE STIFFENER WAS REPLACED IAW SRM 51-10-1 PAGE 4 AND 6A, SRM 51-10-2 AND 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND RT WING FRONT SPAR VERTICAL STIFFENER CORRODED AT STA 244. THE STIFFENER WAS REPLACED IAW SRM 51-10-1 PAGE 4 AND 6A, SRM 51-10-2 AND 51-30-2.