What was found
INSPECTION FOUND A .25 INCH CRACK IN RT WING VERTICAL STIFFENER AT LEADING EDGE UNDER PANEL 6526. THE STIFFENER WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-10-5.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .25 INCH CRACK IN RT WING VERTICAL STIFFENER AT LEADING EDGE UNDER PANEL 6526. THE STIFFENER WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-10-5.