What was found
INSPECTION FOUND A 1.3 CRACK IN LT SIDE VERTICAL FIN INNER ATTACH ANGLE. THE RT SIDE VERTICAL FIN INNER ATTACH ANGLE WAS FOUND BROKEN IN HALF. THE ATTACH ANGLES WERE REPLACED IAW SRM 51-30-5 AND 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1.3 CRACK IN LT SIDE VERTICAL FIN INNER ATTACH ANGLE. THE RT SIDE VERTICAL FIN INNER ATTACH ANGLE WAS FOUND BROKEN IN HALF. THE ATTACH ANGLES WERE REPLACED IAW SRM 51-30-5 AND 51-30-2.