What was found
INSPECTION FOUND VERTICAL FIN INNER ATTACH ANGLE ON RT AND LT SIDES CRACKED. THE ANGLES WERE REMOVED AND REPLACED IAW SRM 51-30-5.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND VERTICAL FIN INNER ATTACH ANGLE ON RT AND LT SIDES CRACKED. THE ANGLES WERE REMOVED AND REPLACED IAW SRM 51-30-5.