What was found
INSPECTION FOUND A .25 INCH CRACK IN VERTICAL STABILIZER FORWARD RT DORSAL FIN ATTACH ANGLE. THE ANGLE WAS REMOVED AND REPLACED IAW EA 5340-01012.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .25 INCH CRACK IN VERTICAL STABILIZER FORWARD RT DORSAL FIN ATTACH ANGLE. THE ANGLE WAS REMOVED AND REPLACED IAW EA 5340-01012.