What was found
CRACK IN THE VERTICAL STABILIZER FIXED LEADING EDGE EXPANSION JOINT AT THE RADIUS RELIEF CUT. REMOVED AND REPLACED THE ANGLE IAW 51-00-05, AND SRM 51-40-02..
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK IN THE VERTICAL STABILIZER FIXED LEADING EDGE EXPANSION JOINT AT THE RADIUS RELIEF CUT. REMOVED AND REPLACED THE ANGLE IAW 51-00-05, AND SRM 51-40-02..