What was found
RIGHT FWD VERTICAL STAB TO FUSELAGE DRAG ANGLE WAS CRACKED AT THE AFT END FASTENER. REMOVED AND REPLACED THE DRAG ANGLE IAW SRM 51-40-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT FWD VERTICAL STAB TO FUSELAGE DRAG ANGLE WAS CRACKED AT THE AFT END FASTENER. REMOVED AND REPLACED THE DRAG ANGLE IAW SRM 51-40-02.