What was found
RT VERTICAL STAB TO FUSELAGE ANGLE T/E CRACKED. NEEDS PAINT REMOVED FOR FURTHER EVALUATION. CRACK CONFIRMED IN RADIUS . CRACK LENGTH MARKED.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RT VERTICAL STAB TO FUSELAGE ANGLE T/E CRACKED. NEEDS PAINT REMOVED FOR FURTHER EVALUATION. CRACK CONFIRMED IN RADIUS . CRACK LENGTH MARKED.