What was found
RIGHT VERTICAL STABILIZER DRAG ANGLE HAS POSSIBLE CRACK AT FRAME 78. REMOVED AND REPLACED RT VERTICAL TO FUSELAGE 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 VERTICAL STABILIZER DRAG ANGLE HAS POSSIBLE CRACK AT FRAME 78. REMOVED AND REPLACED RT VERTICAL TO FUSELAGE DRAG ANGLE IAW SRM 51-40-02.