What was found
CRACK ON RT INTERNAL VERTICAL STABILIZER ATTACH ANGLE AT DORSAL FIN AREA. REPLACED SAME IAW SRM 51-30-02, 51-30-05 AND DWG 5912188.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON RT INTERNAL VERTICAL STABILIZER ATTACH ANGLE AT DORSAL FIN AREA. REPLACED SAME IAW SRM 51-30-02, 51-30-05 AND DWG 5912188.