What was found
RT DRAG ANGLE BETWEEN VERTICAL STAB AND FUSELAGE IS CRACKED AT FRAME 76 STRINGER 3R. REMOVED AND REPLACED VERTICAL STAB DRAG ANGLE TO FUSELAGE AT FR 76 STRG 3R AND REINSTALLED PREVIOUS REPAIR, IAW EMB 145 SRM 51-40-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RT DRAG ANGLE BETWEEN VERTICAL STAB AND FUSELAGE IS CRACKED AT FRAME 76 STRINGER 3R. REMOVED AND REPLACED VERTICAL STAB DRAG ANGLE TO FUSELAGE AT FR 76 STRG 3R AND REINSTALLED PREVIOUS REPAIR, IAW EMB 145 SRM 51-40-02.