What was found
RH FUSELAGE TO VERTICAL STAB DRAG ANGLE IS CRACKED AT FWD FITTING AFT END. REMOVED AND REPLACED FWD RH FUSELAGE TO VERTICAL STABILIZER DRAG ANGLE IAW EMB 145 SRM 51-40-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RH FUSELAGE TO VERTICAL STAB DRAG ANGLE IS CRACKED AT FWD FITTING AFT END. REMOVED AND REPLACED FWD RH FUSELAGE TO VERTICAL STABILIZER DRAG ANGLE IAW EMB 145 SRM 51-40-02.