What was found
CRACK ON RH FWD VERTICAL TO FUSELAGE DRAG ANGLE NEAR AFT END IN RADIUS.-C/A-REMOVED AND REPLACED RH FWD VERTICAL TO FUSELAGE 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.
CRACK ON RH FWD VERTICAL TO FUSELAGE DRAG ANGLE NEAR AFT END IN RADIUS.-C/A-REMOVED AND REPLACED RH FWD VERTICAL TO FUSELAGE DRAG ANGLE IAW EMB 145 SRM 51-40-02.