As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
TYS - DURING A CURRENT 3C INSPECTION THE RIGHT AFT FUSELAGE AT FR 76 WAS FOUND WITH SOME CRACKED RIVETS ON THE CONTOUR FLANGE OF THE VERTICAL STAB. MAINTENANCE REMOVED AND REPLACED THE RIGHT AFT FUSELAGE CONTOUR FLANGE DRAG ANGLE AT FR 76. ALL WORK WAS ACCOMPLISHED IAW EMB 145 XR SRM 51-46-02, 51-20-03 AND CPM 51-21-07. AIRCRAFT WILL BE RELEASED AT THE END OF THE CHECK.