As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
MAJOR REPAIR - CRACK IN VERTICAL STAB JUST AFT OF RT UPPER HOIST POINT. STOP DRILLED CRACK TIPS AND PERFORMED NDI HFEC INSPECTION TO LOCATE CRACK TIPS IAW EMB 175 SRM 51-10-04. ACCOMPLISHED FINAL REPAIR TO RT SKIN OF VERTICAL STAB IAW ETD 2010-170/02797 REV C.