As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RIGHT VERTICAL STAB SKIN CRACK DAMAGE. THE CRACK DAMAGE MEASURES 5.500 INCHES IN LENGTH & IS APPROXIMATELY 0.600 INCHES FROM THE FASTENER THAT INTERSECTS THE REAR SPAR & RIB 12. THE CRACK IS IN A REWORK AREA & IS COMPLETELY THROUGH THE SKIN WHICH MEASURES 0.031 INCHES AT THAT LOCATION. THE ACCOMPLISHMENT OF THIS PERMANENT MAJOR REPAIR WAS ACCOMPLISHED ON EO E175-55MR-005 UNDER WORK ORDER 903933.