As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING MAINTENANCE CHECK FOUND THE FORWARD LEFT VERTICAL STAB TO FUSELAGE ANGLE HAS A CRACK APPROX 1" LONG. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD VERTICAL STAB TO FUSELAGE ANGLE IAW EO EM-53MR-2062. THE AIRCRAFT WAS RETURNED TO SERVICE.