As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK ON LH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE ON 67.5% REAR SPAR DATUM AT AFT FUSELAGE. CRACK ON LH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE ON 67.5% REAR SPAR DATUM AT AFT FUSELAGE WAS REPAIRED PER SRM 55-31-00-201-001-A01