As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK ON RT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE ON 67.5% REAR SPAR DATUM AT AFT FUSELAGE. CRACK ON RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE ON 67.5% REAR SPAR DATUM AT AFT FUSELAGE WAS REPAIRED PER CRJ700 SRM 55-31-00-201-001-A01.