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