As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DAMAGE DESCRIPTION: CRACK ON VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE LH/RH , BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). DRAG ANGLE LH AFT/RH FWD AND AFT WERE REPAIRED PER STEP CRJ-900 SRM 55-31-00-201-001-A01