As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD & AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00 FWD ANGLE NO CRACKS WERE FOUND PER CRJ 700/900/1000 NDT MANUAL PART 06. 53-00-000-250-A01 (EQUIPMENT: NORTEC 600 C/N 4403 EXP 12 MAY 26). LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00 WAS REPAIRED PER CRJ900 SRM 55-31-00-201-001-A01