As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INITIAL INSPECTION: CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL 0.00). CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL 0.00) WERE REPAIRED PER CRJ900 SRM 55-31-00-201-001-A01.