As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACKED FWD AND AFT DRAG ANGLE AT RIGHT STABILIZER TO FUSELAGE ATTACHMENT BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). CRACKED FWD AND AFT DRAG ANGLE AT RIGHT STABILIZER TO FUSELAGE ATTACHMENT BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00) WERE REPAIRED PER CRJ-900 SRM 51-42-21-001-001-A01 ,CRJ900 SRM 51-42-06-001-001-A01,CRJ900 SRM 51-42-22-001-001-A01 AND CRJ900 SRM 55-31-00-201-001-A01