What was found
CRACK ON VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT RH DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00) REPAIRED PER CRJ900 SRM 55-31-00-201-001-A01
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT RH DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00) REPAIRED PER CRJ900 SRM 55-31-00-201-001-A01