As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK ON LH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD & AFT DRAG ANGLE BTW 61.56% STRG DATUM TO 67.5% REAR SPAR DATUM CRACK ON LH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD & AFT DRAG ANGLE BTW 61.56% STRG DATUM TO 67.5% REAR SPAR DATUM WERE REPAIRED PER CRJ-900 SRM 55-31-00-201-001-A01