What was found
CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD/AFT DRAG ANGLES BTW 55.625 % STRG DATUM TO 67.5 % REAR SPAR DATUM (TRACE AT BLO.00). DRAG ANGLE REPAIRED PER CRJ-900 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 RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD/AFT DRAG ANGLES BTW 55.625 % STRG DATUM TO 67.5 % REAR SPAR DATUM (TRACE AT BLO.00). DRAG ANGLE REPAIRED PER CRJ-900 SRM 55-31-00-201-001-A01