What was found
CRACK ON RH/LH ANGLES BTW VERTICAL STAB AND EXTERNAL FUSELAGE (TAIL CONE STA 67.5%). CORRECTIVE ACTION: RH/LH ANGLES BTW VERTICAL STAB AND EXTERNAL FUSELAGE (TAIL CONE STA 67.5%) WERE 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 RH/LH ANGLES BTW VERTICAL STAB AND EXTERNAL FUSELAGE (TAIL CONE STA 67.5%). CORRECTIVE ACTION: RH/LH ANGLES BTW VERTICAL STAB AND EXTERNAL FUSELAGE (TAIL CONE STA 67.5%) WERE REPAIRED PER CRJ-900 SRM 55-31-00-201-001-A01