What was found
CRACK ON FWD AND AFT RH DRAG ANGLE BTW UNION OF VERTICAL STABILIZER AND FUSELAGE (67.5% REAR SPAR DATUM). FWD AND AFT DRAG ANGLE WERE REPAIRED PER CRJ700 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 FWD AND AFT RH DRAG ANGLE BTW UNION OF VERTICAL STABILIZER AND FUSELAGE (67.5% REAR SPAR DATUM). FWD AND AFT DRAG ANGLE WERE REPAIRED PER CRJ700 SRM 55-31-00-201-001-A01