What was found
DURING AN ABCD STRUCTURAL INSPECTION, THE RT FUSELAGE CLOSING ANGLE WAS FOUND CRACKED 2.4 INCHES. THE CRACK WAS REPAIRED IN ACCORDANCE TO THE BEECH SRM 53-90-23 AND RAYTHEON AIRCRAFT COMPANY FIELD REPAIR FR-CO-00934
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING AN ABCD STRUCTURAL INSPECTION, THE RT FUSELAGE CLOSING ANGLE WAS FOUND CRACKED 2.4 INCHES. THE CRACK WAS REPAIRED IN ACCORDANCE TO THE BEECH SRM 53-90-23 AND RAYTHEON AIRCRAFT COMPANY FIELD REPAIR FR-CO-00934