What was found
THE TAIL CONE DID NOT COMPLETELY RELEASE FROM AIRCRAFT WHEN OPERATED FROM AFT VENTRAL DOOR. THE FRAYED CABLE WAS REPLACED AND RIGGED IAW MM 53-53-0.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
THE TAIL CONE DID NOT COMPLETELY RELEASE FROM AIRCRAFT WHEN OPERATED FROM AFT VENTRAL DOOR. THE FRAYED CABLE WAS REPLACED AND RIGGED IAW MM 53-53-0.