What was found
INSPECTION FOUND UPPER LEFT O/B AREA OF TAIL CONE RELEASE CABLE FRAYED. THE CABLE WAS REPLACED AND TAIL CONE RELEASE MECHANISM WAS RIGGED IAW MM 53-53-00.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND UPPER LEFT O/B AREA OF TAIL CONE RELEASE CABLE FRAYED. THE CABLE WAS REPLACED AND TAIL CONE RELEASE MECHANISM WAS RIGGED IAW MM 53-53-00.