What was found
THE FORCE REQUIRED TO RELEASE TAIL CONE DURING FUNCTIONAL CHECK WAS EXCESSIVE. THE TAIL CONE HUNG UP ON RIGHT SIDE LATCH PINS. A SERVICEABLE TAIL CONE WAS INSTALLED AND ADJUSTED IAW MM 53-53-00.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
THE FORCE REQUIRED TO RELEASE TAIL CONE DURING FUNCTIONAL CHECK WAS EXCESSIVE. THE TAIL CONE HUNG UP ON RIGHT SIDE LATCH PINS. A SERVICEABLE TAIL CONE WAS INSTALLED AND ADJUSTED IAW MM 53-53-00.