What was found
THE FORCE REQUIRED TO DROP THE TAIL CONE USING INTERIOR AND EXTERIOR RELEASE HANDLES EXCEEDED 35 POUNDS. THE TAIL CONE RELEASE SYSTEM CABLES WERE 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 DROP THE TAIL CONE USING INTERIOR AND EXTERIOR RELEASE HANDLES EXCEEDED 35 POUNDS. THE TAIL CONE RELEASE SYSTEM CABLES WERE ADJUSTED IAW MM 53-53-00.