What was found
THE INTERIOR TAIL CONE RELEASE HANDLE PULL FORCE WAS EXCESSIVE. THE TAIL CONE HANDLE CLIPS 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 INTERIOR TAIL CONE RELEASE HANDLE PULL FORCE WAS EXCESSIVE. THE TAIL CONE HANDLE CLIPS WERE ADJUSTED IAW MM 53-53-00.