What was found
THE FORCE REQUIRED TO PULL EXTERIOR AND INTERIOR TAIL CONE RELEASE HANDLES FROM THEIR RETAINING CLIPS EXCEEDED LIMITS. THE CLIPS WERE ADJUSTED AND TESTED 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 PULL EXTERIOR AND INTERIOR TAIL CONE RELEASE HANDLES FROM THEIR RETAINING CLIPS EXCEEDED LIMITS. THE CLIPS WERE ADJUSTED AND TESTED IAW MM 53-53-00.