Patent ID: 6889939
Filing Date: 2005-05-10
Classification: B64C,B64D,F16B,Y10S,Y10T

Abstract:
1. A fastener apparatus for attaching a member to a structure of an aircraft, said fastener apparatus comprising: a shank having a first end and a second end opposite side first end, said first end having a head portion, said second end having an external threaded portion and a plain non-thread shank portion between said head portion and said threaded portion, said second end further having an internally threaded hole therein; a lock nut member mounted to said external threaded portion of said second end of said shank to lock said shank to said structure of said aircraft; and means for attaching said member to said shank, said attachment means having an externally threaded portion at one end thereof and a means for mounting at an opposite end thereof, said externally threaded portion of said attaching means being complimentary to said internally threaded hole of said shank.