Patent ID: 7370832
Filing Date: 2008-05-13
Classification: B64C,B64D

Abstract:
1. An aircraft, comprising: a fuselage operatively coupled to an airframe; a propulsion system operatively coupled to the airframe; a floor assembly disposed within and coupled to the fuselage, the floor assembly including at least one floor panel and an elongated support having a support surface engaged with the floor panel, the elongated support further including an engagement member having a plurality of coupling apertures disposed therein; a component disposed within the fuselage and having a support member positioned proximate the floor assembly; and an interface assembly including: at least one lug member operatively coupled to the base and moveable between a first position wherein the clamp arms are positioned in the unsecured position, and a second position wherein the clamp arms are positioned in the secured position, wherein in the second position, the lug member is inserted into an intermediate coupling aperture disposed in the engagement member between the associated coupling apertures.