Patent ID: 7527223

Claim:
An attachment system for coupling a first airplane section to a second airplane section comprising: an attachment section comprising a top, a bottom, a first end, and a second end, said attachment section comprising a first clamp section and a second clamp section coupled to said top, wherein the first clamp section is in the form of a hook, coupled to said bottom is a first button, wherein said second clamp section comprises a clamping tower coupled to said attachment section top in an area of said attachment section second end, wherein a vibration isolator mount is attached to the end of the clamping tower and to said first airplane section, such that the first airplane section is coupled between said hook and said clamping tower, the clamping tower only being in contact with the first airplane section at the vibration isolator mount; and a mount section comprising a top and a bottom, such that said mount section bottom couples to the second airplane section, said mount section further comprising a track coupled to said mount section top, wherein said track comprises an open end comprising outwardly tapered edges and a closed end, wherein said mount section comprises a substantially flat base capable of being bonded to an airplane section, and wherein said substantially flat base forms a pocket with said track; and whereby said first button slides into said track for coupling said attachment section to said mount section; wherein said clamping tower extends at an acute angle relative to said attachment section top; and wherein said first button comprises a cylindrical base portion and a flat cylindrical head.