of the present invention will now be described in detail as illustrated in fig1 and 2 any number of seat groups 24 are secured to the seat track 26 by a suitable fastening device such as the bolt 32 the foot 34 is secured to the legs 30 of any number of seat groups to provide connections to internal wiring 44 of the seat groups 24 the wiring 44 can be connected to for example a power outlet or in flight entertainment system to provide a power data connection between neighboring seat groups 24 each equipped with the foot 34 the cover 28 outfitted with the tube assembly 70 is inserted at the seat track 26 between the feet 34 of the neighboring seat groups 24 specifically the cover 28 is pre cut such that it has a length equal to the distance between the feet 34 of neighboring seat groups 24 desired by the operator of the aircraft 10 the reference marks 45 which indicate the position of the pin 40 provide a guide to ensure that the cover 28 is cut to a proper length the cover 28 can be wedged or u201c inch wormed u201d over the seat track 26 between the neighboring feet 34 to provide an electrical data connection between the neighboring seat groups 24 in particular the cover 28 is positioned so that the pin 40 is inserted within the inner conductive inner layer 74 of the tube assembly 70 and an end portion of the cover 28 is received by the receptacle 38 the pin 40 is locked within the tube assembly 70 by the force exerted by.