US Patent 10553993 Avionics system interface electrical connector

An electrical connector includes a first pass-through connector, a second pass-through connector, and a center portion coupled between the first pass-through connector and the second pass-through connector. The center portion includes a plurality of electrical connection points on an exterior surface of the center portion. The electrical connector also includes a plurality of pass-through wires extending from the first pass-through connector to the second pass-through connector through the center portion, wherein the plurality of electrical connection points are electronically coupled to the plurality of pass-through wires.