An electric power generation and distribution system includes a primary distribution panel, which preferably operates at 230 VAC, and a High Voltage Direct Current (HVDC) panel in direct electrical communication therewith. The HVDC panels power motor controllers which drive electric motors residing in the center or aft sections of the aircraft. As many of the large electrical loads are located in the aft section of the aircraft, an aft electronics bay is located adjacent the aircraft wing roots to house the primary distribution panels and the HVDC panels.