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The 400A has undergone vast design improvements from the original 400.  It is mainly constructed of aerospace light alloys.  Three separate fueling ports (one in each wing and one in the fuselage) combine to hold 4,911 lbs of fuel.  The fuselage’s new fuel tank located under the floor allows more cabin space.  The aircraft is designed to consume fuel in the fuselage compartment first to steady the wings’ bending moment.  Additionally, the brakes incorporate anti-skid logic to allow a greater maximum landing weight.