The concept for the horizontall tail surface is based upon the conventional tail design option for the stock aircraft. While the vertical tail surface needed to be enlarged the horizontal surface was reasonable sized after the 12" aft fuselage was counted for. Both of the tail surfaces differ from the Cruiser conventional tail option in that they use the NACA 0010-64 airfoil. This is a variation on the very common NACA 0010 that shifts the point of maximun thicknedd aft so a deeper spar can be used to provide greater strength.
1) A top view of the aircraft which shows the overall appearance and size of the horizontal tail.
2) This shows the details of the Horizontal Stabilizer and Elevator.
Top View of Aircraft Showing Horizontal Tail Location
