Machine and apparatus for ultra-short take off and landing fixed wing aircraft

An airplane comprising:

• a fuselage, having a nose and a tail;
• a wing comprising port and starboard wing sections, wherein each wing section further comprises a structure integrating aerodynamic elements, including:
• a wing section body, having a top surface and a bottom surface, a leading edge and a trailing edge, and a wing section span, or a distance between a wing section tip and a wing section root connected to the fuselage body, and a flap cove;
• a Fowler flap, having a leading edge and a trailing edge, as well as a span and an effective span;
• flap tracks, wherein the flap tracks are external to the wing section body and extend aftward beyond the trailing edge of the wing section, and wherein the flap tracks are configured to enable the Fowler flap to rotate and deflect at an angle inclined compared to the top surface of the wing section body and to translate, or extend aftward out of the flap cove towards the tail and retract forward into the flap cove towards the nose, and wherein a flap gap or slot between the Fowler flap and the flap cove remains constant from an inboard end of the spoileron to an inboard end of the Fowler flap throughout all deployed positions;
• a Frise aileron having an aileron hinge, a leading edge and a trailing edge, a span, and a mass balance, wherein the Frise aileron is located outboard of the Fowler flap;
• and
• a spoileron, having a leading edge and a trailing edge, and a span, wherein the spoileron is located over the leading edge of the Fowler flap when the flap is in the fully extended position.