The Helio Courier is a cantilever high-wing light STOL utility aircraft designed in 1949. Around 500 of these aircraft were manufactured in Pittsburg, Kansas, from 1954 until 1974 by the Helio Aircraft Company. The design featured four leading edge slats that deployed automatically, and large trailing edge flaps. The engine was the 295 hp Lycoming GO-480, which had a gearbox that lowered the output RPM and allowed for the use of a large three-bladed propeller to further improve takeoff performance. Couriers were famous for their takeoffs, which often took only a few plane lengths and then climbed at very high angles. During airshow demonstrations, it was common for the aircraft to actually take off across a 100 - 200 foot wide runway. The geared engine, however, required constant maintenance and was a major downside to the design. During the early 1980s, new owners (Helio Aircraft Ltd.) made an attempt to build new aircraft with direct-drive Lycoming engines, to replace troublesome and expensive geared engines. In a further effort to reduce weight, a new composite landing gear was featured. The new models also featured modest winglets. Two models were produced, the H-800 and H-700. A total of 18 aircraft were built. The rights to the Helio Stallion and Helio Courier were acquired by Helio Aircraft of Prescott, Arizona. Design and development Professor Otto C. Koppen designed aircraft for the Stout Metal Airplane Division of the Ford Motor Company, including the Ford Flivver, an aircraft that was supposed to be mass-produced by Ford. Koppen went on to design the Helio Courier. The demonstrator for the Courier's concept, "Helioplane #1", was converted by the then-local Wiggins Airways firm from a Piper PA-17 Vagabond Trainer, one of the so-named "short-wing Pipers" in production following World War II. Only the cabin area of the PA-17's original airframe remained unmodified, with the fuselage lengthened by four feet (1.2 meters), given a taller fin-rudder unit, clipped the Vagabond's stock 29 ft-3 inch (8.92 meter) wingspan down to only some 28.5 feet (8.7 meters), fitted the shortened wings with full-span leading-edge slats, long-span wing flaps that forced the ailerons to be much diminished in their span - only occupying the two outermost rib bays inboard of the wingtip; and a longer-travel main landing gear of a taller design, not unlike that of the 1930s-origin Fieseler Fi 156 German military short take-off and landing (STOL) pioneer aircraft. The powerplant