The Aerauto PL.5C was a roadable aircraft developed in Italy in the early 1950s. It was a high-wing two-seat monoplane whose wings could be folded to quickly transform it into an automobile. It was different from many such projects in that it used its pusher propeller for propulsion not only in the air, but on the road as well. Development was abandoned in 1953.
The MKEK-4 Uğur was a basic trainer aircraft which was used by the Turkish Air Force between 1955-1963. Originally developed as the THK-15, in total 57 Uğurs were produced in Turkey, all of which were used in the Turkish AF Flight School except three which were donated to the Royal Jordanian Air Force.
The Dornier Do 27 was a German single-engine STOL utility aircraft, manufactured by Dornier GmbH. Configuration was a classic high-wing, "tail-dragger" aircraft with fixed landing gear.
The Auster J/2 Arrow is a 1940s British single-engined two-seat high-wing touring monoplane built by Auster Aircraft Limited at Rearsby, Leicestershire, England.
The Agusta CP-110, also known as CVV P.110 or Politecnico P.110, was a prototype Italian four-seat light aircraft first flown in 1951 that failed to attract interest from either civil or military operators, although it was evaluated by the Aeronautica Militare. Originally designed and built by the CVV -, production aircraft were to have been built by Agusta, but for lack of interest.
The Avions Fairey Belfair, also known as the Tipsy Belfair after its designer, Ernest Oscar Tips, was a two-seat light aircraft built in Belgium following World War II.
The Widerøe C.5 Polar, sometimes known as the Honningstad C.5 Polar, was a Norwegian general-purpose land or floatplane built by Widerøes Flyveselskap.
The CAP-1 Planalto was a military trainer aircraft built in Brazil during World War II. It was a low-wing cantilever monoplane with fixed tailwheel undercarriage that accommodated the pilot and instructor in tandem open cockpits. The project had been initiated by Instituto de Pesquisas Tecnológicas (IPT) under the designation IPT-4 and although the design work had been contracted to CAP, IPT insisted on a wing profile of its own choosing that led to serious stability problems in the final product.
The Colonial Model C-1 Skimmer was an American small single-engined amphibian flying boat built by the Colonial Aircraft Corporation. It was the start of a line of very similar aircraft designed by David Thurston.
The Hindustan HT-2 is an Indian two-seat primary trainer designed and built by Hindustan Aeronautics Limited. The HT-2 was the first company design to enter production in 1953 for the Indian Air Force and Navy, where it replaced the de Havilland Tiger Moth. The HT-2 is a low-wing cantilever monoplane with a fixed tailwheel landing gear. Powered by a 155 hp (116 kW) Cirrus Major III piston engine, the aircraft has enclosed tandem cockpits with dual controls. Apart from military use, the aircraft was also used by Indian flying schools.
The SIAI-Marchetti SM.102 was a 1940s Italian light transport cabin monoplane designed and built by SIAI-Marchetti.
The SIAI-Marchetti SM.101 was a 1940s Italian single-engined light transport cabin monoplane designed and built by SIAI-Marchetti.
The NAC Fieldmaster was a British agricultural aircraft of the 1980s. A turboprop powered single-engined monoplane, it was built in small numbers and used both as a cropsprayer and a firefighting aircraft.
The Mráz M-3 Bonzo was a light aircraft built in Czechoslovakia in 1948 as a further development in the family of light aircraft that had commenced with the M-1 Sokol. The Bonzo was based on the Sokol airframe, but with a redesigned wing and substantial changes to the fuselage. These included lengthening it to allow for the addition of a fourth seat, reducing the height of the rear fuselage to allow for a new cabin with all-around visibility, and the addition of a semi-retractable nosewheel in place of a tailwheel.
The THK-16 Mehmetçik was an aircraft designed in Turkey in the early 1950s to provide the Turkish Air Force with a domestically designed and built jet trainer. The project was cancelled without the aircraft having been built.
The THK-5 was a twin-engine aircraft developed bt in Turkey in 1945 as an air ambulance. It was a conventional, low-wing cantilever monoplane of wooden construction throughout. The main units of the tailwheel undercarriage retracted into the wing-mounted engine nacelles and the THK-5 could carry two stretcher cases plus a medical attendant. This was followed in production by a six-seat utility transport version designated THK-5A and three examples of an improved version of the 5A designated THK-10. A single example of the type was exported, sold to Denmark.
The Custer CCW-5 was a twin-engined, 5-seat aircraft of pusher configuration, which used a channel wing claimed to enable low speed flight and short take-offs. Two CCW-5s flew, eleven years apart, but the type never entered production.
The Nuri Demirağ Nu D.36 was a 1930s Turkish two-seat training biplane built by the Nuri Demirağ Aircraft Works in Istanbul for the Turkish military.
The THK 11 was a 1940s prototype Turkish four-seat monoplane, designed and built by Türk Hava Kurumu.
The THK-13 was an experimental tail-less glider built by the Turk Hava Kurumu Ucak Fabrikasi (THK) in Turkey in the late 1940s.
