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The Cessna 414 is an American light, pressurized, twin-engine transport aircraft built by Cessna. It first flew in 1968 and an improved variant was introduced from 1978 as the 414A Chancellor.
The Brügger MB-1, MB-2 and MB-3 Colibri is a family of small sports aircraft designed in Switzerland in the 1960s and 1970s for amateur construction.
The Croses EC-9 Para-Cargo is a 1960s French six-seat tandem-wing cargo-carrying homebuilt aircraft designed by Emilien Croses.
The Hindustan Ardhra was a sailplane designed in India for pilot training by the government's Civil Aviation Department in the late 1970s as the ATS-1 Ardhra. It was a two-seat aircraft of conventional configuration and wooden construction. The Indian Air Force ordered fifty examples in the early 1980s to be produced by Hindustan Aeronautics and the type was approved for use for flying by cadets.
The Piel CP-30 Emeraude is an aircraft designed in France in the mid-1950s and widely built both by factories and homebuilders.
The Fauvel AV.50 Lutin was a design for an unorthodox light aircraft produced in France in the 1970s. Like some other Charles Fauvel designs, it was a tailless aircraft with a reverse-delta wing. In this case, it was a single-seater intended to be powered by a converted Volkswagen engine. Only one example was known to have been under construction by 1977, in Australia.
The IAR-46 is a very light two-seater airplane for flight schools, training and tourism. Construction uses conventional riveted joints. The seats are arranged side by side, the conventional left seat being the pilot or student pilot seat. The aircraft has a low trapezoidal wing, empennage in "T" configuration, semi-retractable landing gear (mechanical), with the tailwheel connected to the rudder.
The Jurca MJ-14 Fourtouna was a racing aircraft designed by Marcel Jurca in France in the late 1970s. It was an unconventional, low-wing cantilever monoplane with retractable tailwheel undercarriage. The fuselage had a low profile that required the pilot to sit in a reclined position. The vertical stabiliser was very small, but aft of the cockpit, the fuselage changed shape from being low and broad to being high and narrow. None have been completed.
The Lucas L5 was a sport aircraft designed in France in the late 1970s and marketed for amateur construction. It was a conventional, low-wing cantilever monoplane with side-by-side seating for two in a fully enclosed cabin. Construction was of metal throughout, and the builder was given the option of fixed, tricycle undercarriage, or tailwheel undercarriage in which the main units were manually retractable.
The MacDonald S-20 is a single-seat sport aircraft that was designed in the United States in the early 1970s and marketed for home building.
The McCarley Mini-Mac was a single-seat aerobatic sport aircraft designed in the United States in the early 1970s and marketed for home building. It was a conventional, low-wing cantilever monoplane with a cockpit enclosed by a bubble canopy. The undercarriage was of fixed, tricycle type with spats fitted to the prototype, as well as a small skid fitted as a tail bumper. Construction was of metal throughout.
The Miller WM-2 was a single-seat sport aircraft designed in the United States in the early 1970s and marketed for home building. Although primarily a powered aircraft, the WM-2's high aspect-ratio wings enabled the pilot to stop the engine and soar on thermals as with a sailplane.
The Mini-Hawk TH.E.01 Tiger-Hawk was a single-seat sport aircraft designed in the United States in the early 1970s and marketed for home building. It was a conventional, low-wing cantilever monoplane with a cockpit enclosed by a bubble canopy. The wings were detachable for ease of storage or towing and could be rigged in around ten minutes. The undercarriage was of fixed, tricycle type with spats fitted to the prototype. It was an all-metal construction, and the aircraft could be built from plans or a kit.
The Pazmany PL-4A is a single-seat, single-engine sport aircraft developed in the United States and first flown in 1972. It is marketed for homebuilding from plans, and 686 sets had sold by 1985. The PL-4A is a conventional, low-wing cantilever monoplane with an enclosed cabin and fixed, tailwheel undercarriage. The design features a T-tail, chosen to facilitate folding the wings. Construction throughout is of metal, using standard extruded sections for the longerons and pop rivets as the basic fastener. The standard powerplant is a Volkswagen air-cooled engine of 60 hp (45 kW) Construction time is estimated to be around 1,000–1,500 hours.
The PDQ Aircraft Products PDQ-2 is a very basic light aircraft originally built in 1973 in the United States, and marketed as plans for a homebuilt aircraft. It was a minimalist design, consisting of aluminum alloy tubes carrying the pilot's seat, a set of monoplane wings and a T-tail. The pilot's position was fully exposed at the front of the aircraft. Power is provided by a single engine mounted pusher-fashion on a pylon above the wings. Originally, this was a Rockwell JLO snowmobile engine, but Ison revised the design to use a converted Volkswagen engine, due to a lack of availability of the first choice of engine. The heavier Volkswagen engine required an increase in structural strength, and the design was revised accordingly. The wings have wooden spars with ribs, and skin of polyurethane foam, all coated in epoxy resin. Fixed, tricycle undercarriage was fitted.
The Piel CP.70 Beryl is a French twin-seat, single-engine sport aircraft designed by Claude Piel. It was first flown in France in the 1960s and marketed for amateur construction.
The Piel CP.80 Zephir , Piel CP.801 and Piel CP.802 are racing aircraft developed in France in the 1970s and marketed for homebuilding. They are compact, single-seat, single-engine monoplanes with low, cantilever wings.
The Piel CP.60 Diamant is a single-engine light aircraft designed in France in the 1960s and marketed for home building.
The Piel CP.500 was a light aircraft of unusual configuration designed in France in the 1970s with the intention of marketing it for homebuilding. This did not transpire, however, and no prototype was actually built. It was a tandem wing design, somewhat reminiscent of the Mignet Pou-du-Ciel but considerably larger. Also, unlike the Pou-du-Ciel's unusual control system, the CP.500's pitch and roll control was to come from more conventional elevons mounted on the rear wing. The rear wing was also to carry endplate-style fins and rudders. Twin engines were to be mounted in push-pull fashion at the nose and tail ends of the fuselage, with the aircraft capable of single-engine operation in case of emergency. Two seats were to be provided at the front of the fully enclosed cabin, with a bench seat for three passengers behind them, plus an optional seat for a sixth occupant behind this. The undercarriage was to be of fixed, tricycle configuration. Construction was originally planned to be of wood, with engine cowlings and wingtips of composite construction. However, as development progressed, Piel considered metal as the main construction material.
The Piel CP-150 Onyx is a single-seat, low-cost and low-power ultralight aircraft. The aircraft was designed by French aeronautical engineer Claude Piel. The aircraft is an all-wood single seat microlight based on Mignet principles with fixed tricycle undercarriage and one 12 hp Solo engine.
References
- Jane's All the World's Aircraft 1977–78. London: Jane's Publishing.
- Jane's All the World's Aircraft 1985–86 . London: Jane's Publishing.
- Rivet, Gilles (15 January 1988). "Le CP 90 Pinocchio II". Aviation & Pilot Privé (168): 42–44.
- Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. ISBN 0-7106-0710-5.