Related Research Articles
The Chasle YC-12 Tourbillon ("Whirlwind") was a single-seat light sporting aircraft developed in France in the mid-1960s and marketed for homebuilding via plans. It was a low-wing cantilever monoplane of conventional configuration. As designed, it featured fixed tailwheel undercarriage, but it could also be fitted with fixed tricycle gear.
The Croses EC-6 Criquet ("Locust") is a 1960s French two-seat homebuilt aircraft designed by Emilien Croses.
The Fokker S.IV was a military trainer aircraft produced in the Netherlands in the mid-1920s. It was a conventional, single-bay biplane with staggered wings of unequal span braced with N-struts, essentially a radial-engined development of the S.III. The pilot and instructor sat in tandem, open cockpits and the undercarriage was of fixed, tailskid type with a cross-axle between the main units. The Royal Netherlands Army Aviation Group purchased 30 examples and used them right up to the German invasion of the Netherlands in 1940. On 14 May that year, a few surviving S.IVs escaped to France alongside some S.IX trainers, but never flew again.
The Maestranza Central de Aviación HF XX-02 was a military trainer aircraft developed in Chile in the 1950s.
The Hopfner HS-5/28 was a utility aircraft built in Austria in the late 1920s. It was a conventional, parasol-wing monoplane with seating for two occupants in tandem, open cockpits. The landing gear was of fixed, tailskid type with divided main units. Two examples were built with Walter NZ60 engines, followed by two more with the more powerful NZ85 for Swiss aeroclub use. One of these latter machines remained in service until 1934.
The Nord 1601 was a French aerodynamic research aircraft designed and built by Nord Aviation. The aircraft was designed to investigate the aerodynamics of swept wings and related high-lift devices.
The IAR-824 was a utility aircraft built in Romania in the 1970s.
The LVG C.V was a reconnaissance aircraft produced in large numbers in Germany during World War I.
The Mitsubishi 2MB1 was a light bomber produced in Japan in the mid-1920s to equip the Imperial Japanese Army.
The Morane-Saulnier MS.138 was a military trainer aircraft produced in France in the late 1920s,
The Morane-Saulnier MS.147 and its derivatives, the MS.148 and MS.149 were a family of trainer aircraft produced in France in the late 1920s for civil and military use. They were derived from other machines in Morane-Saulnier's successful line of monoplane trainers, combining the wire-braced parasol wing of the MS.138 with the fuselage and undercarriage of the MS.130.
The IMAM Ro.5 was a sport aircraft produced in Italy in the late 1920s. It was a conventional, parasol wing monoplane with fixed tailskid undercarriage and two open cockpits in tandem. It proved popular with private owners and flying clubs, and was built in large numbers. Some Ro.5s were purchased by the Regia Aeronautica for use as trainers and liaison aircraft. A later version, the Ro.5bis, enclosed the cockpits under a long canopy.
The SABCA S.2 was an airliner built in Belgium in 1926. It was a conventional, high-wing cantilever monoplane with fixed, tailskid undercarriage. The flight deck was open, but the passenger cabin was fully enclosed. Power was provided by a single engine in the nose, driving a two-blade propeller, and whose exhaust was collected in a single stack that extended up over the wing. Metal was construction throughout, with corrugated skin. Only a single example was built, which served with SABENA.
The Partenavia P.70 Alpha was a 1970s Italian two-seat light aerobatic trainer designed by Luigi Pascale and built by Partenavia.
The SITAR GY-100 Bagheera was a light aircraft designed and built in France in the late 1960s. Designed by Yves Gardan, it was a low-wing, cantilever monoplane of conventional layout with fixed, tricycle undercarriage. The fully enclosed cabin had seating for up to four people in 2+2 configuration. Construction was of metal throughout.
The SECAT S-5 was a light, high-wing, two-seat touring monoplane aircraft, designed and built by the Société d'Etudes et de Construction d'Avions de Tourisme in France shortly after the end of World War II. Only one example of the type was ever built, and it flew for a variety of private owners for several decades.
The SECAT RG-75 was a light utility monoplane built in France shortly after World War II. It was a conventional cabin monoplane with two seats side-by-side. The wing was mounted high and was of fully cantilever design. The conventional undercarriage consisted of two fixed, divided main units plus a fixed tailskid. Power was supplied by a tractor-mounted piston engine that drove a two-bladed propeller. Construction was of wood throughout, covered in plywood.
The Spartan C2 is a light aircraft produced in the United States in the early 1930s as a low-cost sport machine that would sell during the Great Depression.
The S.E.C.A.T.-VI La Mouette or S.E.C.A.T. 60T La Mouette was a French two seat tourer built shortly before the outbreak of World War II.
The Gaucher RG.40 Week-End was a high-wing, two-seat, low-power, touring aircraft built in France in 1935. Three were built and later SECAT produced several rather similar designs, all from designer Rémy Gaucher.
References
- Bridgeman, Leonard (1948). Jane's All the World's Aircraft 1948. London: Sampson Low Marston. pp. 153c.
- Gaillard, Pierre (2002). "Les avions de la SECAT". Les Cahiers du RSA. Paris: Le Réseau du Sport de l'Air (239): 40–41.
- The Illustrated Encyclopedia of Aircraft. London: Aerospace Publishing. p. 2839.
- Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. p. 797.