CAB Minicab

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GY-20 Minicab
Type Utility aircraft
Manufacturer Constructions Aéronautiques du Béarn
Designed by Yves Gardan
Maiden flight 1 February 1949
Number built 30 + ca. 130 homebuilt

The CAB Minicab was a two-seat light aircraft built in France in the years following World War II. Its design was in essence a scaled-down version of a plane that Yves Gardan had designed for SIPA, the SIPA 90. It was a conventional, low-wing cantilever monoplane with fixed tailwheel undercarriage. The pilot and passenger sat side-by-side and accessed the cockpit via a one-piece perspex canopy that hinged forwards. Gardan's intention was to produce a low-cost, easy to fly, easy to maintain aircraft with the possibility of homebuilding; a "Simca of the air".

The Minicab's first flight took place on 1 February 1949 with Max Fischl at the controls. French type certification was obtained in mid-April and a period of intense promotional activity followed. By the end of 1950, a Minicab had won the coupe de vitesse de Deauville (Deauville Cup for speed), and the grand prix aérien de Vichy (Vichy Aerial Prize). The following year, a Minicab broke the world air distance record for its class (1,825 km, 1,138 miles) and in 1952 the world airspeed record for its class over a 2,000 km circuit, with an average speed of (183 km/h, 114 mph).



[edit] Variants

  • GY-20 - original production model



[edit] Specifications (GY-20)

General characteristics

  • Crew: one pilot
  • Capacity: 1 passenger
  • Length: 5.45 m (17 ft 11 in)
  • Wingspan: 7.60 m (24 ft 11 in)
  • Height: 1.65 m (5 ft 5 in)
  • Wing area: 10.0 m² (108 ft²)
  • Empty weight: 265 kg (584 lb)
  • Gross weight: 480 kg (1,058 lb)
  • Powerplant: 1 × Continental A65 horizontally-opposed four-cylinder air-cooled engine, 48 kW (65 hp)

Performance

  • Maximum speed: 198 km/h (123 mph)
  • Range: 500 km (310 miles)
  • Service ceiling: 4,000 m (13,120 ft)

[edit] References


[edit] See also

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