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Corvus Racer 312

From Wikipedia, the free encyclopedia

Racer 312
Role Ultralight aircraft and Light-sport aircraft
National origin China
Manufacturer Corvus Aerospace (Suzhou)
First flight 1 November 2013
Status Under development (2015)

The Corvus Racer 312 is a Chinese ultralight and light-sport aircraft under development by Corvus Aerospace (Suzhou) of Suzhou and first flown 1 November 2013. The aircraft is to be supplied complete and ready-to-fly.[1]

Design and development

The Racer 312 was designed as a smaller version of the Corvus Racer 540, to comply with the Fédération Aéronautique Internationale microlight rules and US light-sport aircraft rules. It was designed and the prototype built over a period of 13 months in 2012–13.[1]

The Racer 312 features a cantilever low-wing, two-seats-in-side-by-side configuration under a bubble canopy, fixed tricycle landing gear and a single engine in tractor configuration. The aircraft is made from composite material and its 8.33 m (27.3 ft) span wing employs split flaps. The standard engine fitted is the 100 hp (75 kW) Rotax 912ULS four-stroke powerplant. With this engine the cruise speed is anticipated to be 280 km/h (174 mph).[1]

As of February 2017, the design does not appear on the Federal Aviation Administration's list of approved special light-sport aircraft.[2]

Specifications (Racer 312)

Data from Tacke[1]

General characteristics

  • Crew: one
  • Capacity: one passenger
  • Wingspan: 8.33 m (27 ft 4 in)
  • Empty weight: 295 kg (650 lb)
  • Gross weight: 472.5 kg (1,042 lb)
  • Fuel capacity: 108 litres (24 imp gal; 29 US gal)
  • Powerplant: 1 × Rotax 912ULS four cylinder, liquid and air-cooled, four stroke aircraft engine, 75 kW (101 hp)
  • Propellers: 3-bladed composite

Performance

References

  1. ^ a b c d Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 40. Flying Pages Europe SARL, 2015. ISSN 1368-485X
  2. ^ Federal Aviation Administration (26 September 2016). "SLSA Make/Model Directory". Retrieved 3 February 2017.

External links

This page was last edited on 9 August 2023, at 23:12
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