Chasle Tourbillon

Chasle Tourbillon
YC-12 Tourbillon
The prototype Chasle Tourbillon at Chavenay-Villepreux airfield near Paris in June 1967
Role Recreational aircraft
Manufacturer Homebuilt
Designer Yves Chasle
First flight 9 October 1965

The Chasle YC-12 Tourbillon ("whirlwind") was a single-seat light sporting aircraft developed in France in the mid 1960s and marketed for homebuilding. 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.


Contents

Variants

  • YC-12 - prototype with Continental A65 engine
    • YC-121 - similar to prototype with enlarged tailfin for limited certification
    • YC-122 - similar to YC-121 but with Continental C90 engine
    • YC-123 - similar to YC-121 but with Potez 4E-20b engine


Specifications (typical YC-121)

General characteristics

  • Crew: One pilot
  • Length: 5.95 m (19 ft 6 in)
  • Wingspan: 6.70 m (22 ft 0 in)
  • Height: 2.40 m (7 ft 11 in)
  • Wing area: 7.5 m2 (81 ft2)
  • Empty weight: 285 kg (628 lb)
  • Gross weight: 432 kg (952 lb)
  • Powerplant: 1 × Continental A65, 49 kW (65 hp)

Performance

  • Maximum speed: 235 km/h (146 mph)
  • Range: 800 km (500 miles)

References

  • Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. pp. 254. 
  • Jane's All the World's Aircraft 1977-78. London: Jane's Yearbooks. pp. 484–85. 


See also


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