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Gabardini Lictor

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(Redirected from CANSA Lictor 90)
Lictor
General information
TypeCivil utility aircraft
ManufacturerGabardini
Number built2
History
First flight1935

The Gabardini Lictor was a light aircraft developed in Italy in the mid-1930s. It was a low-wing cantilever monoplane with fixed, tailwheel undercarriage and a fully enclosed cabin. Two versions were built, the Lictor 90 with a 90 hp (67 kW) Fiat engine, and that Lictor 130 with a 130 hp (97 kW) Alfa Romeo 110, a de Havilland Gipsy Major engine built by Alfa Romeo. Development was abandoned in early 1936 when the firm was absorbed by Fiat.

Specifications (Lictor 130)

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General characteristics

  • Crew: One pilot
  • Capacity: 2-3 passengers
  • Length: 8.15 m (26 ft 8 in)
  • Wingspan: 11.40 m (37 ft 5 in)
  • Wing area: 17.5 m2 (188 sq ft)
  • Empty weight: 650 kg (1,433 lb)
  • Gross weight: 1,000 kg (2,200 lb)
  • Powerplant: 1 × Alfa Romeo 110 , 97 kW (130 hp)

Performance

  • Maximum speed: 230 km/h (143 mph, 124 kn)

References

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  • Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. p. 230.