Gabardini Lictor

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 Fiat engine, and that Lictor 130 with a 130-hp de Havilland Gipsy Major engine built by Alfa Romeo. Development was abandoned at the same time as the firm was absorbed by Fiat in early 1936.

Lictor
Role Civil utility aircraft
Manufacturer Gabardini
First flight 1935
Number built 2


Specifications (Lictor 130)

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 ft2)
  • 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)

Armament

References

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


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