Gabardini Lictor
Lictor | |
---|---|
Role | Civil utility aircraft Type of aircraft |
Manufacturer | Gabardini |
First flight | 1935 |
Number built | 2 |
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)
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
- Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. p. 230.
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Gabardini and CANSA aircraft
- monoplane
- biplane
- G.4
- G.6
- G.8
- G.9
- G.51
- A.300
- Lictor
- Lictor 130
- C.4
- C.5
- C.6
- FC.12
- FC.20
- FC.12
- FC.20