Gabardini Lictor
(Redirected from CANSA Lictor 90)
| Lictor | |
|---|---|
| Role | Civil utility 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)[edit]
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[edit]
- Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. p. 230.
