Gabardini Lictor
From Wikipedia, the free encyclopedia
| Lictor | |
|---|---|
| Type | Civil utility aircraft |
| Manufacturer | Gabardini |
| Maiden 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 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.
[edit] 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)
[edit] References
- Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions, 230.
[edit] See also
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