Gabardini Lictor
| 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 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.
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)
References
 |
Wikimedia Commons has media related to Gabardini. |
- Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. p. 230.
This article is issued from Wikipedia - version of the 6/23/2015. The text is available under the Creative Commons Attribution/Share Alike but additional terms may apply for the media files.