avia.wikisort.org - Aeroplane

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.

Lictor
Role	Civil utility aircraft Type of 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 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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