CANSA C.6
The CANSA C.6 was a training biplane developed in Italy during World War II. It was intended as an aerobatic intermediate trainer for the Regia Aeronautica and was of conventional tailskid configuration with a single-bay wing cellule with swept outer panels. Two prototypes were constructed, the single-seat C.6 and the two-seat C.6B, but no production order ensued.
| C.6 Falchetto | |
|---|---|
| Role | Military trainer |
| Manufacturer | CANSA |
| Designer | Giacomo Mosso and Isidoro Martignago |
| First flight | 30 June 1941 |
| Number built | 2 |
Specifications (C.6B)
General characteristics
- Crew: Two, pilot and instructor
- Length: 7.83 m (25 ft 8 in)
- Wingspan: 8.65 m (28 ft 4 in)
- Height: 3.10 m (10 ft 2 in)
- Wing area: 21.7 m2 (233 sq ft)
- Empty weight: 930 kg (2,050 lb)
- Gross weight: 1,255 kg (2,767 lb)
- Powerplant: 1 × Isotta Fraschini Beta RC.10 , 209 kW (280 hp)
Performance
- Maximum speed: 162 km/h (260 mph, 230 kn)
- Range: 1,150 km (717 mi, 623 nmi)
- Service ceiling: 6,500 m (21,320 ft)
References
- Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. p. 230.
- World Aircraft Information Files. London: Bright Star Publishing. pp. File 891 Sheet 06.
- aerei-italiani.net
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