CANSA C.6

C.6 Falchetto
General information
TypeMilitary trainer
ManufacturerCANSA
Designer
Giacomo Mosso and Isidoro Martignago
Number built2
History
First flight30 June 1941

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.

Specifications (C.6B)

Data from Dimensione Cielo[1]

General characteristics

  • Crew: Two, pilot and instructor
  • Length: 7.83 m (25 ft 8 in)
  • Wingspan: 8.65 m (28 ft 5 in)
  • Height: 3.10 m (10 ft 2 in)
  • Wing area: 21.67 m2 (233.3 sq ft)
  • Empty weight: 930 kg (2,050 lb)
  • Gross weight: 1,255 kg (2,767 lb)
  • Powerplant: 1 × Isotta Fraschini Beta RC.10 , 210 kW (280 hp)

Performance

  • Maximum speed: 260 km/h (160 mph, 140 kn)
  • Stall speed: 90 km/h (56 mph, 49 kn)
  • Range: 650 km (400 mi, 350 nmi)
  • Service ceiling: 6,500 m (21,300 ft)
  • Time to altitude: 7 minutes to 3,000 m (9,800 ft)

References

  1. ^ Brotzu & Cosolo 1977, p. 73.
  • Brotzu, E.; Cosolo, G. (1977). Dimensione Cielo: Aerei italiani nella 2a guerra mondiale: Vol. 11 Scuola-Collegamento (in Italian). Rome: Edizioni Dell'Ateneo & Bizzarri.
  • 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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