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
General information
Type	Military trainer
Manufacturer	CANSA
Designer	Giacomo Mosso and Isidoro Martignago
Number built	2
History
First flight	30 June 1941

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)