title: CANSA C.6
text: # 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.
  
  ## 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 $m^2$ (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)
  