Comp Air 12

The Comp Air CA12 is a turboprop-powered civil utility aircraft, currently under development. Comp Air is seeking certification. It is configured as a conventional, low-wing monoplane with tricycle undercarriage. The first flight was on April 14, 2007.

Comp Air CA12
Role Civil utility aircraft
National origin United States
Manufacturer Comp Air

Specifications (as designed)

General characteristics

  • Crew: 1
  • Capacity: 8 to 10
  • Length: 41 ft 5 in (12.62 m)
  • Wingspan: 48 ft (15 m)
  • Wing area: 300 sq ft (28 m2)
  • Empty weight: 5,880 lb (2,667 kg)
  • Max takeoff weight: 10,800 lb (4,899 kg)
  • Powerplant: 1 × Honeywell TPE331-14GR turboprop, 1,650 hp (1,230 kW)

Performance

  • Cruise speed: 300 kn (350 mph, 560 km/h)
  • Stall speed: 73 kn (84 mph, 135 km/h)
  • Range: 2,535 nmi (2,917 mi, 4,695 km)
  • Rate of climb: 2,800 ft/min (14 m/s) at gross weight
  • Wing loading: 35 lb/sq ft (170 kg/m2)

Avionics
Sebastian Communication / OP Technologies

See also

Related development


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