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.

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 (345 mph; 556 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

External links

Wikimedia Commons has media related to Comp Air.

Comp Air 12 on manufacturer's website

Comp Air

Aircraft	Merlin Comp Air 3 Comp Air 4 Comp Air 6 Comp Air 7 Comp Air 8 Comp Air 9 Comp Air 10 Comp Air 11 Comp Air 12 Comp Air Jet

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Comp Air 12

Specifications (as designed)

See also

External links