Comp Air 12

Comp Air CA12
General information
Type	Civil utility aircraft
National origin	United States
Manufacturer	Comp Air

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 (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

• Aerocomp Comp Air Jet

External links

• Official website

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