Comp Air 12
# 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 $m^2)$
* 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 $kg/m^2)$

Avionics Sebastian Communication / OP Technologies

