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)

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General characteristics

Crew: one pilot
Capacity: 8 to 10
Length: 41' 5" ()
Wingspan: 48' ()
Height: ()
Wing area: 300 sq ft ()
Empty weight: 5880 lb. ()
Useful load: 5,000 lb ()
Max takeoff weight: 10,800 lb. ()
Powerplant: 1 × Honeywell TPE331-14GR turboprop, 1,650 shp ()

Performance

Cruise speed: 300 knots.
Stall speed: 73 knots. ()
Range: 2535 nm. ()
Rate of climb: 2800 ft/min (at gross) ()
Wing loading: 35 lbs./sq. ft. ()

Avionics
Sebastian Communication / OP Technologies

External links

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