- Comp Air 12
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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: 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 TechnologiesSee also
- Related development
External links
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 JetLists relating to aviation General Aircraft (manufacturers) · Aircraft engines (manufacturers) · Airlines (defunct) · Airports · Civil authorities · Museums · Registration prefixes · Rotorcraft (manufacturers) · TimelineMilitary Accidents/incidents Records Categories:- Comp Air aircraft
- Single-engine aircraft
- United States civil utility aircraft 2000–2009
- 2000s aircraft stubs
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