Aerocomp Comp Air 12
From Wikipedia, the free encyclopedia
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.
[edit] Specifications (as designed)
This aircraft article is missing some (or all) of its specifications. If you have a source, you can help Wikipedia by adding them.General characteristics
- Crew: one pilot
- Capacity: 8 to 10
- Length: 41' 5" ()
- Wingspan: 48' ()
- Height: ()
- Wing area: 300 sq ft ()
- Empty weight: 5880 lbs. ()
- Useful load: 5,000 lbs ()
- Max takeoff weight: 10,800 lbs. ()
- Powerplant: 1× Honeywell TPE331-14GR turboprop, 1,650 shp ()
Performance
- Cruise speed: 300 Kts.
- Stall speed: 73 Kts. ()
- Range: 2535 nm. ()
- Rate of climb: 2800 fpm (at gross) ()
- Wing loading: 35 lbs./sq. ft. ()
Avionics Sebastian Communication / OP Technologies
[edit] External links
[edit] See also
Related development Aerocomp Comp Air Jet
|
||||||||||||||
|
This article on an aircraft of the 2000s is a stub. You can help Wikipedia by expanding it. |
