Engineering:Comp Air 10
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Short description: Kit aircraft
The Comp Air 10 is a turboprop-powered light civil utility aircraft manufactured in kit form. Very large for a homebuilt aircraft, it is configured as a mainly conventional high-wing monoplane with either taildragger or tricycle undercarriage. Its close-set twin tails are an unusual design feature for an aircraft in its class, intended to ensure that the aircraft can be parked inside standard-size hangars.[1]
A total of eleven examples had been completed and flown by the end of 2011.[1]
The company website does not list it as being in production in 2022.[2]
Specifications (typical Comp Air 10)
General characteristics
- Crew: one
- Capacity: nine passengers
- Length: 31 ft 0 in (9.45 m)
- Wingspan: 39 ft 0 in (11.89 m)
- Height: 8 ft 8 in (2.64 m)
- Wing area: 242 sq ft (22.5 m2)
- Empty weight: 2,750 lb (1,247 kg)
- Max takeoff weight: 5,200 lb (2,359 kg)
- Powerplant: 1 × Walter M601D turboprop, 657 shp (490 kW)
Performance
- Maximum speed: 193 kn (222 mph, 357 km/h)
- Range: 798 nmi (918 mi, 1,477 km)
- Rate of climb: 2,000 ft/min (10 m/s)
See also
Aircraft of comparable role, configuration and era
- Cessna 207
References
- ↑ 1.0 1.1 Vandermeullen, Richard: 2011 Kit Aircraft Buyer's Guide, Kitplanes, Volume 28, Number 12, December 2011, page 49. Belvoir Publications. ISSN 0891-1851
- ↑ Comp Air. "Home". compairaviation.com. http://www.compairaviation.com/.
External links
- Official website archives on Archive.org
Original source: https://en.wikipedia.org/wiki/Comp Air 10.
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