avia.wikisort.org - Aeroplane

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: × 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

External links

• Official website archives on Archive.org

На других языках

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- [en] Comp Air 10

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[fr] Aerocomp Comp Air 10

L'Aerocomp Comp Air 10 est un avion monoplan utilitaire léger turbopropulsé commercialisé en kit pour la construction amateur par la société américaine Aerocomp.

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