Jump to content

Comp Air 10

Edit links
From Wikipedia, the free encyclopedia

This is an old revision of this page, as edited by VKras (talk | contribs) at 12:30, 19 December 2019. The present address (URL) is a permanent link to this revision, which may differ significantly from the current revision.

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]

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

References

  1. ^ a b Vandermeullen, Richard: 2011 Kit Aircraft Buyer's Guide, Kitplanes, Volume 28, Number 12, December 2011, page 49. Belvoir Publications. ISSN 0891-1851
Wikimedia Commons has media related to Comp Air.


Stub icon

This article on an aircraft of the 1990s is a stub. You can help Wikipedia by expanding it.

Retrieved from "https://en.wikipedia.org/w/index.php?title=Comp_Air_10&oldid=931530029"