Aerocomp Comp Air 12

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The Aerocomp Comp Air 12 is a turboprop-powered civil utility aircraft currently under development. Despite its large size (with up to twelve seats), it is intended to be marketed as a homebuilt aircraft. It is configured as a conventional, low-wing monoplane with tricycle undercarriage. The first flight is anticipated in mid-2005.

[edit] Specifications (as designed)

[edit] General characteristics

  • Crew: one pilot
  • Capacity: 11 passengers
  • Length: ft in ( m)
  • Wingspan: ft in ( m)
  • Height: ft in ( m)
  • Wing area: ft² ( m²)
  • Empty: lb ( kg)
  • Loaded: lb ( kg)
  • Maximum takeoff: lb ( kg)
  • Powerplant: 1× Lycoming T53 turboprop, 1,400 shp (1,044 kW)

[edit] Performance

  • Maximum speed: 318 mph (509 km/h)
  • Range: 3,241 miles (5,185 km)
  • Service ceiling: ft ( m)
  • Rate of climb: ft/min ( m/min)
  • Wing loading: lb/ft² ( kg/m²)
  • Power/Mass: hp/lb ( kW/kg)

[edit] External link

[edit] Related content

Related development: Aerocomp Comp Air Jet

Comparable aircraft:

Designation sequence: Comp Air 7 - Comp Air 8 - Comp Air 10 - Comp Air 12

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