- Comp Air 10
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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 largely conventional high-wing monoplane with either taildragger or tricycle undercarriage. Its close-set twin tails are an unusual design feature for aircraft in its class, intended to ensure that the aircraft can be parked inside standard-size hangars.
Specifications (typical Comp Air 10)
General characteristics
- Crew: one pilot
- Capacity: 9 passengers
- Length: 31 ft 0 in (9.45 m)
- Wingspan: 36 ft 6 in (11.89 m)
- Height: 8 ft 8 in (2.64 m)
- Wing area: 242 ft² (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: 222 mph (356 km/h)
- Range: 918 miles (1,472 km)
- Rate of climb: 2,000 ft/min (610 m/min)
See also
- Aircraft of comparable role, configuration and era
- Cessna 207
External links
Comp Air Aircraft Merlin · Comp Air 3 · Comp Air 4 · Comp Air 6 · Comp Air 7 · Comp Air 8 · Comp Air 9 · Comp Air 10 · Comp Air 11 · Comp Air 12 · Comp Air JetLists relating to aviation General Aircraft (manufacturers) · Aircraft engines (manufacturers) · Airlines (defunct) · Airports · Civil authorities · Museums · Registration prefixes · Rotorcraft (manufacturers) · TimelineMilitary Accidents/incidents Records Categories:- Comp Air aircraft
- Homebuilt aircraft
- United States civil utility aircraft 1990–1999
- Single-engine aircraft
- 1990s aircraft stubs
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