Puneet Varma (Editor)

Comp Air 6

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Top speed
  
269 km/h

Length
  
7.47 m

Wingspan
  
11 m

Manufacturer
  
Comp Air

Comp Air 6 Comp Air 6 experimental aircraft

The Comp Air 6 is a light civil utility aircraft manufactured in the United States by Comp Air.

Contents

Design and development

Comp Air 6 Comp Air 6 Specifications A photo

The Comp Air 6 is a stretched and widened development of the four-seat Aerocomp CompMonster which had first flown on 3 April 1995.

Comp Air 6 Comp Air 6 Specifications A photo

The Comp Air 6 has a fore-and-aft fuselage splice to widen and lengthen the cabin from the original design. It is usually supplied in kit form. The design is configured as a conventional high-wing monoplane and may be built with either tricycle or tailwheel undercarriage and may alternately be equipped with floats as the CA6SF, amphibious as the CA6AF, or with skis.

Specifications (Comp Air 6, 220 hp Franklin engine)

Data from Jane's All The World's Aircraft 2003–2004.

General characteristics

Comp Air 6 Comp Air 1998 1998 6 LOW RESERVE WIFE SAYS IT MUST GO Owner

  • Crew: one pilot
  • Capacity: 3 adults and two children
  • Length: 24 ft 6 in (7.47 m)
  • Wingspan: 34 ft 6 in (10.52 m)
  • Height: 8 ft 0 in (2.44 m)
  • Wing area: 212.0 sq ft (19.70 m²)
  • Airfoil: modified Clark Y
  • Empty weight: 1,490lb (676 kg)
  • Max. takeoff weight: 2,580 lb (1,293 kg)
  • Powerplant: 1 × Franklin piston engines, 220 hp (164 kW)

    • Performance

    Comp Air 6 httpsuploadwikimediaorgwikipediacommonsthu

  • Maximum speed: 167 mph (145 knots, 268 km/h)
  • Cruise speed: 153 mph (133 knots, 246 km/h)
  • Stall speed: 40 mph (35 knots, 65 km/h)
  • Range: 800 mi (695 nmi, 1,287 km)
  • Service ceiling: 18,000 ft (5,480 m)
  • Rate of climb: 1,200 ft/min (6.1 m/s)

    • References

    Comp Air 6 Wikipedia
    (Text) CC BY-SA


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