AEA Maverick

   

The Aero Engineers Australia (AEA) Maverick is a single-seat sportsplane of conventional configuration. Constructed largely of composite materials, it is powered by a 74.6 kW (100 hp) TCM 200-A engine and is capable of manoeuvres with loads of up to +6 or -3 Gs.

As of 2004, only one aircraft had been built, which first flew in December 1987.

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Specifications (AEA Maverick)

General Characteristics

  • Crew: one, pilot
  • Length: 5.41 m (17 ft 9 in)
  • Wingspan: 5.79 m (19 ft)
  • Height: 1.83 m (6 ft)
  • Wing area: 5.6 m² (60 ft²)
  • Empty: 295 kg (650 lb)
  • Loaded: 477 kg (1,050 lb)
  • Maximum takeoff: kg ( lb)
  • Powerplant: 1 x TCM 200A, 74.6 kW (100 hp)

Performance

  • Maximum speed: 363 km/h (226 mph)
  • Range: km ( miles)
  • Service ceiling: m (ft)
  • Rate of climb: m/min ( ft/min)
  • Wing loading: 85 kg/m² (17.4 lb/ft²)
  • Power/Mass: 0.16 kW/kg (0.10 hp/lb)


External link

The Maverick on AEA's website (http://www.aeroengaus.com.au/maverick.htm)

Related content

List of Aircraft | Aircraft Manufacturers | Aircraft Engines | Aircraft Engine Manufacturers
Airlines | Air Forces | Aircraft Weapons | Missiles | Timeline of aviation


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