AEA Maverick
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The Aero Engineers Australia (AEA) Maverick is a single-seat sportsplane of conventional configuration. Constructed largely of composite materials, it is powered by a 75 kW (100 hp) TCM 200-A engine and is capable of manoeuvres with loads of up to +6 or -3 g.
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, 75 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: 160 W/kg (0.10 hp/lb)
External link
The Maverick on AEA's website (http://www.aeroengaus.com.au/maverick.htm)
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