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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 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 in aviation. ==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== [http://www.aeroengaus.com.au/maverick.htm The Maverick on AEA's website] ==Related content== Australian sports planes 1980-1989


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Words begining with AEA_Maverick:

AEA_Maverick


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