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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 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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1 Specifications (AEA Maverick)

1.1 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 200 A, 74.6 kW (100 hp)

1.2 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)

2 External link

The Maverick on AEA's website

3 Related content

Australian sports planes 1980-1989

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Topics: AEA Maverick, Specifications (AEA Maverick), General...

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