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) Continental O-200A engine and is capable of manoeuvres with loads of up to +6 or −3 g.

The sole example of the aircraft was registered as VH-JOX and resides in New South Wales, Australia.^[1] This aircraft first flew in December 1987.

Specifications (AEA Maverick)

General characteristics

• Crew: one, pilot
• Length: 5.41 m (17 ft 9 in)
• Wingspan: 5.79 m (19 ft 0 in)
• Height: 1.83 m (6 ft 0 in)
• Wing area: 5.6 m² (60 sq ft)
• Empty weight: 295 kg (650 lb)
• Gross weight: 477 kg (1,050 lb)
• Powerplant: 1 × Continental O-200A , 75 kW (101 hp)

Performance

• Maximum speed: 363 km/h (226 mph, 196 kn)
• Wing loading: 85 kg/m² (17.4 lb/sq ft)
• Power/mass: 160 W/kg (0.10 hp/lb)

References

External links

• The Maverick on AEA's website

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