AEA Maverick

Role  | Light Sport Aircraft
National origin | Australia
Manufacturer  | Aero Engineers Australia
Designer  | Graham Swannell and Geoff Danes
First flight  | December 1987

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

1. ↑ "Aircraft Photo of VH-JOX | AEA Maverick | AirHistory.net #15677" (in en). https://www.airhistory.net/photo/15677/VH-JOX.

## External links

* The Maverick on AEA's website

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