AEA Maverick
| 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.
Only one aircraft had been built, which 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)
- Height: 1.83 m (6 ft)
- Wing area: 5.6 m² (60 ft²)
- Empty weight: 295 kg (650 lb)
- Loaded weight: 477 kg (1,050 lb)
- Powerplant: 1 × Continental O-200A, (75 kW)100 hp
Performance
- Maximum speed: 363 km/h (226 mph)
- Wing loading: 85 kg/m² (17.4 lb/ft²)
- Power/mass: 160 W/kg (0.10 hp/lb)
External links
 |
Wikimedia Commons has media related to Aero Engineers Australia. |
Related content
This article is issued from Wikipedia - version of the 10/1/2016. The text is available under the Creative Commons Attribution/Share Alike but additional terms may apply for the media files.