| Aerodis AA200 Orion ✕ | |
|---|---|
| Manufacturer | Aerodis |
| Description | The Aerodis AA200 Orion is a four-seat prototype light aircraft designed in the United States and which first flew on April 7, 1991. |
| First Flight | 1991-04-07 |
| Designer | David Thurston |
| Length (m) | 7.62 |
| Height (m) | 2.4384 |
| Cockpit Crew | 1 |
| Max Seating | 3 |
| Max Speed (km/h) | 333.3597 |
| Cruise Speed (km/h) | 305.5797 |
| Max Ceiling (m) | 4419.6 |
| Rate of Climb (m/s) | 5.1816 |
| Capacity Description | 3 passengers |
| National Origin | United States of America |
| Powerplant Description | 1 × Lycoming O-360 4-cylinder, horizontally-opposed, air-cooled piston engine, 134 kW (180 hp) each |
| Wikipedia Article (URL) | en.wikipedia.org/wiki/Aerodis_AA200_Orion |
| Flat Wing Span (m) | 9.144 |
| Flat Wing Area (m²) | 12.7277 |
| Aircraft Engine | Lycoming O-360 |
| Number of Engines | 1 |