Aerodis AA200 Orion

· Aerodis · 1 × Lycoming O-360

Airplanes

Length

7.62 m

Flat Wing Span

9.144 m

Height

2.4384 m

Flat Wing Area

12.7277 m²

Max Seating

Cruise Speed

305.5797 km/h

Max Speed

333.3597 km/h

Max Ceiling

4419.6 m

Number of Engines

Aircraft Engine

First Flight

1991-04-07

Maximum Take-Off Weight

1.134 t (paragliders: kg)

Maximum Range

1444.56 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Maximum Range (km)
Aerodis AA200 Orion	1.134	1444.56

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Beechcraft CT-134 Musketeer		7.62	9.7536	2	Compare
American Aviation AA-2 Patriot		7.0104	9.144		Compare
Bernard 70		6.72	9.2		Compare
Aerial Wheel Syndicate Monoplane		7.62	9.144		Compare
American Eagle A-129	Kinner K-5	7.62	9.144		Compare
Boeing-Stearman Model 75		7.3152	9.7536		Compare

All data (21 fields)

Name: 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