| Manufacturer |
Aerodis |
Beechcraft |
| 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. |
The Beechcraft CT-134 Musketeer is a military training derivative of the Musketeer built by Beechcraft for the Canadian Armed Forces. |
| First Flight |
1991-04-07 |
|
| Entry Into service |
|
1971-01-01 |
| Service End |
|
1992-01-01 |
| Designer |
David Thurston |
Beechcraft |
| Type |
|
Basic trainer |
| Length (m) |
7.62 |
7.62 |
| Height (m) |
2.4384 |
2.4384 |
| Cockpit Crew |
1 |
2 |
| Max Seating |
3 |
2 |
| Max Speed (km/h) |
333.3597 |
237.0558 |
| Cruise Speed (km/h) |
305.5797 |
233.3518 |
| Min Speed (km/h) |
|
94.4519 |
| Max Ceiling (m) |
4419.6 |
3840.48 |
| Rate of Climb (m/s) |
5.1816 |
4.0234 |
| Capacity Description |
3 passengers |
2 passengers |
| National Origin |
United States of America |
United States of America |
| Number Built |
|
48 |
| Powerplant Description |
1 × Lycoming O-360 4-cylinder, horizontally-opposed, air-cooled piston engine, 134 kW (180 hp) each |
1 × Lycoming O-360-A4K 4-cylinder air-cooled horizontally-opposed piston engine, 134 kW (180 hp) each |
| Primary Users |
|
Canadian Armed Forces |
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/Aerodis_AA200_Orion |
en.wikipedia.org/wiki/Beechcraft_CT-134_Musketeer |
| Flat Wing Span (m) |
9.144 |
9.7536 |
| Flat Wing Area (m²) |
12.7277 |
13.5638 |
| Aircraft Engine |
Lycoming O-360 |
|
| Number of Engines |
1 |
1 |