| Manufacturer |
Beechcraft |
Beechcraft |
| Description |
The Beechcraft Musketeer is a family of single-engined, low-wing, light aircraft that was produced by Beechcraft. |
The Beechcraft CT-134 Musketeer is a military training derivative of the Musketeer built by Beechcraft for the Canadian Armed Forces. |
| First Flight |
1961-10-23 |
|
| Entry Into service |
|
1971-01-01 |
| Production End |
1983-01-01 |
|
| Service End |
|
1992-01-01 |
| Designer |
Beechcraft |
Beechcraft |
| Type |
Light personal and trainer aircraft |
Basic trainer |
| Length (m) |
7.62 |
7.62 |
| Height (m) |
2.4384 |
2.4384 |
| Cockpit Crew |
|
2 |
| Max Seating |
|
2 |
| Max Speed (km/h) |
235.2038 |
237.0558 |
| Cruise Speed (km/h) |
188.9038 |
233.3518 |
| Min Speed (km/h) |
116.6759 |
94.4519 |
| Max Ceiling (m) |
3962.4 |
3840.48 |
| Rate of Climb (m/s) |
3.6982 |
4.0234 |
| Capacity Description |
three passengers |
2 passengers |
| National Origin |
|
United States of America |
| Number Built |
4366 |
48 |
| Powerplant Description |
1 × Continental IO-346-A four cylinder air-cooled horizontally opposed aircraft piston engine, 123 kW (165 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/Beechcraft_Musketeer |
en.wikipedia.org/wiki/Beechcraft_CT-134_Musketeer |
| Flat Wing Span (m) |
9.7536 |
9.7536 |
| Flat Wing Area (m²) |
13.5638 |
13.5638 |
| Aircraft Engine |
Continental IO-346 |
|
| Number of Engines |
1 |
1 |