| Manufacturer |
Beechcraft |
| Description |
The Beechcraft CT-134 Musketeer is a military training derivative of the Musketeer built by Beechcraft for the Canadian Armed Forces. |
| Entry Into service |
1971-01-01 |
| Service End |
1992-01-01 |
| Designer |
Beechcraft |
| Type |
Basic trainer |
| Length (m) |
7.62 |
| Height (m) |
2.4384 |
| Cockpit Crew |
2 |
| Max Seating |
2 |
| Max Speed (km/h) |
237.0558 |
| Cruise Speed (km/h) |
233.3518 |
| Min Speed (km/h) |
94.4519 |
| Max Ceiling (m) |
3840.48 |
| Rate of Climb (m/s) |
4.0234 |
| Capacity Description |
2 passengers |
| National Origin |
United States of America |
| Number Built |
48 |
| Powerplant Description |
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_CT-134_Musketeer |
| Flat Wing Span (m) |
9.7536 |
| Flat Wing Area (m²) |
13.5638 |
| Number of Engines |
1 |