| Manufacturer |
Allison Gas Turbine Division GMC |
| Description |
The Beechcraft T-34 Mentor is an American propeller-driven, single-engined, military trainer aircraft derived from the Beechcraft Model 35 Bonanza. |
| First Flight |
1948-12-02 |
| Entry Into service |
1953-01-01 |
| Production End |
1959-01-01 |
| Designer |
Allison Gas Turbine Division GMC |
| Type |
Trainer aircraft |
| Length (m) |
8.5344 |
| Height (m) |
2.7432 |
| Cockpit Crew |
2 |
| Cruise Speed (km/h) |
396.3277 |
| Min Speed (km/h) |
98.1559 |
| Max Ceiling (m) |
9144 |
| Rate of Climb (m/s) |
7.5184 |
| Armament |
4 |
| National Origin |
United States of America |
| Number Built |
2300 |
| Powerplant Description |
1 × Pratt & Whitney Canada PT6A-25 turboprop, 410 kW (550 hp) each |
| Primary Users |
United States Air Force, United States Navy , Japan Air Self-Defense Force , Republic of China Air Force |
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/Beechcraft_T-34_Mentor |
| Flat Wing Span (m) |
10.0584 |
| Flat Wing Area (m²) |
16.6854 |
| Aircraft Engine |
Pratt & Whitney Canada PT6 |
| Number of Engines |
1 |