Comparison of Beechcraft T-34 Mentor and Vought SBU Corsair [S]ave
| Attribute |  Beechcraft T-34 Mentor × |  Vought SBU Corsair × |
|---|---|---|
| General | ||
| Manufacturer | Hawker Beechcraft | Vought |
| Model | Beechcraft T-34 Mentor | Vought SBU Corsair |
| Country | United States | United States |
| Manufactured from (year) | 1953 | 1935 |
| Manufactured to (year) | 1990 | 1936 |
| Type | Military Propellor Planes | Military Propellor Planes |
| Icao | T34T | SBU |
| Performance | ||
| Engine | 1x 1 × Pratt & Whitney Canada PT6A-25 turboprop | 1x Pratt & Whitney R-1535-80 Twin Wasp |
| Power, hp (hp) | 550 | 700 |
| Max cruise speed (km/h) | 519 | 330 |
| Approach speed (km/h) | 98 | - |
| Travel range (km) | 1,311 | 883 |
| Fuel economy (km/l) | 3.669 | - |
| Service ceiling (m) | 7,620 | 7,224 |
| Rate of climb (m/sec) | 7.62 | 5.99 |
| Take off distance (m) | 250 | - |
| Landing distance (m) | 128 | - |
| Weights | ||
| Max take off weight (kg) | 1,950 | 2,510 |
| Max payload (kg) | 590 | 420 |
| Fuel tank capacity (l) | 538 | 549 |
| Dimensions | ||
| Seats | 2 | 2 |
| Exterior length (m) | 8.75 | 8.5 |
| Tail height (m) | 2.92 | 3.63 |
| Fuselage diameter (m) | 1.1 | 1.1 |
| Wing span (m) | 10.16 | 10.14 |
| Wing tips | No Winglets | No Winglets |
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