Beechcraft T-34 Mentor vs. de Havilland Canada DHC-2 Beaver
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Beechcraft T-34 Mentor |
versus |
de Havilland Canada DHC-2 Beaver |
7.92 m |
25 ft 11 in |
length |
13.56 m |
44 ft 6 in |
2.95 m |
9 ft 8 in |
height |
5 m |
16 ft 5 in |
10.03 m |
32 ft 11 in |
wingspan |
16.56 m |
54 ft 4 in |
1 x Continental Motors IO-520 engine |
engines |
2 x Armstrong Siddeley Double Mamba turboprop engines |
Approximately 300 hp |
thrust per engine |
Approximately 3,100 hp (2,312 kW) each |
Approximately 300 hp |
total thrust |
Approximately 6,200 hp (4,624 kW) total |
3,100 lb |
1,406 kg |
MTOW |
24,200 lb |
10,977 kg |
1,111 km |
600 nm |
range |
2,535 km |
1,369 nm |
190 mph |
306 km/h |
cruise speed |
228 mph |
367 km/h |
Pilot and one passenger |
capacity |
Pilot and Observer, plus various configurations for reconnaissance, anti-submarine warfare, and aerial refueling |
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rotor diameter |
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rate of climb |
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Please note that these values are indicative and actual values can vary based on specific engine models and configurations.