de Havilland Canada DHC-2 Beaver vs. North American T-6 Texan
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de Havilland Canada DHC-2 Beaver |
versus |
North American T-6 Texan |
13.56 m |
44 ft 6 in |
length |
9.0 m |
29 ft 6 in |
5 m |
16 ft 5 in |
height |
3.56 m |
11 ft 8 in |
16.56 m |
54 ft 4 in |
wingspan |
12.8 m |
42 ft |
2 x Armstrong Siddeley Double Mamba turboprop engines |
engines |
1 x Pratt & Whitney R-1340-AN-1 radial engine |
Approximately 3,100 hp (2,312 kW) each |
thrust per engine |
Approximately 600 hp |
Approximately 6,200 hp (4,624 kW) total |
total thrust |
Approximately 600 hp |
24,200 lb |
10,977 kg |
MTOW |
5,617 lb |
2,548 kg |
2,535 km |
1,369 nm |
range |
1,175 km |
634 nm |
228 mph |
367 km/h |
cruise speed |
145 mph |
233 km/h |
Pilot and Observer, plus various configurations for reconnaissance, anti-submarine warfare, and aerial refueling |
capacity |
Pilot and one passenger |
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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.