de Havilland Canada DHC-2 Beaver vs. Canadair CL-415
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de Havilland Canada DHC-2 Beaver |
versus |
Canadair CL-415 |
13.56 m |
44 ft 6 in |
length |
19.82 m |
65 ft 0 in |
5 m |
16 ft 5 in |
height |
8.66 m |
28 ft 5 in |
16.56 m |
54 ft 4 in |
wingspan |
28.6 m |
93 ft 1 |
2 x Armstrong Siddeley Double Mamba turboprop engines |
engines |
2 x Pratt & Whitney Canada PW123AF turboprop engines |
Approximately 3,100 hp (2,312 kW) each |
thrust per engine |
2,150 to 2,380 shaft horsepower (1,602 to 1,775 kW) |
Approximately 6,200 hp (4,624 kW) total |
total thrust |
4,300 to 4,760 shaft horsepower |
24,200 lb |
10,977 kg |
MTOW |
19,733 kg |
43,525 lb |
2,535 km |
1,369 nm |
range |
1,600 km |
864 nm |
228 mph |
367 km/h |
cruise speed |
290 km/h |
180 mph |
Pilot and Observer, plus various configurations for reconnaissance, anti-submarine warfare, and aerial refueling |
capacity |
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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.