de Havilland Canada DHC-2 Beaver vs. Mil Mi-26

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de Havilland Canada DHC-2 Beaver versus Mil Mi-26
13.56 m 44 ft 6 in length 40.03 m 131.3 ft
5 m 16 ft 5 in height 8.15 m 26.7 ft
16.56 m 54 ft 4 in wingspan
2 x Armstrong Siddeley Double Mamba turboprop engines engines 2 x Lotarev D-136 turboshaft engines
Approximately 3,100 hp (2,312 kW) each thrust per engine 8,380 kW
Approximately 6,200 hp (4,624 kW) total total thrust 16,760 kW
24,200 lb 10,977 kg MTOW 56,000 kg 123,459 lb
2,535 km 1,369 nm range 800 km 432 nm
228 mph 367 km/h cruise speed 255 km/h 158 mph
Pilot and Observer, plus various configurations for reconnaissance, anti-submarine warfare, and aerial refueling capacity Up to 90 passengers
rotor diameter 32.00 m 105 ft 0 in
rate of climb 8 m/s 1,574 ft/min
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.