Canadair CL-415 vs. Mil Mi-26

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Canadair CL-415 versus Mil Mi-26
19.82 m 65 ft 0 in length 40.03 m 131.3 ft
8.66 m 28 ft 5 in height 8.15 m 26.7 ft
28.6 m 93 ft 1 wingspan
2 x Pratt & Whitney Canada PW123AF turboprop engines engines 2 x Lotarev D-136 turboshaft engines
2,150 to 2,380 shaft horsepower (1,602 to 1,775 kW) thrust per engine 8,380 kW
4,300 to 4,760 shaft horsepower total thrust 16,760 kW
19,733 kg 43,525 lb MTOW 56,000 kg 123,459 lb
1,600 km 864 nm range 800 km 432 nm
290 km/h 180 mph cruise speed 255 km/h 158 mph
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.