Antonov An-124 Ruslan vs. Canadair CL-415

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Antonov An-124 Ruslan versus Canadair CL-415
69.10 m 226 ft 9 in length 19.82 m 65 ft 0 in
20.78 m 68 ft 2 in height 8.66 m 28 ft 5 in
73.3 m 240 ft 6 in wingspan 28.6 m 93 ft 1
4 x Ivchenko Progress D-18T turbofan engines engines 2 x Pratt & Whitney Canada PW123AF turboprop engines
Approximately 51,590 lbf thrust per engine 2,150 to 2,380 shaft horsepower (1,602 to 1,775 kW)
Approximately 206,360 lbf total thrust 4,300 to 4,760 shaft horsepower
405,000 kg 893,000 lb MTOW 19,733 kg 43,525 lb
3,700 km 1,998 nm range 1,600 km 864 nm
800 km/h 497 mph cruise speed 290 km/h 180 mph
capacity
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.