Antonov An-124 Ruslan vs. de Havilland Canada DHC-3 Otter

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Antonov An-124 Ruslan versus de Havilland Canada DHC-3 Otter
69.10 m 226 ft 9 in length 10.52 m 34 ft 6 in
20.78 m 68 ft 2 in height 3.84 m 12 ft 7 in
73.3 m 240 ft 6 in wingspan 17.68 m 58 ft
4 x Ivchenko Progress D-18T turbofan engines engines 1 x Pratt & Whitney R-1340 radial engine
Approximately 51,590 lbf thrust per engine 400 to 600 horsepower (298 to 447 kW)
Approximately 206,360 lbf total thrust 400 to 600 horsepower (298 to 447 kW)
405,000 kg 893,000 lb MTOW 5,670 kg 12,500 lb
3,700 km 1,998 nm range 1,296 km 700 nm
800 km/h 497 mph cruise speed 215 km/h 134 mph
capacity 10-11 passengers
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.