Boeing 717-200HGW vs. Mil Mi-26

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Boeing 717-200HGW versus Mil Mi-26
37.80 m 123 ft 11 in length 40.03 m 131.3 ft
8.87 m 29 ft 1 in height 8.15 m 26.7 ft
28.44 m 93 ft 4 in wingspan
2 Rolls-Royce BR715 engines 2 x Lotarev D-136 turboshaft engines
82.3kN (18,500lb) to 93.4kN (21,000lb) thrust per engine 8,380 kW
164.6kN (37,000lb) to 186.8kN (42,000lb) total thrust 16,760 kW
54,885 kg 121,000 lb MTOW 56,000 kg 123,459 lb
2,060 nm 3,814 km range 800 km 432 nm
811 km/h 504 mph cruise speed 255 km/h 158 mph
106 passengers in a 2 class configuration 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.