Airbus A300-600 vs. Mil Mi-26

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Airbus A300-600 versus Mil Mi-26
54.10 m 177 ft 6 in length 40.03 m 131.3 ft
16.5 m 54 ft 2 in height 8.15 m 26.7 ft
44.84 m 147 ft 1 in wingspan
2 x turbofan engines, either Pratt & Whitney PW 4000 or General Electric GE CF6-80C2A1 engines 2 x Lotarev D-136 turboshaft engines
56,000lb to 61,500lb thrust per engine 8,380 kW
112,000–123,000 lb total thrust 16,760 kW
171,700 kg 378,600 lb MTOW 56,000 kg 123,459 lb
7,500 km 4,052 nm range 800 km 432 nm
897 km/h 557 mph cruise speed 255 km/h 158 mph
210-250 passengers 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.