Airbus A300-600F vs. Mil Mi-26

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Airbus A300-600F versus Mil Mi-26
54.08 m 177 ft 5 in length 40.03 m 131.3 ft
17.05 m 55 ft 11 in height 8.15 m 26.7 ft
44.84 m 147 ft 1 in wingspan
2 x General Electric CF6-80C2A5 turbofan engines engines 2 x Lotarev D-136 turboshaft engines
Approximately 59,000 lbf per engine thrust per engine 8,380 kW
Approximately 118,000 lbf total total thrust 16,760 kW
170,000 kg 374,786 lb MTOW 56,000 kg 123,459 lb
4,830 km 2,608 nm range 800 km 432 nm
860 km/h 534 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.