Airbus A310-300 vs. Mil Mi-26

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Airbus A310-300 versus Mil Mi-26
46.66 m 153 ft 1 in length 40.03 m 131.3 ft
15.8 m 51 ft 10 in height 8.15 m 26.7 ft
43.9 m 144 ft wingspan
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines 2 x Lotarev D-136 turboshaft engines
52,000 lb thrust per engine 8,380 kW
104,000 lb total thrust 16,760 kW
148,768 kg 328,000 lb MTOW 56,000 kg 123,459 lb
8,050 km 4,348 nm range 800 km 432 nm
482 knots 279 mph cruise speed 255 km/h 158 mph
190-230 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.