Airbus A330-200 vs. Mil Mi-26

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Airbus A330-200 versus Mil Mi-26
58.82 m 193 ft 0 in length 40.03 m 131.3 ft
17.39 m 57 ft 1 in height 8.15 m 26.7 ft
64 m 210 ft wingspan
2 Turbofans engines 2 x Lotarev D-136 turboshaft engines
GE CF6-80E1A3: 304.7 kN / 68500 lbf, PW4170: 311.4 kN / 70000 lbf, RR Trent 772C-60: 316.3 kN / 71100 lbf thrust per engine 8,380 kW
Depends on the engine variant total thrust 16,760 kW
251,000 kg 553,400 lb MTOW 56,000 kg 123,459 lb
15,094 km 8,150 nm range 800 km 432 nm
531 mph 855 km/h cruise speed 255 km/h 158 mph
220-260 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.