Airbus A330-300 vs. Mil Mi-26

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Airbus A330-300 versus Mil Mi-26
63.66 m 208 ft 9 in length 40.03 m 131.3 ft
16.79 m 55 ft 1 in height 8.15 m 26.7 ft
60.3 m 197 ft 9 in wingspan
General Electric CF6-80E, Pratt & Whitney PW4000 series, Rolls-Royce Trent 700 engines 2 x Lotarev D-136 turboshaft engines
311.4 kN (Pratt & Whitney PW4170), 304.7 kN (General Electric CF6-80E1A3), 316.3 kN (Rolls-Royce Trent 772C-60) thrust per engine 8,380 kW
Depends on the engine type total thrust 16,760 kW
242,000 kg 533,600 lb MTOW 56,000 kg 123,459 lb
11,750 km 6,346 nm range 800 km 432 nm
900 km/h 559 mph cruise speed 255 km/h 158 mph
250-290 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.