Bombardier CRJ1000 vs. Mil Mi-26

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Bombardier CRJ1000 versus Mil Mi-26
39.1 m 128 ft 5 in length 40.03 m 131.3 ft
7.5 m 24 ft 7 in height 8.15 m 26.7 ft
26.2 m 86 ft wingspan
2 GE CF34-8C5A1 turbofans engines 2 x Lotarev D-136 turboshaft engines
13,630 lb of force or 60.6 kN at takeoff, 14,510 lb of force or 64.5 kN thrust APR Automatic Power Reserve thrust per engine 8,380 kW
27,260 lb of force or 121.2 kN at takeoff, 29,020 lb of force or 129 kN thrust APR Automatic Power Reserve total thrust 16,760 kW
41,640 kg 91,800 lb MTOW 56,000 kg 123,459 lb
3,004 km 1,623 nm range 800 km 432 nm
515 mph 829 km/h cruise speed 255 km/h 158 mph
100 (common) 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.