Bombardier CRJ1000 vs. Douglas C-54 Skymaster

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Bombardier CRJ1000 versus Douglas C-54 Skymaster
39.1 m 128 ft 5 in length 28.60 m 93 ft 10 in
7.5 m 24 ft 7 in height 8.38 m 27 ft 6 in
26.2 m 86 ft wingspan 35.81 m 117 ft 6 in
2 GE CF34-8C5A1 turbofans engines 4 x Pratt & Whitney R-2000 Twin Wasp radial 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 1,200 to 1,450 horsepower (895 to 1,080 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 4,800 to 5,800 horsepower
41,640 kg 91,800 lb MTOW 29,484 kg 65,000 lb
3,004 km 1,623 nm range 6,500 km 3,510 nm
515 mph 829 km/h cruise speed 340 km/h 211 mph
100 (common) capacity Up to 50 passengers or 28,500 lb cargo
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.