Bombardier CRJ1000 vs. McDonnell-Douglas DC-10-30

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Bombardier CRJ1000 versus McDonnell-Douglas DC-10-30
39.1 m 128 ft 5 in length 55.35 m 181 ft 8 in
7.5 m 24 ft 7 in height 17.8 m 58 ft 5 in
26.2 m 86 ft wingspan 50.39 m 165 ft 4 in
2 GE CF34-8C5A1 turbofans engines 3x GE CF6-50C Turbofan
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 54,000 lbf
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 162,000 lbf
41,640 kg 91,800 lb MTOW 251,744 kg 555,000 lb
3,004 km 1,623 nm range 9,630 km 5,200 nm
515 mph 829 km/h cruise speed 507 knots 939 km/h
100 (common) capacity Up to 380 passengers
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.