Bombardier CRJ1000 vs. Douglas DC-8

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Bombardier CRJ1000 versus Douglas DC-8
39.1 m 128 ft 5 in length 57.10 m 187 ft 4 in
7.5 m 24 ft 7 in height 16.84 m 55 ft 3 in
26.2 m 86 ft wingspan 45.24 m 148 ft 5 in
2 GE CF34-8C5A1 turbofans engines 4 x Pratt & Whitney JT3D turbofan 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 Approximately 17,000 lbf per engine
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 Approximately 68,000 lbf total
41,640 kg 91,800 lb MTOW 158,760 kg 350,000 lb
3,004 km 1,623 nm range 11,918 km 6,437 nm
515 mph 829 km/h cruise speed 900 km/h 559 mph
100 (common) capacity Up to 259 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.