Bombardier CRJ1000 vs. Douglas DC-8-61

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Bombardier CRJ1000 versus Douglas DC-8-61
39.1 m 128 ft 5 in length 57.0 m 187 ft 0 in
7.5 m 24 ft 7 in height 13.1 m 43 ft
26.2 m 86 ft wingspan 45.24 m 148 ft 5 in
2 GE CF34-8C5A1 turbofans engines 4x P&W JT3D-3B 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 18,000 pound-force
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 72,000 pound-force
41,640 kg 91,800 lb MTOW 147,400 kg 325,000 lb
3,004 km 1,623 nm range 3,200 nm 5,926 km
515 mph 829 km/h cruise speed 483 knots 282 mph
100 (common) capacity 180 to 220 passengers in a mixed-class seating
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.