Bombardier CRJ1000 vs. McDonnell-Douglas DC-9-30

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Bombardier CRJ1000 versus McDonnell-Douglas DC-9-30
39.1 m 128 ft 5 in length 36.36 m 119 ft 3 in
7.5 m 24 ft 7 in height 8.5 m 27 ft 11 in
26.2 m 86 ft wingspan 28.44 m 93 ft 4 in
2 GE CF34-8C5A1 turbofans engines 2x Pratt & Whitney JT8D
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 15,000 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 30,000 pound-force (2 engines)
41,640 kg 91,800 lb MTOW 54,885 kg 121,000 lb
3,004 km 1,623 nm range 2,632 km 1,422 nm
515 mph 829 km/h cruise speed 898 km/h 558 mph
100 (common) capacity Up to 139 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.