Bombardier CRJ1000 vs. McDonnell-Douglas MD-11

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Bombardier CRJ1000 versus McDonnell-Douglas MD-11
39.1 m 128 ft 5 in length 61.20 m 200 ft 10 in
7.5 m 24 ft 7 in height 17.6 m 57 ft 9 in
26.2 m 86 ft wingspan 51.6 m 169 ft 4 in
2 GE CF34-8C5A1 turbofans engines 3 (General Electric CF6-80C2D1F or Pratt & Whitney PW4460 or PW4462)
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 273.1 kN (GE CF6-80C2D1F) or 266.9 kN (PW4460)
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 819.3 kN (GE CF6-80C2D1F) or 800.7 kN (PW4460)
41,640 kg 91,800 lb MTOW 285,990 kg 630,400 lb
3,004 km 1,623 nm range 13,231 km 7,147 nm
515 mph 829 km/h cruise speed 961 km/h 597 mph
100 (common) capacity Max 410 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.