McDonnell-Douglas MD-11 vs. Canadair CL-415

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McDonnell-Douglas MD-11 versus Canadair CL-415
61.20 m 200 ft 10 in length 19.82 m 65 ft 0 in
17.6 m 57 ft 9 in height 8.66 m 28 ft 5 in
51.6 m 169 ft 4 in wingspan 28.6 m 93 ft 1
3 (General Electric CF6-80C2D1F or Pratt & Whitney PW4460 or PW4462) engines 2 x Pratt & Whitney Canada PW123AF turboprop engines
273.1 kN (GE CF6-80C2D1F) or 266.9 kN (PW4460) thrust per engine 2,150 to 2,380 shaft horsepower (1,602 to 1,775 kW)
819.3 kN (GE CF6-80C2D1F) or 800.7 kN (PW4460) total thrust 4,300 to 4,760 shaft horsepower
285,990 kg 630,400 lb MTOW 19,733 kg 43,525 lb
13,231 km 7,147 nm range 1,600 km 864 nm
961 km/h 597 mph cruise speed 290 km/h 180 mph
Max 410 passengers capacity
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.