McDonnell-Douglas MD-11 vs. Sukhoi SSJ 100 95LR

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McDonnell-Douglas MD-11 versus Sukhoi SSJ 100 95LR
61.20 m 200 ft 10 in length 29.94 m 98 ft 2 in
17.6 m 57 ft 9 in height 10.28 m 33 ft 8 in
51.6 m 169 ft 4 in wingspan 27.8 m 91 ft 2 in
3 (General Electric CF6-80C2D1F or Pratt & Whitney PW4460 or PW4462) engines 2 PowerJet SaM146 turbofans
273.1 kN (GE CF6-80C2D1F) or 266.9 kN (PW4460) thrust per engine 15,400 (68.5 KN) to 16,100 (71.6 KN) at NTO, 17,500 (77.9 KN) to 17,800 (79.2 KN) with APR
819.3 kN (GE CF6-80C2D1F) or 800.7 kN (PW4460) total thrust 30,800 (137 KN) to 32,200 (143.2 KN) at NTO, 35,000 (155.8 KN) to 35,600 (158.4 KN) with APR
285,990 kg 630,400 lb MTOW 49,450 kg 109,000 lb
13,231 km 7,147 nm range 4,578 km 2,470 nm
961 km/h 597 mph cruise speed 515 mph 830 km/h
Max 410 passengers capacity 98 (up to 108) 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.