McDonnell-Douglas DC-10-30 vs. Sukhoi SSJ 100 95LR

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McDonnell-Douglas DC-10-30 versus Sukhoi SSJ 100 95LR
55.35 m 181 ft 8 in length 29.94 m 98 ft 2 in
17.8 m 58 ft 5 in height 10.28 m 33 ft 8 in
50.39 m 165 ft 4 in wingspan 27.8 m 91 ft 2 in
3x GE CF6-50C Turbofan engines 2 PowerJet SaM146 turbofans
54,000 lbf 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
162,000 lbf 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
251,744 kg 555,000 lb MTOW 49,450 kg 109,000 lb
9,630 km 5,200 nm range 4,578 km 2,470 nm
507 knots 939 km/h cruise speed 515 mph 830 km/h
Up to 380 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.