Airbus A300-600 vs. Sukhoi SSJ 100 95LR

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Airbus A300-600 versus Sukhoi SSJ 100 95LR
54.10 m 177 ft 6 in length 29.94 m 98 ft 2 in
16.5 m 54 ft 2 in height 10.28 m 33 ft 8 in
44.84 m 147 ft 1 in wingspan 27.8 m 91 ft 2 in
2 x turbofan engines, either Pratt & Whitney PW 4000 or General Electric GE CF6-80C2A1 engines 2 PowerJet SaM146 turbofans
56,000lb to 61,500lb 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
112,000–123,000 lb 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
171,700 kg 378,600 lb MTOW 49,450 kg 109,000 lb
7,500 km 4,052 nm range 4,578 km 2,470 nm
897 km/h 557 mph cruise speed 515 mph 830 km/h
210-250 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.