Sukhoi SSJ 100 95LR vs. Airbus H225 Super Puma

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Sukhoi SSJ 100 95LR versus Airbus H225 Super Puma
29.94 m 98 ft 2 in length 14.06 m 46 ft 2 in
10.28 m 33 ft 8 in height 4.38 m 14 ft 4 in
27.8 m 91 ft 2 in wingspan
2 PowerJet SaM146 turbofans engines 2 x Turbomeca Makila 2A turboshaft engines
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 thrust per engine 2,778 hp
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 total thrust 5,556 hp
49,450 kg 109,000 lb MTOW 11,000 kg 24,251 lb
4,578 km 2,470 nm range 857 km 463 nm
515 mph 830 km/h cruise speed 242 km/h 150 mph
98 (up to 108) passengers capacity 24-28
rotor diameter 16.2 m 53 ft 2 in
rate of climb 10.7 m/s 2,106 ft/min
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.