Sukhoi SSJ 100 95LR vs. de Havilland Canada DHC-2 Beaver

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Sukhoi SSJ 100 95LR versus de Havilland Canada DHC-2 Beaver
29.94 m 98 ft 2 in length 13.56 m 44 ft 6 in
10.28 m 33 ft 8 in height 5 m 16 ft 5 in
27.8 m 91 ft 2 in wingspan 16.56 m 54 ft 4 in
2 PowerJet SaM146 turbofans engines 2 x Armstrong Siddeley Double Mamba turboprop 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 Approximately 3,100 hp (2,312 kW) each
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 Approximately 6,200 hp (4,624 kW) total
49,450 kg 109,000 lb MTOW 24,200 lb 10,977 kg
4,578 km 2,470 nm range 2,535 km 1,369 nm
515 mph 830 km/h cruise speed 228 mph 367 km/h
98 (up to 108) passengers capacity Pilot and Observer, plus various configurations for reconnaissance, anti-submarine warfare, and aerial refueling
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.