Airbus A350-900ULR vs. de Havilland Canada DHC-2 Beaver

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Airbus A350-900ULR versus de Havilland Canada DHC-2 Beaver
66.80 m 219 ft 2 in length 13.56 m 44 ft 6 in
17.05 m 55 ft 11 in height 5 m 16 ft 5 in
64.75 m 212 ft 5 in wingspan 16.56 m 54 ft 4 in
2 Rolls-Royce Trent XWB engines 2 x Armstrong Siddeley Double Mamba turboprop engines
84,000 lbs thrust per engine Approximately 3,100 hp (2,312 kW) each
168,000 lbs total thrust Approximately 6,200 hp (4,624 kW) total
280,000 kg 617,300 lb MTOW 24,200 lb 10,977 kg
17,964 km 9,700 nm range 2,535 km 1,369 nm
552 mph 888 km/h cruise speed 228 mph 367 km/h
300-350 passengers in three classes 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.