Boeing 787-9 vs. de Havilland Canada DHC-2 Beaver

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Boeing 787-9 versus de Havilland Canada DHC-2 Beaver
63.0 m 206 ft 9 in length 13.56 m 44 ft 6 in
17 m 55 ft 9 in height 5 m 16 ft 5 in
60 m 196 ft 1 wingspan 16.56 m 54 ft 4 in
GEnx-1B / Trent 1000 engines 2 x Armstrong Siddeley Double Mamba turboprop engines
76,100 pounds thrust per engine Approximately 3,100 hp (2,312 kW) each
152,200 pounds total thrust Approximately 6,200 hp (4,624 kW) total
254,000 kg 560,000 lb MTOW 24,200 lb 10,977 kg
14,140 km 7,635 nmi range 2,535 km 1,369 nm
652 mph 1,050 kph cruise speed 228 mph 367 km/h
290 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.