Airbus A220-300 vs. de Havilland Canada DHC-2 Beaver

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Airbus A220-300 versus de Havilland Canada DHC-2 Beaver
38.7 m 127 ft 0 in length 13.56 m 44 ft 6 in
11.5 m 37 ft 9 in height 5 m 16 ft 5 in
35.1 m 115 ft 2 in wingspan 16.56 m 54 ft 4 in
2 x Pratt & Whitney PurePower PW1500G engines 2 x Armstrong Siddeley Double Mamba turboprop engines
21,000–23,000 lb thrust per engine Approximately 3,100 hp (2,312 kW) each
42,000–46,000 lb total thrust Approximately 6,200 hp (4,624 kW) total
70,900 kg 156,300 lb MTOW 24,200 lb 10,977 kg
6,297 km 3,402 nm range 2,535 km 1,369 nm
Mach 0.82 101,3 km/h cruise speed 228 mph 367 km/h
Typical seating 2-class 120-150 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.