Airbus A220-100 vs. de Havilland Canada DHC-2 Beaver

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Airbus A220-100 versus de Havilland Canada DHC-2 Beaver
35.0 m 114 ft 10 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 Turbofans (wing mounted) 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
63,100 kg 139,100 lb MTOW 24,200 lb 10,977 kg
6,390 km 3,451 nm range 2,535 km 1,369 nm
871 km/h 541 mph cruise speed 228 mph 367 km/h
Typical seating 2-class 100-120 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.