Airbus A220-100 vs. de Havilland Venom

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Airbus A220-100 versus de Havilland Venom
35.0 m 114 ft 10 in length 6.71 m 22 ft 0 in
11.5 m 37 ft 9 in height 1.88 m 6 ft 2 in
35.1 m 115 ft 2 in wingspan 12.7 m 41 ft 8 in
2 Turbofans (wing mounted) engines 1 (de Havilland Ghost 105)
21,000–23,000 lb thrust per engine 23.6 kN
42,000–46,000 lb total thrust 23.6 kN
63,100 kg 139,100 lb MTOW 6,945 kg 15,300 lb
6,390 km 3,451 nm range 1,730 km 935 nm
871 km/h 541 mph cruise speed 1030 km/h 640 mph
Typical seating 2-class 100-120 capacity
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.