Airbus A220-100 vs. North American F-100 Super Sabre

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Airbus A220-100 versus North American F-100 Super Sabre
35.0 m 114 ft 10 in length 16.46 m 54 ft 2 in
11.5 m 37 ft 9 in height 4.93 m 16 ft 2 in
35.1 m 115 ft 2 in wingspan 11.84 m 38 ft 1
2 Turbofans (wing mounted) engines 1 Pratt & Whitney J57-P-21A
21,000–23,000 lb thrust per engine 16,000 lb. thrust in afterburner
42,000–46,000 lb total thrust 16,000 lb. (afterburner)
63,100 kg 139,100 lb MTOW 17,609 kg 38,800 lb
6,390 km 3,451 nm range 2,673 km 1,444 nm
871 km/h 541 mph cruise speed 587 mph 945 km/h
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.