Airbus A220-100 vs. Lockheed U-2

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Airbus A220-100 versus Lockheed U-2
35.0 m 114 ft 10 in length 19.2 m 63 ft 0 in
11.5 m 37 ft 9 in height 4.8 m 15 ft 9 in
35.1 m 115 ft 2 in wingspan 32 m 105 ft
2 Turbofans (wing mounted) engines 1 × General Electric F118-101
21,000–23,000 lb thrust per engine 17,000 lbf (76 kN)
42,000–46,000 lb total thrust 17,000 lbf (76 kN)
63,100 kg 139,100 lb MTOW 18,144 kg 40,000 lb
6,390 km 3,451 nm range 6,090 nm 11,278 km
871 km/h 541 mph cruise speed 475 mph 764 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.