Airbus A220-300 vs. Lockheed U-2

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Airbus A220-300 versus Lockheed U-2
38.7 m 127 ft 0 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 x Pratt & Whitney PurePower PW1500G 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)
70,900 kg 156,300 lb MTOW 18,144 kg 40,000 lb
6,297 km 3,402 nm range 6,090 nm 11,278 km
Mach 0.82 101,3 km/h cruise speed 475 mph 764 km/h
Typical seating 2-class 120-150 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.