Airbus A318 vs. Lockheed U-2

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Airbus A318 versus Lockheed U-2
31.44 m 103 ft 2 in length 19.2 m 63 ft 0 in
12.56 m 41 ft 3 in height 4.8 m 15 ft 9 in
34.1 m 111 ft 11 in wingspan 32 m 105 ft
2x CFM56-5B or 2x PW6000 engines 1 × General Electric F118-101
23,300 lb thrust per engine 17,000 lbf (76 kN)
46,600 lb total thrust 17,000 lbf (76 kN)
59,000 kg 130,000 lb MTOW 18,144 kg 40,000 lb
5,750 km 3,106 nm range 6,090 nm 11,278 km
963km/h 598mph cruise speed 475 mph 764 km/h
107 to 132 passengers 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.