Boeing 767-400ER vs. Lockheed U-2

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Boeing 767-400ER versus Lockheed U-2
61.3 m 201 ft 3 in length 19.2 m 63 ft 0 in
16.9 m 55 ft 5 in height 4.8 m 15 ft 9 in
51.9 m 170 ft 3 in wingspan 32 m 105 ft
2 Pratt & Whitney PW4060 turbofan engines engines 1 × General Electric F118-101
Up to 63,300 pounds thrust per engine 17,000 lbf (76 kN)
Up to 126,600 pounds total thrust 17,000 lbf (76 kN)
204,120 kg 450,100 lb MTOW 18,144 kg 40,000 lb
9,688 km 5,232 nm range 6,090 nm 11,278 km
530 mph 853 km/h cruise speed 475 mph 764 km/h
Typical three class arrangement for 245 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.