Boeing 767-300ER vs. Lockheed U-2

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Boeing 767-300ER versus Lockheed U-2
54.9 m 180 ft 3 in length 19.2 m 63 ft 0 in
15.85 m 52 ft height 4.8 m 15 ft 9 in
47.57 m 156 ft 1 in wingspan 32 m 105 ft
Two Pratt & Whitney PW4060 turbofan engines engines 1 × General Electric F118-101
Up to 63,300 pounds of thrust each thrust per engine 17,000 lbf (76 kN)
Up to 126,600 pounds of thrust total thrust 17,000 lbf (76 kN)
186,880 kg 412,000 lb MTOW 18,144 kg 40,000 lb
11,070 km 5,980 nm range 6,090 nm 11,278 km
528 MPH 850 km/h cruise speed 475 mph 764 km/h
Typically 218 (3-class) 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.