Lockheed U-2 vs. Cessna 208 Caravan

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Lockheed U-2 versus Cessna 208 Caravan
19.2 m 63 ft 0 in length 12.67 m 41 ft 7 in
4.8 m 15 ft 9 in height 4.49 m 14 ft 9 in
32 m 105 ft wingspan 15.88 m 52 ft 1 in
1 × General Electric F118-101 engines 1 x Pratt & Whitney Canada PT6A-114A turboprop engine
17,000 lbf (76 kN) thrust per engine 675 shaft horsepower (503 kW)
17,000 lbf (76 kN) total thrust 675 shaft horsepower (503 kW)
18,144 kg 40,000 lb MTOW 4,740 kg 10,450 lb
6,090 nm 11,278 km range 1,777 km 960 nm
475 mph 764 km/h cruise speed 340 km/h 211 mph
capacity Up to 14 passengers or 3,034 kg
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.