Lockheed U-2 vs. Piper PA-34 Seneca

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Lockheed U-2 versus Piper PA-34 Seneca
19.2 m 63 ft 0 in length 8.71 m 28 ft 7 in
4.8 m 15 ft 9 in height 2.99 m 9 ft 10 in
32 m 105 ft wingspan 11.64 m 38 ft 2 in
1 × General Electric F118-101 engines 2 x Continental IO-360
17,000 lbf (76 kN) thrust per engine 220 lbs
17,000 lbf (76 kN) total thrust 440 lbs
18,144 kg 40,000 lb MTOW 4,750 lb 2,155 kg
6,090 nm 11,278 km range 980 nm 1,815 km
475 mph 764 km/h cruise speed 165 kts 103 mph
capacity 5
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.