Lockheed P-2 Neptune vs. Piper PA-34 Seneca

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Lockheed P-2 Neptune versus Piper PA-34 Seneca
30.17 m 99 ft 0 in length 8.71 m 28 ft 7 in
10.15 m 33 ft 4 in height 2.99 m 9 ft 10 in
33.53 m 110 ft wingspan 11.64 m 38 ft 2 in
2 x Wright R-3350 radial engines engines 2 x Continental IO-360
Approximately 3,700 hp thrust per engine 220 lbs
Approximately 7,400 hp total thrust 440 lbs
27,216 kg 60,000 lb MTOW 4,750 lb 2,155 kg
7,885 km 4,259 nm range 980 nm 1,815 km
300 mph 483 km/h cruise speed 165 kts 103 mph
based on configuration 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.