Lockheed P-2 Neptune vs. Aero Commander 680

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Lockheed P-2 Neptune versus Aero Commander 680
30.17 m 99 ft 0 in length 11.38 m 37 ft 4 in
10.15 m 33 ft 4 in height 3.6 m 11 ft 10 in
33.53 m 110 ft wingspan 15.02 m 49 ft 3 in
2 x Wright R-3350 radial engines engines 2 x Lycoming TIO-540
Approximately 3,700 hp thrust per engine 380 lbs
Approximately 7,400 hp total thrust 760 lbs
27,216 kg 60,000 lb MTOW 7,500 lb 3,402 kg
7,885 km 4,259 nm range 1,500 nm 2,778 km
300 mph 483 km/h cruise speed 218 kts 135 mph
based on configuration capacity Up to 6 passengers
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.