Lockheed P-2 Neptune vs. Piaggio P.180 Avanti

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Lockheed P-2 Neptune versus Piaggio P.180 Avanti
30.17 m 99 ft 0 in length 14.40 m 47 ft 3 in
10.15 m 33 ft 4 in height 3.98 m 13 ft 1 in
33.53 m 110 ft wingspan 14.03 m 46 ft
2 x Wright R-3350 radial engines engines 2 x Pratt & Whitney Canada PT6A-66 turboprop engines
Approximately 3,700 hp thrust per engine Approximately 634 kW per engine
Approximately 7,400 hp total thrust Approximately 1,268 kW total
27,216 kg 60,000 lb MTOW 5,070 kg 11,177 lb
7,885 km 4,259 nm range 3,322 km 1,794 nm
300 mph 483 km/h cruise speed 732 km/h 455 mph
based on configuration capacity Up to 9 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.