Airbus A350-800 vs. Lockheed P-2 Neptune

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Airbus A350-800 versus Lockheed P-2 Neptune
60.54 m 198 ft 7 in length 30.17 m 99 ft 0 in
17.05 m 55 ft 11 in height 10.15 m 33 ft 4 in
64.7 m 212 ft 5 in wingspan 33.53 m 110 ft
2 Turbofans (wing mounted) engines 2 x Wright R-3350 radial engines
75,760 lb thrust per engine Approximately 3,700 hp
151,520 lb total thrust Approximately 7,400 hp
283,000 kg 623,900 lb MTOW 27,216 kg 60,000 lb
11,708 km 6,319 nm range 7,885 km 4,259 nm
552 mph 888 km/h cruise speed 300 mph 483 km/h
Typically carries 300 to 350 passengers capacity based on configuration
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.