Airbus A318 vs. Lockheed P-2 Neptune

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Airbus A318 versus Lockheed P-2 Neptune
31.44 m 103 ft 2 in length 30.17 m 99 ft 0 in
12.56 m 41 ft 3 in height 10.15 m 33 ft 4 in
34.1 m 111 ft 11 in wingspan 33.53 m 110 ft
2x CFM56-5B or 2x PW6000 engines 2 x Wright R-3350 radial engines
23,300 lb thrust per engine Approximately 3,700 hp
46,600 lb total thrust Approximately 7,400 hp
59,000 kg 130,000 lb MTOW 27,216 kg 60,000 lb
5,750 km 3,106 nm range 7,885 km 4,259 nm
963km/h 598mph cruise speed 300 mph 483 km/h
107 to 132 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.