Airbus A320-200 vs. Lockheed P-2 Neptune

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Airbus A320-200 versus Lockheed P-2 Neptune
38.7 m 127 ft 0 in length 30.17 m 99 ft 0 in
17.4 m 57 ft 1 in height 10.15 m 33 ft 4 in
35.8 m 117 ft 5 in wingspan 33.53 m 110 ft
Choice between Pratt & Whitney GTF™ and the LEAP-1A from CFM International engines 2 x Wright R-3350 radial engines
Between 21,000 - 33,000 lbf thrust per engine Approximately 3,700 hp
Between 42,000 - 66,000 lbf total thrust Approximately 7,400 hp
77,000 kg 169,800 lb MTOW 27,216 kg 60,000 lb
5,700 km 3,078 nm range 7,885 km 4,259 nm
530 mph 853 km/h cruise speed 300 mph 483 km/h
Typically between 140-180 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.