Airbus A320neo vs. Lockheed P-2 Neptune

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Airbus A320neo versus Lockheed P-2 Neptune
37.57 m 123 ft 3 in length 30.17 m 99 ft 0 in
11.76 m 38 ft 7 in height 10.15 m 33 ft 4 in
35.8 m 117 ft 5 in wingspan 33.53 m 110 ft
2 x PW 1100G or 2 x CFM LEAP-1A engines 2 x Wright R-3350 radial engines
120kN (PW 1100G) or 109-156kN (CFM LEAP-1A) thrust per engine Approximately 3,700 hp
240kN (PW 1100G) or 218-312kN (CFM LEAP-1A) total thrust Approximately 7,400 hp
79,000 kg 174,200 lb MTOW 27,216 kg 60,000 lb
6,300 km 3,403 nm range 7,885 km 4,259 nm
M0.82 101,3 km/h cruise speed 300 mph 483 km/h
150-180 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.