Airbus A321-200 vs. Lockheed P-2 Neptune

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Airbus A321-200 versus Lockheed P-2 Neptune
44.51 m 146 ft 0 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 GE CFM56-5B3 engines 2 x Wright R-3350 radial engines
31,600 lbs thrust per engine Approximately 3,700 hp
63,200 lbs total thrust Approximately 7,400 hp
89,000 kg 196,200 lb MTOW 27,216 kg 60,000 lb
4,000 nmi 7,408 km range 7,885 km 4,259 nm
871 km/h 541 mph cruise speed 300 mph 483 km/h
185 to 220 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.