Airbus A321LR vs. Lockheed P-2 Neptune

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Airbus A321LR 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
CFM International’s LEAP-1A or Pratt & Whitney’s PurePower PW1100G-JM engines 2 x Wright R-3350 radial engines
Over 33,000 lbs (147 kN) thrust per engine Approximately 3,700 hp
66,000 lbs (294 kN) total thrust Approximately 7,400 hp
97,000 kg 213,800 lb MTOW 27,216 kg 60,000 lb
7,400 km 4,000 nm range 7,885 km 4,259 nm
832 km/h 517 mph cruise speed 300 mph 483 km/h
180-220 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.