Airbus A321XLR vs. Lockheed P-2 Neptune

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Airbus A321XLR 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 LEAP-1A and P&W PW1100G engines 2 x Wright R-3350 radial engines
33,000 lbs (147 kN) thrust per engine Approximately 3,700 hp
66,000 lbs (294 kN) total thrust Approximately 7,400 hp
101,000 kg 222,700 lb MTOW 27,216 kg 60,000 lb
4,700 nmi 8,704 km range 7,885 km 4,259 nm
963km/h 598mph cruise speed 300 mph 483 km/h
180-220 seats (typical 2-class seating) 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.