Airbus A310-300 vs. Lockheed P-2 Neptune

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Airbus A310-300 versus Lockheed P-2 Neptune
46.66 m 153 ft 1 in length 30.17 m 99 ft 0 in
15.8 m 51 ft 10 in height 10.15 m 33 ft 4 in
43.9 m 144 ft wingspan 33.53 m 110 ft
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines 2 x Wright R-3350 radial engines
52,000 lb thrust per engine Approximately 3,700 hp
104,000 lb total thrust Approximately 7,400 hp
148,768 kg 328,000 lb MTOW 27,216 kg 60,000 lb
8,050 km 4,348 nm range 7,885 km 4,259 nm
482 knots 279 mph cruise speed 300 mph 483 km/h
190-230 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.