Airbus A300-600 vs. Lockheed P-2 Neptune

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Airbus A300-600 versus Lockheed P-2 Neptune
54.10 m 177 ft 6 in length 30.17 m 99 ft 0 in
16.5 m 54 ft 2 in height 10.15 m 33 ft 4 in
44.84 m 147 ft 1 in wingspan 33.53 m 110 ft
2 x turbofan engines, either Pratt & Whitney PW 4000 or General Electric GE CF6-80C2A1 engines 2 x Wright R-3350 radial engines
56,000lb to 61,500lb thrust per engine Approximately 3,700 hp
112,000–123,000 lb total thrust Approximately 7,400 hp
171,700 kg 378,600 lb MTOW 27,216 kg 60,000 lb
7,500 km 4,052 nm range 7,885 km 4,259 nm
897 km/h 557 mph cruise speed 300 mph 483 km/h
210-250 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.