Airbus A330-200 vs. Lockheed P-2 Neptune

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Airbus A330-200 versus Lockheed P-2 Neptune
58.82 m 193 ft 0 in length 30.17 m 99 ft 0 in
17.39 m 57 ft 1 in height 10.15 m 33 ft 4 in
64 m 210 ft wingspan 33.53 m 110 ft
2 Turbofans engines 2 x Wright R-3350 radial engines
GE CF6-80E1A3: 304.7 kN / 68500 lbf, PW4170: 311.4 kN / 70000 lbf, RR Trent 772C-60: 316.3 kN / 71100 lbf thrust per engine Approximately 3,700 hp
Depends on the engine variant total thrust Approximately 7,400 hp
251,000 kg 553,400 lb MTOW 27,216 kg 60,000 lb
15,094 km 8,150 nm range 7,885 km 4,259 nm
531 mph 855 km/h cruise speed 300 mph 483 km/h
220-260 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.