Airbus A330-300 vs. Lockheed P-2 Neptune

versus
... or view the full comparison list here.
Airbus A330-300 versus Lockheed P-2 Neptune
63.66 m 208 ft 9 in length 30.17 m 99 ft 0 in
16.79 m 55 ft 1 in height 10.15 m 33 ft 4 in
60.3 m 197 ft 9 in wingspan 33.53 m 110 ft
General Electric CF6-80E, Pratt & Whitney PW4000 series, Rolls-Royce Trent 700 engines 2 x Wright R-3350 radial engines
311.4 kN (Pratt & Whitney PW4170), 304.7 kN (General Electric CF6-80E1A3), 316.3 kN (Rolls-Royce Trent 772C-60) thrust per engine Approximately 3,700 hp
Depends on the engine type total thrust Approximately 7,400 hp
242,000 kg 533,600 lb MTOW 27,216 kg 60,000 lb
11,750 km 6,346 nm range 7,885 km 4,259 nm
900 km/h 559 mph cruise speed 300 mph 483 km/h
250-290 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.