Airbus A340-500 vs. Lockheed P-2 Neptune

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Airbus A340-500 versus Lockheed P-2 Neptune
67.93 m 222 ft 10 in length 30.17 m 99 ft 0 in
17.53 m 57 ft 6 in height 10.15 m 33 ft 4 in
63.45 m 208 ft 2 in wingspan 33.53 m 110 ft
4 Rolls-Royce Trent 500 engines 2 x Wright R-3350 radial engines
54,000 lbf (240 kN) thrust per engine Approximately 3,700 hp
216,000 lbf (960 kN) total thrust Approximately 7,400 hp
380,000 kg 837,800 lb MTOW 27,216 kg 60,000 lb
16,670 km 9,000 nm range 7,885 km 4,259 nm
475 knots 880 km/h cruise speed 300 mph 483 km/h
Typical seating 3-class 270-310 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.