Airbus A350-900ULR vs. Lockheed P-2 Neptune

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Airbus A350-900ULR versus Lockheed P-2 Neptune
66.80 m 219 ft 2 in length 30.17 m 99 ft 0 in
17.05 m 55 ft 11 in height 10.15 m 33 ft 4 in
64.75 m 212 ft 5 in wingspan 33.53 m 110 ft
2 Rolls-Royce Trent XWB engines 2 x Wright R-3350 radial engines
84,000 lbs thrust per engine Approximately 3,700 hp
168,000 lbs total thrust Approximately 7,400 hp
280,000 kg 617,300 lb MTOW 27,216 kg 60,000 lb
17,964 km 9,700 nm range 7,885 km 4,259 nm
552 mph 888 km/h cruise speed 300 mph 483 km/h
300-350 passengers in three classes 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.