Airbus A350-1000 vs. Lockheed P-2 Neptune

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Airbus A350-1000 versus Lockheed P-2 Neptune
73.79 m 242 ft 1 in length 30.17 m 99 ft 0 in
17.08 m 56 ft height 10.15 m 33 ft 4 in
64.75 m 212 ft 5 in wingspan 33.53 m 110 ft
2 Trent XWB-97 turbofan engines engines 2 x Wright R-3350 radial engines
97,000 lb thrust per engine Approximately 3,700 hp
194,000 lb total thrust Approximately 7,400 hp
319,000 kg 703,300 lb MTOW 27,216 kg 60,000 lb
16,100 km 8,695 nm range 7,885 km 4,259 nm
1,099 km/h 683 mph cruise speed 300 mph 483 km/h
350 to 410 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.