Airbus A220-300 vs. Lockheed P-2 Neptune

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Airbus A220-300 versus Lockheed P-2 Neptune
38.7 m 127 ft 0 in length 30.17 m 99 ft 0 in
11.5 m 37 ft 9 in height 10.15 m 33 ft 4 in
35.1 m 115 ft 2 in wingspan 33.53 m 110 ft
2 x Pratt & Whitney PurePower PW1500G engines 2 x Wright R-3350 radial engines
21,000–23,000 lb thrust per engine Approximately 3,700 hp
42,000–46,000 lb total thrust Approximately 7,400 hp
70,900 kg 156,300 lb MTOW 27,216 kg 60,000 lb
6,297 km 3,402 nm range 7,885 km 4,259 nm
Mach 0.82 101,3 km/h cruise speed 300 mph 483 km/h
Typical seating 2-class 120-150 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.