Airbus A220-100 vs. Lockheed P-2 Neptune

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Airbus A220-100 versus Lockheed P-2 Neptune
35.0 m 114 ft 10 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 Turbofans (wing mounted) 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
63,100 kg 139,100 lb MTOW 27,216 kg 60,000 lb
6,390 km 3,451 nm range 7,885 km 4,259 nm
871 km/h 541 mph cruise speed 300 mph 483 km/h
Typical seating 2-class 100-120 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.