Airbus A220-100 vs. Lockheed P-38 Lightning

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Airbus A220-100 versus Lockheed P-38 Lightning
35.0 m 114 ft 10 in length 11.53 m 37 ft 10 in
11.5 m 37 ft 9 in height 3.91 m 12 ft 10 in
35.1 m 115 ft 2 in wingspan 15.85 m 52 ft
2 Turbofans (wing mounted) engines Engines: Two Allison V-1710-111/113 V-12 supercharged 4-stroke liquid-cooled engines
21,000–23,000 lb thrust per engine 1,425 hp
42,000–46,000 lb total thrust 2,850 hp
63,100 kg 139,100 lb MTOW 9,798 kg 21,600 lb
6,390 km 3,451 nm range 1,100 nm 2,037 km
871 km/h 541 mph cruise speed 239 knots 139 mph
Typical seating 2-class 100-120 capacity
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.