Airbus A220-300 vs. Lockheed P-38 Lightning

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Airbus A220-300 versus Lockheed P-38 Lightning
38.7 m 127 ft 0 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 x Pratt & Whitney PurePower PW1500G 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
70,900 kg 156,300 lb MTOW 9,798 kg 21,600 lb
6,297 km 3,402 nm range 1,100 nm 2,037 km
Mach 0.82 101,3 km/h cruise speed 239 knots 139 mph
Typical seating 2-class 120-150 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.