Airbus A320-200 vs. Lockheed P-38 Lightning

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Airbus A320-200 versus Lockheed P-38 Lightning
38.7 m 127 ft 0 in length 11.53 m 37 ft 10 in
17.4 m 57 ft 1 in height 3.91 m 12 ft 10 in
35.8 m 117 ft 5 in wingspan 15.85 m 52 ft
Choice between Pratt & Whitney GTF™ and the LEAP-1A from CFM International engines Engines: Two Allison V-1710-111/113 V-12 supercharged 4-stroke liquid-cooled engines
Between 21,000 - 33,000 lbf thrust per engine 1,425 hp
Between 42,000 - 66,000 lbf total thrust 2,850 hp
77,000 kg 169,800 lb MTOW 9,798 kg 21,600 lb
5,700 km 3,078 nm range 1,100 nm 2,037 km
530 mph 853 km/h cruise speed 239 knots 139 mph
Typically between 140-180 passengers 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.