Airbus A300-600 vs. Lockheed P-38 Lightning

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Airbus A300-600 versus Lockheed P-38 Lightning
54.10 m 177 ft 6 in length 11.53 m 37 ft 10 in
16.5 m 54 ft 2 in height 3.91 m 12 ft 10 in
44.84 m 147 ft 1 in wingspan 15.85 m 52 ft
2 x turbofan engines, either Pratt & Whitney PW 4000 or General Electric GE CF6-80C2A1 engines Engines: Two Allison V-1710-111/113 V-12 supercharged 4-stroke liquid-cooled engines
56,000lb to 61,500lb thrust per engine 1,425 hp
112,000–123,000 lb total thrust 2,850 hp
171,700 kg 378,600 lb MTOW 9,798 kg 21,600 lb
7,500 km 4,052 nm range 1,100 nm 2,037 km
897 km/h 557 mph cruise speed 239 knots 139 mph
210-250 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.