Airbus A310-300 vs. Lockheed P-38 Lightning

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Airbus A310-300 versus Lockheed P-38 Lightning
46.66 m 153 ft 1 in length 11.53 m 37 ft 10 in
15.8 m 51 ft 10 in height 3.91 m 12 ft 10 in
43.9 m 144 ft wingspan 15.85 m 52 ft
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines Engines: Two Allison V-1710-111/113 V-12 supercharged 4-stroke liquid-cooled engines
52,000 lb thrust per engine 1,425 hp
104,000 lb total thrust 2,850 hp
148,768 kg 328,000 lb MTOW 9,798 kg 21,600 lb
8,050 km 4,348 nm range 1,100 nm 2,037 km
482 knots 279 mph cruise speed 239 knots 139 mph
190-230 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.