Airbus A330-200 vs. Lockheed P-38 Lightning

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Airbus A330-200 versus Lockheed P-38 Lightning
58.82 m 193 ft 0 in length 11.53 m 37 ft 10 in
17.39 m 57 ft 1 in height 3.91 m 12 ft 10 in
64 m 210 ft wingspan 15.85 m 52 ft
2 Turbofans engines Engines: Two Allison V-1710-111/113 V-12 supercharged 4-stroke liquid-cooled engines
GE CF6-80E1A3: 304.7 kN / 68500 lbf, PW4170: 311.4 kN / 70000 lbf, RR Trent 772C-60: 316.3 kN / 71100 lbf thrust per engine 1,425 hp
Depends on the engine variant total thrust 2,850 hp
251,000 kg 553,400 lb MTOW 9,798 kg 21,600 lb
15,094 km 8,150 nm range 1,100 nm 2,037 km
531 mph 855 km/h cruise speed 239 knots 139 mph
220-260 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.