Airbus A340-200 vs. North American P-51 Mustang

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Airbus A340-200 versus North American P-51 Mustang
59.4 m 194 ft 11 in length 9.83 m 32 ft 3 in
16.8 m 55 ft 1 in height 4.08 m 13 ft 5 in
60.3 m 197 ft 9 in wingspan 11.28 m 37 ft
4 x CFM International CFM56-5C4 engines Packard Rolls Royce Merlin V-1650-7
34,000 lbf thrust per engine 1,490 horsepower at 3,000 rpm and 1,720 horsepower at war emergency power (WEP)
136,000 lbf total thrust 1,490 horsepower at 3,000 rpm and 1,720 horsepower at war emergency power (WEP)
275,000 kg 606,300 lb MTOW 5,489 kg 12,100 lb
12,400 km 6,699 nm range 2,200 km 1,188 nm
880 km/h 547 mph cruise speed 325 mph 525 km/h
Typical seating 3-class 210-250 capacity 2,000 pounds of bombs, or ten 5-inch rockets
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.