Airbus A220-300 vs. North American P-51 Mustang

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Airbus A220-300 versus North American P-51 Mustang
38.7 m 127 ft 0 in length 9.83 m 32 ft 3 in
11.5 m 37 ft 9 in height 4.08 m 13 ft 5 in
35.1 m 115 ft 2 in wingspan 11.28 m 37 ft
2 x Pratt & Whitney PurePower PW1500G engines Packard Rolls Royce Merlin V-1650-7
21,000–23,000 lb thrust per engine 1,490 horsepower at 3,000 rpm and 1,720 horsepower at war emergency power (WEP)
42,000–46,000 lb total thrust 1,490 horsepower at 3,000 rpm and 1,720 horsepower at war emergency power (WEP)
70,900 kg 156,300 lb MTOW 5,489 kg 12,100 lb
6,297 km 3,402 nm range 2,200 km 1,188 nm
Mach 0.82 101,3 km/h cruise speed 325 mph 525 km/h
Typical seating 2-class 120-150 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.