Airbus A220-100 vs. North American P-51 Mustang

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Airbus A220-100 versus North American P-51 Mustang
35.0 m 114 ft 10 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 Turbofans (wing mounted) 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)
63,100 kg 139,100 lb MTOW 5,489 kg 12,100 lb
6,390 km 3,451 nm range 2,200 km 1,188 nm
871 km/h 541 mph cruise speed 325 mph 525 km/h
Typical seating 2-class 100-120 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.