Airbus A220-100 vs. McDonnell Douglas F-4 Phantom II

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Airbus A220-100 versus McDonnell Douglas F-4 Phantom II
35.0 m 114 ft 10 in length 19.2 m 63 ft 0 in
11.5 m 37 ft 9 in height 5.03 m 16 ft 6 in
35.1 m 115 ft 2 in wingspan 11.72 m 38 ft 5 in
2 Turbofans (wing mounted) engines Two General Electric J79s
21,000–23,000 lb thrust per engine 17,900 lbs
42,000–46,000 lb total thrust 35,800 lbs
63,100 kg 139,100 lb MTOW 27,965 kg 61,700 lb
6,390 km 3,451 nm range 3,031 km 1,636 nm
871 km/h 541 mph cruise speed Mach 2.2 2,717 km/h
Typical seating 2-class 100-120 capacity Up to 16,000 lbs of externally carried ordnance
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.