Airbus A220-300 vs. McDonnell Douglas F-4 Phantom II

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Airbus A220-300 versus McDonnell Douglas F-4 Phantom II
38.7 m 127 ft 0 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 x Pratt & Whitney PurePower PW1500G 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
70,900 kg 156,300 lb MTOW 27,965 kg 61,700 lb
6,297 km 3,402 nm range 3,031 km 1,636 nm
Mach 0.82 101,3 km/h cruise speed Mach 2.2 2,717 km/h
Typical seating 2-class 120-150 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.