Airbus A319 vs. McDonnell Douglas F-4 Phantom II

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Airbus A319 versus McDonnell Douglas F-4 Phantom II
33.84 m 111 ft 0 in length 19.2 m 63 ft 0 in
11.76 m 38 ft 7 in height 5.03 m 16 ft 6 in
35.8 m 117 ft 5 in wingspan 11.72 m 38 ft 5 in
2 (International Aero Engines V2524-A5) engines Two General Electric J79s
27,000 lb thrust per engine 17,900 lbs
54,000 lb total thrust 35,800 lbs
75,500 kg 166,400 lb MTOW 27,965 kg 61,700 lb
3,700 nmi 6,852 km range 3,031 km 1,636 nm
829 km/h 515 mph cruise speed Mach 2.2 2,717 km/h
124 to 156 passengers 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.