Airbus A319neo vs. McDonnell Douglas F-4 Phantom II

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Airbus A319neo 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 x PW 1100G or 2 x CFM LEAP-1A engines Two General Electric J79s
110kN (PW 1100G) or 109-156kN (CFM LEAP-1A) thrust per engine 17,900 lbs
220kN (PW 1100G) or 218-312kN (CFM LEAP-1A) total thrust 35,800 lbs
75,500 kg 166,400 lb MTOW 27,965 kg 61,700 lb
6,850 km 3,702 nm range 3,031 km 1,636 nm
530 mph 853 km/h cruise speed Mach 2.2 2,717 km/h
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.