Airbus A318 vs. McDonnell Douglas F-4 Phantom II

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Airbus A318 versus McDonnell Douglas F-4 Phantom II
31.44 m 103 ft 2 in length 19.2 m 63 ft 0 in
12.56 m 41 ft 3 in height 5.03 m 16 ft 6 in
34.1 m 111 ft 11 in wingspan 11.72 m 38 ft 5 in
2x CFM56-5B or 2x PW6000 engines Two General Electric J79s
23,300 lb thrust per engine 17,900 lbs
46,600 lb total thrust 35,800 lbs
59,000 kg 130,000 lb MTOW 27,965 kg 61,700 lb
5,750 km 3,106 nm range 3,031 km 1,636 nm
963km/h 598mph cruise speed Mach 2.2 2,717 km/h
107 to 132 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.