Airbus A340-200 vs. McDonnell Douglas F-4 Phantom II

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Airbus A340-200 versus McDonnell Douglas F-4 Phantom II
59.4 m 194 ft 11 in length 19.2 m 63 ft 0 in
16.8 m 55 ft 1 in height 5.03 m 16 ft 6 in
60.3 m 197 ft 9 in wingspan 11.72 m 38 ft 5 in
4 x CFM International CFM56-5C4 engines Two General Electric J79s
34,000 lbf thrust per engine 17,900 lbs
136,000 lbf total thrust 35,800 lbs
275,000 kg 606,300 lb MTOW 27,965 kg 61,700 lb
12,400 km 6,699 nm range 3,031 km 1,636 nm
880 km/h 547 mph cruise speed Mach 2.2 2,717 km/h
Typical seating 3-class 210-250 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.