Airbus A340-500 vs. McDonnell Douglas F-4 Phantom II

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Airbus A340-500 versus McDonnell Douglas F-4 Phantom II
67.93 m 222 ft 10 in length 19.2 m 63 ft 0 in
17.53 m 57 ft 6 in height 5.03 m 16 ft 6 in
63.45 m 208 ft 2 in wingspan 11.72 m 38 ft 5 in
4 Rolls-Royce Trent 500 engines Two General Electric J79s
54,000 lbf (240 kN) thrust per engine 17,900 lbs
216,000 lbf (960 kN) total thrust 35,800 lbs
380,000 kg 837,800 lb MTOW 27,965 kg 61,700 lb
16,670 km 9,000 nm range 3,031 km 1,636 nm
475 knots 880 km/h cruise speed Mach 2.2 2,717 km/h
Typical seating 3-class 270-310 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.