Boeing 727-200ADV vs. McDonnell Douglas F-4 Phantom II

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Boeing 727-200ADV versus McDonnell Douglas F-4 Phantom II
46.69 m 153 ft 2 in length 19.2 m 63 ft 0 in
10.36 m 34 ft height 5.03 m 16 ft 6 in
32.92 m 108 ft wingspan 11.72 m 38 ft 5 in
3x Pratt & Whitney JT8D low-bypass turbofans engines Two General Electric J79s
17,400 lbs thrust per engine 17,900 lbs
52,200 lbs (3 engines x 17,400 lbs/engine) total thrust 35,800 lbs
95,000 kg 209,400 lb MTOW 27,965 kg 61,700 lb
2,550 nm 4,723 km range 3,031 km 1,636 nm
964 km/h 599 mph cruise speed Mach 2.2 2,717 km/h
Typically carries 134 passengers in two classes 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.