Boeing 767-200ER vs. McDonnell Douglas F-4 Phantom II

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Boeing 767-200ER versus McDonnell Douglas F-4 Phantom II
48.5 m 159 ft 2 in length 19.2 m 63 ft 0 in
16.1 m 52 ft 10 in height 5.03 m 16 ft 6 in
47.8 m 156 ft 9 in wingspan 11.72 m 38 ft 5 in
2 x GE CF6-80C2B4F engines Two General Electric J79s
62,020 lbs thrust per engine 17,900 lbs
124,040 lbs total thrust 35,800 lbs
164,200 kg 362,000 lb MTOW 27,965 kg 61,700 lb
12,200 km 6,587 nmi range 3,031 km 1,636 nm
850 km/hour 528 mph cruise speed Mach 2.2 2,717 km/h
249 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.