Boeing 767-300ER vs. McDonnell Douglas F-4 Phantom II
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Boeing 767-300ER |
versus |
McDonnell Douglas F-4 Phantom II |
54.9 m |
180 ft 3 in |
length |
19.2 m |
63 ft 0 in |
15.85 m |
52 ft |
height |
5.03 m |
16 ft 6 in |
47.57 m |
156 ft 1 in |
wingspan |
11.72 m |
38 ft 5 in |
Two Pratt & Whitney PW4060 turbofan engines |
engines |
Two General Electric J79s |
Up to 63,300 pounds of thrust each |
thrust per engine |
17,900 lbs |
Up to 126,600 pounds of thrust |
total thrust |
35,800 lbs |
186,880 kg |
412,000 lb |
MTOW |
27,965 kg |
61,700 lb |
11,070 km |
5,980 nm |
range |
3,031 km |
1,636 nm |
528 MPH |
850 km/h |
cruise speed |
Mach 2.2 |
2,717 km/h |
Typically 218 (3-class) |
capacity |
Up to 16,000 lbs of externally carried ordnance |
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rotor diameter |
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rate of climb |
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Please note that these values are indicative and actual values can vary based on specific engine models and configurations.