Boeing 767-300ER vs. Lockheed P-2 Neptune
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Boeing 767-300ER |
versus |
Lockheed P-2 Neptune |
54.9 m |
180 ft 3 in |
length |
30.17 m |
99 ft 0 in |
15.85 m |
52 ft |
height |
10.15 m |
33 ft 4 in |
47.57 m |
156 ft 1 in |
wingspan |
33.53 m |
110 ft |
Two Pratt & Whitney PW4060 turbofan engines |
engines |
2 x Wright R-3350 radial engines |
Up to 63,300 pounds of thrust each |
thrust per engine |
Approximately 3,700 hp |
Up to 126,600 pounds of thrust |
total thrust |
Approximately 7,400 hp |
186,880 kg |
412,000 lb |
MTOW |
27,216 kg |
60,000 lb |
11,070 km |
5,980 nm |
range |
7,885 km |
4,259 nm |
528 MPH |
850 km/h |
cruise speed |
300 mph |
483 km/h |
Typically 218 (3-class) |
capacity |
based on configuration |
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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.