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
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.