Boeing 767-200ER vs. Lockheed P-2 Neptune

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Boeing 767-200ER versus Lockheed P-2 Neptune
48.5 m 159 ft 2 in length 30.17 m 99 ft 0 in
16.1 m 52 ft 10 in height 10.15 m 33 ft 4 in
47.8 m 156 ft 9 in wingspan 33.53 m 110 ft
2 x GE CF6-80C2B4F engines 2 x Wright R-3350 radial engines
62,020 lbs thrust per engine Approximately 3,700 hp
124,040 lbs total thrust Approximately 7,400 hp
164,200 kg 362,000 lb MTOW 27,216 kg 60,000 lb
12,200 km 6,587 nmi range 7,885 km 4,259 nm
850 km/hour 528 mph cruise speed 300 mph 483 km/h
249 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.