Lockheed P-2 Neptune vs. Bell 206

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Lockheed P-2 Neptune versus Bell 206
30.17 m 99 ft 0 in length 12.11 m 39 ft 9 in
10.15 m 33 ft 4 in height 2.88 m 9 ft 5 in
33.53 m 110 ft wingspan
2 x Wright R-3350 radial engines engines 1 × Allison 250-C20B
Approximately 3,700 hp thrust per engine 420 shp (313 kW)
Approximately 7,400 hp total thrust 420 shp (313 kW)
27,216 kg 60,000 lb MTOW 1,451 kg 3,199 lb
7,885 km 4,259 nm range 374 km 202 nm
300 mph 483 km/h cruise speed 222 km/h 138 mph
based on configuration capacity 1 pilot + 4 passengers
rotor diameter 11.00 m 36 ft 1 in
rate of climb 425 m/min 1,395 ft/min
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.