Lockheed P-2 Neptune vs. North American T-6 Texan

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Lockheed P-2 Neptune versus North American T-6 Texan
30.17 m 99 ft 0 in length 9.0 m 29 ft 6 in
10.15 m 33 ft 4 in height 3.56 m 11 ft 8 in
33.53 m 110 ft wingspan 12.8 m 42 ft
2 x Wright R-3350 radial engines engines 1 x Pratt & Whitney R-1340-AN-1 radial engine
Approximately 3,700 hp thrust per engine Approximately 600 hp
Approximately 7,400 hp total thrust Approximately 600 hp
27,216 kg 60,000 lb MTOW 5,617 lb 2,548 kg
7,885 km 4,259 nm range 1,175 km 634 nm
300 mph 483 km/h cruise speed 145 mph 233 km/h
based on configuration capacity Pilot and one passenger
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.