Lockheed P-2 Neptune vs. Temco TT Pinto

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Lockheed P-2 Neptune versus Temco TT Pinto
30.17 m 99 ft 0 in length 9.33 m 30 ft 7 in
10.15 m 33 ft 4 in height 3.3 m 10 ft 10 in
33.53 m 110 ft wingspan 9.09 m 29 ft 1
2 x Wright R-3350 radial engines engines 1 × Continental YJ69-T-9
Approximately 3,700 hp thrust per engine 920 lb f (4.1 kN)
Approximately 7,400 hp total thrust 920 lb f (4.1 kN)
27,216 kg 60,000 lb MTOW 4,453 lb 2,020 kg
7,885 km 4,259 nm range 300 km 162 nm
300 mph 483 km/h cruise speed 345 mph 555 km/h
based on configuration capacity Fuel capacity: 119 US gal (99 imp gal; 450 L) normal; 165 US gal (137 imp gal; 620 L) max
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.