Lockheed P-2 Neptune vs. Canadair CL-415

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Lockheed P-2 Neptune versus Canadair CL-415
30.17 m 99 ft 0 in length 19.82 m 65 ft 0 in
10.15 m 33 ft 4 in height 8.66 m 28 ft 5 in
33.53 m 110 ft wingspan 28.6 m 93 ft 1
2 x Wright R-3350 radial engines engines 2 x Pratt & Whitney Canada PW123AF turboprop engines
Approximately 3,700 hp thrust per engine 2,150 to 2,380 shaft horsepower (1,602 to 1,775 kW)
Approximately 7,400 hp total thrust 4,300 to 4,760 shaft horsepower
27,216 kg 60,000 lb MTOW 19,733 kg 43,525 lb
7,885 km 4,259 nm range 1,600 km 864 nm
300 mph 483 km/h cruise speed 290 km/h 180 mph
based on configuration capacity
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.