Bombardier CRJ900 vs. Lockheed P-2 Neptune

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Bombardier CRJ900 versus Lockheed P-2 Neptune
36.2 m 118 ft 11 in length 30.17 m 99 ft 0 in
7.5 m 24 ft 7 in height 10.15 m 33 ft 4 in
24.9 m 81 ft 8 in wingspan 33.53 m 110 ft
2 Turbofans (fuselage mounted) engines 2 x Wright R-3350 radial engines
13,360 pounds force thrust per engine Approximately 3,700 hp
26,720 pounds force total thrust Approximately 7,400 hp
38,330 kg 84,500 lb MTOW 27,216 kg 60,000 lb
2,871 km 1,550 nm range 7,885 km 4,259 nm
515 mph 829 km/h cruise speed 300 mph 483 km/h
Up to 90 passengers 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.