Boeing 717-200HGW vs. Lockheed P-2 Neptune

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Boeing 717-200HGW versus Lockheed P-2 Neptune
37.80 m 123 ft 11 in length 30.17 m 99 ft 0 in
8.87 m 29 ft 1 in height 10.15 m 33 ft 4 in
28.44 m 93 ft 4 in wingspan 33.53 m 110 ft
2 Rolls-Royce BR715 engines 2 x Wright R-3350 radial engines
82.3kN (18,500lb) to 93.4kN (21,000lb) thrust per engine Approximately 3,700 hp
164.6kN (37,000lb) to 186.8kN (42,000lb) total thrust Approximately 7,400 hp
54,885 kg 121,000 lb MTOW 27,216 kg 60,000 lb
2,060 nm 3,814 km range 7,885 km 4,259 nm
811 km/h 504 mph cruise speed 300 mph 483 km/h
106 passengers in a 2 class configuration 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.