Lockheed P-2 Neptune Civil Aircraft Model Details

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General Information of Lockheed P-2 Neptune

First Flight : 16574

Introduction : 17227

Manufacturer : Lockheed

Primary Users : United States Navy; Japan Maritime Self Defense Force; Royal Australian Air Force; Royal Canadian Air Force

Retired : 1984 From military use

Role : Maritime Patrol and Anti-Submarine Warfare

Variants : Kawasaki P-2J

General characteristics of Lockheed P-2 Neptune

Crew : 42624

Empty Weight : 34,875 lb (15,819 kg)

Height : 28 ft 4 in (8.56 m)

Length : 77 ft 10 in (23.72 m)

Max Takeoff Weight : 64,100 lb (29,076 kg)

Powerplant : 2 × Wright R-3350-26W Cyclone-18 radial engine, 3,200 hp (2,386 kW) wet each

Propellers : 3 bladed propeller, 1 per engine

Wing Area : 1,000 ft² (92.9 m²)

Wingspan : 100 ft 0 in (30.48 m)

Performance of Lockheed P-2 Neptune

Cruise Speed : 155 kn (174 mph) (286 km/h) (max)

Maximum Speed : 278 kn (313 mph) (515 km/h)

Range : 3,458 nmi (3,903 mi) (6,406 km)

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