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Lockheed P-2 Neptune ✕ Antonov An-74 ✕
Manufacturer Lockheed Corporation Antonov
Description The Lockheed P-2 Neptune (designated P2V by the United States Navy (USN) prior to September 1962) was a maritime patrol and antisubmarine warfare (ASW) aircraft. The Antonov An-74 (Russian: Антонов Ан-74, NATO reporting name: Coaler) is a Soviet/Ukrainian transport aircraft developed by Antonov.
ICAO Code P2
First Flight 1945-05-17 1983-09-29
Entry Into service 1947-03-01 1983-01-01
Service End 1984-01-01
Designer Lockheed Corporation Antonov
Type Maritime patrol and anti-submarine warfare aircraft
Length (m) 27.7368 28.07
Height (m) 8.8392 8.65
Cockpit Crew 7
Max Seating 52
Max Speed (km/h) 584.1919 700
Cruise Speed (km/h) 333.1342 550
Max Ceiling (m) 6827.52 10100
Armament 8,000 lb (3,629 kg) including free-fall bombs, depth charges, and torpedoes; 2.75 in (70 mm) FFAR in removable wing-mounted pods
Capacity Description up to 52 passengers
National Origin United States of America Soviet Union
Number Built 1177 62
Powerplant Description 2 × Wright R-3350-32W Duplex-Cyclone 18-cylinder air-cooled radial piston engine, 2759 kW (3700 hp) each 2 × Lotarev D-36 series 1A, 63.9 kN thrust each
Primary Users United States Navy, Japan Maritime Self-Defense Force , Royal Australian Air Force , Royal Canadian Air Force Islamic Revolutionary Guard Corps Aerospace Force, Utair , Egyptian Air Force , Pouya Air
Status Retired In service
Wikipedia Article (URL) en.wikipedia.org/wiki/Lockheed_P-2_Neptune en.wikipedia.org/wiki/Antonov_An-74
Flat Wing Span (m) 31.3944 31.89
Flat Wing Area (m²) 92.903 98.62
Wake Category M
Aircraft Engine Lotarev D-36
Number of Engines 2 2