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Origin:Curtiss-Wright Corporation
Type:Single-Seat Fighter,fighter-bomber,ground attack,and/or reconnissance
Engine:one 1,040 hp Allison V-1710-33 V-12 liquid-cooled inline
Span:37 ft. 3½ in.
Length:31 ft. 8½ in.
Height:12 ft. 4 in.
Empty Weight:5,812 lbs.
Loaded Weight:7,459 lbs.
Maximum Speed:345 mph.
Initial Climb Rate:2,650 ft. per minute
Service Ceiling:About 30,000 ft.
Range:730 miles
Armament:six 0.303 in. machine guns in wings
History:First Flight(XP-40)-October 1940,(P-40)-January 1940,(P-40D)-1941,(P-40F)-1941,(P-40N)-1943;Final Delivery(P-40N-40 & P-40R)December 1944
Users:Argentina,Australia,Belgium,Brazil,Canada,China,Colombia,Egypt,Finland,France,Iraq,Italy(CB),the Netherlands,New Zealand,Norway,Peru,Portagul,South Africa,Soviet Union,Turkey,United Kingdom(RAF),United Stated(USAAC/USAAF)