ALUMINUM 2014 is a heat treatable alloy having high tensile and fatigue strength. It is recommended for fittings, hardware, aircraft engine components, structures, etc. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and shear strength as well as fatigue. It also includes information on corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Al-185. Producer or source: Aluminum Company of America. Originally published as Aluminum 14S, Alloy Digest Al-17, June 1954, revised March 1969.

aircraft components, Aluminum 2014, chemical composition, corrosion-resistant alloys, elasticity, fatigue strength, hardness, heat treatability, joinability, machinability, physical properties, shear strength, tensile properties, workability
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1996
ASM International
Topics
Aircraft components Corrosion-resistant alloys Aluminum alloys Chemical composition Heat treatability Joinability Machinability Workability Elastic modulus Fatigue properties Hardness Shear strength Tensile properties Physical properties Thermal properties
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