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EN AW-2017A

3.1325
AluminumWrought
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Heat-treatable Al-Cu-Mg alloy (Duralumin family). Higher strength than 6xxx series in T4 condition (UTS ~430 MPa) with excellent machinability. Not suitable for welding due to Cu content. Limited corrosion resistance — usually anodized or clad. Standard material for turned parts, screw machine products, fittings and structural components requiring high strength. One of the original aerospace aluminum alloys.

International equivalents

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🇺🇸AAUSA2017A92017REF

Sources: ASTM B211

Chemical composition comparison (wt%)

Side-by-side: EN AW-2017A (EN) (EN 573-3) vs ASTM

ElementEN AW-2017A (EN)ASTMOverlap
Si0.2–0.8%——
Mn0.4–1%——
Cr≤ 0.1%——
Cu3.5–4.5%——
Ti≤ 0.15%——
Mg0.4–1%——
Fe≤ 0.7%——
Zn≤ 0.25%——

Mechanical properties

T4 (solution treated + naturally aged)

PropertyValueUnit
Tensile Strength390–430MPa
Yield Strength Rp0.2240–280MPa
Elongation A10–14%

General

PropertyValueUnit
Density2.79g/cm³

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All data is for reference only. Equivalents indicate similarity, not identity. Always verify against the applicable specification for safety-critical applications. materialref.com accepts no liability for decisions based on this data.