2017 Aluminum

Verifiedmetal

2017 Aluminum (T4) is a copper-alloyed aluminum with high strength and good machinability, historically used in aircraft structures and fasteners where moderate strength and damage tolerance are required. The T4 temper (solution heat-treated and naturally aged) provides a balance of strength and ductility suitable for riveted airframe applications, with tensile strength approximately 280–310 MPa and superior fatigue resistance compared to harder tempers.

aerospacestructural

Compliance & Regulations

?Conflict Free?FDA?RoHS?REACH?TSCA?Prop 65

Tempers & Conditions

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Form
PropertyValueUnitConditionsSource
Compressive Modulus(Ec)2 entries
Pa22°C · Bar/Rod
Curve (11 pts)
PaL
Poisson's Ratio(ν)
-22°C
Shear Modulus(G)
Pa22°C · Bar/Rod
Young's Modulus(E)2 entries
Pa22°C · Bar/Rod
Curve (11 pts)
PaL
N entriesMultiple entries per property — large groups are collapsed; click a summary row to expand. Use filters above to narrow by form / heat treatment / basis.
Verified Unverified Low confidence (<80%) Link to source
PropertyValueUnitConditionsSource
CTE vs Temperature(α(T))
Curve (24 pts)
1/K
Verified Unverified Low confidence (<80%) Link to source
PropertyValueUnitConditionsSource
Density(ρ)
kg/m³22°C
Verified Unverified Low confidence (<80%) Link to source

Regulatory Screening

Environmental

Safety & Biocompatibility

Quality & Standards

RoHS, REACH, and Prop 65 statuses are validated against official substance lists (ECHA SVHC Candidate List, OEHHA Prop 65, RoHS Annex II). Other regulations are estimated from composition and material classification. All screening is a starting point for due diligence — always verify with your supplier before making compliance decisions.