Alclad 2524-T3
VerifiedmetalAlclad 2524-T3 is a clad aluminum-copper-magnesium alloy in solution heat-treated and cold-worked condition, providing high strength with improved fatigue resistance and corrosion protection via the pure aluminum cladding layer. Primary applications include aircraft fuselage skin and pressurized structures requiring damage tolerance and sustained stress capability at moderate temperatures.
aerospacestructural
Compliance & Regulations
?EAR?Conflict Free?RoHS?REACH?TSCA?Prop 65
Tempers & Conditions
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| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Compressive Modulus(Ec) | — | Pa | 22°C · Sheet/Plate | — | |
Poisson's Ratio(ν) | — | - | 22°C | — | |
Young's Modulus(E) | — | Pa | 22°C · Sheet/Plate | — |
Verified Unverified Low confidence (<80%) Link to source
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Density(ρ) | — | kg/m³ | 22°C | — |
Verified Unverified Low confidence (<80%) Link to source
Regulatory Screening
Environmental
Export Control
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.