Clad 7475 Aluminum T6151
metalClad 7475 aluminum alloy in T6151 temper is a high-strength aerospace aluminum with zinc, magnesium, and copper additions, clad with pure aluminum for corrosion resistance, solution heat-treated, artificially aged, and stress-relieved by controlled stretching to reduce residual stresses while maintaining peak strength. Primary applications include aircraft wing skins and fuselage components requiring high fracture toughness and fatigue resistance combined with excellent damage tolerance in the 250–300 °F operating range.
aerospacestructural
Compliance & Regulations
?Conflict Free?FDA?RoHS?REACH?TSCA?Prop 65
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Compressive Modulus(Ec) | — | ksi | 22°C · Sheet | — | |
Poisson's Ratio(ν) | — | - | 22°C | — | |
Shear Modulus(G) | — | ksi | 22°C · Sheet | — | |
Young's Modulus(E) | — | ksi | 22°C · Sheet | — |
Rows with are inherited from the base material
Verified Unverified Low confidence (<80%) Link to source
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Density(ρ) | — | lb/in³ | 22°C | — |
Rows with are inherited from the base material
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.