7050 Aluminum T7651X

metal

7050 Aluminum T7651X is a high-strength Al-Zn-Mg-Cu alloy in an overaged temper condition that provides improved stress-corrosion cracking (SCC) resistance and exfoliation corrosion resistance compared to T73, while maintaining excellent mechanical properties for critical aerospace structural applications. The T7651X condition delivers reduced fracture toughness but enhanced environmental durability, making it suitable for damage-tolerant design in fuselage skins, wing structures, and other components requiring long-term corrosion resistance in marine and high-altitude environments.

aerospacestructural

Compliance & Regulations

?Conflict Free?FDA?RoHS?REACH?TSCA?Prop 65
7050 Aluminum/7050 Aluminum T7651X
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Orientation
PropertyValueUnitConditionsSource
Compressive Modulus(Ec)
Pa22°C · Hand Forging
Compressive Tangent Modulus vs Stress(Etn(σ))
Pa5 entriesClick to expand
Poisson's Ratio(ν)
-22°C
Shear Modulus(G)
Pa22°C · Hand Forging
S–N Curve (Wöhler)(S–N)
Pa8 entriesClick to expand
Stress–Strain Curve (buckling region, ≤ 2% strain)(σ–ε (low-strain))
Pa8 entriesClick to expand
Young's Modulus(E)
Pa22°C · Hand Forging
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.
Rows with are inherited from the base material
Verified Unverified Low confidence (<80%) Link to source
PropertyValueUnitConditionsSource
Density(ρ)
kg/m³22°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.