7050 Aluminum T7351X

metal

7050-T7351X is a high-strength Al-Zn-Mg-Cu alloy in overaged temper with stress relief, providing yield strengths of 455–480 MPa with enhanced stress-corrosion cracking resistance suitable for critical aerospace structural applications requiring damage tolerance. The T7351X condition delivers improved fracture toughness and environmental cracking resistance compared to T73 by controlled overaging and mechanical stress relief, making it preferred for thick-section forgings and extrusions in military aircraft and pressure vessels.

aerospacestructural

Compliance & Regulations

?Conflict Free?FDA?RoHS?REACH?TSCA?Prop 65
7050 Aluminum/7050 Aluminum T7351X
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Orientation
PropertyValueUnitConditionsSource
Compressive Modulus(Ec)
ksi22°C · Hand Forging
Compressive Tangent Modulus vs Stress(Etn(σ))3 entries
Curve (10 pts)
ksi21°C · L
Curve (11 pts)
ksi21°C · LT
Curve (11 pts)
ksi21°C · ST
Poisson's Ratio(ν)
-22°C
Shear Modulus(G)
ksi22°C · Hand Forging
S–N Curve (Wöhler)(S–N)
ksi5 entriesClick to expand
Stress–Strain Curve (buckling region, ≤ 2% strain)(σ–ε (low-strain))
ksi8 entriesClick to expand
Young's Modulus(E)
ksi22°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)
lb/in³22°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.