7050 Aluminum T7451X

metal
UNS A97050

7050 Aluminum T7451X is a high-strength Al-Zn-Mg-Cu alloy in an overaged temper condition that combines elevated yield strength (>500 MPa) with improved stress-corrosion cracking (SCC) resistance and fracture toughness suitable for critical aircraft structural applications. The T7451X condition—stress-relieved by stretching and then overaged—provides enhanced resistance to exfoliation corrosion and sustained-load cracking compared to T73, making it preferred for thick-section wing and fuselage components operating in aerospace environments.

aerospacestructural

Compliance & Regulations

?Conflict Free?FDA?RoHS?REACH?TSCA?Prop 65
7050 Aluminum/7050 Aluminum T7451X
Filter by
PropertyValueUnitConditionsSource
Compressive Modulus(Ec)
ksi22°C · Hand Forging
Compressive Tangent Modulus vs Stress(Etn(σ))
Curve (10 pts)
ksi21°C · L
Poisson's Ratio(ν)
-22°C
Shear Modulus(G)
ksi22°C · Hand Forging
S–N Curve (Wöhler)(S–N)2 entries
Curve (40 pts)
ksi21°C · L
Curve (40 pts)
ksi21°C · L
Stress–Strain Curve (buckling region, ≤ 2% strain)(σ–ε (low-strain))
Curve (7 pts)
ksi21°C · L
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.