7050 Aluminum T7651

metal

7050 is a high-strength Al-Zn-Mg-Cu alloy designed for critical aerospace structures requiring maximum strength-to-weight ratio and damage tolerance. T7651 is an overaged temper (solution heat-treated, stress-relieved by stretching, then artificially aged) that reduces quench sensitivity and stress-corrosion cracking susceptibility while maintaining tensile strength above 500 MPa, making it suitable for thick-section fuselage and wing components in military and commercial aircraft.

aerospacestructural

Compliance & Regulations

?Conflict Free?FDA?RoHS?REACH?TSCA?Prop 65
7050 Aluminum/7050 Aluminum T7651
Filter by
Orientation
PropertyValueUnitConditionsSource
Compressive Modulus(Ec)
Pa22°C · Hand Forging
Compressive Tangent Modulus vs Stress(Etn(σ))2 entries
Curve (12 pts)
Pa21°C · L
Curve (12 pts)
Pa21°C · LT
Poisson's Ratio(ν)
-22°C
Shear Modulus(G)
Pa22°C · Hand Forging
Stress–Strain Curve (buckling region, ≤ 2% strain)(σ–ε (low-strain))4 entries
Curve (8 pts)
Pa21°C · L
Curve (8 pts)
Pa21°C · L
Curve (10 pts)
Pa21°C · LT
Curve (8 pts)
Pa21°C · LT
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.