7475 Aluminum T6151

metal

7475 aluminum T6151 is a high-strength Al-Zn-Mg-Cu aerospace alloy in a solution heat-treated and artificially aged condition with controlled cold-working, delivering tensile strengths of 435–495 MPa with improved fracture toughness and stress-corrosion cracking resistance compared to standard T6 temper. Primary applications include critical aircraft structural components, fuselage skins, and fastener applications requiring damage-tolerant performance in sustained-load environments.

aerospacestructural

Compliance & Regulations

?Conflict Free?FDA?RoHS?REACH?TSCA?Prop 65

7475 Aluminum/7475 Aluminum T6151

Units:

si imperial

Property	Value	Unit	Conditions
Compressive Modulus(Ec)	72.39	GPa	22°C · Sheet
Poisson's Ratio(ν)	0.3300	-	22°C
Shear Modulus(G)	26.20	GPa	22°C · Sheet
Young's Modulus(E)	68.95	GPa	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)	2.796	kg/m³	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.

7475 Aluminum T6151

Mechanical Properties

Physical Properties

Regulatory Screening

Environmental

Safety & Biocompatibility

Quality & Standards