Clad 7475 Aluminum T7651

metal

Clad 7475-T7651 is a high-strength aluminum-zinc-magnesium-copper alloy with an alclad corrosion-resistant coating, solution heat-treated, artificially aged, and stress-relieved by stretching to provide yield strength of approximately 70 ksi with enhanced stress-corrosion cracking resistance compared to unstretched tempers. Primary applications include aircraft fuselage, wing structures, and pressurized components requiring superior fatigue performance and sustained load capability in aerospace environments.

aerospacestructural

Compliance & Regulations

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

Clad 7475 Aluminum/Clad 7475 Aluminum T7651

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.

Clad 7475 Aluminum T7651

Mechanical Properties

Physical Properties

Regulatory Screening

Environmental

Safety & Biocompatibility

Quality & Standards