Clad 7475 Aluminum T651

metal

Clad 7475 aluminum alloy T651 is a zinc-primary aerospace alloy with copper and magnesium additions, clad with pure aluminum for enhanced corrosion resistance, and solution heat-treated plus artificially aged to T651 condition for high strength and controlled stress-relief properties. It provides tensile strengths in the range of 70–80 ksi with good fatigue resistance and fracture toughness suitable for critical airframe components including wing and fuselage skins in high-performance military and commercial aircraft.

aerospacestructural

Compliance & Regulations

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

Clad 7475 Aluminum/Clad 7475 Aluminum T651

Units:

si imperial

Property	Value	Unit	Conditions
Compressive Modulus(Ec)	10,500	ksi	22°C · Sheet
Poisson's Ratio(ν)	0.3300	-	22°C
Shear Modulus(G)	3,800	ksi	22°C · Sheet
Young's Modulus(E)	10,000	ksi	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)	0.1010	lb/in³	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 T651

Mechanical Properties

Physical Properties

Regulatory Screening

Environmental

Safety & Biocompatibility

Quality & Standards