Clad 7475 Aluminum

Verifiedmetal

Clad 7475 is a high-strength aluminum-zinc-magnesium alloy with copper alloying used primarily in aircraft structures and aerospace applications requiring damage-tolerance and fatigue resistance. The material is clad with pure aluminum for enhanced corrosion resistance and offers yield strengths ranging from approximately 380–505 MPa depending on temper, with excellent fracture toughness characteristics across multiple overaged and retrogressed-and-reaged temper conditions.

aerospacestructural

Compliance & Regulations

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

Tempers & Conditions

T61 T6151 T61511 T651 T7351 T761 T7651 T7751 T77511 T7451

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

Verified Unverified Low confidence (<80%) Link to source

Property	Value	Unit	Conditions	Source
Density(ρ)	0.1010	lb/in³	22°C

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.