Clad 7475 Aluminum T7751

metal

Clad 7475-T7751 is a high-strength aluminum alloy with a thin corrosion-resistant cladding layer, used primarily in aircraft structures and aerospace applications requiring superior fatigue resistance and stress-corrosion cracking resistance. The T7751 temper (solution heat-treated, artificially aged, and stress-relieved by stretching) provides optimized strength-toughness balance with tensile yield strength around 65 ksi and improved resistance to sustained-load cracking compared to peak-aged conditions.

aerospacestructural

Compliance & Regulations

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

Clad 7475 Aluminum/Clad 7475 Aluminum T7751

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 T7751

Mechanical Properties

Physical Properties

Regulatory Screening

Environmental

Safety & Biocompatibility

Quality & Standards