7049/7149 Aluminum T6151

metal

7049/7149 Aluminum T6151 is a high-strength Al-Zn-Mg-Cu aerospace alloy in a overaged temper condition that provides improved stress-corrosion cracking (SCC) resistance and fracture toughness compared to T6, with typical yield strengths of 65–75 ksi and applications in highly stressed structural components, fuselage skins, and wing elements where damage tolerance is critical.

aerospacestructural

Compliance & Regulations

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

7049/7149 Aluminum/7049/7149 Aluminum T6151

Units:

si imperial

Property	Value	Unit	Conditions
Compressive Modulus(Ec)	10,600	ksi	22°C · Hand forging
Poisson's Ratio(ν)	0.3300	-	22°C
Shear Modulus(G)	3,900	ksi	22°C · Die forging
Young's Modulus(E)	10,200	ksi	22°C · Die forging

Rows with are inherited from the base material

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

Property	Value	Unit	Conditions	Source
Density(ρ)	0.1030	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.

7049/7149 Aluminum T6151

Mechanical Properties

Physical Properties

Regulatory Screening

Environmental

Safety & Biocompatibility

Quality & Standards