Clad 7475 Aluminum T7351

metal

Clad 7475-T7351 is a high-strength aluminum alloy (7xxx series, zinc-primary) with a thin corrosion-resistant aluminum or aluminum-alloy cladding layer, solution heat-treated, stress-relieved by controlled stretching, and artificially aged to T7351 condition for maximum stress-corrosion cracking (SCC) resistance while maintaining high yield strength (typically 415–435 MPa). This temper is specified for critical aerospace structures, particularly fuselage skins and other damage-tolerant applications where both strength and SCC resistance in marine or humid environments are required.

aerospacestructural

Compliance & Regulations

?Conflict Free?FDA?RoHS?REACH?TSCA?Prop 65
Clad 7475 Aluminum/Clad 7475 Aluminum T7351
PropertyValueUnitConditionsSource
Compressive Modulus(Ec)
Pa22°C · Sheet
Poisson's Ratio(ν)
-22°C
Shear Modulus(G)
Pa22°C · Sheet
S–N Curve (Wöhler)(S–N)
Pa8 entriesClick to expand
Young's Modulus(E)
Pa22°C · Sheet
N entriesMultiple entries per property — large groups are collapsed; click a summary row to expand. Use filters above to narrow by form / heat treatment / basis.
Rows with are inherited from the base material
Verified Unverified Low confidence (<80%) Link to source
PropertyValueUnitConditionsSource
Density(ρ)
kg/m³22°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.