2124 Aluminum T851

Verifiedmetal

2124 aluminum alloy is a Cu-containing aerospace aluminum with high strength-to-weight ratio, used primarily in aircraft fuselage and structural applications requiring elevated temperature performance. T851 temper (solution heat-treated, stress-relieved, and overaged) provides controlled strength with improved stress-corrosion cracking resistance suitable for critical loaded components.

aerospacestructural

Compliance & Regulations

?Conflict Free?FDA?RoHS?REACH?TSCA?Prop 65
2124 Aluminum/2124 Aluminum T851
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Thickness
e/D Ratio
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PropertyValueUnitConditionsSource
Ultimate Bearing Strength(Fbru)
ksi20 entriesClick to expand
Bearing Yield Strength(Fbry)
ksi20 entriesClick to expand
Compressive Tangent Modulus vs Stress(Etn(σ))3 entries
Curve (13 pts)
ksi21°C · L
Curve (13 pts)
ksi21°C · LT
Curve (15 pts)
ksi21°C · ST
Compressive Yield Strength(Fcy)
ksi32 entriesClick to expand
Elongation at Break(εf)
-19 entriesClick to expand
Fatigue Crack Growth Rate(da/dN)
m/cycle12 entriesClick to expand
Shear Modulus(G)
ksi22°C · Plate
Ultimate Shear Strength(Fsu)
ksi30 entriesClick to expand
Stress–Strain Curve (buckling region, ≤ 2% strain)(σ–ε (low-strain))
ksi6 entriesClick to expand
Ultimate Tensile Strength(σUTS)
ksi34 entriesClick to expand
Yield Strength (0.2% offset)(σy)
ksi34 entriesClick to expand
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
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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.
2124 Aluminum T851 — Properties & Data | MatWorld