2014 Aluminum T62
Verifiedmetal2014 aluminum is a copper-alloyed, high-strength aluminum alloy used primarily in aerospace airframe structures and components requiring elevated strength-to-weight ratios. The T62 temper (solution heat-treated and artificially aged) delivers high yield and tensile strength with moderate ductility, suitable for aircraft skin, fuselage, and structural applications operating at room temperature.
aerospacestructural
Compliance & Regulations
?Conflict Free?FDA?RoHS?REACH?TSCA?Prop 65
Filter by
Form
Thickness
Orientation
Specification
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Compressive Modulus(Ec) | — | Pa | 22°C · Bar/Extrusion/Rod | — | |
Compressive Tangent Modulus vs Stress(Etn(σ))4 entries | Curve (8 pts) | Pa | 21°C · L | — | |
| ↳ | Curve (9 pts) | Pa | 21°C · LT | — | |
| ↳ | Curve (7 pts) | Pa | 21°C · L | — | |
| ↳ | Curve (8 pts) | Pa | 21°C · LT | — | |
Compressive Yield Strength(Fcy) | — | Pa | 22°C · Bar/Extrusion/Rod · T62a · AMS-QQ-A-200/2 · L · t=≤25 in | — | |
Elongation at Break(εf)3 entries | — | - | 22°C · Bar/Rod · T62a · AMS-QQ-A-225/4 · L · t=≤8.000b in | — | |
| ↳ | — | - | 22°C · Bar/Extrusion/Rod · T62a · AMS-QQ-A-200/2 · L · t=≤25 in | — | |
| ↳ | — | - | 22°C · Bar/Extrusion/Rod · T62a · AMS-QQ-A-200/2 · L · t=>25-≤32 in | — | |
Poisson's Ratio(ν) | — | - | 22°C | — | |
Shear Modulus(G) | — | Pa | 22°C · Bar/Extrusion/Rod | — | |
Stress–Strain Curve(σ–ε) | Curve (10 pts) | Pa | 21°C · L | — | |
Stress–Strain Curve (buckling region, ≤ 2% strain)(σ–ε (low-strain)) | — | Pa | 8 entriesClick to expand | ||
Ultimate Tensile Strength(σUTS)3 entries | — | Pa | 22°C · Bar/Rod · T62a · AMS-QQ-A-225/4 · L · t=≤8.000b in | — | |
| ↳ | — | Pa | 22°C · Bar/Extrusion/Rod · T62a · AMS-QQ-A-200/2 · L · t=≤25 in | — | |
| ↳ | — | Pa | 22°C · Bar/Extrusion/Rod · T62a · AMS-QQ-A-200/2 · L · t=>25-≤32 in | — | |
Yield Strength (0.2% offset)(σy)3 entries | — | Pa | 22°C · Bar/Rod · T62a · AMS-QQ-A-225/4 · L · t=≤8.000b in | — | |
| ↳ | — | Pa | 22°C · Bar/Extrusion/Rod · T62a · AMS-QQ-A-200/2 · L · t=≤25 in | — | |
| ↳ | — | Pa | 22°C · Bar/Extrusion/Rod · T62a · AMS-QQ-A-200/2 · L · t=>25-≤32 in | — | |
Young's Modulus(E) | — | Pa | 22°C · Bar/Extrusion/Rod | — | |
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
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
CTE vs Temperature(α(T)) | Curve (15 pts) | 1/K | — | — | |
Specific Heat vs Temperature(Cp(T)) | Curve (12 pts) | J/(kg·K) | — | — | |
Thermal Conductivity vs Temperature(k(T)) | Curve (15 pts) | W/(m·K) | — | — |
Rows with are inherited from the base material
Verified Unverified Low confidence (<80%) Link to source
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Density(ρ) | — | kg/m³ | 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.