5086 Aluminum H112
Verifiedmetal5086 aluminum is a non-heat-treatable Al-Mg alloy (nominally 3-4% Mg) with excellent seawater corrosion resistance and moderate strength, commonly used in marine vessels, automotive fuel tanks, and pressure vessels; H112 temper provides stress-relieved, partially annealed conditions suitable for applications requiring improved dimensional stability after fabrication while maintaining workability for extrusions and plate stock.
aerospacestructural
Compliance & Regulations
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Specification
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Ultimate Bearing Strength(Fbru) | — | ksi | 8 entriesClick to expand | ||
Bearing Yield Strength(Fbry)4 entries | — | ksi | 22°C · Sheet/Plate · H112 · AMS-QQ-A-250/7 · t=0.188-0.499 in · e/D=1.5 | — | |
| ↳ | — | ksi | 22°C · Sheet/Plate · H112 · AMS-QQ-A-250/7 · t=0.500-1.00 in · e/D=1.5 | — | |
| ↳ | — | ksi | 22°C · Sheet/Plate · H112 · AMS-QQ-A-250/7 · t=1.001-2.000 in · e/D=1.5 | — | |
| ↳ | — | ksi | 22°C · Sheet/Plate · H112 · AMS-QQ-A-250/7 · t=2.001-3.000 in · e/D=1.5 | — | |
Compressive Modulus(Ec) | — | ksi | 22°C · Sheet/Plate | — | |
Compressive Tangent Modulus vs Stress(Etn(σ))2 entries | Curve (10 pts) | ksi | 21°C · L | — | |
| ↳ | Curve (13 pts) | ksi | 21°C · LT | — | |
Compressive Yield Strength(Fcy) | — | ksi | 12 entriesClick to expand | ||
Elongation at Break(εf) | — | - | 5 entriesClick to expand | ||
Poisson's Ratio(ν) | — | - | 22°C | — | |
Shear Modulus(G) | — | ksi | 22°C · Sheet/Plate | — | |
Ultimate Shear Strength(Fsu)4 entries | — | ksi | 22°C · Sheet/Plate · H112 · AMS-QQ-A-250/7 · t=0.188-0.499 in | — | |
| ↳ | — | ksi | 22°C · Sheet/Plate · H112 · AMS-QQ-A-250/7 · t=0.500-1.00 in | — | |
| ↳ | — | ksi | 22°C · Sheet/Plate · H112 · AMS-QQ-A-250/7 · t=1.001-2.000 in | — | |
| ↳ | — | ksi | 22°C · Sheet/Plate · H112 · AMS-QQ-A-250/7 · t=2.001-3.000 in | — | |
Stress–Strain Curve (buckling region, ≤ 2% strain)(σ–ε (low-strain))4 entries | Curve (9 pts) | ksi | 21°C · L | — | |
| ↳ | Curve (10 pts) | ksi | 21°C · L | — | |
| ↳ | Curve (9 pts) | ksi | 21°C · LT | — | |
| ↳ | Curve (9 pts) | ksi | 21°C · LT | — | |
Ultimate Tensile Strength(σUTS) | — | ksi | 9 entriesClick to expand | ||
Yield Strength (0.2% offset)(σy) | — | ksi | 9 entriesClick to expand | ||
Young's Modulus(E) | — | ksi | 22°C · Sheet/Plate | — | |
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 (17 pts) | µin/in·°F | — | — | |
Thermal Conductivity vs Temperature(k(T)) | Curve (20 pts) | BTU/(hr·ft·°F) | — | — |
Rows with are inherited from the base material
Verified Unverified Low confidence (<80%) Link to source
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Density(ρ) | — | lb/in³ | 22°C | — |
Rows with are inherited from the base material
Verified Unverified Low confidence (<80%) Link to source
Regulatory Screening
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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.