5154A Aluminum

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5154A Aluminum is an active registered wrought Al–Mg alloy in the 5000 series, designated AlMg3.5(A) in the former ISO cross-reference. Its 3.1–3.9% magnesium content provides useful solid-solution strengthening while retaining the corrosion resistance, weldability and cold-forming character associated with non-heat-treatable aluminum-magnesium sheet alloys. The A suffix is part of the alloy designation: 5154A has its own registered composition and should not be specified interchangeably with 5154, 5154B or 5154C. Final strength is developed principally by strain hardening rather than precipitation heat treatment.
| Chemical Composition wt.% | ||
|---|---|---|
| Element | Min | Max |
| Silicon | — | 0.50 |
| Iron | — | 0.50 |
| Copper | — | 0.10 |
| Manganese | — | 0.50 |
| Magnesium | 3.1 | 3.9 |
| Chromium | — | 0.25 |
| Zinc | — | 0.20 |
| Titanium | — | 0.20 |
| Manganese + Chromium | 0.10 | 0.50 |
| Others, each | — | 0.05 |
| Others, total | — | 0.15 |
| Aluminum | Remainder | |
Composition notes
- Manganese: Also subject to the combined Mn + Cr requirement.
- Chromium: Also subject to the combined Mn + Cr requirement.
- Manganese + Chromium: Combined composition restriction.
- Others, each: Unspecified elements.
- Others, total: Unspecified elements.
Registered wrought composition limits, percent by mass. In addition to the individual manganese and chromium limits, the registered composition requires Mn + Cr to be 0.10–0.50%. “Others” limits apply to unspecified individual and total elements; aluminum is the remainder.
The Aluminum Association lists calculated nominal density for the active wrought 5154A designation. Mechanical values depend on product form, thickness and strain-hardened temper and are not stated in the supplied registered-alloy source.
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| Physical Properties | Metric |
|---|---|
| Density (calculated nominal) | 2.67 × 10³ kg/m³2.67 g/cm³ |
Test conditions & data notes
- Density (calculated nominal): Active wrought 5154A designation; calculated nominal density.
Material Conditions & Tempers
5154A is a non-heat-treatable wrought alloy. It is normally supplied in annealed or strain-hardened conditions; the selected temper should be stated together with the applicable product standard, thickness range and required mechanical properties. No temper-specific mechanical-property table was provided in the supplied source.
| Condition | Description | Notes |
|---|---|---|
| O | Annealed condition, selected where maximum forming latitude and ductility are more important than strain-hardened strength. | Mechanical requirements depend on the applicable product specification and thickness. |
| H1x / H2x | Strain-hardened tempers used to obtain higher strength in sheet, strip or other wrought products; H2x denotes material that is strain hardened and then partially annealed. | Specify the complete temper designation and product standard when ordering. |
| H3x | Strain-hardened and stabilized tempers may be used where a stabilized condition is specified for the product. | Availability and mechanical requirements are product-standard dependent. |
Advantages & Limitations
| Advantages | Limitations |
|---|---|
|
|
Processing & Fabrication
| Process | Description |
|---|---|
| Cold forming | Use the O temper for demanding bends, draws and formed profiles. Strain-hardened tempers offer greater strength but lower forming margin, particularly in tight-radius or severe draws. |
| Welding | The Al–Mg alloy family is generally well suited to conventional fusion-welding fabrication. Use a qualified welding procedure and filler-metal selection appropriate to the joint, service environment and required corrosion performance. |
| Cutting and machining | Sheet and strip can be sheared, punched or formed using normal aluminum practices. Provide clearance and tooling appropriate to the selected temper to control edge quality and distortion. |
| Heat treatment | Do not specify solution heat treatment and artificial aging as a means of raising strength. If stress relief or thermal processing is contemplated, verify the resulting temper and properties against the governing product specification. |
| Surface preparation | Remove lubricants, oxides and shop contamination before welding, coating or bonding. Surface-treatment selection should reflect the intended coating system and exposure environment. |
Applications
5154A is most relevant to wrought sheet, strip and formed fabricated parts where a medium-magnesium 5xxx alloy is desired for corrosion resistance, weldability and useful strain-hardened strength. Suitability should be confirmed against the governing product standard and the selected temper.
- Corrosion-resistant sheet fabrications: The aluminum-magnesium composition supports lightweight formed assemblies intended for atmospheric or moisture-prone service.
- Welded panels and enclosures: Non-heat-treatable 5xxx alloys are valued where formed sheet must be joined by fusion welding without relying on post-weld precipitation aging.
- Transportation and equipment sheet components: Low density, cold-forming capability and available strain-hardened conditions support weight-conscious panels, guards and fabricated components.
- Marine-adjacent fabricated items: The Al–Mg alloy family offers useful resistance in many marine and salt-laden exposures; design, weld procedure and service temperature must still be evaluated for the actual duty.
Standards & Designations
| Designation | Value | Description |
|---|---|---|
| Aluminum Association International Alloy Designation System | 5154A | Active registered wrought aluminum-alloy designation; the registered composition is listed in the Aluminum Association Teal Sheets. |
| Former ISO 209-1 cross-reference | AlMg3.5(A) | The supplied Teal Sheets cross-reference lists 5154A as AlMg3.5(A) and notes that ISO 209-1 has been withdrawn and replaced by ISO 209. |
| AA designation | AA 5154A | The A suffix is integral to the designation and identifies a composition distinct from unsuffixed 5154. |
Frequently Asked Questions
Is 5154A the same alloy as 5154?
No. 5154A is a separately registered wrought designation. Although both are Al–Mg 5xxx alloys, their registered composition limits differ; 5154A, for example, permits up to 0.50% silicon and iron and has a 0.10–0.50% combined Mn + Cr restriction. Specify the exact suffix.
Can 5154A be strengthened by heat treatment?
No. 5154A is a non-heat-treatable aluminum-magnesium alloy. Its practical strength level is established mainly by cold work and the supplied temper, such as annealed O or a strain-hardened H temper.
What information should be included when ordering 5154A sheet or strip?
State 5154A, the required product form and dimensions, complete temper, applicable product specification, and any mechanical-property, corrosion, surface-finish or inspection requirements. The alloy name alone does not establish temper-specific mechanical properties.
References & Data Notes
- (n.d.). The Aluminum Association, International Alloy Designations and Chemical Composition Limits for Wrought Aluminum and Wrought Aluminum Alloys (Teal Sheets), revised December 2025. https://www.aluminum.org/sites/default/files/2026-01/Teal%20Sheets%20December%202025.pdf
Composition limits and calculated nominal density are taken from the supplied Aluminum Association Teal Sheets source for the exact active wrought 5154A designation. No temper-specific mechanical, thermal or electrical numerical data were supplied; those values must be obtained from an applicable 5154A product standard or producer datasheet for the required form and temper.