Sources and scope for this page: Aluminium Association International Alloy Designation System (the designation system is stable; compositions are registered as needed), covering alloy designations, series classification and temper nomenclature. No independent source check is recorded for this page: the content rests on the sources listed and on the working shown on the page. Full sources, values and limits on this page.
Page last changed 2026-10-19 · based on n/a — the designation system is stable; compositions are registered as needed
Quick Answer
Aluminium Alloy Grades
| Designation[1] | Series[1] | Alloying[1] | Typical use[1] | Hardness[1] | Heat treatment[1] |
|---|---|---|---|---|---|
| 1050 # | 1xxx | Pure aluminium, 99.5% | Electrical, chemical equipment | 27 HB | Non-heat-treatable |
| 1100 # | 1xxx | Pure aluminium, 99.0% | Deep drawing, spun parts | 28 HB | Non-heat-treatable |
| 2024 # | 2xxx | Cu-Mg, high strength | Aircraft structures | 120 HB | Heat-treatable |
| 2011 # | 2xxx | Cu, free-machining | Screw machine parts | 95 HB | Heat-treatable |
| 3003 # | 3xxx | Mn, moderate strength | Cooking utensils, signage | 40 HB | Non-heat-treatable |
| 5052 # | 5xxx | Mg, corrosion resistant | Marine, pressure vessels | 60 HB | Non-heat-treatable |
| 5083 # | 5xxx | Mg-Mn, high strength | Welded marine structures | 75 HB | Non-heat-treatable |
| 6061 # | 6xxx | Mg-Si, general structural | Frames, brackets, extrusions | 95 HB | Heat-treatable |
| 6063 # | 6xxx | Mg-Si, extrusion alloy | Architectural extrusions | 73 HB | Heat-treatable |
| 6082 # | 6xxx | Mg-Si-Mn, structural | Bridges, cranes, machined parts | 95 HB | Heat-treatable |
| 7050 # | 7xxx | Zn-Cu-Mg, high strength | Thick aircraft sections | 150 HB | Heat-treatable |
| 7075 # | 7xxx | Zn-Mg-Cu, very high strength | Aircraft, moulds | 150 HB | Heat-treatable |
| 2024-T4 # | 2xxx | 2024 solution treated | Aircraft skins | 120 HB | Heat-treatable |
| 6061-T6 # | 6xxx | 6061 peak aged | General structural | 95 HB | Heat-treatable |
| 7075-T6 # | 7xxx | 7075 peak aged | High-stress aircraft parts | 150 HB | Heat-treatable |
Hardness values are typical for the common temper of each grade. The temper designation — O, H, T4, T6 — follows the alloy number and matters as much as the alloy itself: 6061-O and 6061-T6 differ by a factor of three in strength.
The Four-Digit System
The AA designation encodes both the alloy family and the specific composition:
- First digit — series, set by the principal alloying element. This is the part that matters most when choosing.
- Second digit — a modification of the original alloy, or zero for the original.
- Last two digits — a sequential identifier within the series. They do not encode composition the way steel designations do.
The temper follows a hyphen: 6061-T6 is alloy 6061 in the solution heat-treated and artificially aged condition. O is annealed, H is strain-hardened, T4 is solution treated and naturally aged, T6 is solution treated and artificially aged.
Choosing a Series
- 1xxx — pure. Excellent conductivity and corrosion resistance, very low strength. Electrical busbar, chemical equipment.
- 2xxx — copper. High strength and good fatigue performance, poor corrosion resistance without cladding, effectively unweldable. Aircraft skins.
- 3xxx — manganese. Moderate strength, good formability. Not heat-treatable. Cookware and signage.
- 5xxx — magnesium. Best corrosion resistance of the common series, good weldability, work-hardening. Marine work.
- 6xxx — magnesium and silicon. The general-purpose structural series: extrudable, weldable, heat-treatable, and the easiest aluminium to machine.
- 7xxx — zinc. The highest strength aluminium alloys, at the cost of corrosion resistance and weldability. Aircraft structure and moulds.
Frequently Asked Questions
- What is the difference between 6061 and 7075?
- 7075 is substantially stronger — about 572 MPa tensile against 310 MPa for 6061 in the T6 temper — but it is less corrosion resistant, effectively unweldable and more expensive. 6061 is the general-purpose structural alloy; 7075 is used where strength is the limiting requirement.
- Is aluminium 6061 heat treatable?
- Yes. 6061 is a 6xxx series alloy and responds to solution treatment and artificial ageing, giving the T6 temper. The 1xxx, 3xxx and 5xxx series are not heat-treatable and gain strength only by strain hardening.
- What does T6 mean in aluminium?
- Solution heat treated and then artificially aged — the peak-strength condition for most heat-treatable alloys. Other common tempers are O (annealed), H (strain hardened) and T4 (solution treated and naturally aged).
- Which aluminium is best for machining?
- 6061-T6 is the usual choice: it machines cleanly, holds tolerance well and is widely available. 2011 is a free-machining grade with better chip breaking but poorer corrosion resistance. All aluminium machines far faster than steel — ratings of 150–300% on the machinability scale are normal.
- What is the strongest aluminium alloy?
- The 7xxx series, and within it the high-zinc alloys such as 7075 and 7050, reaching about 570 MPa tensile in the T6 temper. This is comparable to some structural steels at roughly a third of the density.
- Is 5052 or 6061 better for marine use?
- 5052, and the 5xxx series generally, has better corrosion resistance in salt water — it is the standard marine aluminium. 6061 is stronger and heat-treatable but less corrosion resistant, so it is usually specified with a protective coating in marine service.
Related
Value Sources
References and calculation methods used for this page are listed below. Numbered markers connect table columns where present. A reference listing does not itself establish that every value has been independently checked.
| # | Source | Type | Revision / method |
|---|---|---|---|
| [1] | Aluminium Association designation system, with properties from published alloy data | reference | n/a — designation system with periodic composition revisions — source |
Data Sources
| Standard | Revision | What it covers on this page |
|---|---|---|
| Aluminium Association International Alloy Designation System | n/a — the designation system is stable; compositions are registered as needed | alloy designations, series classification and temper nomenclature |
Verification scope
No page-specific independent source review is recorded here. The listed references and formulas explain the basis of the compilation; automated consistency checks do not verify the original sources or establish product conformity.
Typical values for the common temper of each grade. Temper matters as much as alloy — verify the specific temper's properties before design use.
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