O (annealed)
Softest condition and the normal state for cold heading. Rivets are headed in O and then heat-treated, or driven soft where low strength is acceptable.
6053 is a magnesium-silicon aluminium alloy made almost entirely for one job: wire that is cold-headed into solid and tubular rivets. It has more magnesium and less iron than 6061, so it heads cleanly in the soft condition and then reaches useful strength after heat treatment. Metline supplies 6053 wire in coils and straight lengths to ASTM B316 and customer specifications, worldwide.

6053 (UNS A96053) is a heat-treatable 6xxx alloy designed for cold heading. Its magnesium content of 1.1 – 1.4 % is higher than in 6061, while iron, copper and zinc are kept very low. That combination gives a soft, clean wire that forms rivet heads without cracking and still responds to solution treatment and ageing.
In aircraft and general engineering, 6053 sits between the soft 1100 and 3003 rivet alloys and the high-strength 2017, 2024 and 2117 rivet alloys. It is chosen when a rivet must be stronger than a pure-aluminium rivet but must not introduce copper, which can harm corrosion resistance when the rivet sits in a magnesium-silicon or aluminium-magnesium structure. Tubular and semi-tubular rivets, rivets for anodised assemblies and fasteners for interior and secondary structure are typical uses.
The alloy is not a high-strength structural wire. Its value lies in good headability, good corrosion behaviour and a strength level that is predictable after a simple heat treatment.
The silicon limit for 6053 is unusual: it is set as a proportion of the actual magnesium content, so the alloy always has a controlled magnesium-to-silicon balance. Values follow the registered Aluminum Association limits used by ASTM B316.
| Element | Minimum | Maximum | Note |
|---|---|---|---|
| Silicon (Si) | 45 % of Mg | 65 % of Mg | Roughly 0.50 – 0.91 % depending on the magnesium level |
| Iron (Fe) | — | 0.35 | Kept low for headability |
| Copper (Cu) | — | 0.10 | Very low; helps corrosion resistance |
| Magnesium (Mg) | 1.10 | 1.40 | Main alloying element |
| Chromium (Cr) | 0.15 | 0.35 | Grain control, stress-corrosion resistance |
| Zinc (Zn) | — | 0.10 | Impurity |
| Others, each / total | — | 0.05 / 0.15 | |
| Aluminium (Al) | Remainder |
Earlier data circulating for "6053" with 0.4 – 0.7 % copper does not match the registered alloy. Always check that the mill certificate reports magnesium of 1.1 – 1.4 % and copper of 0.10 % maximum.
Softest condition and the normal state for cold heading. Rivets are headed in O and then heat-treated, or driven soft where low strength is acceptable.
Lightly drawn for better straightness and feeding on automatic heading machines while keeping enough ductility for the head.
Solution heat-treated and naturally aged. Used where the rivet is formed after treatment or where moderate strength is enough.
Solution heat-treated and artificially aged. The usual finished condition for 6053 rivets, giving the highest strength the alloy offers.
6053 in T61 is weaker than 6061-T6: it trades some tensile and shear strength for easier heading and better corrosion behaviour. Exact minimum tensile and shear values depend on the temper and diameter in the order specification, and are stated on the mill certificate. When designing a riveted joint, use the allowables in your design code or rivet standard, not general typical values.
Physical constants for 6053 are close to other 6xxx alloys. The density of 2.78 g/cm³ quoted on some sites is too high for this alloy.
Rivet makers usually specify a diameter tolerance, a heading or upset test and a surface free of seams, scratches and laps, because any surface defect opens up when the head is formed. Tell us your heading ratio and the finished rivet temper so the wire condition can be matched to the process.
6053 is not an electrical conductor alloy and not a structural wire for high loads. For high-strength rivets, aircraft structure normally uses 2117-T4 ("AD"), 2017-T4 ("D") or 2024-T4 ("DD") rivets; for the softest rivets, 1100 is used.
| Alloy | Family | Typical rivet temper | Relative strength | Main reason to choose it |
|---|---|---|---|---|
| 1100 | Pure aluminium | F / H14 | Lowest | Very soft, non-structural rivets |
| 5056 | Al-Mg | H32 | Moderate | Rivets for magnesium alloy structures |
| 6053 | Al-Mg-Si | T61 | Moderate | Good headability, copper-free, heat-treatable |
| 6061 | Al-Mg-Si-Cu | T6 | Moderate–higher | Higher strength 6xxx rivets and pins |
| 2117 | Al-Cu | T4 | Higher | Standard aircraft rivet driven as received |
| 2017 / 2024 | Al-Cu | T4 | High | Structural rivets; often driven fresh or refrigerated |
Relative strength is given in words because values depend on the rivet standard and diameter. If you are replacing one rivet alloy with another, check the joint allowables, not just the material tensile strength.
Almost entirely for rivet and cold-heading wire. Its high magnesium and low iron and copper content make it easy to head, and it can be heat-treated to T61 after forming.
No. Both are Al-Mg-Si alloys, but 6053 has more magnesium (1.1 – 1.4 %), much less copper (0.10 % max) and less iron. It is softer and heads more easily; 6061 is stronger.
Most rivet makers buy O or a light H13 temper for heading, then solution treat and age the rivets to T61. Order T4 or T61 wire only if the forming is done after heat treatment.
ASTM B316/B316M, the specification for aluminium and aluminium-alloy rivet and cold-heading wire and rod. Many OEMs also issue their own wire specifications that reference it.
Primary structure normally uses 2117, 2017 or 2024 rivets, which have published design allowables. 6053 is used for secondary structure, interiors and equipment where its corrosion behaviour and headability are worth more than peak strength.
Yes. Metline supplies 6053 wire worldwide from Mumbai, with mill test certificates and export packing on EXW, FOB, CIF or DAP terms.
Send diameter, temper, quantity and the specification. Our team will confirm availability, tests and a delivered price.