Heading
5056 work-hardens faster than 5052, so dies wear more and heavy upsets may need two stages. Good lubrication and burr-free cut-off are essential.
5056 rivet wire is a 5% magnesium aluminium wire, supplied annealed for cold heading, that produces the strongest of the non-heat-treatable aluminium rivets. It is the standard rivet alloy for joining magnesium structures, is widely used for zip fasteners and marine rivets, and needs no heat treatment before driving. Metline supplies 5056 and the European 5056A (now EN AW-5019) chemistry from 1.6 to 10 mm, with certificates, worldwide.

Most aluminium rivets fall into two groups: heat-treatable 2xxx rivets, which are strong but must be driven within a short time after solution treatment, and non-heat-treatable rivets in 1xxx, 3xxx and 5xxx alloys, which can be stored indefinitely. 5056 is the strongest member of the second group.
Its high magnesium content gives annealed wire that is still soft enough to head, yet the cold work of heading raises the rivet to a useful shear strength. In US military and aerospace fastener standards, 5056 rivets carry the material code B (for example MS20470B and MS20426B) and are supplied in the H32 condition, with a design shear strength of about 193 MPa (28 ksi), close to that of 2117-T4 "AD" rivets.
The main reason 5056 rivets exist, however, is galvanic compatibility. Magnesium alloys corrode rapidly when joined with copper-bearing 2xxx rivets; 5056 is close enough to magnesium in the galvanic series to be the specified rivet for magnesium parts in aircraft, helicopters and electronics housings.
5056 is the Aluminum Association / ASTM designation. 5056A is the older European designation for a closely related AlMg5 chemistry that EN 573-3 now registers as EN AW-5019. The main difference is that 5019 allows more manganese and iron. Confirm on your order which one your drawing calls for.
| Element | 5056 (UNS A95056) | EN AW-5019 (ex 5056A) |
|---|---|---|
| Magnesium (Mg) | 4.5 – 5.6 | 4.5 – 5.6 |
| Manganese (Mn) | 0.05 – 0.20 | 0.10 – 0.6 |
| Chromium (Cr) | 0.05 – 0.20 | 0.20 max |
| Silicon (Si) | 0.30 max | 0.40 max |
| Iron (Fe) | 0.40 max | 0.50 max |
| Copper (Cu) | 0.10 max | 0.10 max |
| Zinc (Zn) | 0.10 max | 0.20 max |
| Titanium (Ti) | — | 0.20 max |
| Others, each / total | 0.05 / 0.15 | 0.05 / 0.15 |
| Aluminium (Al) | Remainder | Remainder |
5019 limits as commonly listed from EN 573-3; the certificate for each lot gives the governing values.
Rivet wire standards set a maximum tensile strength for O-temper wire so that it heads without splitting. For 5056-O this cap is about 320 MPa (46 ksi). Typical values and the strength of driven rivets are shown for reference.
| Condition | Tensile strength | Yield strength | Elongation | Shear strength |
|---|---|---|---|---|
| 5056-O wire, specified | ≤ 320 MPa (max) | — | — | — |
| 5056-O, typical | 290 MPa | 150 MPa | 35 % | 180 MPa |
| 5056-H32 rivet, design value | — | — | — | ≈ 193 MPa (28 ksi) |
| 5056-H38, typical | 415 MPa | 345 MPa | 15 % | 234 MPa |
| Diameter (mm) | Class A | Class B | Class C | Class D |
|---|---|---|---|---|
| > 1.6 – 4.0 | +0 / −0.025 | +0.025 / −0.015 | ±0.025 | +0 / −0.05 |
| > 4.0 – 6.0 | +0 / −0.030 | +0.025 / −0.025 | ±0.040 | +0 / −0.08 |
| > 6.0 – 10.0 | +0 / −0.040 | +0.050 / −0.025 | ±0.060 | +0 / −0.12 |
Tolerance classes as commonly used for drawn rivet wire (GB/T 3195). ASTM B316 and EN 1301-3 tolerances are supplied when ordered to those standards.
5056 work-hardens faster than 5052, so dies wear more and heavy upsets may need two stages. Good lubrication and burr-free cut-off are essential.
Rivets can be driven as received at any time; there is no ageing clock as there is with 2017 or 2024 rivets.
Use 5056 rivets, ideally wet-installed with sealant, for magnesium skins and castings to minimise galvanic attack.
With more than 3 % magnesium, 5056 can become sensitised after long exposure above about 65 °C, making it prone to intergranular and stress corrosion. Use 5052 or 2117 rivets for warm service.
Very good resistance to seawater and marine air at normal temperatures; widely used for marine and coastal riveting.
Rivets can be anodised or chemically coated; aerospace rivets are often supplied with a conversion coating.
| Factor | 5056 | 5052 |
|---|---|---|
| Magnesium | 4.5 – 5.6 % | 2.2 – 2.8 % |
| Rivet strength | Higher | Medium |
| Ease of heading | Good | Very good |
| Use with magnesium | Standard choice | Less common |
| Service above 65 °C | Avoid long exposure | Suitable |
Choose 5056 for strength and magnesium compatibility; choose 5052 for easier heading and warm service. See the 5052 rivet wire guide for details.
5056 is the US-registered alloy. 5056A was a European AlMg5 variant, now designated EN AW-5019, which allows higher manganese and iron. Mechanical behaviour is similar, but the two are not identical on paper, so order the one your drawing specifies.
Magnesium corrodes quickly next to copper-bearing aluminium alloys. 5056 contains almost no copper and sits close to magnesium in the galvanic series, which keeps galvanic corrosion low.
No. It is non-heat-treatable, does not age, and can be headed and driven at any time after delivery.
For long-term service keep below about 65 °C. Above that, high-magnesium alloys can become sensitised and lose resistance to intergranular and stress corrosion.
In MS/NAS rivet part numbers, B denotes 5056 aluminium alloy, supplied in H32 condition. AD is 2117-T4, D is 2017-T4 and DD is 2024-T4.
Tell us the alloy, diameter, tolerance and coil size. We will reply with availability, certification and a delivered price.