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6013
AMS 4216 / AlMg1Si0.8CuMn / 6013 / T6
| Chemical Properties | % Value |
| Silicon (Si) | 0,60 - 1,00 |
| Chromium (Cr) | 0,00 - 0,10 |
| Manganese (Mn) | 0,20 - 0,80 |
| Magnesium (Mg) | 0,80 - 1,20 |
| Copper (Cu) | 0,60 - 1,10 |
| Titanium (Ti) | 0,00 - 0,10 |
| Iron (Fe) | 0,00 - 0,50 |
| Zinc (Zn) | 0,00 - 0,25 |
| Aluminium (Al) | Balance |
| Physical Properties | Value |
| Density | 2,72 g/cm³ |
| Melting Point | 579 °C |
| Thermal Expansion | 21.7 µm/m-°C |
| Modulus of Elasticity | 71 GPa |
| Thermal Conductivity | 150 W/m.K |
| Electrical Resistivity | %38 IACS |
| Mechanical Properties | Value |
| Proof Strength | 350 MPa |
| Yield Strength | 410 MPa |
| Shear Strength | 240 MPa |
| Elongation A50 mm | 9.1% |
| Hardness | 130 HB |
| 6013 T6 Temperature – Ultimate Tensile Strength Graph |
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| 6013 T6 Thickness – Ultimate Tensile Strength Graph |
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| 6013 T6 Diameter – Ultimate Tensile Strength Graph |
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6013 T6 aluminum alloy is a high-performance Al-Mg-Si-Cu (6xxx series) alloy that has been solution heat-treated and artificially aged (T6). This alloy stands out with its high strength, good corrosion resistance, and especially high fatigue resistance. It has been developed as an alternative to 2xxx series alloys in aerospace and structural applications.
In terms of strength, 6013 T6 provides higher strength than 6061-T6 and can reach levels close to 2024 alloy in some cases. Compared to 2024 alloy, it offers near similar strength levels while providing significantly better corrosion resistance. When compared to 7075 alloy, it has lower strength but offers better formability and surface durability.
In terms of machinability, 6013 T6 is at a good level and suitable for machining operations. However, due to the T6 temper, its bending capability is limited, and forming operations are generally performed in T4 condition. Due to its high strength, cold forming capability is limited, but it provides structural rigidity advantages.
In terms of coating capability, 6013 T6 performs well and is suitable for painting and anodizing. It provides advantages in surface protection and durability in aerospace applications. In terms of vibration response, it offers high fatigue resistance and long service life under dynamic loads.
Its weldability is moderate and it can be welded using appropriate techniques. Strength reductions may occur after welding. The 6013 T6 alloy is used in applications such as aircraft structures, aerospace panels, high-strength load-bearing systems, automotive structures, and advanced engineering applications. It stands out especially in applications requiring strength, lightweight, and fatigue resistance.
Selection Criteria for 6013 T6
- Strength: High
- Machinability: Satisfactory
- Weldability: Suitable
- Formability: Good
- Corrosion Resistance: Excellent
- Heat Treatment: Yes
Some Common Applications of 6013 T6
As ammunition components in the defense industry,
In rollerblade parts,
Used in automotive engine hoods.
6013 T6 is produced and supplied in sheet, round/plate rod, and tube/profile forms.
- Rod / Round Rod / Plate
- Sheet
- Tube/Profile



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