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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
Density2,72 g/cm³
Melting Point579 °C
Thermal Expansion21.7 µm/m-°C
Modulus of Elasticity71 GPa
Thermal Conductivity150 W/m.K
Electrical Resistivity%38 IACS
Mechanical Properties Value
Proof Strength350 MPa
Yield Strength410 MPa
Shear Strength240 MPa
Elongation A50 mm9.1%
Hardness130 HB
6013 T6 Temperature – Ultimate Tensile Strength Graph
6013 T6 Temperature – Ultimate Tensile Strength Graph
6013 T6 Thickness – Ultimate Tensile Strength Graph
6013 T6 Thickness – Ultimate Tensile Strength Graph
6013 T6 Diameter – Ultimate Tensile Strength Graph
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.

 

ALLOY DESIGNATIONS

6013 T6 can be supplied according to the following standards:
• 6013 T6 Sheet; AMS 4216, UNS A96013, ASTM B209, ISO AlMg1Si0.8CuMn
• 6013 T6 Extrusion Round Bar; UNS A96013, ASTM B221, ISO AlMg1Si0.8CuMn
• 6013 T6 Extrusion Plate; UNS A96013, ASTM B221, ISO AlMg1Si0.8CuMn
• 6013 T6 Extrusion Wire; UNS A96013, ASTM B221, ISO AlMg1Si0.8CuMn
• 6013 T6 Extrusion Tube; UNS A96013, ASTM B221, ISO AlMg1Si0.8CuMn

 

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.

 

SUPPLIED FORMS
6013 T6 is produced and supplied in sheet, round/plate rod, and tube/profile forms.
  • Rod / Round Rod / Plate
  • Sheet
  • Tube/Profile
 
DELIVERY: