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7050
AMS 4340 / AlZn6CuMgZr / 7050 / T76511
| Chemical Properties | % Value |
| Silicon (Si) | 0,00 - 0,12 |
| Chromium (Cr) | 0,00 - 0,04 |
| Manganese (Mn) | 0,00 - 0,10 |
| Magnesium (Mg) | 1,90 - 2,60 |
| Copper (Cu) | 0,00 - 0,15 |
| Titanium (Ti) | 0,00 - 0,06 |
| Iron (Fe) | 0,00 - 0,15 |
| Zinc (Zn) | 5,70 - 6,70 |
| Aluminium (Al) | Balance |
| Physical Properties | Value |
| Density | 2,83 g/cm³ |
| Melting Point | 488 °C |
| Thermal Expansion | 23.5 µm/m.°C |
| Modulus of Elasticity | 71,7 GPa |
| Thermal Conductivity | 153 W/m.K |
| Electrical Resistivity | 35 % IACS |
| Mechanical Properties | Value |
| Proof Strength | 490 MPa |
| Yield Strength | 552 MPa |
| Shear Strength | 324 MPa |
| Elongation A50 mm | %11 |
| Hardness | 147 HB |
| 7050 T76511 Temperature – Ultimate Tensile Strength Graph |
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| 7050 T76511 Thickness – Ultimate Tensile Strength Graph |
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| 7050 T76511 Diameter – Ultimate Tensile Strength Graph |
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| 7050 T76511 Diameter-Yield Tensile Strength |
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7050 T76511 aluminum alloy belongs to the Al-Zn-Mg-Cu based 7000 series and represents a high-performance temper condition optimized for extrusion products. The T76511 temper includes solution heat treatment, advanced overaging, and stretching/straightening processes. Compared to T74511, it provides higher resistance to stress corrosion cracking (SCC), with a slight reduction in strength, making it particularly suitable for critical aerospace extrusion applications.
In terms of corrosion resistance, 7050 T76511 is one of the most SCC-resistant tempers within the 7000 series. Compared to 7075-T6 and T74511, it offers superior resistance to stress corrosion cracking. However, its general corrosion resistance is still lower than that of 6000 series alloys, and protective surface treatments are recommended in aggressive environments.
Regarding strength and mechanical properties, 7050 T76511 provides very high strength, although slightly lower than T6 and T74511 tempers. In return, toughness and resistance to crack propagation are significantly improved. Compared to 2024 alloy, it is superior in both strength and damage tolerance. It also offers high dimensional stability in extrusion products.
In terms of machinability, bendability, and weldability, 7050 T76511 has moderate machinability. Machining is possible but not as easy as with 6000 series alloys. Its weldability is limited and it is generally not preferred for welded applications. Its bending capability is low, and forming operations are typically performed before heat treatment. It provides advantages in dimensional stability and reduced internal stresses in extrusion products.
Regarding coating ability, vibration behavior, and applications, 7050 alloy is suitable for anodizing and protective coatings, although its decorative surface quality is limited. Its vibration damping capacity is low. Main application areas include aerospace industry, extrusion structural profiles, aircraft frame components, military systems, and critical load-bearing parts. 7050 T76511 is especially preferred in extrusion applications where maximum SCC resistance and stability are required.
7050 T76511 is available according to the following standards:
• 7050 T76511 Extrusion Bar; AMS 4340, WNR 3.4144, UNS A97050, ISO AlZn6CuMgZr
• 7050 T76511 Extrusion Plate; AMS 4340, WNR 3.4144, UNS A97050, ISO AlZn6CuMgZr
• 7050 T76511 Extrusion Wire; AMS 4340, WNR 3.4144, UNS A97050, ISO AlZn6CuMgZr
• 7050 T76511 Extrusion Tube; AMS 4340, WNR 3.4144, UNS A97050, ISO AlZn6CuMgZr
Selection Factors for 7050 T76511
- Strength: Excellent
- Machinability: Good
- Weldability: Poor
- Formability: Moderate
- Corrosion Resistance: Very Good
- Heat Treatment: Yes
Common Applications for 7050 T76511
Mainly in the aerospace industry,
Used as a component in aircraft seat rails,
Also used in the frame structures of motorcycles and bicycles.
7050 T76511 is produced and supplied in round/plate bars and tube/profile forms.
- Bar / Round Bar / Plate
- Tube / Profile




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