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7050
ASTM B221 / AlZn6CuMgZr / 7050 / T76
| 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) | 2,00 - 2,60 |
| Titanium (Ti) | 0,08 - 0,21 |
| Iron (Fe) | 0,00 - 0,15 |
| Zinc (Zn) | 5,70 - 6,70 |
| Aluminium (Al) | Balance |
| Physical Properties | Value |
| Density | 2,80 g/cm³ |
| Melting Point | 610 °C |
| Thermal Expansion | 21.7 µm/m.°C |
| Modulus of Elasticity | 71 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 T76 Temperature – Ultimate Tensile Strength Graph |
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| 7050 T76 Thickness – Ultimate Tensile Strength Graph |
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| 7050 T76 Diameter – Ultimate Tensile Strength Graph |
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| 7050 T76 Diameter-Yield Tensile Strength |
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7050 T76 aluminum alloy belongs to the Al-Zn-Mg-Cu based 7000 series and represents a temper condition optimized for applications requiring high strength along with improved resistance to stress corrosion cracking (SCC). The T76 temper includes solution heat treatment and overaging, providing significantly higher corrosion and crack resistance compared to T6, at the expense of slightly reduced strength. Therefore, it is widely preferred in aerospace and critical structural applications.
In terms of corrosion resistance, 7050 T76 offers high performance within the 7000 series. Its resistance to stress corrosion cracking is significantly superior to 7075-T6. However, its general corrosion resistance is lower than that of 6000 series alloys. In marine and aggressive environments, it is generally recommended to use protective coatings.
Regarding strength and mechanical properties, 7050 T76 provides very high strength, although slightly lower than the T6 temper. In return, toughness and resistance to crack propagation are significantly improved. Compared to 2024 alloy, it offers higher strength and better damage tolerance. Its performance is particularly stable in thick sections.
In terms of machinability, bendability, and weldability, 7050 T76 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. Similar to 7075, it is mainly used in machined and forged components.
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, aircraft wing and fuselage components, military applications, and high-safety structural parts. 7050 T76 is preferred especially in applications where both high strength and high crack resistance are critical.
• 7050 T76 Plate; EN 4449, WNR 3.4144, UNS A97050, ISO AlZn6CuMgZr
• 7050 T76 Extruded Round Bar; WNR 3.4144, UNS A97050, ISO AlZn6CuMgZr
• 7050 T76 Extruded Flat Bar; WNR 3.4144, UNS A97050, ISO AlZn6CuMgZr
• 7050 T76 Extruded Tube; WNR 3.4144, UNS A97050, ISO AlZn6CuMgZr
• 7050 T76 Extruded Wire; WNR 3.4144, UNS A97050, ISO AlZn6CuMgZr
Choosing Factors for 7050 T76
- Strength: Excellent
- Machining: Okay
- Weldability: Low
- Formability: Medium
- Corrosion Resistance: Very good
- Heat Treating: Yes
Some Well-Known Applications for 7050 T76
As fasteners in airplanes and aircrafts,
In the automotive sector,
Also used in the nuclear industry.
7050 T76 is produced/supplied in plate/sheet round/flat bar and tube/profile forms.
- Rod / Round Bar / Flat Bar
- Plate
- Sheet
- Tube/Profile




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