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7050
AMS 4201 / AlZn6CuMgZr / 7050 / T7651
| Chemical Properties | % Value |
| Silicon (Si) | 0,00 - 0,12 |
| Tin (Sn) | 0,00 - 0,00 |
| Chromium (Cr) | 0,00 - 0,04 |
| Manganese (Mn) | 0,00 - 0,10 |
| Magnesium (Mg) | 1,90 - 2,60 |
| Copper (Cu) | 2,00 - 2,60 |
| Lead (Pb) | 0,00 - 0,00 |
| Titanium (Ti) | 0,08 - 0,21 |
| Iron (Fe) | 0,00 - 0,15 |
| Zinc (Zn) | 5,70 - 6,70 |
| Nickel (Ni) | 0,00 - 0,00 |
| Aluminium (Al) | Balance |
| Titanium + Zirconium (Ti+Zr) | 0,08 - 0,15 |
| 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 | 500 MPa |
| Yield Strength | 552 MPa |
| Shear Strength | 324 MPa |
| Elongation A50 mm | 10 % |
| Hardness | 147 HB |
| 7050 T7651 Temperature – Ultimate Tensile Strength Graph |
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| 7050 T7651 Thickness – Ultimate Tensile Strength Graph |
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| 7050 T7651 Diameter – Ultimate Tensile Strength Graph |
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7050 T7651 aluminum alloy belongs to the Al-Zn-Mg-Cu based 7000 series and is developed for applications requiring very high strength, enhanced toughness, and superior resistance to stress corrosion cracking (SCC). The T7651 temper includes solution heat treatment, stress relieving, and a more advanced level of overaging. Compared to T7451, it provides higher SCC resistance while resulting in a slight reduction in strength, making it especially suitable for critical aerospace applications.
In terms of corrosion resistance, 7050 T7651 is one of the most SCC-resistant tempers within the 7000 series. Its stress corrosion cracking resistance is higher than both 7075-T6 and even T7451. However, its general corrosion resistance is lower than that of 6000 series alloys. In marine and aggressive environments, protective coatings are strongly recommended.
Regarding strength and mechanical properties, 7050 T7651 offers very high strength, although slightly lower than T6 or T7451 tempers. In return, toughness and resistance to crack propagation are significantly improved. Compared to 2024 alloy, it provides much higher strength and better damage tolerance. It is especially suitable for thick-section components and critical structural parts.
In terms of machinability, bendability, and weldability, 7050 T7651 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 carried out before heat treatment. Similar to other 7050/7075 alloys, it is mainly used in machined and forged 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, aircraft wing and fuselage components, military structures, and critical safety components. 7050 T7651 is preferred especially in applications where maximum crack resistance and reliability are required.
• 7050 T7651 Plate; EN 3983, WNR 3.4144, UNS A97050, ISO AlZn6CuMgZr, AMS 4201
• 7050 T7651 Extruded Rod; WNR 3.4144, UNS A97050, ISO AlZn6CuMgZr
• 7050 T7651 Extruded Bar; WNR 3.4144, UNS A97050, ISO AlZn6CuMgZr
• 7050 T7651 Extruded Wire; WNR 3.4144, UNS A97050, ISO AlZn6CuMgZr
• 7050 T7651 Extruded Tube; WNR 3.4144, UNS A97050, ISO AlZn6CuMgZr
Selection Criteria for 7050 T7651
- Strength: Very Good
- Machinability: Suitable
- Weldability: Poor
- Formability: Moderate
- Corrosion Resistance: Excellent
- Heat Treatable: Yes
Common Applications for 7050 T7651
In commercial and military aircraft,
Aircraft wings and fuselage structures,
Aircraft and ship bulkheads.
Supply Forms
7050 T7651 is produced and supplied in plate/sheet, rod/bar, and tube/profile forms.
- Rod / Round Rod / Bar
- Plate
- Sheet
- Tube / Profile
| Mechanical Properties | |||
| Thickness (mm) | Proof Strength (Min.) | Yield Strength (Min.) | Elongation A50 mm % |
| Over 6.3 up to & incl. 51 | 441 MPa | 510 MPa | 9 |
| Over 51 up to & incl. 76 | 434 MPa | 503 MPa | 8 |
| Over 76 up to & incl. 102 | 427 MPa | 496 MPa | 6 |
| Over 102 up to & incl. 127 | 421 MPa | 490 MPa | 5 |
| Over 127 up to & incl. 152 | 414 MPa | 483 MPa | 4 |
| Over 152 up to & incl. 178 | 407 MPa | 476 MPa | 4 |
| Over 178 up to & incl. 203 | 400 MPa | 469 MPa | 4 |



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