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7178
AMS QQ-A-200/14 / AlZn7MgCu / 7178 / T76
| Chemical Properties | % Value |
| Silicon (Si) | 0,00 - 0,40 |
| Chromium (Cr) | 0,18 - 0,28 |
| Manganese (Mn) | 0,00 - 0,30 |
| Magnesium (Mg) | 2,40 - 3,10 |
| Copper (Cu) | 1,60 - 2,40 |
| Titanium (Ti) | 0,00 - 0,20 |
| Iron (Fe) | 0,00 - 0,50 |
| Zinc (Zn) | 6,30 - 7,30 |
| Aluminium (Al) | Balance |
| Physical Properties | Value |
| Density | 2,83 g/cm³ |
| Melting Point | 477 °C |
| Thermal Expansion | 23.5 µm/m.°C |
| Modulus of Elasticity | 71.0 GPa |
| Thermal Conductivity | 130 W/m.K |
| Electrical Resistivity | 31 % IACS |
| Mechanical Properties | Value |
| Proof Strength | 510 MPa |
| Yield Strength | 575 MPa |
| Shear Strength | 340 MPa |
| Elongation A50 mm | 8% |
| Hardness | 152 HB |
| 7178 T76 Temperature – Ultimate Tensile Strength Graph |
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| 7178 T76 Thickness – Ultimate Tensile Strength Graph |
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| 7178 T76 Diameter – Ultimate Tensile Strength Graph |
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| 7178 T76 Diameter-Yield Tensile Strength |
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7178-T76 aluminum alloy is a very high-strength wrought aluminum alloy belonging to the 7xxx series Al-Zn-Mg-Cu group. This alloy was developed for applications requiring high mechanical strength, fatigue resistance, and structural performance. The T76 temper is a special aging treatment that maintains high strength while improving resistance to stress corrosion cracking (SCC). For this reason, 7178-T76 is widely preferred in aerospace and defense industries for heavily loaded structural components.
One of the most significant characteristics of this alloy is its high tensile and yield strength. 7178-T76 generally provides higher strength than the 7075 alloy and in some applications can show performance similar to the 7050 alloy. However, its corrosion resistance, improved by the T76 temper, is better than standard 7178 tempers and usually better than 2024 alloy, but slightly lower than medium-strength alloys such as 6061. Therefore, anodizing or protective coatings are commonly applied to improve surface protection.
In terms of machinability, the 7178-T76 alloy performs well and can be processed efficiently in CNC machining operations. However, due to its high strength, cutting forces are relatively high. Bendability and formability are limited, especially in the T76 temper, and therefore machining processes are generally preferred over cold forming. Weldability is generally considered poor, so structural parts are usually joined using riveting or mechanical fastening methods.
The 7178-T76 alloy also demonstrates good resistance to vibration and fatigue loading. This property increases the reliability of the material in environments where high dynamic loads occur. Aircraft wing structures, landing gear components, military aircraft parts, and high-performance structural components are among the most common application areas of this alloy. It is particularly preferred in designs requiring a high strength-to-weight ratio.
Overall, when 7178-T76 is compared with alloys such as 7075, 7050, and 2024, it offers extremely high strength but more limited formability. Nevertheless, when used with appropriate surface treatments and engineering design, it provides a highly reliable material solution, particularly in aerospace, defense, and high-performance engineering applications.
7178 T76 can be supplied according to the following standards:
• 7178 T76 Sheet; AMS QQ-A-250/21 (enhanced pitting corrosion resistance), AMS QQ-A-250/14, ASTM B209, UNS A97178, ISO AlZn7MgCu
• 7178 T76 Plate; AMS QQ-A-250/21 (enhanced pitting corrosion resistance), AMS QQ-A-250/14, ASTM B209, UNS A97178, ISO AlZn7MgCu
• 7178 T76 Extruded Round Bar; AMS QQ-A-200/13, AMS QQ-A-200/14 (enhanced pitting corrosion resistance), ASTM B221, UNS A97178, ISO AlZn7MgCu
• 7178 T76 Extruded Bar; AMS QQ-A-200/13, AMS QQ-A-200/14 (enhanced pitting corrosion resistance), ASTM B221, UNS A97178, ISO AlZn7MgCu
• 7178 T76 Extruded Wire; AMS QQ-A-200/13, AMS QQ-A-200/14 (enhanced pitting corrosion resistance), ASTM B221, UNS A97178, ISO AlZn7MgCu
• 7178 T76 Extruded Tube; AMS QQ-A-200/13, AMS QQ-A-200/14 (enhanced pitting corrosion resistance), ASTM B221, UNS A97178, ISO AlZn7MgCu
Selection Factors for 7178 T76
- Durability: Excellent
- Machinability: Poor
- Weldability: Medium
- Formability: Good
- Corrosion Resistance: Medium
- Heat Treatment: Yes
Some Known Applications of 7178 T76
In the construction sector, in roofing systems,
Mainly in the aerospace industry,
Used in aircraft structures and wing spars.
7178 T76 is produced/supplied in round/plate rods and tube/profile forms.
- Sheet
- Tube/Profile
- Round/Plate Rod
- Plate




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