
EN AW-7075 (AlZn5.5MgCu) is the "super-strength" grade of the aluminum world. Primarily used in aerospace and high-end engineering, it provides a strength profile comparable to many steels while remaining lightweight.
The mechanical performance of 7075 is entirely dependent on its temper (heat treatment).
Choosing the right temper is critical for the success of your fabrication process.
| Temper | State | Best Used For... | Characteristics |
| 7075-O | Annealed | Cold Forming / Deep Drawing | The softest state. High ductility allows for complex bending, but it has very low strength until heat-treated. |
| 7075-T6 | Artificially Aged | Maximum Strength | Peak hardness and tensile strength. However, it can harbor internal stresses from the quenching process. |
| 7075-T651 | Stress Relieved | Precision Machining | The standard for plates. The material is stretched after quenching to "reset" internal stresses, preventing warping during CNC milling. |
7075 is specifically engineered for high-stress environments where weight must be minimized.
Tensile Strength ($R_m$): 540 600 MPa
Yield Strength ($R_{p0.2}$): 480 540 MPa
Hardness (Brinell): 150 HBW
Modulus of Elasticity: 71 GPa
Fatigue Strength: Excellent, though sensitive to surface notches.
Fuselage & Wing Skins: High tensile loads require the extreme strength of 7075.
Alclad Versions: Since 7075 has poor corrosion resistance (due to Zinc and Copper), sheets are often "Clad" with a thin layer of pure aluminum to provide a sacrificial barrier against oxidation.
Tooling & Mold Making: Used for high-pressure injection molds and vacuum forming tools due to its high thermal conductivity and ability to hold a mirror finish.
Structural Bulkheads: Heavy-duty load-bearing parts in aircraft and high-performance automotive chassis.
Gears and Shafts: Often used for high-speed rotating parts where low inertia is required.
While 7075 is exceptionally strong, it comes with specific limitations:
ð« Welding: 7075 is generally not weldable. Fusion welding creates severe brittle zones and micro-cracking. Mechanical fastening (rivets/bolts) is the industry standard for this alloy.
ï Corrosion: It is highly susceptible to Stress Corrosion Cracking (SCC) and exfoliation. If the part will be exposed to marine or industrial environments, it must be anodized or primed/painted.
ðï Formability: In the T6/T651 state, 7075 is very brittle. If you try to bend it at a tight radius, it will likely crack. If heavy forming is required, use 7075-O and then heat-treat to T6 afterward.
| Standard | Designation |
| EN (EU) | EN AW-7075 / EN AW-AlZn5.5MgCu |
| Werkstoff Nr. | 3.4365 |
| UNS (USA) | A97075 |
| ISO | Al Zn5.5 Mg Cu |
| Aeronautical | LN 9073, AMS 4544, QQ-A-225/9 |
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