7075 is a heat-treatable aluminum-zinc-magnesium-copper alloy known for high strength. It is used where strength-to-weight performance is more important than easy forming, welding or decorative finishing. Typical sectors include aerospace, precision equipment, performance machinery, tooling and highly loaded components.
Published September 30, 2026 · 2 min read
7075 is a heat-treatable aluminum-zinc-magnesium-copper alloy known for high strength. It is used where strength-to-weight performance is more important than easy forming, welding or decorative finishing. Typical sectors include aerospace, precision equipment, performance machinery, tooling and highly loaded components.
The principal reason to specify 7075 is mechanical performance. In suitable tempers it can provide substantially higher strength than common 6xxx-series alloys. This can support lighter components or higher loads, but the complete design must also consider fatigue, fracture behavior, corrosion environment, joining and inspection.
7075 is widely machined for precision parts. Stable stock condition, appropriate workholding, sharp tooling, chip control and a planned machining sequence help manage distortion and surface quality. Thin walls, deep pockets and heavy material removal may require stress-relieved material or staged machining.
7075 should not be treated as a routine substitute for 6061 or 6063 extrusion. High-strength 7xxx alloys are more demanding to process, and available shapes, section complexity, minimum quantities and lead times may be limited. A supplier must confirm billet, tooling, press capability, heat treatment and inspection before quotation.
Environmental exposure and galvanic contact should be reviewed carefully. Welding can significantly affect properties and is generally not the default joining method for highly loaded 7075 components. Mechanical fastening or other engineered joints may be more appropriate. Anodizing and protective coating requirements should be specified with cosmetic and dimensional expectations.
Finished-part drawing and 3D model
Required temper and mechanical properties
Material form: plate, bar, forging or special extrusion
Critical dimensions and inspection requirements
Machining, surface treatment and corrosion environment
Prototype, production and annual quantities
Chengdacai will confirm whether 7075 is appropriate and available for the requested manufacturing route. Alternative 6xxx alloys should be considered when extrusion complexity, welding or decorative appearance is the primary requirement.
Send your drawing, application, mechanical requirements, finish, tolerances and quantity. Alloy availability and manufacturing feasibility are confirmed during quotation.
Upload Drawing and Request a Quote Download the Aluminum Extrusion RFQ Checklist (PDF)
Yes. Alloy, temper, material form and manufacturing feasibility are confirmed during drawing review and quotation.
Substitution should only occur after mechanical, corrosion, forming, finishing and dimensional requirements have been reviewed.
Provide drawings, material and temper, critical tolerances, finish, application, quantity and required documentation. Technical references: The Aluminum Association and applicable ASTM/EN material specifications. Final requirements must be confirmed on the project drawing.
Composition, temper options, mechanical properties and selection notes for each grade discussed above.
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