2017 Aluminum Sheet and Plate
Grade: 2017
Coil: 0.3mm-3.0mm
Sheet: 0.3mm-300mm
Width: 50mm-2000mm
Standard: ASTM, AMS, BS etc.
- Fast Shipping / Ready Stock
- ISO 9001 Factory
- Custom Cutting
- 100% MTC & SGS Inspection
2017 is a heat treatable wrought aluminum copper magnesium silicon alloy traditionally associated with naturally aged high strength components. It offers useful fatigue performance and good machining behavior in T4 and stress relieved T451 conditions. Annealing improves formability but reduces strength. Corrosion resistance is lower than that of commercially pure aluminum, so protective finishes may be required. Sheet and plate procurement needs a product specific specification; widely cited ASTM and AMS references for this grade often cover bars, rods or wire instead.
Chemical composition
| Element | Limit wt % | Element | Limit wt % |
| Al | Balance | Si | 0.20–0.80 |
| Fe | 0.70 max | Cu | 3.50–4.50 |
| Mn | 0.40–1.00 | Mg | 0.40–0.80 |
| Cr | 0.10 max | Zn | 0.25 max |
| Ti | 0.15 max | Other each | 0.05 max |
| Other total | 0.15 max |
Mechanical properties by temper
| Temper | Thickness mm or basis | Rm MPa | Rp0.2 MPa | Elongation % |
| O | General wrought reference | 180 typical | 70 typical | Not assigned |
| T4 | General wrought reference | 425 typical | 275 typical | Not assigned |
| T451 | General wrought reference | 425 typical | 275 typical | Not assigned |
Application areas
- High strength machined engineering components
- Aircraft and mechanically fastened structural components
- Machine construction and military equipment
- Fasteners and rivets from appropriate nonplate product forms


2017 is a heat treatable wrought aluminum copper magnesium silicon alloy traditionally associated with naturally aged high strength components. It offers useful fatigue performance and good machining behavior in T4 and stress relieved T451 conditions. Annealing improves formability but reduces strength. Corrosion resistance is lower than that of commercially pure aluminum, so protective finishes may be required. Sheet and plate procurement needs a product specific specification; widely cited ASTM and AMS references for this grade often cover bars, rods or wire instead.
Chemical composition
| Element | Limit wt % | Element | Limit wt % |
| Al | Balance | Si | 0.20–0.80 |
| Fe | 0.70 max | Cu | 3.50–4.50 |
| Mn | 0.40–1.00 | Mg | 0.40–0.80 |
| Cr | 0.10 max | Zn | 0.25 max |
| Ti | 0.15 max | Other each | 0.05 max |
| Other total | 0.15 max |
Mechanical properties by temper
| Temper | Thickness mm or basis | Rm MPa | Rp0.2 MPa | Elongation % |
| O | General wrought reference | 180 typical | 70 typical | Not assigned |
| T4 | General wrought reference | 425 typical | 275 typical | Not assigned |
| T451 | General wrought reference | 425 typical | 275 typical | Not assigned |
Application areas
- High strength machined engineering components
- Aircraft and mechanically fastened structural components
- Machine construction and military equipment
- Fasteners and rivets from appropriate nonplate product forms
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