| Alloy 7075 |
| Principal Alloy |
Zinc |
| Characteristics |
Very high strength, heat treatable |
| Typical Application |
Aircraft applications |
| Common Forms |
Sheet, plate, rod, bar, |
|
| Alloy 7075 Alclad |
| Principal Alloy |
Zinc |
| Characteristics |
Clad with 2.5% to 5% pure aluminum on one or both sides for increased corrosion resistance with very good strength |
| Typical Application |
Exposed aircraft parts. Higher strength than 2024 Alclad. |
| Common Forms |
Sheet |
|