Mechanically, 7075 T7351 is quite impressive. Its tensile strength typically ranges between 500–560 MPa, while the yield strength is approximately 435 MPa. These values make it much stronger than most standard aluminum alloys, making it ideal for structural components requiring high strength. Additionally, the T7351 temper increases the material's fatigue resistance and fracture toughness; therefore, it is commonly used in aircraft fuselage parts, helicopter rotors, and high-performance vehicle chassis components.

Regarding machinability, 7075 T7351 has moderate workability. Machining processes require care because its high strength demands proper cutting tools and lower cutting speeds. The alloy is sensitive to welding, with a high risk of cracking during welding; therefore, mechanical fasteners or special brazing techniques are usually preferred over welding. Nevertheless, forging, milling, drilling, and surface treatments can be successfully performed with T7351.

In terms of corrosion resistance, 7075 T7351 may perform lower than some aluminum alloys due to its high zinc content. However, the T7351 temper allows a natural passive layer to form on the surface, and additional surface treatments like anodizing can significantly enhance corrosion resistance. These properties make it suitable for use in environments with harsh conditions, such as maritime and aerospace industries. Overall, 7075 T7351 stands out as an ideal alloy for engineering applications requiring high strength and durability.