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  • 7075 Aluminum Sheet Sample Pack, Unpolished (Mill) Finish, T6 Temper, ASTM B209/AMS QQ-A 250-12/AMS 4045, Varying Thicknesses, 4" Width, 4" Length (Pack of 6)
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7075 Aluminum Sheet Sample Pack, Unpolished (Mill) Finish, T6 Temper, ASTM B209/AMS QQ-A 250-12/AMS 4045, Varying Thicknesses, 4" Width, 4" Length (Pack of 6)


Price: $13.81 & FREE Shipping on orders over $35. Details
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Specifications for this item
Brand Name Small Parts
Part Number 13003
Item Shape Sheet
Material Type Aluminum
Exterior Finish Unpolished (Mill)
Grade 7075
Temper T6
System of Measurement Inch
Thickness 0.08  inches
Thickness Tolerance +/-0.0015  inches
Overall Width 4  inches
Width Tolerance +0.125/-0  inches
Overall Length 4  inches
Length Tolerance +0.125/-0  inches
Specification Met ASTM B209 , AMS QQ-A 250-12 , AMS 4045
Indentation Hardness 150  Brinell
LowerTemperature Range -320  Degrees Fahrenheit
Material Composition Solid
Number of Items 6
Tensile Strength Max 83000  PSI
UNSPSC Code 30000000
Upper Temperature Range 212  Degrees Fahrenheit

The six 7075 aluminum sheets with T6 temper have an unpolished (mill) surfa... Read full product description



Product Features

  • 7075 aluminum is an aircraft alloy that provides high strength and hardness and offers good machinability
  • Meets ASTM B209, AMS-QQ-A-250-12, and AMS-4045 specifications
  • Unpolished (mill) surface has no finish
  • Heat treated for increased strength

Product Details


Frequently Bought Together

7075 Aluminum Sheet Sample Pack, Unpolished (Mill) Finish, T6 Temper, ASTM B209/AMS QQ-A 250-12/AMS 4045, Varying Thicknesses, 4" Width, 4" Length (Pack of 6) + 2024 Aluminum Sheet Sample Pack, Unpolished (Mill) Finish, T3 Temper, AMS QQ-A-250/4/ASTM B209/AMS 4037, Varying Thicknesses, 4" Width, 4" Length (Pack of 6) + 6061 Aluminum Sheet Sample Pack, Unpolished (Mill) Finish, T6 Temper, AMS QQ-A-250/11/ASTM B209, Varying Thicknesses,  4" Width, 4" Length (Pack of 6)
Price for all three: $37.57

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Product Description

The six 7075 aluminum sheets with T6 temper have an unpolished (mill) surface and meet American Society for Testing and Materials International ASTM B209, and SAE Aerospace Material Specifications AMS-QQ-A-250-12 and AMS-4045 standards. The pack contains one each of the following thicknesses: 0.032", 0.04", 0.05", 0.063", 0.071", and 0.08". The 7075 aluminum alloy provides high strength and hardness and offers good machinability. The material, also known as an aircraft alloy, is heat treatable. It has a T6 temper, meaning it has been heat treated for increased strength.

Aluminum and aluminum alloys are lightweight compared to steel, brass, and copper, and have high strength-to-weight ratios. They offer good corrosion resistance and conductivity of heat and electricity, as well as moderate formability and machinability. Aluminum alloys include elements that modify the aluminum to achieve specific properties such as better weldability or greater strength. All series of aluminum alloys are nonmagnetic. Aluminum alloys have temper designations, indicating that the material has undergone a process to achieve certain properties of strength and hardness.

Tensile strength, used to indicate the material’s overall strength, is the peak stress it can withstand before it breaks. Corrosion resistance describes the material's ability to prevent deterioration caused by atmosphere, moisture, or other medium. Wear resistance indicates the ability to prevent surface damage caused by contact with other surfaces. Toughness describes the material's ability to absorb energy before breaking, while hardness (commonly measured as indentation hardness) describes its resistance to permanent surface deformation. Formability indicates how easily the material can be permanently shaped. Machinability describes how easily it can be cut, shaped, finished, or otherwise machined, while weldability characterizes the ability to be welded.

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