Product Details, Specifications, and Technical Information

See Aluminum Tolerances

Aluminum Sheet 7075-T6 has high strength, light weight, good fatigue resistance, good corrosion resistance, and average machinability. 7075, one of the strongest aluminum alloys, was specifically designed for aircraft frames and offers strength slightly superior to steel while maintaining the light weight of aluminum. It is typically used in aerospace, high-end automotive, and defense applications.

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Dimension Name Specification
Thickness 0.09
Max Width 48
Max Length 144
Alloy 7075
Temper T6
Covering Pvc 1 Side
MTR Availability Yes
Full Length true
Material Aluminum
Shape Sheet/Plate
Custom Cut Warehouse 1
Material Specifications

This material meets the following specs: ASTM -B209, AMS -4045, AMS -QQ-A-250/12

Weight/Lineal Foot
1.33 pounds
Please note that this data is to be used ONLY FOR REFERENCE, NOT FOR DESIGN, and by using it,you agree that any decisions you make regarding materials for your project are at your own discretion.
Mechanical Properties
Property Value
Density g/cm^3 3
Ultimate Tensile Strength KSI 76
Yield Tensile Strength KSI 67
Brinell Hardness 500 kg load 150
Rockwell Hardness B Scale 87
Elongation % in 2 in. 11
Machinability % 70
Shear Strength KSI 46
Melting Point °F 890 - 1180
Electrical Conductivity % IACS 33
Density g/cm^3 3
Ultimate Tensile Strength KSI 83
Yield Tensile Strength KSI 73
Rockwell Hardness B Scale 87
Brinell Hardness 500 kg load 150
Melting Point °F 890 - 1180
Elongation % in 2 in. 11
Shear Strength KSI 48
Machinability % 70
Electrical Conductivity % IACS 33
Chemistry Information: 7075 Aluminum
Element Percentage
Al 90
Cr 0.18 - 0.28
Cu 1.2 - 2
Fe 0.5 max
Mg 2.1 - 2.9
Mn 0.3 max
Si 0.4 max
Ti 0.2 max
Zn 5.1 - 6.1
Zr+Ti 0.25 max
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