​2024-T3511 aluminum is a high-strength alloy renowned for its excellent strength-to-weight ratio and fatigue resistance. The T3511 temper indicates that the material has been solution heat-treated, stress-relieved by stretching, and then straightened to meet standard tolerances. This process enhances its mechanical properties, making it ideal for aerospace applications such as aircraft structures, wing skins, and fuselage frames. While it offers good machinability, 2024-T3511 is more susceptible to corrosion compared to other aluminum alloys, necessitating appropriate protective measures
MTR MTR Available
USA U.S.A. Made
Return Non-returnable
DFARS DFARS Compliant
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Product Information

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Please note:

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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.
Legs
1.75" x 1.75"
Thickness
0.094
Inside Radius
0.25
Alloy
2024
Temper
T3511
Production Method
Extruded
Metal Type
Aluminum
Shape
Angle
Ships
1-3 Business Days
Brand
Aircraft Extrusion Co
Weight/Lineal Foot
0.3987 pounds
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Mechanical Properties

Density g/cm^3
3
Ultimate Tensile Strength KSI
67
Yield Tensile Strength KSI
46
Rockwell Hardness B Scale
75
Brinell Hardness 500 kg load
120
Melting Point °F
935 - 1180
Elongation % in 2 in.
9
Shear Strength KSI
49
Machinability %
70
Electrical Conductivity % IACS
30
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Chemistry Information : 2024 Aluminum

Element
Percentage
Element
Percentage
Element
Percentage
Al
93.5
Cr
0.1  max
Cu
3.8 - 4.9
Mg
1.2 - 1.8
Fe
0.5  max
Mn
0.3 - 0.9
Si
0.5  max
Zn
0.25  max
Ti
0.15  max
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