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6061 T6 Aluminum I Beam 5.0000 X 3.0000 X 0.21000 " Extruded American Standard
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6061 T6 Aluminum I Beam 5.0000 X 3.0000 X 0.21000 " Extruded American Standard
Part Number:
ALI00012
Material:
Aluminum
Alloy:
6061
Shape:
I Beam
Temper:
T6
Mfg Method:
Extruded American Standard
Weight:
3.43 lb/ft
Height:
5"
Thickness:
0.21"
Width:
3"
Specification/Revision:
ASTM B 221|SAE AMS-QQ-A-200/8
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Product Properties
Chemical
This table contains the chemical composition limits of wrought aluminum alloys in percent by weight maximum unless shown as a range or minimum. Except for “aluminum” and “others, ” analysis normally is made for elements for which specific limits are shown. For purposes of determining conformance to these limits, an observed value or a calculated value obtained from analysis is rounded off to the nearest unit in the last right-hand place of figures used in expressing the specified limit, in accordance with ASTM Recommended Practice E29.
(1) Includes listed elements for which no specific limit is shown.
(2) A .0008 weight percent maximum beryllium is applicable to any alloy to be used as welding electrode or welding rod.
(3) The sum of those “others” metallic elements 0.010 percent or more each, expressed to the second decimal before determining the sum.
(4) The aluminum content for unalloyed aluminum not made by a refining process is the difference between 100.00 percent and the sum of all other metallic elements present in amounts of 0.010 percent or more each, expressed to the second decimal before determining the sum.
(5) Beryllium 0.0008 maximum for welding electrode and welding rod only.
(6) Also contains 0.20 to 0.6 percent each of lead and bismuth.
(9) Boron 0.06 percent maximum.
(10) Also contains 0.40 to 0.7 percent each of lead and bismuth.
(12) Also contains 0.08 to 0.15 percent of zirconium.
Mechanical
The following typical properties are not guaranteed since in most cases they are averages for various sizes, product forms, and methods of manufacture and may not be exactly representative of any particular product or size. These data are intended only as a basis for comparing alloys and tempers and should not be specified as engineering requirements or used for design purposes. The indicated typical mechanical properties for all except 0 temper material are higher than the specified minimum properties. For 0 temper products, typical ultimate and yield values are slightly lower than specified (maximum) values.
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(1) Based on 500,000,000 cycles of completely reversed stress using the R.R. Moore type of machine and specimen.
(2) Average of tension and compression moduli. Compression modulus is about 2% greater than tension modulus.
Physical
The following typical properties are not guaranteed since in most cases they are averages for various sizes, product forms, and methods of manufacture and may not be exactly representative of any particular product or size. These data are intended only as a basis for comparing alloys and tempers and should not be specified as engineering requirements or used for design purposes.
Note: Use the arrows above to scroll left or right to show additional fields
Fabrication
Note: Use the arrows above to scroll left or right to show additional fields
- Ratings A through E are relative ratings in decreasing order of merit, based on exposures to sodium chloride solution by intermittent spraying or immersion. Alloys with A and B ratings can be used in industrial and seacoast atmospheres without protection. Alloys with C, D, and E ratings generally should be protected at least on faying surfaces
- Stress corrosion cracking ratings are based on service experience and on laboratory tests of specimens exposed to the 3.5% sodium chloride alternate immersion test and are expressed as follows:
- A = No known instance of failure in service or in laboratory tests.
- B = No known instance of failure in service; limited failures in laboratory tests of short transverse specimens.
- C = Service failures with sustained tension stress acting in short transverse direction relative to grain structure; limited failures in laboratory tests of long transverse specimens.
- D = limited service failures with sustained longitudinal or long transverse stress.
- This rating may be different for material held at elevated temperature for long periods
- Ratings A through D for Workability (cold), and A through E for Machinability, are relative ratings in decreasing order of merit.
- Ratings A through D for Weldability and Brazeability are relative ratings defined as follows:
- A = Generally weldable by all commercial procedures and methods.
- B = Weldable with special techniques or for specific applications which justify preliminary trials or testing to develop welding procedure and weld performance.
- C = Limited Weldability because of crack sensitivity or loss in resistance to corrosion and mechanical properties.
- D = No commonly used welding methods have been developed.
Aluminum Metal Values
Below you'll find today's price for Aluminum and see how it compares to the last month, last year, and last two years. To see more graphs like this for other materials, you can visit our Daily Metal Values page.
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Product Properties
Chemical
This table contains the chemical composition limits of wrought aluminum alloys in percent by weight maximum unless shown as a range or minimum. Except for “aluminum” and “others, ” analysis normally is made for elements for which specific limits are shown. For purposes of determining conformance to these limits, an observed value or a calculated value obtained from analysis is rounded off to the nearest unit in the last right-hand place of figures used in expressing the specified limit, in accordance with ASTM Recommended Practice E29.
(1) Includes listed elements for which no specific limit is shown.
(2) A .0008 weight percent maximum beryllium is applicable to any alloy to be used as welding electrode or welding rod.
(3) The sum of those “others” metallic elements 0.010 percent or more each, expressed to the second decimal before determining the sum.
(4) The aluminum content for unalloyed aluminum not made by a refining process is the difference between 100.00 percent and the sum of all other metallic elements present in amounts of 0.010 percent or more each, expressed to the second decimal before determining the sum.
(5) Beryllium 0.0008 maximum for welding electrode and welding rod only.
(6) Also contains 0.20 to 0.6 percent each of lead and bismuth.
(9) Boron 0.06 percent maximum.
(10) Also contains 0.40 to 0.7 percent each of lead and bismuth.
(12) Also contains 0.08 to 0.15 percent of zirconium.
Mechanical
The following typical properties are not guaranteed since in most cases they are averages for various sizes, product forms, and methods of manufacture and may not be exactly representative of any particular product or size. These data are intended only as a basis for comparing alloys and tempers and should not be specified as engineering requirements or used for design purposes. The indicated typical mechanical properties for all except 0 temper material are higher than the specified minimum properties. For 0 temper products, typical ultimate and yield values are slightly lower than specified (maximum) values.
Note: Use the arrows above to scroll left or right to show additional fields
(1) Based on 500,000,000 cycles of completely reversed stress using the R.R. Moore type of machine and specimen.
(2) Average of tension and compression moduli. Compression modulus is about 2% greater than tension modulus.
Physical
The following typical properties are not guaranteed since in most cases they are averages for various sizes, product forms, and methods of manufacture and may not be exactly representative of any particular product or size. These data are intended only as a basis for comparing alloys and tempers and should not be specified as engineering requirements or used for design purposes.
Note: Use the arrows above to scroll left or right to show additional fields
Fabrication
Note: Use the arrows above to scroll left or right to show additional fields
- Ratings A through E are relative ratings in decreasing order of merit, based on exposures to sodium chloride solution by intermittent spraying or immersion. Alloys with A and B ratings can be used in industrial and seacoast atmospheres without protection. Alloys with C, D, and E ratings generally should be protected at least on faying surfaces
- Stress corrosion cracking ratings are based on service experience and on laboratory tests of specimens exposed to the 3.5% sodium chloride alternate immersion test and are expressed as follows:
- A = No known instance of failure in service or in laboratory tests.
- B = No known instance of failure in service; limited failures in laboratory tests of short transverse specimens.
- C = Service failures with sustained tension stress acting in short transverse direction relative to grain structure; limited failures in laboratory tests of long transverse specimens.
- D = limited service failures with sustained longitudinal or long transverse stress.
- This rating may be different for material held at elevated temperature for long periods
- Ratings A through D for Workability (cold), and A through E for Machinability, are relative ratings in decreasing order of merit.
- Ratings A through D for Weldability and Brazeability are relative ratings defined as follows:
- A = Generally weldable by all commercial procedures and methods.
- B = Weldable with special techniques or for specific applications which justify preliminary trials or testing to develop welding procedure and weld performance.
- C = Limited Weldability because of crack sensitivity or loss in resistance to corrosion and mechanical properties.
- D = No commonly used welding methods have been developed.
Aluminum Metal Values
Below you'll find today's price for Aluminum and see how it compares to the last month, last year, and last two years. To see more graphs like this for other materials, you can visit our Daily Metal Values page.
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