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3003 Alloy Aluminum

Aluminum Mill Product Specifications

Available Forms:
Sheet and Plate ASTM-B209, FEDERAL-QQ-A-250/2, ASME-SB209
Wire, Rod and Bar, Rolled or Cold Finished ASTM-B211, FEDERAL-QQ-A-225/2
Wire, Rod, Bar, Tube, Extruded ASTM-B221
Tube, Extruded, Seamless ASTM-B241
Tube, Extruded, Coiled ASTM-B491
Tube, Drawn ASTM-B483
Tube, Drawn, Seamless ASTM-B210, FEDERAL-WW-T-700/2, ASME-4065
Tube, Welded ASTM-B313
Pipe ASTM-B241, MILITARY-MIL-P-25995, ASME-SB241


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5052 Alloy Aluminum

The following specifications cover Aluminum 5052

  • ASTM B209
  • ASTM B211
  • QQ-A-250/8
  • QQ-Q-225/7
  • ASME SB209

    5052 is the alloy most suited to forming operations, with good workability and higher strength than that of the 1100 or 3003 alloys that are commercially available.

    5052 is not heat-treatable, but is stronger than most of the 5xxx series of alloys. It has very good corrosion resistance, and can be easily welded. 5052 is not a good choice for extensive machining operations, as it has only a fair machinability rating.

    5052-H32 Aluminum

    Minimum Properties:
    Ultimate Tensile Strength: 33,000 psi
    Yield Strength: 28,000 psi
    Brinell Hardness: 60

    Chemistry:
    Aluminum (Al): 95.7–97.7 %
    Chromium (Cr): 0.15–0.35 %
    Copper (Cu): 0.1 % max.
    Iron (Fe): 0.4 % max.
    Magnesium (Mg): 2.2–2.8 %
    Manganese (Mn): 0.1 % max.
    Silicon (Si): 0.25 % max.

    Aluminum Mill Product Specifications

    Available Forms:
    Sheet and Plate ASTM-B209, FEDERAL-QQ-A-250/8, ASME-SB209
    Wire, Rod and Bar, Rolled or Cold Finished ASTM-B211, FEDERAL QQ-Q-225/7

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    5083 Marine Grade Aluminum Alloy

    The following specifications cover Aluminum 5083

  • AMS 4057 (Sheet)
  • AMS 4058 (Sheet)
  • ASTM B928
  • ASTM B209
  • ASTM B210
  • ASTM B221
  • ASTM B241 (Pipe- Seamless)
  • ASTM B247 (Forging - Open Die)
  • ASTM B345 (Pipe- Seamless)
  • ASTM B361
  • ASTM B547
  • ASTM B548 (Plate)
  • DIN 3.3547
  • MIL A-45225
  • MIL A-46027
  • MIL A-46083
  • MIL G-S-24149/2
  • QQ A-200/4
  • QQ A-367 (Forging - Open Die)
  • QQ A250/6
  • SAE J454
  • UNS A95083


  • Chemistry Data:

    Aluminum: Balance
    Chromium: 0.05–0.25
    Copper: 0.1 max.
    Iron: 0.4 max.
    Magnesium: 4–4.9
    Manganese: 0.4–1
    Remainder Each: 0.05 max.
    Remainder Total: 0.15 max.
    Silicon: 0.4 max.
    Titanium: 0.15 max.
    Zinc: 0.25 max.

    Principal Design Features
    This is a non-heat treatable alloy for strengthening. It has very good corrosion resistance, is easily welded and does have good strength.

    Applications
    Commonly used in the manufacture of unfired, welded pressure vessels, marine, auto aircraft cryogenics, drilling rigs, TV towers, transportation equipment, and in missile components.

    Machinability
    No specific data. However the alloy is machinable by conventional means.

    Forming
    Forming characteristics are good for either hot or cold working.

    Welding
    Weldability of this alloy is very good by conventional means. When filler rod is required it should be the same alloy, 5083.

    Heat Treatment
    This is a non-heat treatable alloy.

    Forging
    Forging may be done in the range of 850 to 750 °F.

    Hot Working
    Hot forming, when sever deformation is required, may be done at 400 °F or higher to 700 °F.

    Cold Working
    AL 5083 is readily cold worked by conventional methods. In the annealed (O temper) condition plate of 0.250" thick can be bent on 1.5 T radius.

    Annealing
    Annealing may be done at 650 F for sufficient time for thorough heating, followed by air cooling.

    Aging
    Not applicable to this alloy.

    Tempering
    Not applicable.

    Hardening
    Hardening is accomplished by means of cold working only.

    Other Physical Props
    Electrical conductivity 28 % of copper.

    Other Mechanical Props
    Shear strength in O temper is 25 ksi.


    Physical Data
    Density: 0.096 lb/cu. in.
    Specific Gravity: 2.66
    Melting Point: 1070 Deg F
    Poissons Ratio: 0.33
    Modulus of Elasticity Tension: 10.3
    Modulus of Elasticity Torsion: 3.8

    Aluminum Mill Product Specifications

    Available Forms:
    Sheet and Plate ASTM-B928 , FEDERAL-QQ-A-250/6 , ASME-SB209
    Wire, Rod, Bar,Shapes, Tube, Extruded ASTM-B221 , FEDERAL-QQ-A-200/4 , ASME-SB221
    Tube, Extruded, Seamless ASTM-B241 , FEDERAL-QQ-A-250/6, ASME-SB241
    Tube, Drawn, Seamless ASTM-B210


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    5086 Marine Grade Aluminum Alloy

    The following specifications cover Aluminum 5086

  • ASTM B928
  • ASTM B209
  • ASTM B210
  • ASTM B221
  • ASTM B241 (Pipe- Seamless)
  • ASTM B313
  • ASTM B345 (Pipe- Seamless)
  • ASTM B361
  • ASTM B547
  • ASTM B548 (Plate)
  • MIL C-26094
  • MIL S-24149/2
  • QQ A-200/5
  • QQ A-250/7
  • QQ WW-T-700/5
  • SAE J454
  • UNS A95086

    Property Results

    Chemistry Data :
    Aluminum : Balance
    Chromium : 0.05 - 0.25
    Copper : 0.1 max
    Iron : 0.5 max
    Magnesium : 3.5 - 4.5
    Manganese : 0.2 - 0.7
    Remainder Each : 0.05 max
    Remainder Total : 0.15 max
    Silicon : 0.4 max
    Titanium : 0.15 max
    Zinc : 0.25 max

    Principal Design Features
    This is a high strength structural alloy. It is not heat treatable.

    Applications
    Commonly used in the manufacture of unfired, welded pressure vessels, marine, auto aircraft cryogenics, drilling rigs, tanks, TV towers, transportation equipment, and in missile components.

    Machinability
    Machinability in the strain hardened tempers (H34, H36, H38) is relatively good. In the annealed (O temper) machining is difficult, but still can be accomplished. Use of lubricants is advised.

    Forming
    Forming characteristics are best with the alloy in the O temper -- less good in the H36 or H38 tempers.

    Welding
    This alloy is readily weldable by conventional methods. Use of electric arc welding in particular produces excellent results.

    Heat Treatment
    The alloy is non-heat treatable.

    Forging
    No specific data as to hot working range. However the alloy is forgeable.

    Hot Working
    No data in regard to hot forming. Cold forming characteristics are excellent and usually would not necessitate hot working.

    Cold Working
    Excellent cold working characteristics in the O temper and somewhat less good in H36 and H38 tempers.

    Annealing
    Anneal at 650 F for long enough to insure thorough heating. Air cool.

    Aging
    Not applicable to this alloy.

    Tempering
    Not applicable.

    Hardening
    Hardens by cold working only.

    Other Physical Props
    Electrical conductivity 30% of copper.

    Other Mechanical Props
    Shear strength for O temper is 23 ksi, for H34 it is 27 ksi

    Physical Data :
    Density (lb / cu. in.) : 0.096
    Specific Gravity : 2.66
    Melting Point (Deg F) : 1090
    Modulus of Elasticity Tension : 10.3

    Mechanical Data :
    Form : Sheet
    Condition : H112
    Temperature : 68
    Tensile Strength : 39
    Yield Strength : 19
    Elongation : 14

    Form : Sheet
    Condition : H116
    Temperature : 68
    Tensile Strength : 42
    Yield Strength : 30
    Elongation : 12

    Form : Sheet
    Condition : H32
    Temperature : 68
    Tensile Strength : 42
    Yield Strength : 30
    Elongation : 12

    Form : Sheet
    Condition : H34
    Temperature : 68
    Tensile Strength : 47
    Yield Strength : 37
    Elongation : 10

    Aluminum Mill Product Specifications

    Available Forms:
    Sheet and Plate ASTM-B928 , FEDERAL-QQ-A-250/7 , ASME-SB209
    Wire, Rod, Bar, Shapes Tube, Extruded ASTM-B221 , ASME-SB221-QQ-A-200/5
    Tube, Extruded, Seamless ASTM-B241 , ASME-SB241-QQ-A-200/5
    Pipe, Tube, Drawn, Seamless ASTM-B210 , FEDERAL-WW-T-700/5
    Tube, Welded ASTM-B313

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    6061 Structural Marine Grade Alloy Aluminum

    The following specifications cover Aluminum 6061

    6061 Aluminum is, by most any measure, the most commonly used aluminum alloy. It is specified in most any application due to its strength, heat treatability, comparatively easy machining, and weldability. If that were not enough, it is also capable of being anodized, adding a layer of protection for finished parts.
    The main alloy ingredients of 6061 aluminum are magnesium and silicon.

    6061-T6 & 6061-T6511 Aluminum

    Physical and Mechanical Properties
    Ultimate Tensile Strength, psi : 45,000
    Yield Strength, psi : 40,000
    Brinell Hardness : 95
    Rockwell Hardness : B60

    •AMS 4117•ASTM B209•ASTM B210•ASTM B211•ASTM B221•ASTM B234•ASTM B241 (Pipe- Seamless)• ASTM B247 (Forging - Open Die)•ASTM B307•ASTM B313• ASTM B316• ASTM B345 (Pipe- Seamless)• ASTM B361• ASTM B404• ASTM B429• ASTM B483• ASTM B547• ASTM B548 (Plate)• ASTM B632 (Plate)•ASTM F467 (Nuts)• ASTM F468 (Nuts)• DIN 3.3211• MIL A-12545• MIL A-22771• MIL F-17132A (Tread Plate)• MIL F-18280• MIL F-39000• MIL F-3922• MIL G-18014• MIL G-18015• MIL P-25995• MIL T-7081• MIL W-23351• MIL W-85• QQ A-200/16• QQ A-200/8 (Extruded Shapes)• QQ A-225/8• QQ A-250/11• QQ A-367 (Forging - Open Die)• QQ A-430• QQ WW-T-700/6• SAE J454

    Chemistry Data :
    Aluminum : Balance
    Chromium : 0.04 - 0.35
    Copper : 0.15 - 0.4
    Iron : 0 - 0.7
    Magnesium : 0.8 - 1.2
    Manganese : 0.15 max
    Other : 0.15 max
    Remainder Each : 0.05 max
    Silicon : 0.4 - 0.8
    Titanium : 0.15 max
    Zinc : 0.25 max

    Principal Design Features
    Probably the most commonly available, heat treatable aluminum alloy.

    Applications
    Commonly used in the manufacture of heavy-duty structures requiring good corrosion resistance, truck and marine components, railroad cars, furniture, tank fittings, general structural and high pressure applications, wire products, and in pipelines.

    Machinability
    Machinability in the harder T 4 and T6 tempers is good. It is notably less easy to machine in the annealed temper.

    Forming
    Easily cold worked and formed in the annealed condition. Stamping, bending, spinning, deep drawing are all readily accomplished using standard methods.

    Welding
    The alloy has very good welding characteristics and may be welded by all of the common welding techniques. Gas tungsten arc welding is generally used for thin sections (less than 0.032") and gas metal arc welding is used for heavier sections. Use alloy 4043 filler wire for best results, although a decrease in T 6 properties will result.

    Heat Treatment
    Solution heat treat at 990 F for adequate time to allow for thorough heating and then water quench. Precipitation hardening is done at 320 F for 18 hours and air cool, followed by 350 F for 8 hours and air cooling.

    Forging
    The alloy is capable of being hot forged at temperatures in the range of 900 F to 750 F.

    Hot Working
    Hot working may be done in the temperature range of 700 F to 500 F.

    Cold Working
    Cold working in the O temper condition is readily performed. The alloy is notably less easy to cold form in the T 4 and T 6 tempers.

    Annealing
    Annealing should be done at 775 F for 2 to 3 hours followed by controlled cooling at 50 f per hour down to 500 F, then air cool.

    Aging
    The aging precipitation heat treatment is done at 350 F for 8 hours followed by air cooling. This produces the T6 temper.

    Tempering
    Not applicable.

    Hardening
    See "Aging".

    Other Physical Props
    Electrical conductivity 40% of copper.

    Physical Data
    Density (lb / cu. in.) : 0.098
    Specific Gravity : 2.7
    Melting Point (Deg F) : 1090
    Modulus of Elasticity Tension : 10
    Modulus of Elasticity Torsion : 3.8

    Aluminum Mill Product Specifications

    Available Forms:
    Sheet and Plate ASTM-B209 , FEDERAL-QQ-A-250/11 , ASME-SB209
    Tread Plate MIL-F-17132
    Wire, Rod and Bar, Rolled or Cold Finished ASTM-B211 , FEDERAL-QQ-A-225/8, ASME-SB211
    Wire, Rod, Bar, Profiles (Shapes) and Tube, Extruded ASTM-B221, QQ-A-200/8
    Structural Profiles (Shapes) ASTM-B308, ASME-SM308, QQ-A-200/8
    Tube, Extruded, Seamless ASTM-B241, ASME-SB241
    Pipe, Tube, Drawn, Seamless ASTM-B210, FEDERAL-WW-T-700/6, ASME-SB210
    Pipe ASTM-B241 , MILITARY-MIL-P-25995, ASME-SB241
    Structural Pipe and Tube, Extruded


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    6063 Alloy Aluminum

    The following specifications cover Aluminum 6063

    6063 is often called architectural aluminum for two reasons - first, it has a surface finish that is far smoother than the other commercially available alloys, and second, its strength is significantly less (roughly half the strength of 6061), making it suited for applications where strength is not the foremost consideration.
    6063 is rated as "Good" for forming and cold working operations, "Excellent" for anodizing, and "Fair" for machining.

    6063-T5 & 6063-T52 Aluminum

    Minimum Properties
    Ultimate Tensile Strength, psi : 27,000
    Yield Strength, psi : 21,000
    Brinell Hardness : 60

    Chemistry
    Aluminum (Al) : 97.5% max
    Chromium (Cr) : 0.1% max
    Copper (Cu) : 0.1% max
    Iron (Fe) : 0.35% max
    Magnesium (Mg) : 0.45 - 0.90%
    Manganese (Mn) : 0.1% max
    Silicon (Si) : 0.2 - 0.6%

    Specifications
  • ASTM B210
  • ASTM B221
  • ASTM B241 (Pipe- Seamless)
  • ASTM B345 (Pipe)
  • ASTM B429
  • MIL P-25995
  • QQ A-200/9

    Chemistry Data
    Aluminum : Balance
    Chromium : 0.1 max
    Copper : 0.1 max
    Iron : 0.35 max
    Magnesium : 0.45 - 0.9
    Manganese : 0.1 max
    Remainder Each : 0.05 max
    Remainder Total : 0.15 max
    Silicon : 0.2 - 0.6
    Titanium : 0.1 max
    Zinc : 0.1 max

    Principal Design Features
    This is generally considered to be an extrusion alloy that is heat treatable for strengthening.

    Applications
    Commonly used in the manufacture of furniture, windows, stair rails, and in pipe railing. Commonly used in architectural extrusions.

    Machinability
    Machinability is considered to be average for this alloy.

    Forming
    Forming ability, either hot or cold, is good.

    Welding
    The alloy is readily welded by all of the conventional methods. Filler rod should be of the same alloy or AL 4043 alloy.

    Heat Treatment
    Solution heat treat at 970 F for 1 hour followed by water quench. This produces T 4 temper. Other tempers are accomplished by aging.

    Forging
    Hot forging may be done in the range of 500 F to 950 F.

    Hot Working
    Hot working, as with forging, may be done at temperatures above 500 F up to maximum of 950 F.

    Cold Working
    Cold working characteristics are good for all conventional forming methods.

    Annealing
    Anneal at 775 F for 3 hours and use controlled cooling at rate of 50 F per hour down to 500 F. Then air cool.

    Aging
    Aging is done at a temperature of 350 F for 8 hours for T 6 and T 62 tempers. Age at 360 F for 3 hours to get T5 temper.

    Tempering
    Not applicable.

    Hardening
    Hardens due to aging heat treatment and cold working. See "Aging".

    Other Physical Props
    Electrical conductivity 50% of copper.

    Other Mechanical Props
    Shear strength for various tempers is: O temper 10, ksi . T 5 temper 17 ksi. T 83 temper 22 ksi

    Physical Data :
    Density (lb / cu. in.) : 0.097
    Specific Gravity : 2.7
    Melting Point (Deg F) : 1150
    Modulus of Elasticity Tension : 10
    Modulus of Elasticity Torsion : 3

    Aluminum Mill Product Specifications

    Available Forms:
    Wire, Rod, Bar, Profiles (Shapes), And Tube ASTM-B221 , ASME-SB221, QQ-A-200/9
    Tube, Extruded, Seamless ASTM-B241 , ASME-SB241
    Tube, Drawn, Seamless ASTM-B210 , ASME-SB210
    Pipe ASTM-B241 , MILITARY-MIL-P-25995, ASME-SB241
    Structural Pipe and Tube, Extruded B429

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