AS9100D ISO 9001:2015

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  • 6AL-4V Titanium

    Alternate Names: Grade 5 Titanium, 6-4 Titanium

    Description: 6AL-4V is the most common alloy of Titanium. As an alloyed Grade of Titanium, it is strengthened by the inclusion of roughly 6% Aluminum and 4% Vanadium. It is known as an alpha-beta Titanium alloy, containing both alpha and beta phases at room temperature. 6AL-4V typically comes in the Annealed condition, but it can be strengthened by heat treatment, such as Solution Treating and Aging. 6AL-4V offers good weldability. Overall, 6AL-4V exhibits high strength, light weight, and corrosion resistance, which make it an excellent choice for applications in aerospace, medical, oil and gas, marine, and recreational industries.

    Machinability: The American Iron and Steel Institute (AISI) determined a rating system of machinability of different materials. 160 Brinell B1112 steel was arbitrarily assigned a machinability rating of 100%. Using this as a comparable standard, ratings less than 100% are more challenging to machine, and ratings more than 100% are easier to machine. Titanium 6AL-4V is rated at 22% of B1112. Low cutting speeds, heavy feed rates, sharp tools, and ample cutting fluid are prescribed.

    6AL-4V Titanium is available in the following Product Forms:

    Round Bar (Rod), Rectangular Flat Bar (Block), Plate, and Sheet.

    6AL-4V Titanium is available in the following Specifications:

    AMS 4911AMS 4928AMS 4965
    AMS 4967AMS 6930AMS 6931
    AMS-T-9046 (AB-1 6AL4V)AMS-T-9047 (6AL-4V)MIL-T-9046 (AB-1 6AL-4V)
    MIL-T-9047 (6AL-4V)ASTM B348 (Grade 5)ASTM B265 (Grade 5)
    ASTM F1472DMS 1592DMS 1570
    Don’t see what you want? Call us at 888-772-8984 for a Quote on 6AL-4V Titanium, or Email us at Sales@performancetitanium.com!

    The use of this information is strictly voluntary and should be used as a guideline only. This data contains generalizations and is in no way a substitute for your own research. This information is not intended as a warranty or fitness of any application. Should you require further information about Titanium 6AL-4V Grade 5, please contact us and we will gladly refer you to additional sources.

  • MIL-T-9047 6AL-4V

    MIL-T-9047
    Revision: “G, Amendment 2” issued 09/1986 ***Obsolete, S/S by AMS-T-9047***
    Alloy: 6AL-4V
    Product Forms: Titanium and Titanium Alloy Bars (Rolled or Forged) and
    Reforging Stock, Aircraft Quality
    Condition: Annealed

    Please note, the MIL-T-9047 specification covers various Alloys and Conditions. This Spec Sheet is only for the Alloy and Condition listed above.

    Composition Analysis
    Aluminum: 5.5 – 6.75%Nitrogen (Maximum): 0.05%
    Vanadium: 3.5 – 4.5%Hydrogen (Maximum): 0.015%
    Iron (Maximum): 0.30%Yttrium (Maximum): 0.005%
    Oxygen (Maximum): 0.20%Other Elements (Total): 0.40%
    Carbon (Maximum): 0.08%Titanium: Balance
    Tensile Properties (Minimums)*
    Tensile: 130 ksiElongation: 8 – 10%
    Yield: 120 ksiReduction of Area: 15 – 25%

    *Tensile property requirements vary based on orientation, section thickness/diameter, and cognizant engineering organization requirements.

    Required Acceptance Tests

    • Chemical Composition
    • Microstructure
    • Macrostructure
    • Ultrasonic (where required)
    • Tensile Properties

    Disclaimer
    The use of this information is strictly voluntary. Information may contain typographical errors, and should be used as a guideline only. This Material Spec Sheet contains generalizations and is in no way a substitution for the MIL-T-9047 specification.

    To download MIL-T-9047G, please visit: https://assist.dla.mil/online/start/

    Changes may be made to the information contained herein.

  • ASTM B348 6AL-4V Grade 5

    ASTM B348 Grade 5
    Revision: “-21” issued 2021
    Alloy: 6AL-4V (Grade 5)
    Product Forms: Titanium and Titanium Alloy Bars and Billets


    Please note, the ASTM B348 specification covers various Alloys. This Spec Sheet is only for the Alloy listed above.

    Composition Analysis
    Aluminum: 5.5 – 6.75%Nitrogen (Maximum): 0.05%
    Vanadium: 3.5 – 4.5%Hydrogen (Maximum): 0.0125%
    Iron (Maximum): 0.40%Other Elements (Maximum, Each): 0.10%
    Oxygen (Maximum): 0.20%Other Elements (Total): 0.40%
    Carbon (Maximum): 0.08%Titanium: Balance
    Tensile Properties (Minimums)*
    Tensile: 130 ksiElongation: 10%
    Yield: 120 ksiReduction of Area: 25%

    *Tensile property requirements vary based on orientation, section thickness/diameter, and cognizant engineering organization requirements.

    Required Acceptance Tests

    • Chemical Composition
    • Tensile Properties

    Disclaimer
    The use of this information is strictly voluntary. Information may contain typographical errors, and should be used as a guideline only. This Material Spec Sheet contains generalizations and is in no way a substitution for the ASTM B348 specification.

    To purchase ASTM B348, please visit: http://www.astm.org/Standards/B348.htm

    Changes may be made to the information contained herein.

  • AMS 4928

    AMS 4928
    Revision: “X” issued 10/2025
    Alloy: 6AL-4V
    Product Forms: Titanium Alloy Bars, Wire, Forgings, Rings, and Drawn Shapes
    Condition: Annealed

    Composition Analysis
    Aluminum: 5.5 – 6.75%Nitrogen (Maximum): 0.05%
    Vanadium: 3.5 – 4.5%Hydrogen (Maximum): 0.0125%
    Iron (Maximum): 0.30%Yttrium (Maximum): 0.005%
    Oxygen (Maximum): 0.20%Other Elements (Total): 0.40%
    Carbon (Maximum): 0.08%Titanium: Balance
    Tensile Properties (Minimums)*
    Tensile: 130 – 135 ksiElongation: 8 – 10%
    Yield: 119 – 125 ksiReduction of Area: 15 – 25%

    *Tensile property requirements vary based on orientation, section thickness/diameter, and cognizant engineering organization requirements.

    Required Acceptance Tests

    • Chemical Composition
    • Tensile Properties
    • Microstructure
    • Surface Contamination

    Disclaimer
    The use of this information is strictly voluntary. Information may contain typographical errors, and should be used as a guideline only. This Material Spec Sheet contains generalizations and is in no way a substitution for the AMS 4928 specification.

    To purchase AMS 4928X, please visit: https://www.sae.org/standards/content/ams4928x/

    Changes may be made to the information contained herein.

  • AMS 6931

    AMS 6931
    Revision: “D” issued 12/2017
    Alloy: 6AL-4V
    Product Forms: Titanium Alloy Bars, Forgings, and Forging Stock
    Condition: Annealed

    Composition Analysis
    Aluminum: 5.5 – 6.75%Nitrogen (Maximum): 0.05%
    Vanadium: 3.5 – 4.5%Hydrogen (Maximum): 0.0125%
    Iron (Maximum): 0.30%Yttrium (Maximum): 0.005%
    Oxygen (Maximum): 0.20%Other Elements (Total): 0.40%
    Carbon (Maximum): 0.08%Titanium: Balance
    Tensile Properties (Minimums)*
    Tensile: 130 ksiElongation: 8 – 10%
    Yield: 119-120 ksiReduction of Area: 15 – 25%

    *Tensile property requirements vary based on orientation, section thickness/diameter, and cognizant engineering organization requirements.

    Required Acceptance Tests

    • Chemical Composition
    • Tensile Properties
    • Microstructure
    • Surface Contamination
    • Macrostructure
    • Ultrasonic (where required)

    Disclaimer
    The use of this information is strictly voluntary. Information may contain typographical errors, and should be used as a guideline only. This Material Spec Sheet contains generalizations and is in no way a substitution for the AMS 6931 specification.

    To purchase AMS 6931D, please visit: https://www.sae.org/standards/content/ams6931d/

    Changes may be made to the information contained herein.

  • AMS-T-9047 6AL-4V

    AMS-T-9047
    Revision: “N/A” issued 05/2003 ***Obsolete, S/S by AMS 6931***
    Alloy: 6AL-4V
    Product Forms: Titanium and Titanium Alloy Bars (Rolled or Forged) and
    Reforging Stock, Aircraft Quality
    Condition: Annealed

    Please note, the AMS-T-9047 specification covers various Alloys and Conditions. This Spec Sheet is only for the Alloy and Condition listed above.

    Composition Analysis
    Aluminum: 5.5 – 6.75%Nitrogen (Maximum): 0.05%
    Vanadium: 3.5 – 4.5%Hydrogen (Maximum): 0.015%
    Iron (Maximum): 0.30%Yttrium (Maximum): 0.005%
    Oxygen (Maximum): 0.20%Other Elements (Total): 0.40%
    Carbon (Maximum): 0.08%Titanium: Balance
    Tensile Properties (Minimums)*
    Tensile: 130 ksiElongation: 8 – 10%
    Yield: 120 ksiReduction of Area: 15 – 25%

    *Tensile property requirements vary based on orientation, section thickness/diameter, and cognizant engineering organization requirements.

    Required Acceptance Tests

    • Chemical Composition
    • Microstructure
    • Macrostructure
    • Ultrasonic (where required)
    • Tensile Properties

    Disclaimer
    The use of this information is strictly voluntary. Information may contain typographical errors, and should be used as a guideline only. This Material Spec Sheet contains generalizations and is in no way a substitution for the AMS-T-9047 specification.

    To purchase AMS-T-9047, please visit: https://www.sae.org/standards/content/amst9047/

    Changes may be made to the information contained herein.

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