AS9100D ISO 9001:2015

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AS9100D ISO 9001:2015

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  • CP GRADE 2

    Alternate Names: CP Grade 2 Titanium, CP 2, Grade 2, CP 40

    Description: Commercially Pure (CP) Grade 2 Titanium is one of the most common grades of unalloyed titanium. CP Titanium mechanical properties are controlled by chemistry; specifically the input of Nitrogen, Oxygen and Iron which will increase strength of material. CP Grade 2 is higher in strength than CP Grade 1, but lower than CP Grades 3 and 4. It is also commonly called “CP 40” which is in reference to its approximate yield strength. It is an attractive grade of titanium due to its excellent corrosion resistance, good formability, and limited strength. It is used in a variety of industries such as chemical, marine, medical, recreational, and aerospace.

    Machinability: Low cutting speeds, heavy feed rates, sharp tools, and ample cutting fluid are prescribed.

    CP Grade 2 Titanium is available in the following Product Forms:
    Round Bar (Rod), Plate, and Sheet

    CP Grade 2 Titanium is available in the following Specifications:

    AMS 4902ASTM F67 (Grade 2)
    ASTM B348 (Grade 2)AMS-T-9046 (CP-3 Grade 2)
    ASTM B265 (Grade 2)MIL-T-9046 (CP-3 Grade 2)
    Don’t see what you want? Call us at 888-772-8984 for a Quote on CP Grade 2 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 CP Grade 2, please contact us and we will gladly refer you to additional sources.

  • ASTM B265 GRADE 4

    ASTM B265 Grade 4
    Revision: “-25” issued 2025
    Grade: Commercially Pure Grade 4
    Product Forms: Titanium and Titanium Alloy Strip, Sheet, and Plate
    Condition: Annealed

    Please note, the ASTM B265 specification covers various Alloys. This Spec Sheet is only for the Grade listed above.

    Composition Analysis
    Iron (Maximum): 0.50%Hydrogen (Maximum): 0.015%
    Oxygen (Maximum): 0.40%Other Elements (Maximum, Each): 0.10%
    Carbon (Maximum): 0.08%Other Elements (Total): 0.40%
    Nitrogen (Maximum): 0.05%Titanium: Balance
    Tensile Properties (Minimums)*
    Tensile: 80 ksiElongation: 15%
    Yield: 70 – 95 ksi

    *Tensile property requirements vary based on orientation, section thickness, 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 B265 specification.

    To purchase ASTM B265-25, please visit: http://www.astm.org/Standards/B265.htm

    Changes may be made to the information contained herein.

  • ASTM B265 6AL-4V Grade 5

    ASTM B265 Grade 5
    Revision: “-25” issued 2025
    Alloy: 6AL-4V (Grade 5)
    Product Forms: Titanium and Titanium Alloy Strip, Sheet, and Plate
    Condition: Annealed

    Please note, the ASTM B265 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): 0.015%
    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 ksi

    *Tensile property requirements vary based on orientation, section thickness, 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 B265 specification.

    To purchase ASTM B265-25, please visit: http://www.astm.org/Standards/B265.htm

    Changes may be made to the information contained herein.

  • ASTM B265 GRADE 2

    ASTM B265 Grade 2
    Revision: “-25” issued 2025
    Grade: Commercially Pure Grade 2
    Product Forms: Titanium and Titanium Alloy Strip, Sheet, and Plate
    Condition: Annealed

    Please note, the ASTM B265 specification covers various Alloys. This Spec Sheet is only for the Grade listed above.

    Composition Analysis
    Iron (Maximum): 0.30%Hydrogen (Maximum): 0.015%
    Oxygen (Maximum): 0.25%Other Elements (Maximum, Each): 0.10%
    Carbon (Maximum): 0.08%Other Elements (Total): 0.40%
    Nitrogen (Maximum): 0.03%Titanium: Balance
    Tensile Properties (Minimums)*
    Tensile: 50 ksiElongation: 20%
    Yield: 40 – 65 ksi

    *Tensile property requirements vary based on orientation, section thickness, 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 B265 specification.

    To purchase ASTM B265-25, please visit: http://www.astm.org/Standards/B265.htm

    Changes may be made to the information contained herein.

  • ASTM B265 6AL-4V ELI Grade 23

    ASTM B265 Grade 23
    Revision: “-25” issued 2025
    Alloy: 6AL-4V Eli (Grade 23)
    Product Forms: Titanium and Titanium Alloy Strip, Sheet, and Plate
    Condition: Annealed

    Please note, the ASTM B265 specification covers various Alloys. This Spec Sheet is only for the Alloy listed above.

    Composition Analysis
    Aluminum: 5.5 – 6.5%Nitrogen (Maximum): 0.03%
    Vanadium: 3.5 – 4.5%Hydrogen (Maximum): 0.0125%
    Iron (Maximum): 0.25%Other Elements (Maximum, Each): 0.10%
    Oxygen (Maximum): 0.13%Other Elements (Total): 0.40%
    Carbon (Maximum): 0.08%Titanium: Balance
    Tensile Properties (Minimums)*
    Tensile: 120 ksiElongation: 10%
    Yield: 110 ksi

    *Tensile property requirements vary based on orientation, section thickness, 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 B265 specification.

    To purchase ASTM B265-25, please visit: http://www.astm.org/Standards/B265.htm

    Changes may be made to the information contained herein.

  • ASTM F1472

    ASTM F1472
    Revision: “-20a” issued 2020
    Alloy: 6AL-4V (UNS R56400)
    Product Forms: Wrought Titanium-6Aluminum-4Vanadium Alloy for Surgical
    Implant Applications (Bars, Forgings, Sheet, Strip, Plate)

    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%Titanium: Balance
    Carbon (Maximum): 0.08%
    Tensile Properties (Minimums)*
    Tensile: 130 – 135 ksiElongation: 8 – 10%
    Yield: 120 – 126 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 ASTM F1472 specification.

    To purchase ASTM F1472-20a, please visit: http://www.astm.org/Standards/F1472.htm

    Changes may be made to the information contained herein.

  • AMS 4911

    AMS 4911
    Revision: “T” issued 11/2025
    Alloy: 6AL-4V
    Product Forms: Titanium Alloy, Sheet, Strip, and Plate
    Condition: Annealed

    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 – 134 ksiElongation: 6 – 10%
    Yield: 120 – 126 ksi

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

    Required Acceptance Tests

    • Chemical Composition
    • Tensile Properties
    • Bend Test
    • Microstructure
    • Surface Contamination
    • 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 4911 specification.

    To purchase AMS 4911T, please visit: https://www.sae.org/standards/content/ams4911T/

    Changes may be made to the information contained herein.

  • AMS 4902

    AMS 4902
    Revision: “M” issued 03/2023
    Grade: Commercially Pure Grade 2 (40 ksi min yield)
    Product Forms: Titanium Sheet, Strip, and Plate
    Condition: Annealed

    Composition Analysis
    Carbon (Maximum): 0.08%Hydrogen (Maximum): 0.015%
    Nitrogen (Maximum): 0.05%Other Elements (Each): 0.10%
    Iron (Maximum): 0.30%Other Elements (Total): 0.30%
    Oxygen (Maximum): 0.20%Titanium: Balance
    Tensile Properties (Minimums)*
    Tensile: 50 ksi MinElongation: 20% Min
    Yield: 40 – 65 ksi

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

    Required Acceptance Tests

    • Chemical Composition
    • Tensile Properties
    • Bend Test (where required)
    • Grain Size
    • 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 4902 specification.

    To purchase AMS 4902M, please visit: https://www.sae.org/standards/content/ams4902m/

    Changes may be made to the information contained herein.

  • ASTM F67 CP GRADE 4

    ASTM F67 Grade 4
    Revision: “-24” issued 2024
    Grade: Commercially Pure Grade 4
    Product Forms: Unalloyed Titanium, for Surgical Implant Applications (Strip,
    Sheet, Plate, Bar, Billet, Forging, and Wire)

    Please note, the ASTM F67 specification covers various Grades. This Spec Sheet is only for the Grade listed above.

    Composition Analysis
    Iron (Maximum): 0.50%Hydrogen (Maximum): 0.0125%
    Oxygen (Maximum): 0.40%Nitrogen (Maximum): 0.05%
    Carbon (Maximum): 0.08%Titanium: Balance
    Tensile Properties (Minimums)*
    Tensile: 80 ksiElongation: 15%
    Yield: 70 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
    • 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 ASTM F67 specification.

    To purchase ASTM F67, please visit: http://www.astm.org/Standards/F67

    Changes may be made to the information contained herein.

  • ASTM F67 GRADE 2

    ASTM F67 Grade 2
    Revision: “-24” issued 2024
    Grade: Commercially Pure Grade 2
    Product Forms: Unalloyed Titanium, for Surgical Implant Applications (Strip,
    Sheet, Plate, Bar, Billet, Forging, and Wire)

    Please note, the ASTM F67 specification covers various Grades. This Spec Sheet is only for the Grade listed above.

    Composition Analysis
    Iron (Maximum): 0.30%Hydrogen (Maximum): 0.0125%
    Oxygen (Maximum): 0.25%Nitrogen (Maximum): 0.03%
    Carbon (Maximum): 0.08%Titanium: Balance
    Tensile Properties (Minimums)*
    Tensile: 50 ksiElongation: 20%
    Yield: 40 ksiReduction of Area: 30%

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

    Required Acceptance Tests

    • Chemical Composition
    • Tensile Properties
    • 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 ASTM F67 specification.

    To purchase ASTM F67, please visit: http://www.astm.org/Standards/F67

    Changes may be made to the information contained herein.

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