AS9100D ISO 9001:2015

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AS9100D ISO 9001:2015

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Sheet

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  • AMS 4907

    AMS 4907
    Revision: “-M” issued 08/2020
    Alloy: 6AL-4V Eli
    Product Forms: Titanium Alloy, Sheet, Strip, and Plate
    Condition: Annealed

    Composition Analysis
    Aluminum: 5.5 – 6.5%Nitrogen (Maximum): 0.05%
    Vanadium: 3.5 – 4.5%Hydrogen (Maximum): 0.0125%
    Iron (Maximum): 0.25%Other Elements (Each): .10%
    Oxygen (Maximum): 0.13%Other Elements (Total): .40%
    Carbon (Maximum): 0.08%Titanium: Balance
    Yttrium (Maximum): .005%
    Tensile Properties (Minimums)*
    Tensile: 125 – 130 ksiElongation: 6 – 10%
    Yield: 115 – 120 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)
    • 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 4907 specification.

    To purchase AMS 4907M, please visit: https://www.sae.org/standards/content/ams4907m/

    Changes may be made to the information contained herein.

  • AMS 4918

    AMS 4918
    Revision: “P” issued 08/2018
    Alloy: 6AL-6V-2SN
    Product Forms: Titanium Alloy, Sheet, Strip, and Plate
    Condition: Annealed

    Composition Analysis
    Aluminum: 5.0 – 6.0%Carbon (Maximum): 0.05%
    Vanadium: 5.0 – 6.0%Nitrogen (Maximum): 0.04%
    Tin: 1.5 – 2.5%Hydrogen (Maximum): 0.015%
    Iron: 0.35 – 1.0%Yttrium (Maximum): 0.005%
    Copper: 0.35 – 1.0%Other Elements (Total): 0.40%
    Oxygen (Maximum): 0.20%Titanium: Balance
    Tensile Properties (Minimums)*
    Tensile: 145-155 ksiElongation: 6 – 10%
    Yield: 135-170 ksi

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

    Required Acceptance Tests

    • Tensile Properties
    • Microstructure
    • Surface Contamination
    • Chemical Composition
    • Bend Test (where required)
    • Ultrasonic (where required)
    • Fracture toughness (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 4918 specification.

    To purchase AMS 4918P, please visit: https://www.sae.org/standards/content/ams4918p/

    Changes may be made to the information contained herein.

  • AMS-T-9046 AB-1 6AL-4V

    AMS-T-9046
    Revision: “A” issued 07/2002 ***Obsolete, S/S by AMS 4911***
    Alloy: 6AL-4V “AB-1”
    Product Forms: Titanium and Titanium Alloy, Sheet, Strip, and Plate
    Condition: Annealed

    Please note, the AMS-T-9046 specification covers various Alloys and Conditions. This Spec Sheet is only for the Alloy and Condition listed above.

    Composition Analysis
    Aluminum: 5.5 – 6.75Nitrogen (Maximum): 0.05%
    Vanadium: 3.5 – 4.5%Hydrogen (Maximum): 0.0125%
    Iron (Maximum): 0.30%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 – 134 ksiElongation: 8 – 10%
    Yield: 120 – 126 ksi

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

    Required Acceptance Tests

    • Chemical Composition
    • Microstructure
    • Ultrasonic (where required)
    • Tensile Properties
    • Bend Test (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-T-9046 specification.

    To purchase AMS-T-9046A, please visit: https://www.sae.org/standards/content/amst9046a/

    Changes may be made to the information contained herein.

  • AMS-T-9046 AB-2 6AL-4V ELI

    AMS-T-9046
    Revision: “A” issued 07/2002 ***Obsolete, S/S by AMS 4907***
    Alloy: 6AL-4V “AB-2”
    Product Forms: Titanium and Titanium Alloy, Sheet, Strip, and Plate
    Condition: Annealed

    Please note, the AMS-T-9046 specification covers various Alloys and Conditions. This Spec Sheet is only for the Alloy and Condition listed above.

    Composition Analysis
    Aluminum: 5.5 – 6.5%Nitrogen (Maximum): 0.05%
    Vanadium: 3.5 – 4.5%Hydrogen (Maximum): 0.0125%
    Iron (Maximum): 0.25%Other Elements (Total): 0.30%
    Oxygen (Maximum): 0.13%Titanium: Balance
    Carbon (Maximum): 0.08%
    Tensile Properties (Minimums)*
    Tensile: 125 – 130 ksiElongation: 6 – 10%
    Yield: 115 – 120 ksi

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

    Required Acceptance Tests

    • Chemical Composition
    • Microstructure
    • Ultrasonic (where required)
    • Tensile Properties
    • Bend Test (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-T-9046 specification.

    To purchase AMS-T-9046A, please visit: https://www.sae.org/standards/content/amst9046a/

    Changes may be made to the information contained herein.

  • AMS-T-9046 AB-3 6AL-6V-2Sn

    AMS-T-9046
    Revision: “A” issued 07/2002 ***Obsolete, S/S by AMS 4918***
    Alloy: 6AL-6V-2Sn “AB-3”
    Product Forms: Titanium and Titanium Alloy, Sheet, Strip, and Plate
    Condition: Annealed

    Please note, the AMS-T-9046 specification covers various Alloys and Conditions. This Spec Sheet is only for the Alloy and Condition listed above.

    Composition Analysis
    Aluminum: 5-6%Carbon (Maximum): 0.05%
    Vanadium: 5-6%Nitrogen (Maximum): 0.04%
    Tin: 1.5-2.5%Hydrogen (Maximum): 0.015%
    Iron (Maximum): 0.35-1.0%Yttrium (Maximum): 0.005%
    Oxygen (Maximum): 0.20%Other Elements (Total): 0.30%
    Copper: 0.35-1.0%Titanium: Balance
    Tensile Properties (Minimums)*
    Tensile: 145-155 ksiElongation: 6 – 10%
    Yield: 135-170 ksi

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

    Required Acceptance Tests

    • Chemical Composition
    • Microstructure
    • Ultrasonic (where required)
    • Tensile Properties
    • Bend Test (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-T-9046 specification.

    To purchase AMS-T-9046B, please visit: https://www.sae.org/standards/content/amst9046b/

    Changes may be made to the information contained herein.

  • AMS-T-9046 CP-1 GRADE 4

    AMS-T-9046
    Revision: “A” issued 07/2002 ***Obsolete, S/S by AMS 4901***
    Grade: Commercially Pure Grade 4 (CP-1, 70 ksi min yield)
    Product Forms: Titanium and Titanium Alloy, Sheet, Strip, and Plate
    Condition: Annealed

    Please note, the AMS-T-9046 specification covers various Alloys and Conditions. This Spec Sheet is only for the Alloy and Condition listed above.

    Composition Analysis
    Carbon (Maximum): 0.08%Hydrogen (Maximum): 0.015%
    Nitrogen (Maximum): 0.05%Other Elements (Total): 0.30%
    Iron (Maximum): 0.50%Titanium: Balance
    Oxygen (Maximum): 0.40%
    Tensile Properties (Minimums)*
    Tensile: 80 ksi MinElongation: 15% Min
    Yield: 70 – 95 ksi

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

    Required Acceptance Tests

    • Chemical Composition
    • Microstructure
    • Ultrasonic (where required)
    • Tensile Properties
    • Bend Test (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-T-9046 specification.

    To purchase AMS-T-9046A, please visit: https://www.sae.org/standards/content/amst9046a/

    Changes may be made to the information contained herein.

  • AMS-T-9046 CP-3 Grade 2

    AMS-T-9046
    Revision: “A” issued 07/2002 ***Obsolete, S/S by AMS 4902***
    Grade: Commercially Pure Grade 2 (CP-3, 40 ksi min yield)
    Product Forms: Titanium and Titanium Alloy, Sheet, Strip, and Plate
    Condition: Annealed

    Please note, the AMS-T-9046 specification covers various Alloys and Conditions. This Spec Sheet is only for the Alloy and Condition listed above.

    Composition Analysis
    Carbon (Maximum): 0.08%Hydrogen (Maximum): 0.015%
    Nitrogen (Maximum): 0.05%Other Elements (Total): 0.30%
    Iron (Maximum): 0.30%Titanium: Balance
    Oxygen (Maximum): 0.20%
    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
    • Microstructure
    • Ultrasonic (where required)
    • Tensile Properties
    • Bend Test (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-T-9046 specification.

    To purchase AMS-T-9046A, please visit: https://www.sae.org/standards/content/amst9046a/

    Changes may be made to the information contained herein.

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