AS9100D ISO 9001:2015

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AS9100D ISO 9001:2015

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  • ASTM F136

    ASTM F136
    Revision: “-13” issued 2013
    Alloy: 6AL-4V Eli
    Product Forms: Titanium Alloy Strip, Sheet, Plate, Bar, Forging Bar, and Wire
    Condition: Annealed

    Composition Analysis
    Aluminum: 5.5 – 6.5%Carbon (Maximum): 0.08%
    Vanadium: 3.5 – 4.5%Nitrogen (Maximum): 0.05%
    Iron (Maximum): 0.25%Hydrogen (Maximum): 0.012%
    Oxygen (Maximum): 0.13%Titanium: Balance
    Tensile Properties (Minimums)*
    Tensile: 120 – 125 ksiElongation: 8 – 10%
    Yield: 110 – 115 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
    • Bend Testing (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 ASTM F136 specification.

    To purchase ASTM F136-13, please visit: http://www.astm.org/Standards/F136.htm

    Changes may be made to the information contained herein.

  • 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.

  • 6AL-4V ELI

    Alternate Names: Grade 23 Titanium, 6-4 Eli Titanium

    Description: 6AL-4V Eli is an alloyed Grade of Titanium. It is strengthened by the inclusion of roughly 6% Aluminum and 4% Vanadium. Titanium 6AL-4V Eli (Extra-Low Interstitial) is considered a higher purity than 6AL-4V Grade 5 due to its lower inclusions of Iron, and the interstitial elements, Carbon and Oxygen. 6AL-4V Eli typically comes in the annealed condition, but can be found in beta annealed condition as well. 6AL-4V Eli Grade 23 shows high strength and toughness, as well as good corrosion resistance. It is found in aerospace applications where fracture toughness and fatigue strength are important. As a biocompatible Grade of Titanium, it is also known for its applications in medical and dental 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 Eli is rated at 22% of B1112. Low cutting speeds, heavy feed rates, sharp tools, and ample cutting fluid are prescribed.

    6AL-4V Eli Titanium  is available in the following Product Forms:
    Round Bar (Rod), Rectangular Flat Bar (Block), Plate, and Sheet.

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

    AMS 4907ASTM B265 (Grade 23)AMS-T-9046 (AB-2 6AL-4V ELI)
    AMS 4930ASTM B348 (Grade 23)AMS-T-9047 (6AL-4V ELI)
    AMS 6932ASTM F136MIL-T-9046 (AB-2 6AL-4V ELI)
    MIL-T-9047 (6AL-4V ELI)
    Don’t see what you want? Call us at 888-772-8984 for a Quote on 6AL-4V Eli Grade 23 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 Eli Grade 23, please contact us and we will gladly refer you to additional sources.

  • 6AL-6V-2SN Titanium

    Alternate Names: 662 Titanium

    Description: 6AL-6V-2SN is an alloyed Grade of alpha-beta Titanium. 6AL-6V-2SN is similar to 6AL-4V in many ways, but exhibits higher strength properties due to additional Vanadium, Iron, and Copper. Welding is not typically recommended. 6AL-6V-2SN is often found in the Annealed condition, or heat treated to the higher strength Solution Treated & Aged condition. 6AL-6V-2SN exhibits extra high strength, and light weight. It is often used in aerospace, and oil & gas applications.

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

    6AL-6V-2SN Titanium is available in the following Product Forms:
    Round Bar (Rod), Rectangular Flat Bar (Block), Sheet, and Plate.

    6AL-6V-2SN Titanium is available in the following Specifications:

    MIL-T-9047 (6AL-6V-2SN)AMS 6936AMS 4971
    AMS-T-9047 (6AL-6V-2SN)AMS 6935AMS 4978
    AMS-T-9046 (6AL-6V-2SN)AMS 4979AMS 4918
    MIL-T-9046 (6AL-6V-2SN)
    Don’t see what you want? Call us at 888-772-8984 for a Quote on 6AL-6V-2SN 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-6V-2SN, 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.

  • MIL-T-9047 6AL-4V ELI

    MIL-T-9047
    Revision: “G, Amendment 2” issued 09/1986 ***Obsolete, S/S by AMS-T-9047***
    Alloy: 6AL-4V Eli
    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 – 6.5%Nitrogen (Maximum): 0.05%
    Vanadium: 3.5 – 4.5%Hydrogen (Maximum): 0.0125%
    Iron (Maximum): 0.25%Yttrium (Maximum): 0.005%
    Oxygen (Maximum): 0.13%Other Elements (Total): 0.30%
    Carbon (Maximum): 0.08%Titanium: Balance
    Tensile Properties (Minimums)*
    Tensile: 125 – 130 ksiElongation: 10%
    Yield: 115 – 120 ksiReduction of Area: 20 – 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.

  • MIL-T-9047 6AL-6V-2SN

    MIL-T-9047
    Revision: “G, Amendment 2” issued 09/1986 ***Obsolete, S/S by AMS-T-9047***
    Alloy: 6AL-6V-2SN
    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: 5.0 – 6.0%Nitrogen (Maximum): 0.04%
    Vanadium: 5.0 – 6.0%Hydrogen (Maximum): 0.015%
    Iron (Maximum): 0.35 – 1.0%Yttrium (Maximum): 0.005%
    Oxygen (Maximum): 0.20%Other Elements (Total): 0.30%
    Carbon (Maximum): 0.05%Copper: 0.35 – 1.0%
    Tin (Maximum): 1.5 – 2.5%Titanium: Balance
    Tensile Properties (Minimums)*
    Tensile: 150 – 175 ksiElongation: 6 – 8%
    Yield: 140 – 160 ksiReduction of Area: 15 – 20%

    *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.

  • MIL-T-9047 CP-70 GRADE 4

    MIL-T-9047
    Revision: “G, Amendment 2” issued 09/1986 ***Obsolete, S/S by AMS-T-9047***
    Grade: Commercially Pure Grade 4 (CP-70)
    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
    Carbon (Maximum): 0.08%Hydrogen (Maximum): 0.0125%
    Nitrogen (Maximum): 0.05%Other Elements (Total): 0.30%
    Iron (Maximum): 0.50%Titanium: Balance
    Oxygen (Maximum): 0.40%
    Tensile Properties (Minimums)*
    Tensile: 80 ksiElongation: 15%
    Yield: 70 ksiReduction of Area: 30%

    *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.

  • CP GRADE 4

    Alternate Names: CP Grade 4 Titanium, CP 4, Grade 4, CP 70

    Description: Commercially Pure (CP) Grade 4 Titanium is a grade 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 4 is higher in strength than CP Grades 1, 2, and 3. It is also commonly called “CP 70” which is in reference to its approximate yield strength. CP Grade 4 exhibits excellent corrosion resistance, as well as high strength. It is used in a variety of industries such as chemical, marine and aerospace.

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

    CP Grade 4 Titanium is available in the following Product Forms:
    Round Bar (Rod), Plate, and Sheet

    CP Grade 4 Titanium is available in the following Specifications:

    AMS 4901ASTM B348 Grade 4AMS-T-9047 (CP-70 Grade 4)
    AMS 4921ASTM F67 Grade 4MIL-T-9046 (CP-1 Grade 4)
    ASTM B265 Grade 4AMS-T-9046 (CP-1 Grade 4)MIL-T-9047 (CP-70 Grade 4)
    Don’t see what you want? Call us at 888-772-8984 for a Quote on CP Grade 4 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 4, please contact us and we will gladly refer you to additional sources.

  • 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.

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