Sheet

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 ksi	Elongation: 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 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 ksi	Elongation: 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
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 ksi	Elongation: 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 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 ksi	Elongation: 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.

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 ksi	Elongation: 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
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 Min	Elongation: 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.

AMS 4901
Revision: “V” issued 02/2025
Grade: Commercially Pure Grade 4
Product Forms: Titanium Sheet, Strip, and Plate
Condition: Annealed

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): 0.30%
Nitrogen (Maximum): 0.05%	Titanium: Balance

Tensile Properties (Minimums)*
Tensile: 80 ksi	Elongation: 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
• Bend Testing
• 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 4901 specification.

To purchase AMS 4901V, please visit: www.sae.org/standards/content/ams4901v/

Changes may be made to the information contained herein.