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SAE AMS4910

Titanium Alloy, Sheet, Strip, and Plate 5Al - 2.5Sn Annealed

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Organization: SAE
Publication Date: 1 January 2017
Status: active
Page Count: 8
scope:

Form

This specification covers a titanium alloy in the form of sheet, strip, and plate up to 4.000 inches (101.60 mm), inclusive, in thickness

Application

These products have been used typically for parts requiring strength up to 800 °F (427 °C) and where such parts may require welding during fabrication, but usage is not limited to such applications

Certain processing procedures and service conditions may cause these products to become subject to stresscorrosion cracking; ARP982 recommends practices to minimize such conditions.

Classification Product supplied to this specification shall be classified as follows:

Type 1 - Product that has been ultrasonically inspected.

Type 2 - Product not requiring ultrasonic inspection.

Unless a specific type is ordered, Type 2 may be supplied.

Document History

SAE AMS4910
January 1, 2017
Titanium Alloy, Sheet, Strip, and Plate 5Al - 2.5Sn Annealed
Form This specification covers a titanium alloy in the form of sheet, strip, and plate up to 4.000 inches (101.60 mm), inclusive, in thickness Application These products have been used typically...
SAE AMS4910
September 1, 2012
Titanium Alloy, Sheet, Strip, and Plate 5Al - 2.5Sn Annealed
Form This specification covers a titanium alloy in the form of sheet, strip, and plate. Application These products have been used typically for parts requiring strength up to 800 °F (427 °C) and...
SAE AMS4910
February 1, 2008
Titanium Alloy, Sheet, Strip, and Plate 5Al - 2.5Sn Annealed
Form This specification covers a titanium alloy in the form of sheet, strip, and plate. Application These products have been used typically for parts requiring strength up to 800 °F (427 °C) and...
SAE AMS4910
February 1, 2003
Titanium Alloy, Sheet, Strip, and Plate 5Al - 2.5Sn Annealed
Form: This specification covers a titanium alloy in the form of sheet, strip, and plate. Application: These products have been used typically for parts requiring strength up to 800 °F (427 °C) and...
SAE AMS4910
November 1, 2001
Titanium Alloy, Sheet, Strip, and Plate 5Al - 2.5Sn Annealed
SCOPE: Form: This specification covers a titanium alloy in the form of sheet, strip, and plate. Application: These products have been used typically for parts requiring strength up to 800°F (427°C)...
SAE AMS4910
March 1, 1994
Titanium Alloy, Sheet, Strip, and Plate 5Al - 2.5Sn Annealed (UNS R54520)
SCOPE: Form: This specification covers a titanium alloy in the form of sheet, strip, and plate. Application: These products have been used typically for parts requiring strength up to 800 °F (427 °C)...
SAE AMS4910
April 1, 1988
TITANIUM ALLOY SHEET, STRIP, AND PLATE 5Al - 2.5Sn Annealed
Form: This specification covers a titanium alloy in the form of sheet, strip, and plate. Application: Primarily for parts requiring strength up to 800° F (425°C) and where such parts may require...
SAE AMS4910
January 1, 1983
TITANIUM ALLOY SHEET, STRIP, AND PLATE 5Al - 2.5Sn Annealed
Form: This specification covers a titanium alloy in the form of sheet, strip, and plate. Application: Primarily for parts requiring strength up to 8000 F (4250C) and where such parts may require...
SAE AMS4910
May 15, 1972
TITANIUM ALLOY SHEET, STRIP, AND PLATE 5Al - 2.5Sn Annealed
Form: This specification covers a titanium-base alloy in the form of sheet, strip, and plate. Application: Primarily for parts requiring strength up to 800 F (427 C) and weldability. Certain...
SAE AMS4910
November 15, 1971
TITANIUM ALLOY SHEET, STRIP, AND PLATE 5Al - 2.5Sn Annealed
Form: This specification covers a titanium-base alloy in the form of sheet, strip, and plate. Application: Primarily for parts requiring strength up to 800 F (427 C) and weldability. Certain...
SAE AMS4910
May 1, 1968
TITANIUM ALLOY SHEET, STRIP, AND PLATE 5Al - 2.5Sn Annealed
APPLICATION: Primarily for parts requiring strength up to 800 F (427 C). and weldability.
SAE AMS4910
September 30, 1966
TITANIUM ALLOY SHEET, STRIP, AND PLATE 5Al - 2.5Sn Annealed, 110,000 psi Yield
APPLICATION: Primarily for parts requiring weldability, and strength up to 800 F (427 C).
SAE AMS4910
September 1, 1965
TITANIUM ALLOY SHEET, STRIP, AND PLATE 5Al - 2.5Sn Annealed, 110,000 psi Yield
APPLICATION: Primarily for parts requiring weldability, and strength up to 800 F (427 C).
SAE AMS4910
June 30, 1964
TITANIUM ALLOY SHEET, STRIP, AND PLATE 5Al - 2.5Sn Annealed, 110,000 psi Yield
APPLICATION: Primarily for parts requiring weldability, and strength up to 800 F (425 C).
SAE AMS4910
January 15, 1959
TITANIUM ALLOY SHEET, STRIP, AND PLATE 5Al - 2.5Sn Annealed
Form: This specification covers a titanium alloy in the form of sheet, strip, and plate. Application: Primarily for parts requiring strength up to 800º F (425º C) and where such parts may require...
SAE AMS4910
January 15, 1959
TITANIUM ALLOY SHEET AND STRIP 5Al - 2.5Sn Annealed – 110,000 psi Yield
APPLICATION: Primarily for parts requiring weldability, and strength up to 800 F.
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References

This document references:
ASTM E1409 - Standard Test Method for Determination of Oxygen and Nitrogen in Titanium and Titanium Alloys by Inert Gas Fusion
Published by ASTM on October 1, 2013
This test method covers the determination of oxygen in titanium and titanium alloys in mass fractions from 0.01 % to 0.5 % and the determination of nitrogen in titanium and titanium alloys in mass...
This document references:
ASTM E1447 - Standard Test Method for Determination of Hydrogen in Titanium and Titanium Alloys by Inert Gas Fusion Thermal Conductivity/Infrared Detection Method
Published by ASTM on March 1, 2009
This test method applies to the determination of hydrogen in titanium and titanium alloys in concentrations from 0.0006 % to 0.0260 %. The values stated in SI units are to be regarded as standard. No...
This document references:
ASTM E1941 - Standard Test Method for Determination of Carbon in Refractory and Reactive Metals and Their Alloys by Combustion Analysis
Published by ASTM on December 1, 2010
This test method applies to the determination of carbon in refractory and reactive metals and their alloys in quantities from 20 μg to 500 μg. This corresponds to mass fractions ranging from 0.004 wt...
This document references:
ASTM E2371 - Standard Test Method for Analysis of Titanium and Titanium Alloys by Direct Current Plasma and Inductively Coupled Plasma Atomic Emission Spectrometry (Performance-Based Test Methodology)
Published by ASTM on June 15, 2013
This method describes the analysis of titanium and titanium alloys, such as specified by committee B10, by inductively coupled plasma atomic emission spectrometry (ICP-AES) and direct current plasma...
This document references:
ASTM E290 - Standard Test Methods for Bend Testing of Material for Ductility
Published by ASTM on May 1, 2014
These test methods cover bend testing for ductility of materials. Included in the procedures are four conditions of constraint on the bent portion of the specimen; a guided-bend test using a mandrel...
This document is referenced by:
MIL-STD-1587 - MATERIAL AND PROCESS REQUIREMENTS FOR AEROSPACE WEAPONS SYSTEMS
Published by NPFC on July 23, 2018
This standard establishes the requirements for materials and processes used during design and production of aerospace weapons systems and associated support equipment. When used in conjunction with...
This document is referenced by:
MMPDS-13 CHAPTER 6 - MMPDS-13 - Metallic Materials Properties Development and Standardization
Published by BATTELLE on July 1, 2018
A description is not available for this item.
This document is referenced by:
MMPDS-13 CHAPTER 2 - MMPDS-13 - Metallic Materials Properties Development and Standardization
Published by BATTELLE on July 1, 2018
A description is not available for this item.
This document is referenced by:
MMPDS-13 CHAPTER 8 - MMPDS-13 - Metallic Materials Properties Development and Standardization
Published by BATTELLE on July 1, 2018
A description is not available for this item.
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