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SAE AMS4908G

Current

Current

The latest, up-to-date edition.

Titanium Alloy Sheet and Strip 8mn Annealed, 110 Ksi (760 Mpa) Yield Strength

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

07-01-2003

€85.07
Excluding VAT

1 Scope
  1.1 Form
  1.2 Application
2 Applicable documents
  2.1 SAE publications
  2.2 ASTM publications
  2.3 U.S. government publications
3 Technical requirements
  3.1 Composition
  3.2 Condition
  3.3 Annealing
  3.4 Properties
  3.5 Quality
  3.6 Tolerances
4 Quality assurance provisions
  4.1 Responsibility for inspection
  4.2 Classification of tests
  4.3 Sampling
  4.4 Reports
  4.5 Resampling and retesting
5 Preparation for delivery
  5.1 Identification
  5.2 Packaging
6 Acknowledgement
7 Rejections
8 Notes

Specifies a titanium alloy in the form of sheet and strip. Mainly for parts requiring good formability and strength up to 600 Deg F (315 Deg. C).

DocumentType
Standard
Pages
8
PublisherName
SAE International
Status
Current
Supersedes

This specification has been declared NONCURRENT by the Aerospace Materials Division, SAE, as of April 1994. It is recommended, therefore, that this specification not be specified for new designs.

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MIL-PRF-8188 Revision D:1997 CORROSION-PREVENTIVE, AIRCRAFT TURBINE ENGINE, SYNTHETIC BASE
MIL L 87100 : 0 LUBRICATING OIL, AIRCRAFT TURBINE ENGINE, POLYPHENYL ETHER BASE
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MIL-PRF-87100 Revision A:1997 LUBRICATING OIL, AIRCRAFT TURBINE ENGINE, POLYPHENYL ETHER BASE

SAE AMS 2809 : 2007(R2011) IDENTIFICATION, TITANIUM AND TITANIUM ALLOY WROUGHT PRODUCTS
ASTM E 120 : 2000 Standard Test Methods for Chemical Analysis of Titanium and Titanium Alloys (Withdrawn 2003)
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MIL-STD-163 Revision C:1978 STEEL MILL PRODUCTS PREPARATION FOR SHIPMENT AND STORAGE
SAE AMS 2242 : 2014 TOLERANCES, CORROSION AND HEAT RESISTANT STEEL, IRON ALLOY, TITANIUM, AND TITANIUM ALLOY SHEET, STRIP, AND PLATE
ASTM E 8 : 2004 Standard Test Methods for Tension Testing of Metallic Materials
ASTM E 290 : 2014 : REDLINE Standard Test Methods for Bend Testing of Material for Ductility
SAE ARP 982 : 2016 MINIMIZING STRESS-CORROSION CRACKING IN WROUGHT TITANIUM ALLOY PRODUCTS

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