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SAE AMS6478B

Current

Current

The latest, up-to-date edition.

Steel, Bars and Forgings, 3.1Cr - 11.5Ni - 13.5Co - 1.2Mo (0.21 - 0.25C), Vacuum Melted, Annealed, Heat Treatable to 290 ksi (1999 MPa) Tensile Strength

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

30-09-2005

€89.37
Excluding VAT

1 SCOPE
2 APPLICABLE DOCUMENTS
3 TECHNICAL REQUIREMENTS
4 QUALITY ASSURANCE PROVISIONS
3 PREPARATION FOR DELIVERY
6 ACKNOWLEDGMENT
7 REJECTIONS
8 NOTES

Covers a premium aircraft-quality alloy steel in the form of bars, forgings, and forging stock.

DocumentType
Standard
Pages
9
PublisherName
SAE International
Status
Current
SupersededBy
Supersedes

This specification covers a premium aircraft-quality alloy steel in the form of bars, forgings, and forging stock.These products have been used typically for parts requiring a combination of high strength, high toughness, and weldability, but usage is not limited to such applications. Product after proper heat treatment should attain a minimum tensile strength of 290 ksi (1999 MPa) and yield strength of 245 ksi (1689 MPa).

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SAE AMS2808E Identification Forgings
SAE MAM2300D Steel Cleanliness, Premium Aircraft-Quality Magnetic Particle Inspection Procedure, Metric (SI) Measurement
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