SAE AMS 5405B-2007

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SAE Technical Standards Board Rules provide that: “This report is published by SAE to advance the state of technical and engineering sciences. The use of this report is entirely

voluntary, and its applicability and suitability for any particular use, including any patent infringement arising therefrom, is the sole responsibility of the user.”

SAE reviews each technical report at least every five years at which time it may be reaffirmed, revised, or cancelled. SAE invites your written comments and suggestions.

or otherwise, without the prior written permission of SAE.

TO PLACE A DOCUMENT ORDER: Tel: 877-606-7323 (inside USA and Canada)

Tel: 724-776-4970 (outside USA)

Fax: 724-776-0790

Email: CustomerService@sae.org

SAE WEB ADDRESS: http://www.sae.org

AMS 5405B

AEROSPACE

MATERIAL

SPECIFICATION Issued OCT 1982

Noncurrent NOV 1995

Reaf. Noncur. MAR 2001

Cancelled APR 2007

Superseding AMS 5405A

Alloy Castings, Investment, Corrosion and Heat Resistant

64Ni - 8.0Cr - 10Co - 6.0Mo - 1.0Ti - 4.2Ta - 6.0Al - 0.015B - 0.08Zr

Vacuum Melted, Vacuum Cast

As Cast

RATIONALE

AMS 5405A has been designated cancelled because survey of aerospace users and producers determined that this

product is not produced to this specification.

CANCELLATION NOTICE

This specification has been declared "CANCELLED" by the Aerospace Materials Division, SAE, as of April, 2007. By this

action, this document will remain listed in the Numerical Section of the Index of Aerospace Material Specifications,

indicating that it has been "CANCELLED".

Cancelled specifications are available from SAE.

AEROSPACE

MATERIAL

SPECIFICATION

AMS 5405A

Issued OCT 1982

Noncurrent NOV 1995

Reaf. Noncur. MAR 2001

Superseding AMS 5405

Alloy Castings, Investment, Corrosion and Heat Resistant

64Ni - 8.0Cr - 10Co - 6.0Mo - 1.0Ti - 4.2Ta - 6.0Al - 0.015B - 0.08Zr

Vacuum Melted, Vacuum Cast

As Cast

NONCURRENT NOTICE

This specification has been declared “NONCURRENT” by the Aerospace Materials Division, SAE,

as of November 1995. It is recommended, therefore, that this specification not be specified for new

designs.

“NONCURRENT” refers to those materials which have previously been widely used and which may

be required on some existing designs in the future. The Aerospace Materials Division, however,

does not recommend these as standard materials for future use in new designs. Each of these

“NONCURRENT” specifications is available.

SAE Technical Standards Board Rules provide that: “This report is published by SAE to advance the state of technical and engineering sciences. The use of this report is entirely

voluntary, and its applicability and suitability for any particular use, including any patent infringement arising therefrom, is the sole responsibility of the user.”

SAE reviews each technical report at least every five years at which time it may be reaffirmed, revised, or cancelled. SAE invites your written comments and suggestions.

QUESTIONS REGARDING THIS DOCUMENT: (724) 772-7161 FAX: (724) 776-0243

TO PLACE A DOCUMENT ORDER: (724) 776-4970 FAX: (724) 776-0790

SAE WEB ADDRESS: http://www.sae.org

400 Commonwealth Drive, Warrendale, PA 15096-0001

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摘要：

SAE AMS 5405B-2007 是美国汽车工程师学会（SAE）发布的一项航空航天材料规范，主要规定了耐腐蚀钢（通常为440C型或类似马氏体不锈钢）的化学成分、热处理要求、力学性能及质量控制标准。该标准替代了早期版本（如AMS 5405A），旨在确保材料在高温、高应力及腐蚀性环境下的可靠性与一致性，广泛应用于飞机发动机部件、轴承、阀门及其他航空机械结构的制造与维修。符合该规范的材料需经过严格的熔炼、锻造及回火处理，以达到规定的硬度、抗拉强度和抗腐蚀性指标。对于从事航空航天、国防及精密工业的工

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SAE AMS 5405B-2007

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