SAE AMS 5600G-2024

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For more information on this standard, visit

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AEROSPACE

MATERIAL SPECIFICATION

AMS5600™

REV. G

Issued 1968-11

Reaffirmed 2012-10

Revised 2024-09

Superseding AMS5600F

Steel, Corrosion-Resistant, Sheet

Laminated, Edge Bonded

(Composition similar to UNS S30200)

RATIONALE

AMS5600F is the result of a Five-Year Review and update of the specification. The revision updates the composition

reporting requirements (see 3.1.1) and the exceptions requirements (see 8.4).

1. SCOPE

1.1 Form

This specification covers a corrosion-resistant steel in the form of laminated sheet.

1.2 Application

This sheet has been used primarily for shims of special shapes in which the thickness is adjusted by removal of laminations

as required, but usage is not limited to such applications.

2. APPLICABLE DOCUMENTS

The issue of the following documents in effect on the date of the purchase order forms a part of this specification to the

extent specified herein. The supplier may work to a subsequent revision of a document unless a specific document issue is

specified. When the referenced document has been cancelled and no superseding document has been specified, the last

published issue of that document shall apply.

2.1 SAE Publications

Available from SAE International, 400 Commonwealth Drive, Warrendale, PA 15096-0001, Tel: 877-606-7323 (inside USA

and Canada) or +1 724-776-4970 (outside USA), www.sae.org.

AMS2248 Chemical Check Analysis Limits, Corrosion- and Heat-Resistant Steels and Alloys, Maraging and Other

Highly Alloyed Steels, and Iron Alloys

AMS2371 Quality Assurance Sampling and Testing, Corrosion and Heat-Resistant Steels and Alloys, Wrought

Products and Forging Stock

AS7766 Terms Used in Aerospace Metals Specifications

SAE INTERNATIONAL AMS5600™G Page 2 of 5

2.2 ASTM Publications

Available from ASTM International, 100 Barr Harbor Drive, P.O. Box C700, West Conshohocken, PA 19428-2959,

Tel: 610-832-9585, www.astm.org.

ASTM A751 Chemical Analysis of Steel Products

2.3 Definitions

Terms used in AMS are defined in AS7766.

3. TECHNICAL REQUIREMENTS

3.1 Composition

Composition shall conform to the percentages by weight shown in Table 1, determined in accordance with ASTM A751 or

by other analytical methods acceptable to the purchaser.

Table 1 - Composition

Element

Min

Max

Carbon

0.15

Manganese

2.00

Silicon

1.00

Phosphorus

0.040

Sulfur

0.030

Chromium

17.00

19.00

Nickel

8.00

10.00

Molybdenum

0.75

Copper

0.75

3.1.1 The producer may test for any element not listed in Table 1 and include this analysis in the report of 4.4. Reporting

of any element not listed in the composition table is not a basis for rejection unless limits of acceptability are

specified by the purchaser.

3.1.2 Check Analysis

Composition variations shall meet the requirements of AMS2248.

3.1.3 Adhesive

Adhesive shall be of a composition meeting the fabrication (see 3.2) and quality (see 3.3) requirements.

3.2 Fabrication

Shim stock shall be fabricated from corrosion-resistant steel laminations in a temper suitable for shearing. Stock shall consist

completely of laminations 0.002 inch ± 0.0002 inch (0.05 mm ± 0.005 mm) thick or 0.003 inch ± 0.0003 inch

(0.08 mm ± 0.008 mm) thick, or partly of such laminations in combination with a single thicker lamination, as ordered, precut

to the desired shape, stacked to the desired thickness, and bonded on the outside edge with adhesive.

3.2.1 Laminations shall be bonded together in such a manner that normal handling shall not cause separation of the

laminated shim stock. The layers shall readily peel to provide the required thickness of laminations.

3.3 Quality

The product, as received by the purchaser, shall be uniform in quality and condition, sound, and free from foreign materials

and from imperfections detrimental to usage of the product.

SAE INTERNATIONAL AMS5600™G Page 3 of 5

3.4 Tolerances

Tolerances shall be as specified in Table 2.

Table 2A - Tolerances, inch/pound units

Nominal Total Thickness

Inch

Tolerance

Inch

Plus

Tolerance

Inch

Minus

Up to 0.010, incl

Over 0.010 to 0.021, incl

Over 0.021 to 0.047, incl

Over 0.047 to 0.078, incl

Over 0.078

0.0005

0.001

0.002

0.003

0.005

0.0005

0.001

0.002

Table 2B - Tolerances, SI units

Nominal Total Thickness

Millimeters

Tolerance

Millimeters

Plus

Tolerance

Millimeters

Minus

Up to 0.25, incl

Over 0.25 to 0.53, incl

Over 0.53 to 1.19, incl

Over 1.19 to 1.98, incl

Over 1.98

0.013

0.025

0.05

0.08

0.13

0.013

0.025

0.05

3.5 Exceptions

Any exceptions shall be authorized by the purchaser and reported as in 4.4.1.

4. QUALITY ASSURANCE PROVISIONS

4.1 Responsibility for Inspection

The producer of the product shall supply all samples for the producer’s tests and shall be responsible for the performance

of all required tests. The purchaser reserves the right to sample and to perform any confirmatory testing deemed necessary

to ensure that the product conforms to specified requirements.

4.2 Classification of Tests

All technical requirements are acceptance tests and shall be performed to represent each lot.

4.3 Sampling and Testing

Sampling and testing shall be in accordance with AMS2371; a lot shall be all laminated shim stock of the same thickness

and shape from one heat of steel processed at the same time and presented for the producer’s inspection at one time.

4.4 Reports

The producer of the product shall furnish with each shipment a report stating the producer’s name, country where the metal

was melted (e.g., final melt in the case of metal processed by multiple melting operations), the results of tests for composition

of each heat, and stating that the product conforms to the other technical requirements. This report shall include the

purchase order number, heat and lot numbers, AMS5600G, shim stock thickness, lamination thickness, size, and quantity.

4.4.1 When material produced to this specification has exceptions authorized by the purchaser taken to the technical

requirements listed in Section 3 (see 5.1.3), the report shall contain a statement “This material is certified as

AMS5600G(EXC) because of the following exceptions:” and the specific exceptions shall be listed.

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摘要：

SAE AMS 5600G-2024 是国际自动机工程师学会（SAE International）发布的最新版航空材料规范，专门针对适用于高温环境下的耐腐蚀钢板、钢带及型材。该标准替代了之前的AMS 5600F版本，主要更新了化学成分控制范围、热处理工艺要求以及力学性能指标，以确保材料在航空发动机、机身结构件及关键液压系统中的可靠性与耐久性。遵循该规范的材料通常为真空熔炼或重熔工艺生产的马氏体或沉淀硬化型不锈钢，适用于制造需要在中等温度下保持高强度、抗氧化及抗腐蚀性能的零部件。本标准不仅是航空制

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