SAE AMS 5583F-2019

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AEROSPACE

MATERIAL SPECIFICATION

AMS5583™

REV. F

Issued 1977-07

Revised 2019-01

Superseding AMS5583E

Nickel Alloy, Corrosion and Heat-Resistant, Seamless Tubing

72Ni - 15.5Cr - 0.95Cb (Nb) - 2.5Ti - 0.70Al - 7.0Fe

Vacuum Melted

Solution Heat Treated, Precipitation Hardenable to 170 ksi (1172 MPa) Tensile

Strength

(Composition similar to UNS N07750)

RATIONALE

AMS5583F prohibits unauthorized exceptions (3.9), revises fabrication (3.5), reports (4.4), and identification (5.2.1), and

results from a Five-Year Review and update of this specification.

1. SCOPE

1.1 Form

This specification covers a precipitation hardenable corrosion and heat-resistant nickel alloy in the form of seamless tubing.

1.2 Application

This tubing has been used typically for fluid lines requiring high strength up to 1300 °F (704 °C) and oxidation resistance up

to 1800 °F (982 °C), but usage is not limited to such applications. Parts may be formed and then heat treated to improve

strength at elevated temperatures.

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.

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SAE INTERNATIONAL AMS5583™F Page 2 of 7

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.

AMS2263 Tolerances, Nickel, Nickel Alloy, and Cobalt Alloy Tubing

AMS2269 Chemical Check Analysis Limits, Nickel, Nickel Alloys, and Cobalt Alloys

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

Products and Forging Stock

AMS2634 Ultrasonic Inspection, Thin Wall Metal Tubing

AMS2750 Pyrometry

AMS2807 Identification, Carbon and Low-Alloy Steels, Corrosion and Heat-Resistant Steels and Alloys, Sheet,

Strip, Plate, and Aircraft Tubing

ARP1917 Clarification of Terms Used in Aerospace Metals Specifications

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 E8/E8M Tension Testing of Metallic Materials

ASTM E18 Rockwell Hardness of Metallic Materials

ASTM E112 Determining Average Grain Size

ASTM E140 Hardness Conversion Tables for Metals Relationship Among Brinell Hardness, Vickers Hardness,

Rockwell Hardness, Superficial Hardness, Knoop Hardness, Scleroscope Hardness, and Leeb

Hardness

ASTM E354 Chemical Analysis of High-Temperature, Electrical, Magnetic, and Other Similar Iron, Nickel, and

Cobalt Alloys

ASTM E426 Electromagnetic (Eddy-Current) Examination of Seamless and Welded Tubular Products, Titanium,

Austenitic Stainless Steel and Similar Alloys

ASTM E1417/E1417M Liquid Penetrant Testing

3. TECHNICAL REQUIREMENTS

3.1 Composition

Shall conform to the percentages by weight shown in Table 1, determined by wet chemical methods in accordance with

ASTM E354, by spectrochemical methods, or by other analytical methods acceptable to purchaser.

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SAE INTERNATIONAL AMS5583™F Page 3 of 7

Table 1 - Composition

Element

Min

Max

Carbon

0.08

Manganese

0.35

Silicon

0.35

Phosphorus

0.015

Sulfur

0.010

Chromium

14.00

17.00

Nickel

70.00

Columbium (Niobium)

0.70

1.20

Titanium

2.25

2.75

Aluminum

0.40

1.00

Iron

5.00

9.00

Cobalt (3.1.1)

1.00

Tantalum

0.05

Copper

0.50

3.1.1 Determination not required for lot acceptance.

3.1.2 Check Analysis

Composition variations shall meet the applicable requirements of AMS2269.

3.2 Melting Practice

Alloy shall be multiple melted using consumable electrode practice in the remelt cycle. If consumable electrode remelting is

not performed in vacuum, electrodes which have been produced by vacuum induction melting shall be used for remelting.

3.3 Condition

Solution heat treated, and unless solution heat treatment is performed in an atmosphere yielding a bright finish, pickled as

required.

3.4 Heat Treatment

Tubing shall be solution heat treated by heating to a temperature not lower than 1800 °F (982 °C), holding at the selected

temperature within ±25 °F (±14 °C) for a time commensurate with cross-sectional thickness, and cooling at a rate equivalent

to an air cool or faster. Pyrometry shall be in accordance with AMS2750.

3.5 Fabrication

Tubing shall be produced by a seamless and drawn process. Any surface finishing operation applied to remove

objectionable pits and blemishes shall be performed prior to solution heat treatment. Only light polishing to improve external

surface appearance is permitted after solution heat treatment. Bore conditioning is permitted after final anneal providing the

tubing is not sized by metal removal methods and the tubing is passivated after any such conditioning (see 8.3.1).

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摘要：

SAE AMS 5583F-2019 是2019年发布的航空航天材料规范，专门用于规定耐腐蚀、耐高温的18-8型不锈钢无缝或焊接管材的技术要求。该标准涵盖了化学成分、机械性能、热处理工艺及尺寸公差等关键指标，适用于飞机液压系统、燃油管路及其他需要高可靠性的航空部件。作为取代AMS 5583E的更新版本，它确保了材料在极端温度与压力环境下的稳定性和抗腐蚀性，是航空航天制造与维修行业采购、质检及工程设计的权威参考依据。

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