ASTM B209

NOTICE: This standard has either been superseded and replaced by a new version or discontinued. Contact ASTM International (www.astm.org) for the latest information. Designation: B 209M – 02 METRIC

Standard Specification for

Aluminum and Aluminum-Alloy Sheet and Plate [Metric]1 This standard is issued under the fixed designation B 209M; the number immediately following the designation indicates the year of original adoption or, in the case of revision, the year of last revision. A number in parentheses indicates the year of last reapproval. A superscript epsilon (e) indicates an editorial change since the last revision or reapproval. This standard has been approved for use by agencies of the Department of Defense.

Alloy Wrought Products for Aerospace Applications2 B 632/B 632M Specification for Aluminum-Alloy Rolled Tread Plate2 B 660 Practices for Packaging/Packing of Aluminum and Magnesium Products2 B 666/B 666M Practice for Identification Marking of Aluminum and Magnesium Products2 B 918 Practice for Heat Treatment of Wrought Aluminum Alloys2 E 3 Methods of Preparation of Metallographic Specimens3 E 29 Practice for Using Significant Digits in Test Data to Determine Conformance with Specifications4 E 34 Test Methods for Chemical Analysis of Aluminum and Aluminum-Base Alloys5 E 55 Practice for Sampling Wrought Nonferrous Metals and Alloys for Determination of Chemical Composition5 E 290 Test Method for Bend Test for Ductility3 E 407 Practice for Microetching Metals and Alloys3 E 527 Practice for Numbering Metals and Alloys (UNS)6 E 607 Test Method for Optical Emission Spectrometric Analysis of Aluminum and Aluminum Alloys by the Point-to-Plane Technique, Nitrogen Atmosphere5 E 716 Practices for Sampling Aluminum and Aluminum Alloys for Spectrochemical Analysis5 E 1004 Practice for Determining Electrical Conductivity Using the Electromagnetic Eddy-Current Method7 E 1251 Test Method for Optical Emission Spectrometric Analysis of Aluminum and Aluminum Alloys by the Argon Atmosphere, Point-to-Plane, Unipolar Self-Initiating Capacitor Discharge5 G 34 Test Method for Exfoliation Corrosion Susceptibility in 2XXX and 7XXX Series Aluminum Alloys (EXCO Test)8,9

1. Scope * 1.1 This specification covers aluminum and aluminum alloy flat sheet, coiled sheet, and plate, in the alloys (Note 1) and tempers shown inTables 2 and 3, and in the following finishes: 1.1.1 Plate in all alloys and sheet in heat-treatable alloys: mill finish. 1.1.2 Sheet in nonheat-treatable alloys: mill finish, one-side bright mill finish, standard one-side bright finish, and standard two-sides bright finish. 1.2 Alloy and temper designations are in accordance with ANSI H35.1M. The equivalent Unified Numbering System alloy designations are those of Table 1 preceded by A9, for example, A91100 for aluminum 1100 in accordance with Practice E 527. NOTE 1—Throughout this specification, use of the term alloy in the general sense includes aluminum as well as aluminum alloy. NOTE 2—See Specification B 632/B 632M for Tread Plate.

1.3 This specification is the metric counterpart of Specification B 209. 1.4 For acceptance criteria for inclusion of new aluminum and aluminum alloys in this specification, see Annex A2. 2. Referenced Documents 2.1 The following documents of the issue in effect on the date of material purchase, unless otherwise noted, form a part of this specification to the extent referenced herein: 2.2 ASTM Standards: B 209 Specification for Aluminum and Aluminum-Alloy Sheet and Plate2 B 548 Method for Ultrasonic Inspection of AluminumAlloy Plate for Pressure Vessels2 B 557M Test Methods for Tension Testing Wrought and Cast Aluminum- and Magnesium-Alloy Products [Metric]2 B 594 Practice for Ultrasonic Inspection of Aluminum-

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Annual Book of ASTM Standards, Vol 03.01. Annual Book of ASTM Standards, Vol 14.02. Annual Book of ASTM Standards, Vol 03.05. 6 Annual Book of ASTM Standards, Vol 01.01. 7 Annual Book of ASTM Standards, Vol 03.03. 8 The applicable edition in the use of this specification is G34 – 72—available in the gray pages of the Annual Book of ASTM Standards, Vol 02.02. 9 Annual Book of ASTM Standards, Vol 03.02. 4 5

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This specification is under the jurisdiction of ASTM Committee B07 on Light Metals and Alloys and is the direct responsibility of Subcommittee B07.03 on Aluminum Alloy Wrought Products. Current edition approved Apr. 10, 2002. Published June 2002. Originally published as B 209M – 78. Last previous edition B 209M – 01. 2 Annual Book of ASTM Standards, Vol 02.02.

*A Summary of Changes section appears at the end of this standard. Copyright © ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959, United States.

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NOTICE: This standard has either been superseded and replaced by a new version or discontinued. Contact ASTM International (www.astm.org) for the latest information. B 209M TABLE 1 Chemical Composition LimitsA,B,C Alloy 1060 1100 1230H 2014 Alclad 2014 2024 Alclad 2024 2124 2219 Alclad 2219 3003 Alclad 3003 3004 Alclad 3004 3005 3105 5005 5010 5050 5052 5083 5086 5154 5252 5254 5454 5754 5456 5457 5652 5657 6003H 6013 6061 Alclad 6061 7008H 7072H 7075 Alclad 7075 7008 Alclad 7075 7178 Alclad 7178

Silicon

Iron

0.25 0.35 0.95 Si + Fe 0.70 Si + Fe 0.50–1.2 0.7

Manganese

Magnesium

0.05 0.05–0.20 0.10 3.9–5.0

0.03 0.05 0.05 0.40–1.2

0.03 ... 0.05 0.20–0.8 2014 1.2–1.8 2024 1.2–1.8 0.02 2219 ... 3003 0.8–1.3 3004 0.20–0.6 0.20–0.8 0.50–1.1 0.20–0.6 1.1–1.8 2.2–2.8 4.0–4.9 3.5–4.5 3.1–3.9 2.2–2.8 3.1–3.9 2.4–3.0 2.6-3.6 4.7–5.5 0.8–1.2 2.2–2.8 0.6–1.0 0.8–1.5 0.8–1.2 0.8–1.2 6061 0.7–1.4 0.10 2.1–2.9 7075 7075 2.4–3.1 7178

Copper

0.50

0.50

3.8–4.9

0.30–0.9

0.20 0.20

0.30 0.30

3.8–4.9 5.8–6.8

0.30–0.9 0.20–0.40

0.6

0.7

0.05–0.20

1.0–1.5

0.30

0.7

0.25

1.0–1.5

0.30 0.30 0.20 0.25 0.20 0.10 0.10 0.10 0.10 0.10 0.05 0.10 0.10 0.10 0.20 0.04 0.10 0.10 0.6–1.1 0.15–0.40

1.0–1.5 0.30–0.8 0.20 0.10–0.30 0.10 0.10 0.40–1.0 0.20–0.7 0.10 0.10 0.01 0.50–1.0 0.50J 0.50–1.0 0.15–0.45 0.01 0.03 0.8 0.20–0.8 0.15

0.10 0.7 Si + Fe 0.40 0.50

0.05 0.10 1.2–2.0

0.05 0.10 0.30

0.40

1.6–2.4

0.30

0.6 0.7 0.6 0.7 0.30 0.7 0.40 0.7 0.40 0.7 0.25 0.40 0.40 0.40 0.40 0.50 0.25 0.40 0.08 0.10 0.45 Si + Fe 0.25 0.40 0.40 0.40 0.25 0.40 0.08 0.10 0.40 Si + Fe 0.08 0.10 0.35–1.0 0.6 0.6–1.0 0.50 0.40–0.8 0.7 0.10

0.50

Chromium

Zinc

... 0.05 ... 0.10 ... 0.10 0.10 0.25 clad with 6003 alloy 0.10 0.25 clad with 1230 alloy 0.10 0.25 ... 0.10 clad with 7072 alloy ... 0.10 clad with 7072 alloy ... 0.25 clad with 7072 alloy 0.10 0.25 0.20 0.40 0.10 0.25 0.15 0.30 0.10 0.25 0.15–0.35 0.10 0.05–0.25 0.25 0.05–0.25 0.25 0.15–0.35 0.20 ... 0.05 0.15–0.35 0.20 0.05–0.20 0.25 0.30J 0.20 0.05–0.20 0.25 ... 0.05 0.15–0.35 0.10 ... 0.05 0.35 0.20 0.10 0.25 0.04–0.35 0.25 clad with 7072 alloy 0.12–0.25 4.5–5.5 ... 0.8–1.3 0.18–0.28 5.1–6.1 clad with 7072 alloy clad with 7008 alloy 0.18–0.28 6.3–7.3 clad with 7072 alloy

Other ElementsD

Titanium

Each

TotalE

Aluminum

0.03 ... 0.03 0.15

0.03F 0.05 0.03F 0.05

... 0.15 ... 0.15

99.60 minG 99.00 minG 99.30 minG remainder

0.15

0.05

0.15

remainder

0.15 0.02–0.10

0.05 0.05I

0.15 0.15I

remainder remainder

...

0.05

0.15

remainder

...

0.05

0.15

remainder

0.10 0.10 ... 0.10 ... ... 0.15 0.15 0.20 ... 0.05 0.20 0.15 0.20 ... ... ... 0.10 0.10 0.15

0.05 0.05 0.05 0.05 0.05 0.05 0.05 0.05 0.05 0.03F 0.05 0.05 0.05 0.05 0.03F 0.05 0.02K 0.05 0.05 0.05

0.15 0.15 0.15 0.15 0.15 0.15 0.15 0.15 0.15 0.10F 0.15 0.15 0.15 0.15 0.10F 0.15 0.05K 0.15 0.15 0.15

remainder remainder remainder remainder remainder remainder remainder remainder remainder remainder remainder remainder remainder remainder remainder remainder remainder remainder remainder remainder

0.05 ... 0.20

0.05 0.05 0.05

0.10 0.15 0.15

remainder remainder remainder

0.20

0.05

0.15

remainder

A

Limits are in mass percent maximum unless shown as a range or stated otherwise. Analysis shall be made for the elements for which limits are shown in this table. For purposes of determining conformance to these limits, an observed value or a calculated value attained from analysis shall be rounded to the nearest unit in the last righthand place of figures used in expressing the specified limit, in accordance with the rounding-off method of Practice E 29. D Others includes listed elements for which no specific limit is shown as well as unlisted metallic elements. The producer may analyze samples for trace elements not specified in the specification. However, such analysis is not required and may not cover all metallic Others elements. Should any analysis by the producer or the purchaser establish that an Others element exceeds the limit of Each or that the aggregate of several Others elements exceeds the limit of Total, the material shall be considered non-conforming. E Other Elements—Total shall be the sum of unspecified metallic elements 0.010 % or more, rounded to the second decimal before determining the sum. F Vanadium 0.05 max. The total for other elements does not include vanadium. G The aluminum content shall be calculated by subtracting from 100.00 % the sum of all metallic elements present in amounts of 0.010 % or more each, rounded to the second decimal before determining the sum. H Composition of cladding alloy as applied during the course of manufacture. Samples from finished sheet or plate shall not be required to conform to these limits. I Vanadium, 0.05–0.15, zirconium, 0.10–0.25. The total for other elements does not include vanadium and zirconium. J 0.10-0.6 Mn + Cr. K Gallium 0.03 max, vanadium 0.05 max. The total for other elements does not include vanadium and gallium. B

C

Chemical Composition and Forms of Product10 ISO2107 Aluminum, Magnesium and their Alloys-Temper Designation10 ISO6361-2 Wrought Aluminum and Aluminum Alloys, Sheets, Strips, and Plates10 2.4 ANSI Standards:

G 47 Test Method for Determining Susceptibility to StressCorrosion Cracking of High Strength Aluminum Alloy Products9 G 66 Test Method for Visual Assessment of Exfoliation Corrosion Susceptibility of 5XXX Series Aluminum Alloys (ASSET Test)9 2.3 ISO Standards: ISO209-1 Wrought Aluminum and Aluminum Alloys-

10 Available from American National Standards Institute, 25 W. 43rd St., 4th Floor, New York, NY 10036.

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NOTICE: This standard has either been superseded and replaced by a new version or discontinued. Contact ASTM International (www.astm.org) for the latest information. B 209M 4. Ordering Information

H35.1M Alloy and Temper Designation Systems for Aluminum11 H35.2M Dimensional Tolerances for Aluminum Mill Products11 2.5 AMS Specification: AMS 2772 Heat Treatment of Aluminum Alloy Raw Materials12

4.1 Orders for material to this specification shall include the following information: 4.1.1 This specification designation (which includes the number, the year, and the revision letter, if applicable), 4.1.2 Quantity in pieces or kilograms, 4.1.3 Alloy (7.1), 4.1.4 Temper (9.1), 4.1.5 Finish for sheet in nonheat-treatable alloys (Section 1), 4.1.6 For sheet, whether flat or coiled, 4.1.7 Dimensions (thickness, width, and length or coil size), 4.2 Additionally, orders for material to this specification shall include the following information when required by the purchaser: 4.2.1 Whether supply of one of the pairs of tempers where shown in Table 2, H14 or H24, H34 or H24 is specifically excluded (Table 2, footnote E), 4.2.2 Whether bend tests are required (12.1), 4.2.3 Whether heat treatment in accordance with Practice B 918 is required (8.2), 4.2.4 Whether testing for stress-corrosion cracking resistance of alloy 2124-T851 is required (13.1). 4.2.5 Whether ultrasonic inspection for aerospace applications is required (Section 17), 4.2.6 Whether inspection or witness of inspection and tests by the purchaser’s representative is required prior to material shipment (Section 18), 4.2.7 Whether certification is required (Section 22), 4.2.8 Whether marking for identification is required (20.1), and 4.2.9 Whether Practices B 660 applies and, if so, the levels of preservation, packaging, and packing required (21.3).

3. Terminology 3.1 Definitions: 3.1.1 sheet—a rolled product rectangular in cross section and form over 0.15 through 6.30 mm in thickness with sheared, slit, or sawed edges. 3.1.1.1 alclad sheet—composite sheet comprised of an aluminum-alloy core having on both surfaces (if on one side only, alclad one side sheet) a metallurgically bonded aluminum or aluminum-alloy coating that is anodic to the core, thus electrolytically protecting the core against corrosion. 3.1.1.2 coiled sheet—sheet in coils with slit edges. 3.1.1.3 flat sheet—sheet with sheared, slit, or sawed edges, which has been flattened or leveled. 3.1.1.4 mill finish sheet—sheet having a nonuniform finish which may vary from sheet to sheet and within a sheet, and may not be entirely free from stains or oil. 3.1.1.5 one-side bright mill finish sheet—sheet having a moderate degree of brightness on one side, and a mill finish on the other. 3.1.1.6 standard one-side bright finish sheet—sheet having a uniform bright finish on one side, and a mill finish on the other. 3.1.1.7 standard two-sides bright finish sheet—sheet having a uniform bright finish on both sides. 3.1.2 plate—a rolled product rectangular in cross section and form over 6.30 mm in thickness with either sheared or sawed edges. 3.1.2.1 alclad plate—composite plate comprised of an aluminum-alloy core having on both surfaces (if on one side only, alclad one-side plate) a metallurgically bonded aluminum or aluminum-alloy coating that is anodic to the core, thus electrolytically protecting the core against corrosion. 3.1.2.2 parent coil or plate—a coil of sheet or a plate that has been processed to final temper as a single unit and subsequently cut into two or more smaller coils or individual sheets or into smaller plates to provide the required width or length or both. 3.1.3 producer—the primary manufacturer of the material. 3.1.4 supplier—includes only the category of jobbers and distributors as distinct from producers. 3.2 Definitions of Terms Specific to This Standard: 3.2.1 capable of—The term capable of as used in this specification means that the test need not be performed by the producer of the material. However, should testing by the purchaser establish that the material does not meet these requirements, the material shall be subject to rejection.

5. Responsibility for Quality Assurance 5.1 Responsibility for Inspection and Tests—Unless otherwise specified in the contract or purchase order, the producer is responsible for the performance of all inspection and test requirements specified herein. The producer may use his own or any other suitable facilities for the performance of the inspection and test requirements specified herein, unless disapproved by the purchaser in the order or at the time of contract signing. The purchaser shall have the right to perform any of the inspections and tests set forth in this specification where such inspections are deemed necessary to assure that material conforms to prescribed requirements. 5.2 Lot Definition—An inspection lot shall be defined as follows: 5.2.1 For heat-treated tempers, an inspection lot shall consist of an identifiable quantity of material of the same mill form, alloy, temper, and thickness traceable to a heat-treat lot or lots, and subjected to inspection at one time. 5.2.2 For nonheat-treated tempers, an inspection lot shall consist of an identifiable quantity of material of the same mill form, alloy, temper, and thickness subjected to inspection at one time.

11 Available in the Related Materials section (gray pages) of the Annual Book of ASTM Standards, Vol 02.02. 12 Available from Society of Automotive Engineers (SAE), 400 Commonwealth Dr., Warrendale, PA 15096-0001.

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NOTICE: This standard has either been superseded and replaced by a new version or discontinued. Contact ASTM International (www.astm.org) for the latest information. B 209M when no published ASTM method is available. In case of dispute, the methods of analysis shall be agreed upon between the producer and purchaser.

6. General Quality 6.1 Unless otherwise specified, the material shall be supplied in the mill finish and shall be uniform as defined by the requirements of this specification and shall be commercially sound. Any requirement not so covered is subject to negotiation between producer and purchaser. 6.2 Each sheet and plate shall be examined to determine conformance to this specification with respect to general quality and identification marking. On approval of the purchaser, however, the producer may use a system of statistical quality control for such examinations.

8. Heat Treatment 8.1 Unless specified in 8.2, producer or supplier heat treatment for the applicable tempers in Table 3 shall be in accordance with AMS 2772. 8.2 When specified, heat treatment of applicable tempers in Table 3 shall be in accordance with Practice B 918. 9. Tensile Properties of Material as Supplied 9.1 Limits—The sheet and plate shall conform to the requirements for tensile properties as specified in Table 2 and Table 3 for nonheat-treatable and heat-treatable alloys, respectively. 9.2 Number of Samples—One sample shall be taken from each end of each parent coil, or parent plate, but no more than one sample per 1000 kg of sheet or 2000 kg of plate, or part thereof, in a lot shall be required. Other procedures for selecting samples may be employed if agreed upon between the producer and purchaser. 9.3 Test Specimens—Geometry of test specimens and the location in the product from which they are taken shall be as specified in Test Methods B 557M. 9.4 Test Methods—The tension test shall be made in accordance with Test Methods B 557M.

7. Chemical Composition 7.1 Limits—The sheet and plate shall conform to the chemical composition limits specified in Table 1. Conformance shall be determined by the producer by analyzing samples taken at the time the ingots are cast, or samples taken from the finished or semifinished product. If the producer has determined the chemical composition of the material during the course of manufacture, additional sampling and analysis of the finished product shall not be required. NOTE 3—It is standard practice in the United States aluminum industry to determine conformance to the chemical composition limits prior to further processing of ingots into wrought products. Due to the continuous nature of the process, it is not practical to keep a specific ingot analysis identified with a specific quantity of finished material.

7.2 Number of Samples—The number of samples taken for determination of chemical composition shall be as follows: 7.2.1 When samples are taken at the time the ingots are cast, at least one sample shall be taken for each group of ingots cast simultaneously from the same source of molten metal. 7.2.2 When samples are taken from the finished or semifinished product, a sample shall be taken to represent each 2000 kg, or fraction thereof, of material in the lot, except that not more than one sample shall be required per piece. 7.3 Methods of Sampling—Samples for determination of chemical composition shall be taken in accordance with one of the following methods: 7.3.1 Samples for chemical analysis shall be taken by drilling, sawing, milling, turning, or clipping a representative piece or pieces to obtain a prepared sample of not less than 75 g. Sampling shall be in accordance with Practice E 55. 7.3.2 Sampling for spectrochemical analysis shall be in accordance with Practices E 716. Samples for other methods of analysis shall be suitable for the form of material being analyzed and the type of analytical method used.

10. Producer Confirmation of Heat-Treat Response 10.1 In addition to the requirements of 9.1, material in the O or F temper of alloys 2014, Alclad 2014, 2024, Alclad 2024, 11⁄2 % Alclad 2024, Alclad one side 2024, 11⁄2 % Alclad one side 2024, 6061, and Alclad 6061 shall, upon proper solution heat treatment and natural aging at room temperature, develop the properties specified in Table 3 for T42 temper material. The natural aging period at room temperature shall be not less than 4 days, but samples of material may be tested prior to 4 days aging, and if the material fails to conform to the requirements of T42 temper material, the tests may be repeated after completion of 4 days aging without prejudice. 10.2 Also, material in the O or F temper of alloys 2219, Alclad 2219, 7075, Alclad 7075, Alclad one-side 7075, 7008 Alclad 7075, 7178, and Alclad 7178 shall, upon proper solution heat treatment and precipitation heat treatment, develop the properties specified in Table 3 for T62 temper material. 10.3 Mill-produced material in the O or F temper of 7008 Alclad 7075 shall, upon proper solution heat treatment and stabilizing, be capable of attaining the properties specified in Table 3 for the T76 temper. 10.4 Number of Specimens—The number of specimens from each lot of O temper material and F temper material to be tested to verify conformance with 10.1-10.3 and shall be as specified in 9.2.

NOTE 4—It is difficult to obtain a reliable analysis of each of the components of clad materials using material in its finished state. A reasonably accurate determination of the core composition can be made if the cladding is substantially removed prior to analysis. The cladding composition is more difficult to determine because of the relatively thin layer and because of diffusion of core elements to the cladding. The correctness of cladding alloy used can usually be verified by a combination of metallographic examination and spectrochemical analysis of the surface at several widely separated points.

11. Heat Treatment and Reheat-Treatment Capability 11.1 Mill-produced material in the O or F temper of alloys 2014, Alclad 2014, 2024, Alclad 2024, 11⁄2 % Alclad 2024, Alclad one side 2024, 11⁄2 % Alclad one side 2024, 6061, and Alclad 6061 (without the subsequent imposition of cold work

7.4 Methods of Analysis—The determination of chemical composition shall be made in accordance with suitable chemical (Test Methods E 34), or spectrochemical (Test Methods E 607 and E 1251), methods. Other methods may be used only 4

NOTICE: This standard has either been superseded and replaced by a new version or discontinued. Contact ASTM International (www.astm.org) for the latest information. B 209M without cracking, the value of N being as prescribed in Table 2 for the different alloys, tempers, and thicknesses. The test need not be conducted unless specified on the purchase order. 12.2 Test Specimens—When bend tests are made, the specimens for sheet shall be the full thickness of the material, approximately 20 mm in width, and when practical, at least 150 mm in length. Such specimens may be taken in any direction and their edges may be rounded to a radius of approximately 2 mm. For sheet less than 20 mm in width, the specimens should be the full width of the material. 12.3 Test Methods—The bend tests shall be made in accordance with Test Method E 290 except as stated otherwise in 12.2.

or forming operations) shall, upon proper solution heat treatment and natural aging at room temperature, develop the properties specified in Table 3 for T42 temper material. The natural aging period at room temperature shall be not less than 4 days, but samples of material may be tested prior to 4 days aging, and if the material fails to conform to the requirements of T42 temper material, the tests may be repeated after completion of 4 days aging without prejudice. 11.2 Mill-produced material in the O or F temper of alloys 2219, Alclad 2219, 7075, Alclad 7075, Alclad one-side 7075, 7008 Alclad 7075, 7178, and Alclad 7178 (without the subsequent imposition of cold work or forming operations) shall, upon proper solution heat treatment and precipitation heat treatment, develop the properties specified in Table 3 for T62 temper material. 11.3 Mill-produced material in the O or F temper of 7008 Alclad 7075 (without the subsequent imposition of cold work or forming operations) shall, upon proper solution heat treatment and stabilizing, be capable of attaining the properties specified in Table 3 for the T76 temper. 11.4 Mill-produced material in the following alloys and tempers shall after proper resolution heat treatment and natural aging for 4 days at room temperature, be capable of attaining the properties specified in Table 3 for the T42 temper. Alloys 2014 and Alclad 2014 2024 and Alclad 2024 11⁄2 % Alclad 2024, Alclad one side 2024 and 11⁄2 % Alclad on side 2024

13. Stress-Corrosion Resistance 13.1 When specified on the purchase order or contract, alloy 2124-T851 plate shall be subjected to the test specified in 13.3 and shall exhibit no evidence of stress-corrosion cracking. One sample shall be taken from each parent plate in each lot and a minimum of three adjacent replicate specimens from this sample shall be tested. The producer shall maintain records of all lot acceptance test results and make them available for examination at the producer’s facility. 13.2 Alloy 7075 in the T73-type and T76-type tempers, and alloys Alclad 7075, 7008 Alclad 7075, 7178, and Alclad 7178 in the T76-type tempers, shall be capable of exhibiting no evidence of stress-corrosion cracking when subjected to the test specified in 13.3. 13.2.1 For lot-acceptance purposes, resistance to stresscorrosion cracking for each lot of material shall be established by testing the previously selected tension-test samples to the criteria shown in Table 4. 13.2.2 For surveillance purposes, each month the producer shall perform at least one test for stress-corrosion resistance in accordance with 13.3 on each applicable alloy-temper for each thickness range 20.00 mm and over listed in Table 3, produced that month. Each sample shall be taken from material considered acceptable in accordance with lot-acceptance criteria of Table 4. A minimum of three adjacent replicate specimens shall be taken from each sample and tested. The producer shall maintain records of all lots so tested and make them available for examination at the producer’s facility. 13.3 The stress-corrosion cracking test shall be performed on plate 20.00 mm and over in thickness as follows: 13.3.1 Specimens shall be stressed in tension in the short transverse direction with respect to grain flow and held at constant strain. For alloy 2124-T851, the stress levels shall be 50 % of the specified minimum long transverse yield strength. For T73-type tempers, stress level shall be 75 % of the specified minimum yield strength and for T76-type it shall be 170 MPa. 13.3.2 The stress-corrosion test shall be made in accordance with Test Method G 47. 13.3.3 There shall be no visual evidence of stress-corrosion cracking in any specimen, except that the retest provisions of 19.2 shall apply.

Tempers T3, T4, T451, T6, T651 T3, T4, T351, T81, T851 T3, T351, T81, T851

NOTE 5—Beginning with the 1974 revision of Specification B 209, 6061 and Alclad 6061 T4, T451, T6, and T651 were deleted from this paragraph because experience has shown that reheat treated material may develop large recrystallized grains and may fail to develop the tensile properties shown in Table 3.

11.5 Mill-produced material in the following alloys and tempers shall, after proper resolution heat treatment and precipitation heat treatment, be capable of attaining the mechanical properties specified in Table 3 for the T62 temper. Alloys 2219 and Alclad 2219 7075 Alclad 7075, 7008 Alclad 7075, 7178, and Alclad 7178 Alclad one-side 7075

Tempers T31, T351, T81, T851 T6, T651, T73, T7351, T76, T7651 T6, T651, T76, T7651 T6, T651

11.6 Mill-produced material in the following alloys and tempers and T42 temper material shall, after proper precipitation heat treatment, be capable of attaining the properties specified in Table 3 for the aged tempers listed below. Alloy and Temper 2014 and Alclad 2014-T3, T4, T42, T451 2024, Alclad 2024, 11⁄2 % Alclad 2024, Alclad one side 2024 and 11⁄2 % Alclad one side 2024-T3, T351, T361, T42 2219 and Alclad 2219-T31, T351, T37 6061 and Alclad 6061-T4, T451, T42

Temper after Aging T6, T6, T62, T651, respectively T81, T851, T861, T62 or T72, respectively

T81, T851, T87, respectively T6, T651, T62, respectively

12. Bend Properties 12.1 Limits—Sheet and plate shall be capable of being bent cold through an angle of 180 deg around a pin having a diameter equal to N times the thickness of the sheet or plate

14. Exfoliation-Corrosion Resistance 14.1 Alloys 5083, 5086, and 5456 in the H116 temper shall 5

NOTICE: This standard has either been superseded and replaced by a new version or discontinued. Contact ASTM International (www.astm.org) for the latest information. B 209M tance for each alloy for each thickness range listed in Table 3, produced that month. The samples for test shall be selected at random from material considered acceptable in accordance with the lot-acceptance criteria of Table 4. The producer shall maintain records of all surveillance test results and make them available for examination. 14.3 The test for exfoliation-corrosion resistance shall be made in accordance with Test for Exfoliation Corrosion Susceptibility in 7XXX Series Copper Containing Aluminum Alloys (EXCO Test) (G 34-72)13 and the following: 14.3.1 The specimens shall be a minimum of 50 mm by 100 mm with the 100-mm dimension in a plane parallel to the direction of final rolling. They shall be full-section thickness specimens of the material except that for material 2.5 mm or more in thickness, 10 % of the thickness shall be removed by machining one surface. The cladding of alclad sheet of any thickness shall be removed by machining the test surface; the cladding on the back side (nontest surface) of the specimen for any thickness of alclad material shall also either be removed or masked off. For machined specimens, the machined surface shall be evaluated by exposure to the test solution.

be capable of exhibiting no evidence of exfoliation corrosion when subjected to the test described in Method G 66. 14.1.1 For lot-acceptance purposes, the acceptability of each lot of material in the alloys and temper listed in 14.1 shall be determined by the producer by metallographic examination of one sample per lot selected from midsection at one end of a random sheet or plate. The microstructure of the sample from each production lot shall be compared to that of a producerestablished reference photomicrograph of acceptable material in the same thickness range which is characterized by being predominantly free of a continuous grain boundary network of aluminum-magnesium (Mg2Al3) precipitate. A reference photomicrograph taken at 5003 shall be established for each of the thickness ranges shown in Table 2 in which materials are produced and shall be taken from a sample within that thickness range. A longitudinal section perpendicular to the rolled surface shall be prepared for metallographic examination (see Methods E 3, symbol E in Fig. 1) and shall be microetched for metallographic examination using 40 % phosphoric acid etch for 3 min at 35°C or using etchant No. 6 in accordance with Test Methods E 407, Table 2, for 2 min. The metallographic examination shall be conducted at 5003 magnification. If the microstructure shows evidence of aluminummagnesium precipitate in excess of the producer-established reference photomicrograph of acceptable material, the lot is either rejected or tested for exfoliation-corrosion resistance in accordance with 14.1. The sample for corrosion test should be selected in the same manner specified for metallographic tests and shall be taken from the same sheet or plate used for metallographic test. Specimens prepared from the sample shall be full section thickness except that for material 2.5 mm or more in thickness, 10 % of the thickness shall be removed, by machining, from one as-rolled surface. Both the machined surface and the remaining as-rolled surface shall be evaluated after exposure to the test solution. Production practices shall not be changed after establishment of the reference micrograph except as provided in 14.1.3. 14.1.2 The producer shall maintain at the producing facility all records relating to the establishment of reference photomicrographs and production practices. 14.1.3 Significant changes in production practices that alter the microstructures of the alloy shall require qualification of the practice in accordance with 14.1.1. 14.2 Alloys 7075, Alclad 7075, 7008 Alclad 7075, 7178, and Alclad 7178, in the T76-type tempers, shall be capable of exhibiting no evidence of exfoliation corrosion equivalent to or in excess of that illustrated by Category B in Fig. 2 of Test for Exfoliation Corrosion Susceptibility in 7XXX Series Copper Containing Aluminum Alloys (EXCO Test) (G34-72)13 when subjected to the test in 14.3. 14.2.1 For lot-acceptance purposes, resistance to exfoliation corrosion for each lot of material in the alloys and tempers listed in 14.2 shall be established by testing the previously selected tension-test samples to the criteria shown in Table 4. 14.2.2 For surveillance purposes, each month the producer shall perform at least one test for exfoliation-corrosion resis13

15. Cladding 15.1 Preparatory to rolling alclad sheet and plate to the specified thickness, the aluminum or aluminum-alloy plates which are bonded to the alloy ingot or slab shall be of the composition shown in Table 1 and shall each have a thickness not less than that shown in Table 5 for the alloy specified. 15.2 When the thickness of the cladding is to be determined on finished material, not less than one transverse sample approximately 20 mm in length shall be taken from each edge and from the center width of the material. Samples shall be mounted to expose a transverse cross section and shall be polished for examination with a metallurgical microscope. Using 1003 magnification, the maximum and minimum cladding thickness on each surface shall be measured in each of five fields approximately 2.5 mm apart for each sample. The average of the ten values (five minima plus five maxima) on each sample surface is the average cladding thickness and shall meet the minimum average and, when applicable, the maximum average specified in Table 5. 16. Dimensional Tolerances 16.1 Thickness—The thickness of flat sheet, coiled sheet, and plate shall not vary from that specified by more than the respective permissible variations prescribed in Tables 3.1, 3.2, and 3.14 of ANSI H35.2M. Permissible variations in thickness of plate specified in thicknesses exceeding 160 mm shall be the subject of agreement between the purchaser and the producer or the supplier at the time the order is placed. 16.2 Length, Width, Lateral Bow, Squareness, and Flatness—Coiled sheet shall not vary in width or in lateral bow from that specified by more than the permissible variations prescribed in Tables 3.6 and 3.7, respectively, of ANSI H35.2M. Flat sheet and plate shall not vary in width, length, lateral bow, squareness, or flatness by more than the permissible variations prescribed in the following tables of ANSI H35.2M except that where the tolerances for sizes ordered are not covered by this standard the permissible variations shall be

The Aluminum Association, 900 19th St., NW, Washington, DC 20006.

6

NOTICE: This standard has either been superseded and replaced by a new version or discontinued. Contact ASTM International (www.astm.org) for the latest information. B 209M 19.2 When there is evidence that a failed specimen was not representative of the inspection lot and when no other sampling plan is provided or approved by the purchaser through the contract or purchase order, at least two additional specimens shall be selected to replace each test specimen that failed. All specimens so selected for retest shall meet the requirements of the specification or the lot shall be subject to rejection. 19.3 Material in which defects are discovered subsequent to inspection may be rejected. 19.4 If material is rejected by the purchaser, the producer or supplier is responsible only for replacement of the material to the purchaser. As much as possible of the rejected material shall be returned to the producer or supplier by the purchaser.

the subject of agreement between the purchaser and the producer or supplier at the time the order is placed: Table No. 3.3 3.4 3.5 3.8 3.9 3.12 3.13

Title width, sheared flat sheet and plate width and length, sawed flat sheet and plate length, sheared flat sheet and plate lateral bow, flat sheet and plate squareness, flat sheet and plate flatness, flat sheet flatness, sawed or sheared plate

16.3 Sampling for Inspection—Examination for dimensional conformance shall be made to ensure conformance to the tolerance specified. 17. Internal Quality 17.1 When specified by the purchaser at the time of placing the order, plate over 12.50 mm through 115.00 mm in thickness and up to a maximum mass of 1000 kg in alloys 2014, 2024, 2124, 2219, 7075, and 7178, both bare and alclad where applicable, shall be tested in accordance with Practice B 594 to the discontinuity acceptance limits of Table 6. 17.2 When specified by the purchaser at the time of placing the order, plate over 12.50 mm in thickness for ASME pressure vessel applications in alloys 1060, 1100, 3003, Alclad 3003, 3004, Alclad 3004, 5052, 5083, 5086, 5154, 5254, 5454, 5456, 5652, 6061, and Alclad 6061 shall be tested in accordance with Method B 548. In such cases the material will be subject to rejection if the following limits are exceeded unless it is determined by the purchaser that the area of the plate containing significant discontinuities will be removed during the subsequent fabrication process or that the plate may be repaired by welding. 17.2.1 If the longest dimension of the marked area representing a discontinuity causing a complete loss of back reflection (95 % or greater) exceeds 25 mm. 17.2.2 If the length of the marked area representing a discontinuity causing an isolated ultrasonic indication without a complete loss of back reflection (95 % or greater) exceeds 25 mm. 17.2.3 If each of two marked areas representing two adjacent discontinuities causing isolated ultrasonic indications without a complete loss of back reflection (95 % or greater) is longer than 25 mm, and if they are located within 75 mm of each other.

20. Identification Marking of Product 20.1 When specified on the purchase order or contract, all sheet and plate shall be marked in accordance with Practice B 666/B 666M. 20.2 In addition, alloys in the 2000 and 7000 series in the T6, T651, T73, T7351, T76, T7651, or T851 tempers shall be marked with the lot number in at least one location on each piece. 20.3 The requirements specified in 20.1 and 20.2 are minimum; marking systems that involve added information, larger characters, and greater frequencies are acceptable under this specification. 21. Packaging and Package Marking 21.1 The material shall be packaged to provide adequate protection during normal handling and transportation and each package shall contain only one size, alloy and temper of material unless otherwise agreed. The type of packaging and gross mass of containers shall, unless otherwise agreed, be at the producer’s or supplier’s discretion, provided that they are such as to ensure acceptance by common or other carriers for safe transportation at the lowest rate to the delivery point. 21.2 Each shipping container shall be marked with the purchase order number, material size, specification number, alloy and temper, gross and net masses, and the producer’s name or trademark. 21.3 When specified in the contract or purchase order, material shall be preserved, packaged, and packed in accordance with the requirements of Practices B 660. The applicable levels shall be as specified in the contract or order.

18. Source Inspection 18.1 If the purchaser desires that his representative inspect or witness the inspection and testing of the material prior to shipment, such agreement shall be made by the purchaser and producer as part of the purchase contract. 18.2 When such inspection or witness of inspection and testing is agreed upon, the producer shall afford the purchaser’s representative all reasonable facilities to satisfy him that the material meets the requirements of this specification. Inspection and tests shall be conducted so there is no unnecessary interference with the producer’s operations.

22. Certification 22.1 The producer or supplier shall, on request, furnish to the purchaser a certificate stating that each lot has been sampled, tested, and inspected in accordance with this specification, and has met the requirements. 23. Keywords

19. Retest and Rejection 19.1 If any material fails to conform to all of the applicable requirements of this specification, it shall be cause for rejection of the inspection lot.

23.1 aluminum alloy; aluminum-alloy plate; aluminumalloy sheet

7

NOTICE: This standard has either been superseded and replaced by a new version or discontinued. Contact ASTM International (www.astm.org) for the latest information. B 209M TABLE 2 Mechanical Property Limits for Nonheat-Treatable AlloysA,B Specified Thickness, mm

Tensile Strength, MPa

Yield Strength (0.2 % offset), MPa

Elongation, min, %C

max

in 50 mm

in 5 3 Diameter (5.65 =A!

Bend Diameter Factor, N

... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ...

15 18 23 25 25 6 7 12 12 1 2 6 10 10 1 2 4 5 1 2 3 4 10 ... ... ...

... ... ... ... 22 ... ... ... 10 ... ... ... ... 9 ... ... ... ... ... ... ... ... ... 18 22 ...

... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ...

... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ...

15 17 22 30 28 3 5 8 10 10 1 2 3 5 7 7 1 2 3 4 1 1 2 4 9 ... ... ...

... ... ... ... 25 ... ... ... 9 9 ... ... ... ... 6 6 ... ... ... ... ... ... ... ... ... 12 18 ...

0 0 0 0 0 0 0 0 0 ... 0 0 0 0 0 ... 4 4 4 4 ... ... ... ... ... ... ... ...

... ... ... ... ... ... ... ... ... ... ...

14 20 22 25 23 3 4 6 9 1 2

... ... ... ... 21 ... ... ... 8 ... ...

0 0 0 0 ... 0 0 0 ... 0 0

Temper over

through

min

max

0.15 0.32 0.63 1.20 6.30 0.40 0.63 1.20 6.30 0.20 0.32 0.63 1.20 6.30 0.15 0.32 0.63 1.20 0.15 0.32 0.63 1.20 6.30 12.50 40.00 6.30

0.32 0.63 1.20 6.30 80.00 0.63 1.20 6.30 50.00 0.32 0.63 1.20 6.30 25.00 0.32 0.63 1.20 4.00 0.32 0.63 1.20 3.20 12.50 40.00 80.00 80.00

55 55 55 55 55 75 75 75 75 85 85 85 85 85 95 95 95 95 110 110 110 110 75 70 60 ...

95 95 95 95 95 110 110 110 110 120 120 120 120 120 130 130 130 130 ... ... ... ... ... ... ... ...

0.15 0.32 0.63 1.20 6.30 0.40 0.63 1.20 6.30 12.50 0.20 0.32 0.63 1.20 6.30 12.50 0.15 0.32 0.63 1.20 0.15 0.32 0.63 1.20 6.30 12.50 40.00 6.30

0.32 0.63 1.20 6.30 80.00 0.63 1.20 6.30 12.50 50.00 0.32 0.63 1.20 6.30 12.50 25.00 0.32 0.63 1.20 4.00 0.32 0.63 1.20 3.20 12.50 40.00 80.00 80.00

75 75 75 75 75 95 95 95 95 95 110 110 110 110 110 110 130 130 130 130 150 150 150 150 90 85 80 ...

105 105 105 105 105 130 130 130 130 130 145 145 145 145 145 145 165 165 165 165 ... ... ... ... ... ... ... ...

0.15 0.32 0.63 1.20 6.30 0.40 0.63 1.20 6.30 0.20 0.32

0.32 0.63 1.20 6.30 80.00 0.63 1.20 6.30 50.00 0.32 0.63

95 95 95 95 95 120 120 120 120 140 140

130 130 130 130 130 160 160 160 160 180 180

min Aluminum 1060

0

H12D or H22D H14D or H24D

H16D or H26D H18D or H28D H112

FE

15 15 15 15 15 60 60 60 60 70 70 70 70 70 75 75 75 75 85 85 85 85 ... ... ... ... Aluminum 1100

O

H12D or H22D

H14D or H2D

H16D or H26D H18D or H28D H112

FE

25 25 25 25 25 75 75 75 75 75 95 95 95 95 95 95 115 115 115 115 ... ... ... ... 50 40 30 ... Alloy 3003

O

H12D or H22D H14D or

35 35 35 35 35 85 85 85 85 115 115

8

NOTICE: This standard has either been superseded and replaced by a new version or discontinued. Contact ASTM International (www.astm.org) for the latest information. B 209M TABLE 2 Continued Specified Thickness, mm

Tensile Strength, MPa

Yield Strength (0.2 % offset), MPa

Elongation, min, %C

over

through

min

max

min

max

in 50 mm

in 5 3 Diameter (5.65 =A!

Bend Diameter Factor, N

0.63 1.20 3.20 6.30 0.15 0.32 0.63 1.20 0.15 0.32 0.63 1.20 6.30 12.50 40.00 6.30

1.20 3.20 6.30 25.00 0.32 0.63 1.20 4.00 0.32 0.63 1.20 3.20 12.50 40.00 80.00 80.00

140 140 140 140 165 165 165 165 185 185 185 185 115 105 100 ...

180 180 180 180 205 205 205 205 ... ... ... ... ... ... ... ...

115 115 115 115 145 145 145 145 165 165 165 165 70 40 40 ...

... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ...

3 5 5 8 1 2 3 4 1 1 2 4 8 ... ... ...

... ... ... 7 ... ... ... ... ... ... ... ... ... 10 16 ...

0 0 2 ... 4 4 4 6 ... ... ... ... ... ... ... ...

... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ...

14 20 22 25 23 ... 4 5 6 9 ... 1 2 3 5 8 ... 1 2 3 4 1 1 2 4 8 ... ... ...

... ... ... ... ... 21 ... ... ... ... 8 ... ... ... ... ... 7 ... ... ... ... ... ... ... ... ... 10 16 ...

... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ...

... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ...

9 12 15 18 16 1 3 5 5 6 1 2 3 4 4 5 1 2 3 4 ... 1

... ... ... ... 14 ... ... ... ... 5 ... ... ... ... ... 4 ... ... ... ... ... ...

0 0 0 0 ... 0 1 2 ... ... 2 2 3 4 ... ... 6 6 6 8 ... ...

Temper

H24D

H16D or H26D H18D or H28D H112

FF

Alclad Alloy 3003 O

H12D or H22D

H14D or H24D

H16D or H26D H18

H112

FE

0.15 0.32 0.63 1.20 6.30 12.50 0.40 0.63 1.20 6.30 12.50 0.20 0.32 0.63 1.20 6.30 12.50 0.15 0.32 0.63 1.20 0.15 0.32 0.63 1.20 6.30 12.50 40.00 6.30

0.32 0.63 1.20 6.30 12.50 80.00 0.63 1.20 6.30 12.50 50.00 0.32 0.63 1.20 6.30 12.50 25.00 0.32 0.63 1.20 4.00 0.32 0.63 1.20 3.20 12.50 40.00 80.00 80.00

90 90 90 90 90 95F 115 115 115 115 120F 135 135 135 135 135 140F 160 160 160 160 180 180 180 180 110 105F 100F ...

125 125 125 125 125 130F 155 155 155 155 160F 175 175 175 175 175 180F 200 200 200 200 ... ... ... ... ... ... ... ...

0.15 0.32 0.63 1.20 6.30 0.40 0.63 1.20 3.20 6.30 0.20 0.32 0.63 1.20 3.20 6.30 0.15 0.32 0.63 1.20 0.15 0.32

0.32 0.63 1.20 6.30 80.00 0.63 1.20 3.20 6.30 50.00 0.32 0.63 1.20 3.20 6.30 25.00 0.32 0.63 1.20 4.00 0.32 0.63

150 150 150 150 150 190 190 190 190 190 220 220 220 220 220 220 240 240 240 240 260 260

200 200 200 200 200 240 240 240 240 240 265 265 265 265 265 265 285 285 285 285 ... ...

30 30 30 30 30 35F 80 80 80 80 85F 110 110 110 110 110 115F 140 140 140 140 ... ... ... ... 65 40F 40F ... Alloy 3004

O

H32D or H22D

H34D or H24D

H36D or H26D H38D or

60 60 60 60 60 145 145 145 145 145 170 170 170 170 170 170 190 190 190 190 215 215

9

NOTICE: This standard has either been superseded and replaced by a new version or discontinued. Contact ASTM International (www.astm.org) for the latest information. B 209M TABLE 2 Continued Specified Thickness, mm

Tensile Strength, MPa

Yield Strength (0.2 % offset), MPa

Elongation, min, %C

over

through

min

max

min

max

in 50 mm

in 5 3 Diameter (5.65 =A!

Bend Diameter Factor, N

0.63 1.20 6.30 12.50 40.00 6.30

1.20 3.20 12.50 40.00 80.00 80.00

260 260 160 160 160 ...

... ... ... ... ... ...

215 215 60 60 60 ...

... ... ... ... ... ...

2 4 7 ... ... ...

... ... ... 6 6 ...

... ... ... ... ... ...

0.15 0.32 0.63 1.20 6.30 12.50 0.40 0.63 1.20 6.30 12.50 0.20 0.32 0.63 1.20 6.30 12.50 0.15 0.32 0.63 1.20 0.15 0.32 0.63 1.20 6.30 12.50 40.00 6.30

0.32 0.63 1.20 6.30 12.50 80.00 0.63 1.20 6.30 12.50 50.00 0.32 0.63 1.20 6.30 12.50 25.00 0.32 0.63 1.20 4.00 0.32 0.63 1.20 3.20 12.50 40.00 80.00 80.00

145 145 145 145 145 150F 185 185 185 185 190F 215 215 215 215 215 220F 235 235 235 235 255 255 255 255 155 160F 160F ...

195 195 195 195 195 200F 235 235 235 235 240F 260 260 260 260 260 265F 280 280 280 280 ... ... ... ... .... ... ... ...

... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ...

9 12 15 18 16 ... 1 3 5 6 ... 1 2 3 4 5 ... 1 2 3 4 ... 1 2 4 7 ... ... ...

... ... ... ... ... 14 ... ... ... ... 5 ... ... ... ... ... 4 ... ... ... ... ... ... ... ... ... 6 6 ...

... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ...

... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ...

10 14 17 20 1 2 3 1 1 2 3 1 1 2 2 1 1 2 2 ... 1 1 1 1 2 3 4 1 2 3 4 1

... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ...

... ... ... ... ...

Temper

H28D H112

FE

Alclad Alloy 3004 O

H32D or H22D

H34D or H24D

H36D or H26D H38

H112

FE

55 55 55 55 55 60F 140 140 140 140 145F 165 165 165 165 165 170F 185 185 185 185 ... ... ... ... 55 60F 60F ... Alloy 3005

O

H12

H14

H16

H18

H19

H25

H27

H28

0.15 0.32 0.63 1.20 0.40 0.63 1.20 0.20 0.32 0.63 1.20 0.15 0.32 0.63 1.20 0.15 0.32 0.63 1.20 0.15 0.32 0.63 1.20 0.15 0.32 0.63 1.20 0.15 0.32 0.63 1.20 0.15

0.32 0.63 1.20 6.30 0.63 1.20 6.30 0.32 0.63 1.20 6.30 0.32 0.63 1.20 4.00 0.32 0.63 1.20 3.20 0.32 0.63 1.20 1.60 0.32 0.63 1.20 2.00 0.32 0.63 1.20 2.00 0.32

115 115 115 115 140 140 140 165 165 165 165 190 190 190 190 220 220 220 220 235 235 235 235 180 180 180 180 205 205 205 205 215

165 165 165 165 190 190 190 215 215 215 215 240 240 240 240 ... ... ... ... ... ... ... ... 235 235 235 235 260 260 260 260 ...

45 45 45 45 115 115 115 145 145 145 145 170 170 170 170 200 200 200 200 ... ... ... ... 150 150 150 150 175 175 175 175 185

10

... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ...

NOTICE: This standard has either been superseded and replaced by a new version or discontinued. Contact ASTM International (www.astm.org) for the latest information. B 209M TABLE 2 Continued Specified Thickness, mm

Tensile Strength, MPa

Yield Strength (0.2 % offset), MPa

Elongation, min, %C

over

through

min

max

min

max

in 50 mm

in 5 3 Diameter (5.65 =A!

Bend Diameter Factor, N

0.32 0.63 1.20 0.63 1.20

0.63 1.20 2.00 1.20 2.00

215 215 215 230 230

... ... ... ... ...

185 185 185 195 195

... ... ... ... ...

2 3 4 1 2

... ... ... ... ...

... ... ... ... ...

0.32 0.63 1.20 0.40 0.63 1.20 0.32 0.63 1.20 0.32 0.63 1.20 0.32 0.63 1.20 0.32 0.63 1.20

0.63 1.20 2.00 0.63 1.20 2.00 0.63 1.20 2.00 0.63 1.20 2.00 0.63 1.20 2.00 0.63 1.20 2.00

95 95 95 130 130 130 150 150 150 170 170 170 190 190 190 160 160 1.60

145 145 145 180 180 180 200 200 200 220 220 220 ... ... ... ... ... ...

..... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ...

16 19 20 1 2 3 1 2 2 1 1 2 1 1 2 2 4 6

... ... ... ... ... ... .... ... ... ... ... ... ... ... ... ... ... ...

... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ...

0.15 0.32 0.63 1.20 6.30 0.40 0.63 1.20 6.30 0.20 0.32 0.63 1.20 6.30 0.15 0.32 0.63 1.20 0.15 0.32 0.63 1.20 0.40 0.63 1.20 6.30 0.20 0.32 0.63 1.20 6.30 0.15 0.32 0.63 1.20 0.15 0.32 0.63 1.20 6.30 12.50 40.00 6.30

0.32 0.63 1.20 6.30 80.00 0.63 1.20 6.30 50.00 0.32 0.63 1.20 6.30 25.00 0.32 0.63 1.20 4.00 0.32 0.63 1.20 3.20 0.63 1.20 6.30 50.00 0.32 0.63 1.20 6.30 25.00 0.32 0.63 1.20 4.00 0.32 0.63 1.20 3.20 12.50 40.00 80.00 80.00

105 105 105 105 105 125 125 125 125 145 145 145 145 145 165 165 165 165 185 185 185 185 120 120 120 120 140 140 140 140 140 160 160 160 160 180 180 180 180 115 105 100 ...

145 145 145 145 145 165 165 165 165 185 185 185 185 185 205 205 205 205 ... ... ... ... 160 160 160 160 180 180 180 180 180 200 200 200 200 ... ... ... ... ... ... ... ...

... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ...

12 16 19 21 22 2 4 6 9 1 1 2 3 8 1 1 2 3 1 1 2 3 3 4 7 10 2 3 4 5 8 1 2 3 4 1 2 3 4 8 ... ... ...

... ... ... ... 20 ... ... ... 8 ... ... ... ... 7 ... ... ... ... ... ... ... ... ... ... ... 9 ... ... ... ... 7 ... ... ... ... ... ... ... ... ... 10 16 ...

... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ...

Temper

H29

Alloy 3105 O

H12

H14

H16

H18

H25

35 35 35 105 105 105 125 125 125 145 145 145 165 165 165 130 130 130 Alloy 5005

O

H12

H14

H16

H18

H32D or H22D H34D or H24D

H36D or H26D H38

H112

FE

35 35 35 35 35 95 95 95 95 115 115 115 115 115 135 135 135 135 ... ... ... ... 85 85 85 85 105 105 105 105 105 125 125 125 125 ... ... ... ... ... ... ... ...

11

NOTICE: This standard has either been superseded and replaced by a new version or discontinued. Contact ASTM International (www.astm.org) for the latest information. B 209M TABLE 2 Continued Specified Thickness, mm

Tensile Strength, MPa

Yield Strength (0.2 % offset), MPa

Elongation, min, %C

max

in 50 mm

in 5 3 Diameter (5.65 =A!

Bend Diameter Factor, N

... ... ... ... ...

3 2 1 1 ...

... ... ... ... ...

... ... ... ... ...

... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ...

15 17 19 20 20 4 5 6 3 3 4 5 2 2 3 4 1 2 3 4 12 ... ... ...

... ... ... ... 18 ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... 10 10 ...

0 0 0 0 2 1 1 2 1 1 1 3 3 3 3 4 ... ... ... ... ... ... ... ...

... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ...

13 15 17 19 18 4 5 7 7 11 3 3 4 6 6 10 2 3 4 4 2 3 4 4 7 ... ... ...

... ... ... ... 16 ... ... ... ... 10 ... ... ... ... ... 9 ... ... ... ... ... ... ... ... ... 10 14 ...

0 0 0 0 ... 0 1 2 3 ... 1 1 2 3 4 ... 4 4 5 5 ... ... ... ... ... ... ... ...

200 200 ... ... ... ...

16 16 ... ... ... 12

... 14 12 12 10 ...

... ... ... ... ... ...

Temper over

through

min

max

0.25 0.25 0.25 0.25 0.25

18.00 18.00 18.00 18.00 18.00

105 120 140 160 180

145 160 180 200 ...

0.15 0.32 0.63 1.20 6.30 0.40 0.63 1.20 0.20 0.32 0.63 1.20 0.15 0.32 0.63 1.20 0.15 0.32 0.63 1.20 6.30 12.50 40.00 6.30

0.32 0.63 1.20 6.30 80.00 0.63 1.20 6.30 0.32 0.63 1.20 6.30 0.32 0.63 1.20 4.00 0.32 0.63 1.20 3.20 12.50 40.00 80.00 80.00

125 125 125 125 125 150 150 150 170 170 170 170 185 185 185 185 200 200 200 200 140 140 140 ...

165 165 165 165 165 195 195 195 215 215 215 215 230 230 230 230 ... ... ... ... ... ... ... ...

0.15 0.32 0.63 1.20 6.30 0.40 0.63 1.20 3.20 6.30 0.20 0.32 0.63 1.20 3.20 6.30 0.15 0.32 0.63 1.20 0.15 0.32 0.63 1.20 6.30 12.50 40.00 6.30

0.32 0.63 1.20 6.30 80.00 0.63 1.20 3.20 6.30 50.00 0.32 0.63 1.20 3.20 6.30 25.00 0.32 0.63 1.20 4.00 0.32 0.63 1.20 3.20 12.50 40.00 80.00 80.00

170 170 170 170 170 215 215 215 215 215 235 235 235 235 235 235 255 255 255 255 270 270 270 270 190 170 170 ...

215 215 215 215 215 265 265 265 265 265 285 285 285 285 285 285 305 305 305 305 ... ... ... ... ... ... ... ...

1.25 6.30 80.00 120.00 160.00 6.30

6.30 80.00 120.00 160.00 200.00 12.50

275 270 260 255 250 275

350 345 ... ... ... ...

min Alloy 5010

O H22 H24 H26 H28

35 95 120 145 ... Alloy 5050

O

H32D or H22D H34D or H24D H36D or H26D H38

H112

FE

40 40 40 40 40 110 110 110 140 140 140 140 150 150 150 150 ... ... ... ... 55 55 55 ... Alloy 5052

O

H32D or H22D

H34D or H24D

H36D or H26D H38D or H28D

FE

65 65 65 65 65 160 160 160 160 160 180 180 180 180 180 180 200 200 200 200 220 220 220 220 110 65 65 ... Alloy 5083

O

H112

125 115 110 105 100 125

12

NOTICE: This standard has either been superseded and replaced by a new version or discontinued. Contact ASTM International (www.astm.org) for the latest information. B 209M TABLE 2 Continued Specified Thickness, mm

Tensile Strength, MPa

Yield Strength (0.2 % offset), MPa

Elongation, min, %C in 5 3 Diameter (5.65 =A!

Bend Diameter Factor, N

...

10 10 ... 10 10 ... 10 10 10 ...

... ... ... ... ... ... ... ... ... ...

... ... ... ... ... ... ... ... ... ... ... ... ... .. . ... ... ... ...

15 16 18 16 6 6 8 12 4 4 5 6 10 3 3 4 6 3

... ... ... 14 ... ... ... 10 ... ... ... ... 9 ... ... ... ... ...

... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ...

... ... ... ... ... ... ... ...

8 ... ... 8 10 ... ... ...

... 9 12 ... ... 9 9 ...

... ... ... ... ... ... ... ...

... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ...

12 13 16 18 5 6 8 12 4 4 5 6 10 3 3 4 4 3 3 3 4 8 ... ... ...

... ... ... 16 ... ... ... 10 ... ... ... ... 9 ... ... ... ... ... ... ... ... ... 9 13 ...

... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ...

... ...

10 9

... ...

... ...

Temper

H321

H116G

FE

over

through

min

max

min

max

in 50 mm

12.50 40.00 4.00 12.50 40.00 1.60 12.50 30.00 40.00 6.30

40.00 80.00 12.50 40.00 80.00 12.50 30.00 40.00 80.00 200.00

275 270 305 305 285 305 305 305 285 ...

... ... 385 385 385 ... ... ... ... ...

125 115 215 215 200 215 215 215 200 ...

... ... 295 295 295 ... ... ... ... ...

... ... 12 ... ... 10 ... ...

0.50 0.63 1.20 6.30 0.50 0.63 1.20 6.30 0.20 0.32 0.63 1.20 6.30 0.15 0.32 0.63 1.20 0.15

0.63 1.20 6.30 50.00 0.63 1.20 6.30 50.00 0.32 0.63 1.20 6.30 25.00 0.32 0.63 1.20 4.00 0.63

240 240 240 240 275 275 275 275 300 300 300 300 300 325 325 325 325 345

305 305 305 305 325 325 325 325 350 350 350 350 350 375 375 375 375 ...

95 95 95 95 195 195 195 195 235 235 235 235 235 260 260 260 260 285

4.00 12.50 40.00 1.60 6.30 12.50 30.00 6.30

12.50 40.00 80.00 6.30 12.50 30.00 50.00 80.00

250 240 235 275 275 275 275 ...

... ... ... ... ... ... ... ...

125 105 95 195 195 195 195 ...

0.50 0.63 1.20 6.30 0.50 0.63 1.20 6.30 0.20 0.32 0.63 1.20 6.30 0.15 0.32 0.63 1.20 0.15 0.32 0.63 1.20 6.30 12.50 40.00 6.30

0.63 1.20 6.30 80.00 0.63 1.20 6.30 50.00 0.32 0.63 1.20 6.30 25.00 0.32 0.63 1.20 4.00 0.32 0.63 1.20 3.20 12.50 40.00 80.00 80.00

205 205 205 205 250 250 250 250 270 270 270 270 270 290 290 290 290 310 310 310 310 220 210 205 ...

285 285 285 285 300 300 300 300 320 320 320 320 320 340 340 340 340 ... ... ... ... ... ... ... ...

0.63 0.63

2.50 2.50

205 215

260 270

Alloy 5086 O

H32D or H22D H34D or H24D

H36D or H26D H38D or H28D H112

H116G

FE

Alloy 5154 O

H32D or H22D H34D or H24D

H36D or H26D H38D or H28D H112

FE

75 75 75 75 180 180 180 180 200 200 200 200 200 220 220 220 220 240 240 240 240 125 90 75 ... Alloy 5252

H24 H25

... ...

13

NOTICE: This standard has either been superseded and replaced by a new version or discontinued. Contact ASTM International (www.astm.org) for the latest information. B 209M TABLE 2 Continued Specified Thickness, mm

Tensile Strength, MPa

Yield Strength (0.2 % offset), MPa

Elongation, min, %C

min

max

in 50 mm

in 5 3 Diameter (5.65 =A!

Bend Diameter Factor, N

...

...

3

...

...

... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ...

12 13 16 18 5 6 8 12 4 4 5 6 10 3 3 4 4 3 3 3 4 8 ... ... ...

... ... ... 16 ... ... ... 10 ... ... ... ... 9 ... ... ... ... ... ... ... ... ... 9 13 ...

... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ...

... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ...

12 13 16 18 5 6 8 12 4 5 6 10 8 ... ... ...

... ... ... 16 ... ... ... 10 ... ... ... 9 ... 9 13 ...

... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ...

Temper over H28

0.63

through

min

max

2.50

260

...

Alloy 5254 O

H32D or H22D H34D or H24D

H36D or H26D H38D or H28D H112

FE

0.50 0.63 1.20 6.30 0.50 0.63 1.20 6.30 0.20 0.32 0.63 1.20 6.30 0.15 0.32 0.63 1.20 0.15 0.32 0.63 1.20 6.30 12.50 40.00 6.30

0.63 1.20 6.30 80.00 0.63 1.20 6.30 50.00 0.32 0.63 1.20 6.30 25.00 0.32 0.63 1.20 4.00 0.32 0.63 1.20 3.20 12.50 40.00 80.00 80.00

205 205 205 205 250 250 250 250 270 270 270 270 270 290 290 290 290 310 310 310 310 220 210 205 ...

285 285 285 285 300 300 300 300 320 320 320 320 320 340 340 340 340 ... ... ... ... ... ... ... ...

75 75 75 75 180 180 180 180 200 200 200 200 200 220 220 220 220 240 240 240 240 125 90 75 ...

0.50 0.63 1.20 6.30 0.50 0.63 1.20 6.30 0.50 0.63 1.20 6.30 6.30 12.50 40.00 6.30

0.63 1.20 6.30 80.00 0.63 1.20 6.30 50.00 0.63 1.20 6.30 25.00 12.50 40.00 80.00 80.00

215 215 215 215 250 250 250 250 270 270 270 270 220 215 215 ...

285 285 285 285 305 305 305 305 325 325 325 325 ... ... ... ...

0.75

1.40

200

270

80

...

17

...

...

1.40

2.20

200

270

80

...

18

...

...

2.20

3.50

200

270

80

...

19

...

...

205 205 ... ... ... ... ... ... ... ... ... ... ... 315 305 295

16 16 ... ... ... 12 ... ... 10 ... ... ... ... 12 ... ...

... 14 12 12 10 ... 10 10 ... 10 10 10 10 ... 10 10

... ... ... ... ... ... ... ... ... ... ... ... ... .... ... ...

Alloy 5454 O

H32D or H22D H34D or H24D H112

FE

85 85 85 85 180 180 180 180 200 200 200 200 125 85 85 ... Alloy 5754

O

Alloy 5456 O

H112

H116G

H321

1.25 6.30 80.00 120.00 160.00 6.30 12.50 40.00 1.60 12.50 30.00 40.00 80.00 4.00 12.50 40.00

6.30 80.00 120.00 160.00 200.00 12.50 40.00 80.00 12.50 30.00 40.00 80.00 110.00 12.50 40.00 80.00

290 285 275 270 265 290 290 285 315 315 305 285 275 315 305 285

365 360 ... ... ... ... ... ... ... ... ... ... ... 405 385 370

130 125 120 115 105 130 130 125 230 230 215 200 170 230 215 200

14

NOTICE: This standard has either been superseded and replaced by a new version or discontinued. Contact ASTM International (www.astm.org) for the latest information. B 209M TABLE 2 Continued Specified Thickness, mm

Tensile Strength, MPa

Yield Strength (0.2 % offset), MPa

Elongation, min, %C

min

max

in 50 mm

in 5 3 Diameter (5.65 =A!

Bend Diameter Factor, N

...

...

...

...

...

...

20

...

...

... ... ... ... ... ... ... ... ... ... ... ...

19 18 7 7 11 6 6 10 7 ... ... ...

... 16 ... ... 10 ... ... 9 ... 10 14 ...

0 ... 2 3 ... 3 4 ... ... ... ... ...

... ... ... ...

13 8 7 5

... ... ... ...

... ... ... ...

Temper

FE

over

through

min

max

6.30

200.00

...

...

Alloy 5457 O

0.63

2.50

110

150

... Alloy 5652

O H32D or H22D H34D or H24D H112

FE

1.20 6.30 1.20 3.20 6.30 1.20 3.20 6.30 6.30 12.50 40.00 6.30

6.30 80.00 3.20 6.30 50.00 3.20 6.30 25.00 12.50 40.00 80.00 80.00

170 170 215 215 215 235 235 235 190 170 170 ...

215 215 265 265 265 285 285 285 ... ... ... ...

0.63 0.63 0.63 0.63

2.50 2.50 2.50 2.50

125 140 150 170

180 195 205 ...

65 65 160 160 160 180 180 180 110 65 65 ... Alloy 5657

H241H H25 H26 H28

... ... ... ...

A To determine conformance to this specification each value for tensile strength and for yield strength shall be rounded to the nearest 1 MPa and each value for elongation to the nearest 0.5 %, both in accordance with the rounding method of Practice E 29. B The basis for establishment of mechanical property limits is shown in Annex A1. C Elongations in 50 mm apply for thicknesses up through 12.50 mm and in 5 3 diameter (5.65 =A ) for thicknesses over 12.50 mm where A is the cross-sectional area of the specimen. D Materials in either of these tempers (H32 or H22), (H34 or H24), (H36 or H26), (H38 or H28), (H12 or H22), (H14 or H24), (H16 or H26), (H18 or H28), may be supplied at the option of the supplier, unless one is specifically excluded by the contract or purchase order. When ordered as H2x tempers, the maximum tensile strength and minimum yield strength do not apply. When H2x tempers are supplied instead of ordered H1x or H3x tempers, the supplied H2x temper material shall meet the respective H1x or H3x temper tensile property limits. E Tests of F temper plate for tensile properties are not required. F The tension test specimen from plate over 12.50 mm in thickness is machined from the core and does not include the cladding alloy. G The -H116 temper designation now also applies to products previously designated -H117. H This material is subject to some recrystallization and an attendant loss of brightness.

15

NOTICE: This standard has either been superseded and replaced by a new version or discontinued. Contact ASTM International (www.astm.org) for the latest information. B 209M TABLE 3 Tensile Property Limits for Heat-Treatable AlloysA,B Specified Thickness, mm

Tensile Strength, MPa

Yield Strength (0.2 % offset), MPa

Elongation,C min, %

min

max

in 50 mm

in 5 3 Diameter (5.65 =A!

... ... 240 250 240 250 250 250 250 235 235 395 400 405 405 405 400 395 380 ...

110 ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ...

16 ... 14 14 14 14 ... ... ... 14 ... 6 7 7 ... ... ... ... ... ...

... 9 ... ... ... ... 12 10 7 ... 12 ... ... ... 5 3 1 1 ... ...

... ... ... ... ... 230 235 240 240 215 220 235 235 250 250H 250H 250H 215 220 235 235 235H 370 380 395 395 395 405H 40H 400H 395H 380H ...

95 95 95 95 ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ...

16 16 16 16 ... 14 14 15 15 14 14 15 15 15 ... ... ... 14 14 15 15 ... 7 7 8 8 8 ... ... ... ... ... ...

... ... ... ... 9 ... ... ... ... ... ... ... ... ... 12 10 7 ... ... ... ... 12 ... ... ... ... ... 5 3 1 1 ... ...

... ... 290 290 290 290 290 290 290 290 290 285

95 ... ... ... ... ... ... ... ... ... ... ...

12 ... 10 12 15 15 12 ... ... ... ... ...

... 10 ... ... ... ... ... 7 6 5 3 3

Temper over

through

min

0.50 12.50 0.50 1.00 0.50 6.30 12.50 25.00 50.00 0.50 12.50 0.50 1.00 6.30 12.50 25.00 50.00 60.00 80.00 6.30

12.50 25.00 1.00 6.30 6.30 12.50 25.00 50.00 80.00 12.50 25.00 1.00 6.30 12.50 25.00 50.00 60.00 80.00 100.00 25.00

... ... 405 405 405 400 400 400 395 400 400 440 455 460 460 460 450 435 405 ...

0.50 0.63 1.00 2.50 12.50 0.50 0.63 1.00 2.50 0.50 0.63 1.00 2.50 6.30 12.50 25.00 50.00 0.50 0.63 1.00 2.50 12.50 0.50 0.63 1.00 2.50 6.30 12.50 25.00 50.00 60.00 80.00 6.30

0.63 1.00 2.50 12.50 25.00 0.63 1.00 2.50 6.30 0.63 1.00 2.50 6.30 12.50 25.00 50.00 80.00 0.63 1.00 2.50 12.50 25.00 0.63 1.00 2.50 6.30 12.50 25.00 50.00 60.00 80.00 100.00 25.00

... ... ... ... ... 370 380 395 395 370 380 395 395 395 400H 400H 395H 370 380 395 395 400H 425 435 440 440 440 460H 460H 450H 435H 405H ...

0.24 12.50 0.19 0.25 0.50 3.20 6.30 12.50 25.00 40.00 50.00 80.00

12.50 45.00 0.25 0.50 3.20 6.30 12.50 25.00 40.00 50.00 80.00 100.00

... ... 435 435 435 435 440 435 425 425 415 395

max Alloy 2014

O T3 T4D T451E

T42F T6, T62F T6F, T651E

FG

220 220 ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... Alclad Alloy 2014

O

T3

T4E

T451E

T42F

T6, T62F

T62F, T651E

FG

205 205 205 205 220H ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... Alloy 2024

O T3

T351E

220 220 ... ... ... ... ... ... ... ... ... ...

16

NOTICE: This standard has either been superseded and replaced by a new version or discontinued. Contact ASTM International (www.astm.org) for the latest information. B 209M TABLE 3 Continued Specified Thickness, mm

Tensile Strength, MPa

Yield Strength (0.2 % offset), MPa

Elongation,C min, %

over

through

min

max

min

max

in 50 mm

in 5 3 Diameter (5.65 =A!

0.50 1.60 6.30 12.50 0.24 0.50 0.24 0.50 6.30 12.50 25.00 40.00 50.00 0.24 12.50 0.24 0.24 6.30 12.50 25.00 0.50 1.60 6.30 12.50 6.30

1.60 6.30 12.50 12.70 0.50 6.30 0.50 6.30 12.50 25.00 40.00 50.00 80.00 12.50 80.00 6.30 6.30 12.50 25.00 40.00 1.60 6.30 12.50 12.70 80.00

460 470 455 455 425 425 425 425 425 420 415 415 400 440 435 415 460 460 455 455 480 490 480 480 ...

... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ...

345 350 340 340 275 275 260 260 260 260 260 260 260 345 345 315 400 400 400 395 425 455 440 440 ...

... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... .... ... ... ... ... ... ... ...

8 9 9 ... 12 15 12 15 12 ... ... ... ... 5 ... 5 5 5 ... ... 3 4 4 ... ...

... ... ... 9 ... ... ... ... ... 7 6 5 3 ... 4 ... ... ... 4 4 ... ... ... 3 ...

... ... ... ... 270 270 270 275 275 275 290H 290H 290H 290H 285H 325 330 330 340H 245 245 260 235 235 235 250 250 260H 260H 260H 260H 325 335 295 310 370 385 385 400H 400 440 425 440H ...

95 95 95 ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ...

10 12 12 ... 10 12 15 15 15 12 ... ... ... ... ... 8 9 9 ... 12 15 15 10 12 15 15 12 ... ... ... ... 5 5 5 5 5 5 5 ... 3 4 4 ... ...

... ... ... 10 ... ... ... ... ... ... 7 6 5 3 3 ... ... ... 9 ... ... ... ... ... ... ... ... 7 6 5 3 ... ... ... ... ... ... ... 4 ... ... ... 3 ...

Temper

T361

T4D T42F

T62F T72F,I T81 T851E

T861

FG

Alclad Alloy 2024 O

T3

T351E

T361

T4D

T42F

T62F T72F,I T81 T851E T861

FG

0.19 0.25 1.60 12.50 0.19 0.25 0.50 1.60 3.20 6.30 12.50 25.00 40.00 50.00 80.00 0.50 1.60 6.30 12.50 0.24 0.50 1.60 0.19 0.25 0.50 1.60 6.30 12.50 25.00 40.00 50.00 0.24 1.60 0.24 1.60 0.24 1.60 6.30 12.50 0.50 1.60 6.30 12.50 6.30

0.25 1.60 12.50 45.00 0.25 0.50 1.60 3.20 6.30 12.50 25.00 40.00 50.00 80.00 100.00 1.60 6.30 12.50 12.70 0.50 1.60 3.20 0.25 0.50 1.60 6.30 12.50 25.00 40.00 50.00 80.00 1.60 12.50 1.60 6.30 1.60 6.30 12.50 25.00 1.60 6.30 12.50 12.70 80.00

... ... ... ... 400 405 405 420 420 425 435H 425H 425H 415H 395H 420 440 440 455H 400 400 420 380 395 395 415 415 420H 415H 415H 400H 415 425 385 400 425 445 445 455H 440 475 470 480H ...

205 205 220 220H ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ...

17

NOTICE: This standard has either been superseded and replaced by a new version or discontinued. Contact ASTM International (www.astm.org) for the latest information. B 209M TABLE 3 Continued Specified Thickness, mm

Tensile Strength, MPa

Yield Strength (0.2 % offset), MPa

Elongation,C min, %

min

max

in 50 mm

in 5 3 Diameter (5.65 =A!

... ... 285 285 290H 290H 290H 290H 285H 340 330 340H 255 255 260H 260H 260H 260H 340 310 395 395 400H 450 435 440H ...

95 ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ...

12 ... 15 12 ... ... ... ... ... 9 9 ... 15 12 ... ... ... ... 5 5 5 5 ... 4 4 ... ...

... 10 ... ... 7 6 5 3 3 ... ... 9 ... ... 7 6 5 3 ... ... ... ... 4 ... ... 3 ...

... ... ... 275 275 285 285 285 330 340 330 240 250 255 255 330 340 305 310 385 395 395 415 450 435 ...

95 95 95 ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ...

10 12 12 12 15 15 15 12 8 9 9 12 15 15 12 5 5 5 5 5 5 5 3 4 4 ...

... ... ... ... ... ... ... ... ... ... ... ... ... ... ... .... ... ... ... ... ... ... ... ... ... ...

Temper over

through

min

max 11⁄2 % Alclad Alloy 2024

O T3 T351E

T361

T42F

T62F T72F,I T81 T851E T861

FG

4.00 12.50 4.00 6.30 12.50 25.00 40.00 50.00 80.00 4.00 6.30 12.50 4.00 6.30 12.50 25.00 40.00 50.00 4.00 4.00 4.00 6.30 12.50 4.00 6.30 12.50 6.30

12.50 45.00 6.30 12.50 25.00 40.00 50.00 80.00 100.00 6.30 12.50 12.70 6.30 12.50 25.00 40.00 50.00 80.00 12.50 6.30 6.30 12.50 25.00 6.30 12.50 12.70 80.00

... ... 430 435 435H 425H 425H 415H 395H 450 450 455H 420 420 420H 415H 415H 400H 425 405 455 455 455H 480 475 480H ...

0.19 0.25 1.60 0.24 0.50 1.60 3.20 6.30 0.50 1.60 6.30 0.24 0.50 1.60 6.30 0.24 1.60 0.24 1.60 0.24 1.60 6.30 0.50 1.60 6.30 6.30

0.25 1.60 12.50 0.50 1.60 3.20 6.30 12.50 1.00 6.30 12.50 0.50 1.60 6.30 12.50 1.60 12.50 1.60 6.30 1.60 6.30 12.50 1.60 6.30 12.50 12.50

... ... ... 420 420 425 430 435 440 455 450 405 405 420 420 425 435 400 405 440 455 455 460 485 475 ...

220 220H ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... Alclad One Side Alloy 2024

O

T3

T351E T361

T42F

T62F T72F,I T81 T851E T861

FG

215 215 220 ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ...

18

NOTICE: This standard has either been superseded and replaced by a new version or discontinued. Contact ASTM International (www.astm.org) for the latest information. B 209M TABLE 3 Continued Specified Thickness, mm

Tensile Strength, MPa

Yield Strength (0.2 % offset), MPa

Elongation,C min, %

max

in 50 mm

in 5 3 Diameter (5.65 =A!

95 ... ... ...

12 15 12 9 9 15 12 5 5 5 5 4 4 ...

... ... ... ... ... ... ... ... ... ... ... ... ... ...

Temper over

through

min

max

min

11⁄2 % Alclad One Side Alloy 2024 O T3 T351E T361

4.00 4.00 6.30 4.00 6.30 4.00 6.30 4.00 4.00 4.00 6.30 4.00 6.30 6.30

T42F F

T62 T72F,I T81 T851E T861 FG

12.50 6.30 12.50 6.30 12.50 6.30 12.50 12.50 6.30 6.30 12.50 6.30 12.50 12.50

... 430 435 455 450 420 420 435 405 455 455 480 475 ...

Specified Thickness, mm Temper

220 ... ... ...

... 285 285 340 330 255 255 340 310 395 395 450 435 ...

... ... ... ... ... ... ... ... ...

Tensile Strength, MPa

... ... ... ... ... ... ... ... ...

Yield Strength (0.2 % offset), MPa

Elongation,C min, %

Axis of Test Specimen over

through

25.00

50.00

50.00

80.00

80.00

100.00

100.00

130.00

130.00

150.00

min

max

min

max

in 50 mm

in 5 3 Diameter (5.65 =A!

... ... ... ... ... ... ... ... ... ... ... ... ... ... ...

395 395 380J 395 395 380 385 385 370 380 380 365 370 370 350

... ... ... ... ... ... ... ... ... ... ... ... ... ... ...

... ... ... ... ... ... ... ... ... ... ... ... ... ... ...

5 4 1 5 4 1 4 3 1 4 3 1 4 3 1

Alloy 2124 T851E

Longitudinal Long Transverse Short Transverse Longitudinal Long Transverse Short Transverse Longitudinal Long Transverse Short Transverse Longitudinal Long Transverse Short Transverse Longitudinal Long Transverse Short Transverse

Specified Thickness, mm

455 455 440J 450 450 435 450 450 425 440 440 420 435 435 400

Tensile Strength, MPa

Yield Strength (0.2 % offset), MPa

Elongation,C min, %

min

max

in 50 mm

in 5 3 Diameter (5.65 =A!

... ... 200 195 195 195 195 185 180 170 260 255 255 250 240 235 250 250 250 250 250 315

110 110 ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ...

12 ... 8 10 10 ... ... ... ... ... 6 6 ... ... ... ... 6 7 8 ... ... 6

... 10 ... ... ... 9 9 8 8 7 ... ... 5 5 4 3 ... ... ... 7 6 ...

Temper over

through

min

0.50 12.50 0.50 1.00 6.30 12.50 50.00 80.00 100.00 130.00 0.50 1.00 12.50 60.00 80.00 100.00 0.50 1.00 6.30 12.50 25.00 0.50

12.50 50.00 1.00 6.30 12.50 50.00 80.00 100.00 130.00 150.00 1.00 12.50 60.00 80.00 100.00 120.00 1.00 6.30 12.50 25.00 50.00 1.00

... ... 315 315 315 315 305 290 275 270 340 340 340 325 310 295 370 370 370 370 370 425

max Alloy 2219

O T31K (flat sheet) T351E,H plate (formerly T31 plate)

T37K

T62F

T81 sheet

220 220 ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ...

19

NOTICE: This standard has either been superseded and replaced by a new version or discontinued. Contact ASTM International (www.astm.org) for the latest information. B 209M TABLE 3 Continued Specified Thickness, mm

Tensile Strength, MPa

Yield Strength (0.2 % offset), MPa

Elongation,C min, %

over

through

min

max

min

max

in 50 mm

in 5 3 Diameter (5.65 =A!

1.00 6.30 12.50 25.00 50.00 80.00 100.00 130.00 0.50 1.00 6.30 12.50 25.00 80.00 100.00 6.30

6.30 12.50 25.00 50.00 80.00 100.00 130.00 150.00 1.00 6.30 12.50 25.00 80.00 100.00 120.00 50.00

425 425 425 425 425 415 405 395 440 440 440 440 440 425 420 ...

... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ...

315 315 315 315 310 305 295 290 360 360 350 350 350 345 340 ...

... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ...

7 8 ... ... ... ... ... ... 5 6 7 ... ... ... ... ...

... ... 7 6 5 4 4 3 ... ... ... 6 5 3 2 ...

0.50 1.00 2.50 12.50 1.00 2.50 6.30

1.00 2.50 12.50 50.00 2.50 6.30 12.50

... ... ... ... 290 305 305

220 220 220 220H ... ... ...

... ... ... ... 170 180 180

110 110 110 110H ... ... ...

12 12 12 ... 10 10 10

... ... ... 10 ... ... ...

1.00 2.50 0.50 1.00 2.50 6.30 12.50 25.00 0.50 1.00 2.50 6.30

2.50 12.50 1.00 2.50 6.30 12.50 25.00 50.00 1.00 2.50 6.30 12.50

310 325 305 340 350 350 370H 370H 340 380 400 400

... ... ... ... ... ... ... ... ... ... ... ...

235 240 200 220 235 235 250H 250H 255 285 295 290

... ... ... ... ... ... ... ... ... ... ... ...

6 6 6 7 7 8 ... ... 6 7 7 8

... ... ... ... ... ... 7 6 ... ... ... ...

1.00 2.50 6.30 6.30

2.50 6.30 12.50 50.00

395 415 415 ...

... ... ... ...

315 330 330 ...

... ... ... ...

6 6 7 ...

... ... ... ...

T4 T6 T651E

0.50 0.50 6.30 40.00 80.00

6.30 6.30 40.00 80.00 160.00

275 360 365 370 380

145 315 305 325 325

... ... ... ... ...

20 8 ... ... ...

... ... 4 4 3

0

0.15 0.20 0.25 0.50 3.20 12.50 25.00 0.15 0.20 0.25 0.50 6.30 12.50 25.00 0.15 0.20 0.25

0.20 0.25 0.50 3.20 12.50 25.00 80.00 0.20 0.25 0.50 6.30 12.50 25.00 80.00 0.20 0.25 0.50

... ... ... ... ... ... ... 205 205 205 205 205 205 205 205 205 205

... ... ... ... ... ... ... 110 110 110 110 110 110 110 95 95 95

85 85 85 85 85 ... ... ... ... ... ... ... ... ... ... ... ...

10 12 14 16 18 ... ... 10 12 14 16 18 ... ... 10 12 14

... ... ... ... ... 16 14 ... ... ... ... ... 16 14 ... ... ...

Temper

T851E (formerly T81 plate)

T87

FG

Alclad Alloy 2219 O

T31K (flat sheet) T351EK plate (formerly T31 plate)K T37K T62F

T81 (flat sheet)

T851E plate (formerly T81 plate) T87

FG

Alloy 6013 ... ... ... ... ... Alloy 6061

T4

T451E

T42F

150 150 150 150 150 150 150 ... ... ... ... ... ... ... ... ... ...

20

NOTICE: This standard has either been superseded and replaced by a new version or discontinued. Contact ASTM International (www.astm.org) for the latest information. B 209M TABLE 3 Continued Specified Thickness, mm

Tensile Strength, MPa

Yield Strength (0.2 % offset), MPa

Elongation,C min, %

over

through

min

max

min

max

in 50 mm

in 5 3 Diameter (5.65 =A!

0.50 6.30 12.50 25.00 0.15 0.20 0.25 0.50 6.30 12.50 25.00 50.00 100.00 6.30

6.30 12.50 25.00 80.00 0.20 0.25 0.50 6.30 12.50 25.00 50.00 100.00 150.00L 80.00

205 205 205 205 290 290 290 290 290 290 290 290 275 ...

... ... ... ... ... ... ... ... ... ... ... ... ... ...

95 95 95 95 240 240 240 240 240 240 240 240 240 ...

... ... ... ... ... ... ... ... ... ... ... ... ... ...

16 18 ... ... 4 6 8 10 10 ... ... ... ... ...

... ... 16 14 ... ... ... ... ... 8 7 5 5 ...

0.24 0.50 3.20 12.50 25.00 0.24 0.50 6.30

0.50 3.20 12.50 25.00 80.00 0.50 6.30 12.50

... ... ... ... ... 185 185 185

... ... ... ... ... 95 95 95

25.00 80.00 0.50 6.30 12.50 25.00 80.00 0.50 6.30 12.50 25.00 50.00 100.00 120.00 80.00

205 205 185 185 185 205H 205H 260 260 260 290H 290H 290H 275H ...

110H 110H 85 85 85 95H 95H 220 220 220 240H 240H 240H 240H ...

16 16 18 ... ... 14 16 18 ... ... ... ... 14 16 18 ... ... 8 10 10 ... ... ... ... ...

... ... ... 16 14 ... ... ...

12.50 25.00 0.24 0.50 6.30 12.50 25.00 0.24 0.50 6.30 12.50 25.00 50.00 100.00 6.30

85 85 85 ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ...

16 14 ... ... ... 16 14 ... ... ... 8 7 5 5 ...

0.39 12.50 0.19 0.32 1.00 3.20 6.30 12.50 25.00 50.00 60.00 80.00 90.00 1.00 6.30 12.50 25.00 50.00 60.00 3.10 6.30 12.50 6.30

12.50 50.00 0.32 1.00 3.20 6.30 12.50 25.00 50.00 60.00 80.00 90.00 100.00 6.30 12.50 25.00 50.00 60.00 80.00 6.30 12.50 25.00 100.00

... ... 510 525 540 540 540 540 530 525 495 490 460 460 475 475 475 455 440 500 495 490 ...

... ... 435 460 470 475 460 470 460 440 420 400 370 385 390 390 390 360 340 425 420 415 ...

145 ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ...

10 ... 5 7 8 8 9 ... ... ... ... ... ... 8 7 ... ... ... ... 8 8 ... ...

... 9 ... ... ... ... ... 6 5 4 4 4 2 ... ... 6 5 5 5 ... ... 5 ...

0.19 0.40 1.60

0.40 1.60 4.00

... ... ...

140 140 140

9 10 10

... ... ...

Temper

T6, T62F

T62F, T651E

FG

Alclad Alloy 6061 0

T4 T451E

T42F

T6, T62F T62F, T651E

FG

140 140 140 150H 150H ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... Alloy 7075

O T6, T62

F

T62F, T651E

T73 sheet T7351E plate

T76 sheet T7651E plate FG

275 275 ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... Alclad Alloy 7075

O

... ... ...

250 250 260

21

NOTICE: This standard has either been superseded and replaced by a new version or discontinued. Contact ASTM International (www.astm.org) for the latest information. B 209M TABLE 3 Continued Specified Thickness, mm

Tensile Strength, MPa

Yield Strength (0.2 % offset), MPa

Elongation,C min, %

over

through

min

max

min

max

in 50 mm

in 5 3 Diameter (5.65 =A!

4.00 12.50 0.19 0.32 1.00 1.60 3.20 4.00 6.30 12.50 25.00 50.00 60.00 80.00 90.00 3.10 4.00 6.30 12.50 6.30

12.50 25.00 0.32 1.00 1.60 3.20 4.00 6.30 12.50 25.00 50.00 60.00 80.00 90.00 100.00 4.00 6.30 12.50 25.00 100.00

... ... 470 485 495 505 505 515 515 540H 530H 525H 495H 490H 460H 470 485 475 490H ...

270 275H ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ...

... ... 400 415 425 435 435 440 445H 470H 460H 440H 420H 400H 370H 390 405 400 415H ...

145 ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ...

10 ... 5 7 8 8 8 8 9 ... ... ... ... ... ... 8 8 8 ... ...

... 9 ... ... ... ... ... ... ... 6 5 4 4 4 2 ... ... ... 5 ...

0.39 1.60 4.00 12.50 0.31 1.00 1.60 3.20 4.00 6.30 12.50 25.00 6.30

1.60 4.00 12.50 25.00 1.00 1.60 3.20 4.00 6.30 12.50 25.00 50.00 50.00

... ... ... ... 505 510 515 515 525 525 540H 530H ...

... ... ... ... 435 440 445 445 455 455 470H 460H ...

145 145 145 ... ... ... ... ... ... ... ... ... ...

10 10 10 ... 7 8 8 8 8 9 ... ... ...

... ... ... 9 ... ... ... ... ... ... 6 5 ...

0.39 1.60 4.00 12.50 0.39 1.00 1.60 3.20 4.00 6.30 12.50 25.00 50.00 60.00 80.00 90.00 1.00 1.60 4.00 6.30 12.50 6.30

1.60 4.00 12.50 50.00 1.00 1.60 3.20 4.00 6.30 12.50 25.00 50.00 60.00 80.00 90.00 100.00 1.60 4.00 6.30 12.50 25.00 100.00

... ... ... ... 505 515 515 515 525 525 540H 530H 525H 495H 490H 460H 485 490 495 490 490H ...

... ... ... ... 435 445 445 445 455 455 470H 460H 440H 420H 400H 370H 405 415 420 415 415H ...

145 145 145 ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ...

10 10 10 ... 7 8 8 8 8 9 ... ... ... ... ... ... 8 8 8 8 ... ...

... ... ... 9 ... ... ... ... ... ... 6 5 4 4 4 2 ... ... ... ... 5 ...

0.39 12.50 0.39 1.20 6.30 12.50 25.00 40.00 1.00 6.30

12.50 12.70 1.20 6.30 12.50 25.00 40.00 50.00 6.30 12.50

... ... 570 580 580 580 580 550 515 510

... ... 495 505 505 505 505 480 440 435

145... ... ... ... ... ... ... ... ... ...

10... ... 7 8 8 ... ... ... 8 8

... 9 ... ... ... 5 3 2 ... ...

Temper

T6, T62

F

T62F, T651E

T76 sheet T7651E plate FG

Alclad One Side Alloy 7075 O

T6, T62F

T62F, T651E

FG

260 270 270 275H ... ... ... ... ... .... ... ... ... 7008 Alclad Alloy 7075

O

T6, T62F

T62F, T651E

T76 sheet

T7651H plate FG

275 275 275 275H ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... Alloy 7178

O T6, T62F T62F, T651E

T76 T7651E

275 275 ... ... ... ... ... ... ... ...

22

NOTICE: This standard has either been superseded and replaced by a new version or discontinued. Contact ASTM International (www.astm.org) for the latest information. B 209M TABLE 3 Continued Specified Thickness, mm

Tensile Strength, MPa

Yield Strength (0.2 % offset), MPa

Elongation,C min, %

over

through

min

max

min

max

in 50 mm

in 5 3 Diameter (5.65 =A!

12.50 6.30

25.00 50.00

500 ...

... ...

425 ...

... ...

... ...

5 ...

0.39 1.60 4.00 12.50 0.39 1.20 1.60 4.00 6.30 12.50 25.00 40.00 1.00 1.60 4.00 6.30 12.50 6.30

1.60 4.00 12.50 12.70 1.20 1.60 4.00 6.30 12.50 25.00 40.00 50.00 1.60 4.00 6.30 12.50 25.00 50.00

... ... ... ... 525 540 550 565 565 580H 580H 550H 490 490 500 495 500H ...

... ... ... ... 455 470 480 490 490 505H 505H 480H 415 415 420 415 425H ...

140 140 145 ... ... ... ... ... ... ... ... ... ... ... ... ... ... ...

10 10 10 ... 7 8 8 8 8 ... ... ... 8 8 8 8 ... ...

... ... ... 9 ... ... ... ... ... 5 3 2 ... ... ... ... 5 ...

Temper

FG

Alclad Alloy 7178 O

T6, T62F

T62F, T651E

T76

T7651E FG

250 265 275 275H ... ... ... ... ... ... ... ... ... ... ... ... ... ...

A To determine conformance to this specification each value for tensile strength shall be rounded to the nearest 1 MPa and each value for elongation to the nearest 0.5 %, both in accordance with the rounding method of Practice E 29. B The basis for establishment of mechanical property limits is shown in Annex AI. C Elongations in 50 mm apply for thicknesses up through 12.50 mm and in 5 3 diameter (5.65 = A ) for thicknesses over 12.50 mm where A is the cross-sectional area of the specimen. D Coiled sheet. E For stress-relieved tempers (T351, T451, T651, T7351, T7651 and T851), characteristics and properties other than those specified may differ somewhat from the corresponding characteristics and properties of material in the basic temper. F Material in the T42, T62, and T72 tempers is not available from the material producer. G Test for tensile properties in the F temper are not required. H The tension test specimen from plate over 12.50 mm in thickness is machined from the core and does not include the cladding. I The T72 temper is applicable only to Alloys 2024 and Alclad 2024 sheet solution heat treated and artificially overaged by the user to develop increased resistance to stress-corrosion cracking. J Short transverse tensile properties are not applicable to material less than 40 mm in thickness. K Use of Alloys 2219 and Alclad 2219 in the T31, T351, and T37 tempers for finished products is not recommended. L The properties for this thickness apply only to the T651 temper.

TABLE 4 Lot Acceptance Criteria for Resistance to Stress Corrosion and Exfoliation Corrosion

23

NOTICE: This standard has either been superseded and replaced by a new version or discontinued. Contact ASTM International (www.astm.org) for the latest information. B 209M TABLE 5 Components of Clad Products

TABLE 6 Ultrasonic Discontinuity Limits for Plate

ANNEXES (Mandatory Information) A1. BASIS FOR INCLUSION OF PROPERTY LIMITS

limits for the respective size ranges are based on the analyses of at least 100 data from standard production material with no more than ten data from a given lot. All tests are performed in accordance with the appropriate ASTM test methods. For

A1.1 Limits are established at a level at which a statistical evaluation of the data indicates that 99 % of the population obtained from all standard material meets the limit with 95 % confidence. For the products described, mechanical property 24

NOTICE: This standard has either been superseded and replaced by a new version or discontinued. Contact ASTM International (www.astm.org) for the latest information. B 209M informational purposes, refer to “Statistical Aspects of Mechanical Property Assurance” in the Related Material section of the Annual Book of ASTM Standards, Vol 02.02. Mechanical property limits in this metric issue were derived from the

inch-pound system limits that were developed under the above principles. As test data on metric dimensioned specimens are accumulated, some refinement of limits, particularly for elongations measured in 5D, can be anticipated.

A2. ACCEPTANCE CRITERIA FOR INCLUSION OF NEW ALUMINUM AND ALUMINUM ALLOYS IN THIS SPECIFICATION

refinement and for which minimum and maximum limits are specified. Unalloyed aluminum contains a minimum of 99.00 % aluminum. A2.2.6 Standard limits for alloying elements and impurities are expressed to the following decimal places:

A2.1 Prior to acceptance for inclusion in this specification, the composition of wrought or cast aluminum or aluminum alloy shall be registered in accordance with ANSI H35.1(M). The Aluminum Association13 holds the Secretariat of ANSI H35 Committee and administers the criteria and procedures for registration.

Less than 0.001 % 0.001 to but less than 0.01 % 0.01 to but less than 0.10 % Unalloyed aluminum made by a refining process Alloys and unalloyed aluminum not made by a refining process 0.10 through 0.55 % (It is customary to express limits of 0.30 through 0.55 % as 0.X0 or 0.X5.) Over 0.55 % (except that combined Si+Fe limits for 99.00 % minimum aluminum must be expressed as 0.XX or 1.XX)

A2.2 If it is documented that the Aluminum Association could not or would not register a given composition, an alternative procedure and the criteria for acceptance shall be as follows: A2.2.1 The designation submitted for inclusion does not utilize the same designation system as described in ANSI H35.1(M). A designation not in conflict with other designation systems or a trade name is acceptable. A2.2.2 The aluminum or aluminum alloy has been offered for sale in commercial quantities within the prior twelve months to at least three identifiable users. A2.2.3 The complete chemical composition limits are submitted. A2.2.4 The composition is, in the judgment of the responsible subcommittee, significantly different from that of any other aluminum or aluminum alloy already in the specification. A2.2.5 For codification purposes, an alloying element is any element intentionally added for any purpose other than grain

0.000X 0.00X 0.0XX 0.0X 0.XX

0.X, X.X, etc.

A2.2.7 Standard limits for alloying elements and impurities are expressed in the following sequence: Silicon; Iron; Copper; Manganese; Magnesium; Chromium; Nickel; Zinc (Note A2.1); Titanium; Other Elements, Each; Other Elements, Total; Aluminum (Note A2.2). NOTE A2.1—Additional specified elements having limits are inserted in alphabetical order of their chemical symbols between zinc and titanium, or are specified in footnotes. NOTE A2.2—Aluminum is specified as minimum for unalloyed aluminum and as a remainder for aluminum alloys.

APPENDIX (Nonmandatory Information) X1. ISO EQUIVALENTS OF ANSI ALLOYS AND TEMPERS TABLE X1.1 ISO Equivalents of Alloys in B 209M

X1.1 International Organization for Standardization equivalents of the ANSI alloys and tempers given in Table X1.1 and Table X1.2 are included in ISO 209-1, Part 1, Chemical Composition, and ISO 2107. Mechanical property limits shown in ISO 6361-2, Part 2, Mechanical Properties, are similar to B209M but not necessarily identical.

Alloys ANSI 1060 1100 2014 2024 2219 3003 3004 3005 3105 5005

25

Al Al Al Al Al Al Al Al Al Al

ISO

ANSI

99.6 99.0 Cu Cu4SiMg Cu4Mg1 Cu6Mn Mn1Cu Mn1Mg1 Mn1Mg0.5 Mn0.5Mg0.5 Mg1 (B)

5050 5052 5083 5086 5154 5454 5456 6061 7075 7178

ISO Al Al Al Al Al Al Al Al Al Al

Mg1.5 (C) Mg2.5 Mg4.5Mn0.7 Mg4 Mg3.5 Mg3Mn Mg5Mn1 Mg1SiCu Zn5.5MgCu Zn7MgCu

NOTICE: This standard has either been superseded and replaced by a new version or discontinued. Contact ASTM International (www.astm.org) for the latest information. B 209M TABLE X1.2 ISO Equivalents of Tempers in B 209M Tempers ANSI

H12, H14, H16, H18, H19, H112

F O H22, H24, H26, H28, H29

H32 H34 H36 H38

ISO F O H1B, H2B, H3B H1D, H2D, H3D H1F, H2F, H3F H1H, H2H, H3H H1J,H2J M

ANSI

ISO

T3 T4 T6 T7 T8

TD TB TF TM TH

SUMMARY OF CHANGES Committee B07 has identified the location of selected changes to this standard since the last issue (B 209M – 01) that may impact the use of this standard. (1) In Section 2.2, updated Referenced Documents by deleting Practice B 597 and replacing with Practice B 918. (2) In Section 4, replaced reference to Practice B 597 with reference to Practice B 918. (3) In Section 8, replaced reference to Practice B 597 with reference to Practice B 918. (4) In Table 1, added chemical composition limits for 5457 alloy.

(5) In Table 2, added tensile properties for 5457-O sheet. (6) In Table 3, 2124-T851, specified thickness “over 40.00 mm” was changed to “over 25.00 mm” for consistency with Specification B 209 and AS&D-1998 Metric SI. (7) In Table 3, footnote Jwas added and applied to 2124-T851 for consistency with Specification B 209 and AS&D-1998 Metric SI.

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