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SPECIF SPECIFICAT ICATION ION FOR ALUMIN ALUMINUM UM AND ALUMIN ALUMINUMUMALLO ALLOY Y EXTR EXTRUD UDED ED BARS BARS,, RODS RODS,, AND PROFIL PROFILES ES

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(Identical with ASTM Specification B 221-96 for the alloys, tempers, and product forms covered except for editorial differences. Certification has been made mandatory.)

1. A99

Scope

B 557 Test Test Method Methodss of Tensio Tension n Testin Testing g Wrough Wroughtt and Cast Aluminum- and Magnesium-Alloy Products B 597 Practice for Heat Treatment of Aluminum Alloys B 660 Practice Practicess for Packaging/ Packaging/ Packing Packing of Aluminum Aluminum and Magnesium Products B 666/B 666M Practice for Identification Marking of Aluminum Products B 807 Practice for Extrusion Press Solution Heat Treatment of Aluminum Alloys E 29 Practice Practice for Using Significant Significant Digits Digits in Test Test Data to Determine Conformance With Specifications E 34 Test Methods for Chemical Analysis of Aluminum and Aluminum-Base Alloys E 55 Practice for Sampling Sampling Wrought Nonferrous Nonferrous Metals and Alloys for Determinatio Determination n of Chemical Composition E 101Test Methodfor Methodfor Spectro Spectrogra graphi phicc Analys Analysis is of AlumiAluminumand Alumin Aluminum um Alloysby Alloysby the PointPoint-toto-Pla Plane ne TechTechniqu niquee E 227 Test Method for Optical Emission Spectrometric Analysis of Aluminum and Aluminum Alloys by the Point-to-Plane Technique E 527 Practice for Numbering Metals and Alloys (UNS) E 607 Test Method for Optical Emission Spectrometric Analysis of Aluminum and Aluminum Alloys by the Point-to-Plane Technique, Nitrogen Atmosphere E 716 Practices for Sampling Aluminum and Aluminum Alloys for Spectrochemical Analysis

1.1 This specification specification covers covers aluminum aluminum and aluminum-alloy extruded bar, rod, and profile in the aluminum alloys alloys (Note 1) and tempers tempers shown shown in Table Table 2. NOTE 1 — Throughout this specification, the use of the term alloy in the general general sense includes aluminum as well as aluminum aluminum alloy. NOTE 2 — For rolled or cold-finished bar and rod refer to Specification SB-211, for drawn tube to Specification Specification SB-210, for structural structural pipe and tube to Specificat Specification ion B 429, 429, and for seamle seamless ss pipe and tube to Specification Specification SB-241/SB-241M.

1.2 Alloy 1.2 Alloy and temper designations are in accordance with ANSI H35.1. H35.1. The equivalent Unified Numbering System alloy designations are those of Table 1 preceded by A 9; for example, A91100 for Aluminum 1100 in accordance accordance with Practice Practice E 527. 1.3 For For accept acceptanc ancee criter criteria ia for inclus inclusion ion of new alum alumin inum um and and alu alumi minu num m all alloy oyss in in thi thiss spe speci cific ficat atio ion, n, see Annex A2. 1.4 A 1.4 A complete metric companion to B 221 has been developed — B 221M; therefore, no metric equivalents are presented in this specification. specification.

2.

Refe Referen rence ced d Docu Docume ment ntss

2.1 The following documents of the issue in effect on the the date date of mater materia iall purc purcha hase se,, unle unless ss othe otherw rwis isee noted, noted, form a part part of this this specifi specificati cation on to the extent referenced referenced herein: herein:

Standards 2.1.2 ANSI Standards H35.1 Alloy and Temper Designation Systems for Aluminum

Standards 2.1.1 ASTM Standards 269

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1998 SECTION II

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1998 SECTION II

H35.2 Dimensional Tolerances for Aluminum Mill Products

4.1.3 alloy (Section 7 and Table 1); 4.1.4 temper (Section 8 and Table 2);

2.1.3 Federal Standard Fed. Std. No. 123 Marking for Shipment (Civil Agencies)

4.1.5 nominal follows:

2.1.4 Military Standard MIL-STD-129 Marking for Shipment and Storage

4.1.5.2 for square-cornered bar — depth and

4.1.5.3 for sharp-cornered hexagonal or octagonal bar — distance across flats;

Terminology

4.1.5.4 for round-cornered bars and profiles — drawing required; and

3.1.1 extruded bar — an extruded solid product that is long in relation to cross section, which is square or rectangular (excluding plate and flattened wire) with sharp or rounded corners or edges, or is a regular hexagon or octagon, and in which at least one perpendicular distance between parallel faces is 0.375 in. or greater

4.1.6 length. 4.2 Additionally, orders for material to this specification shall include the following information when required by the purchaser: 4.2.1 whether heat treatment in accordance with Practice B 597 is required (9.2);

3.1.2 extruded rod — an extruded solid product 0.375 in. or greater in diameter that is long in relation to cross section 3.1.3 extruded profile — a hollow or solid extruded section, long in relation to its cross-sectional dimensions, whose cross section is other than that of wire, rod, bar, or tube 3.1.4 producer — the primary manufacturer of the material

4.2.2 whether inspection or witness of inspection and tests by the purchaser’s representative is required prior to material shipment (Section 12);

4.2.3 whether marking for identification is required (Section 15), and whether marking of lot number for alloy 2024 in the T3-type temper and alloy 6061 in the T6-type temper is required (15); 4.2.4 whether Practices B 660 applies and, if so, the levels of preservation, packaging, and packing required (16); and

3.1.5 supplier — includes only the category of jobbers and distributors as distinct from producers

4.2.5 requirements for tensile property and dimensional tolerance for sizes not specifically covered (8.1.3 and 10.1.1).

3.2 Description of Term 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 subsequent testing by the purchaser establish that the material does not meet these requirements, the material shall be subject to rejection.

4.

as

width;

3.1 Definitions

A99

dimensions

4.1.5.1 for rod — diameter;

2.1.5 Military Specification MIL-H-6088 Heat Treatment of Aluminum Alloys

3.

cross-sectional

5.

Materials and Manufacture

5.1 The products covered by this specification shall be produced by the hot extrusion method or by similar methods at the option of the producer, provided that the resulting products comply with the requirements in this specification.

Ordering Information

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);

6.

Quality Assurance

6.1 Responsibility for Inspection and Tests — Unless otherwise specified in the contract or purchase order, the producer is responsible for the performance of all

4.1.2 quantity in pieces or pounds; 270

PART B — NONFERROUS MATERIAL SPECIFICATIONS

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7.3 Methods of Sampling

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 ensure that material conforms to prescribed requirements.

7.3.1 Samples for determination of chemical composition shall be taken in accordance with one of the following methods. 7.3.1.1 Samples for chemical analysis shall be taken from the material 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.

6.2 Lot Definition — An inspection lot shall be defined as follows. 6.2.1 For heat-treated tempers, an inspection lot shall consist of an identifiable quantity of material of the same mill form, alloy, temper, and nominal dimensions traceable to a heat-treat lot or lots, and subjected to inspection at one time.

7.3.1.2 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.

6.2.2 For nonheat-treated tempers, an inspection lot shall consist of an identifiable quantity of material of the same mill form, alloy, temper, and nominal dimensions subjected to inspection at one time.

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 101, E 227, or E 607) or other methods. Other methods may be used only when no published ASTM method is available. In case of dispute, the methods of analysis shall be agreed upon between the producer and purchaser.

7.

Chemical Composition 7.1 Limits

7.1.1 The material shall conform to the chemical composition limits in Table 1. Conformance shall be determined by analyzing samples taken when the ingots are poured, or samples taken from the finished or semifinished product. If the chemical composition has been determined during the course of manufacture, analysis of the finished product shall not be required.

8.

Tensile Properties of Material From the Producer

8.1 Limits — The material shall conform to the tensile property requirements specified in Table 2.

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.

8.1.1 The elongation requirements shall not be applicable to the following: 8.1.1.1 material of such dimensions that a standard test specimen cannot be taken in accordance with Test Methods B 557, and of such profile that it cannot be satisfactorily tested in full section;

7.2 Number of Samples 7.2.1 The number of samples taken for determination of chemical composition shall be as follows.

8.1.1.2 material thinner than 0.062 in.; and

7.2.1.1 When samples are taken at the time the ingots are poured, at least one sample shall be taken for each group of ingots poured simultaneously from the same source of molten metal.

8.1.1.3 wire less than 0.125 in. in diameter. 8.1.2 The measurement for yield strength is not required for wire less than 0.125 in. in diameter.

7.2.1.2 When samples are taken from the finished or semifinished product, a sample shall be taken to represent each 4,000 lb, or fraction thereof, in the lot, except that not more than one sample shall be required per piece.

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8.1.3 Tensile property limits for sizes not covered in Table 2 shall be as agreed upon between the producer and purchaser and shall be so specified in the contract or purchase order.

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S B 2 2 1

TABLE 1 CHEMICAL COMPOSITION LIMITS [NOTES (1), (2), (3)] Other Elements [Note (4)]

2 7 2

Alloy

Silicon

Iron

1060 1100 2024 3003 5083 5086 5154 5454 5456 6061 [Note (8)] 6063

0.25 0.35 0.95 Si + Fe 0.50 0.50 0.6 0.7 0.40 0.40 0.40 0.50 0.25 0.40 0.25 0.40 0.25 0.40 0.40–0.8 0.7 0.20–0.6 0.35

Copper

Manganese

Magnesium

Chromium

Z inc

0.05 0.05–0.20 3.8–4.9 0.05–0.20 0.10 0.10 0.10 0.10 0.10 0.15–0.40 0.10

0.03 0.05 0.30–0.9 1.0–1.5 0.40–1.0 0.20–0.7 0.10 0.50–1.0 0.50–1.0 0.15 0.10

0.03 ... 1.2–1.8 ... 4.0–4.9 3.5–4.5 3.1–3.9 2.4–3.0 4.7–5.5 0.8–1.2 0.45–0.9

... ... 0.10 ... 0.05–0.25 0.05–0.25 0.15–0.35 0.05–0.20 0.05–0.20 0.04–0.35 0.10

0.05 0.10 0.25 0.10 0.25 0.25 0.20 0.25 0.25 0.25 0.10

Vanadium Titanium 0.05 ... ... ... ... ... ... ... ... ... ...

Eac h

0.03 ... 0.15 [Note (7)] ... 0.15 0.15 0.20 0.20 0.20 0.15 0.10

Total [Note (5)] Aluminum

0.03 0.05 0.05 0.05 0.05 0.05 0.05 0.05 0.05 0.05 0.05

... 0.15 0.15 0.15 0.15 0.15 0.15 0.15 0.15 0.15 0.15

99.60 min. [Note (6)] 99.00 min. [Note (6)] Remainder Remainder Remainder Remainder Remainder Remainder Remainder Remainder Remainder

NOTES: (1) Limits are in weight percent maximum unless shown as a range, or stated otherwise. (2) Analysis shall regularly be made for the elements specified in this Table. If, however, the presenc e of other elements is suspected or indicated in amounts greater than the specified limits, further analysis shall be made to determine that these elements are not present in amounts in excess of the specified limits. (3) For the purpose of determining conformance to these limits, an observed value or a calculated value obtained from analysis shall be rounded to the nearest unit in the last right-hand place of the figures used in expressing the specified limit, in accordance with the rounding-off method of Practice E 29. (4) Includes listed element for which no specific limit is shown. (5) Other Elements—Total shall be the sum of unspecified metallic elements 0.010% or more, rounded to the second decimal before determining the sum. (6) 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. (7) Upon agreement between the purchaser and producer or supplier, a Zr + Ti limit of 0.20% max is permitted. (8) In 1965 the requirements for 6062 were combined with those for 6061 by revising the minimum chromium from 0.15% to 0.04%. This action cancelled alloy 6062.


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TABLE 2 MECHANICAL PROPERTY LIMITS [NOTES (1), (2)]

Temper

Specified Section or Wall Thickness, in.

Area, in. 2

Min.

Yield Strength (0.2% Offset), ksi

Max

Min.

Max

Elongation in 2 in. or 4 × Dia, Min., % [Notes (3), (4)]

14.0 ...

2.5 2.5

... . ..

25 25

15.5 ...

3.0 3.0

... ...

25 25

Tensile Strength, ksi

Aluminum 1060 O H112

All All

All All

8.5 8.5


All All

All All

11.0 11.0

Alloy 2024

1 9 9 8 S E C T I O N I I


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TABLE 2 MECHANICAL PROPERTY LIMITS [NOTES (1), (2)]

Temper


Area, in. 2

Min.

Yield Strength (0.2% Offset), ksi

Max

Min.

Max


14.0 ...

2.5 2.5

... . ..

25 25

15.5 ...

3.0 3.0

... ...

25 25

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

42.0 44.0 46.0 52.0 48.0

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

12 12 10 10 8

19.0 ...

5.0 5.0

... ...

25 25

51.0 ... ...

16.0 24.0 16.0

... ... ...

14 12 12

...

14.0

...

12

41.0 ...

11.0 11.0

... ...

... ...

41.0 ... ...

12.0 19.0 12.0

... ... ...

14 12 12

53.0 ... ...

19.0 26.0 19.0

... ... ...

14 12 12

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

16.0 16.0 16.0 35.0 35.0 35.0 35.0

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

16 16 16 8 10 8 10

Tensile Strength, ksi


All All

All All

8.5 8.5


All All

All All

11.0 11.0

Alloy 2024 T3

Up through 0.249 0.250–0.749 0.750–1.499 1.500 and over

All All All Up through 25 Over 25 through 32

57.0 60.0 65.0 70.0 68.0

Alloy 3003 O H112

All All

All All

14.0 14.0

Alloy 5083 O H111 H112

Up through 5.000 Up through 5.000 Up through 5.000

Up through 32 Up through 32 Up through 32

39.0 40.0 39.0

Alloy 5086 H112

Up through 5.000

Up through 32

35.0

Alloy 5154 O H112

All All

All All

30.0 30.0

Alloy 5454 O H111 H112



31.0 33.0 31.0

Alloy 5456 O H111 H112



41.0 42.0 41.0

Alloy 6061 T4 T4510 [Note (5)] T4511 [Note (5)] T6 T6510 [Note (5)]

All All All Up through 0.249 0.250 and over Up through 0.249 0.250 and over

All All All All All All All

26.0 26.0 26.0 38.0 38.0 38.0 38.0

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TABLE 2 (CONT’D) MECHANICAL PROPERTY LIMITS [NOTES (1), (2)]

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Temper


Area, in.

2

Min.

Yield Strength (0.2% Offset), ksi Min.

Max


... ...

35.0 35.0

... ...

8 10

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

9.0 8.0 16.0 15.0 25.0 25.0

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

12 12 8 8 8 10

Tensile Strength, ksi Max

Alloy 6061 (Cont’d) T6511 [Note (5)]

Up through 0.249 0.250 and over

All All

38.0 38.0

Alloy 6063 T1 T5 T6

Up through 0.500 0.501–1.000 Up through 0.500 0.501–1.000 Up through 0.124 0.125–1.000

All All All All All All

17.0 16.0 22.0 21.0 30.0 30.0

GENERAL NOTE: Strength values shown in parentheses are for information only. NOTES: (1) The basis for establishment of tensile property limits is shown in Annex A1. (2) To determine conformance to this specification, each value shall be rounded to the nearest 0.1 ksi for strength and nearest 0.5% for elongation in accordance with the rounding-off method of Practice E 29. (3) Elongation of full-section and cut-out sheet-type specimens is measured in 2 in. Elongation of cut-out round specimens is measured in 4 × specimen diameter. (4) See 8.1.1.1 and 8.1.1.2 for conditions under which measurements are not required. (5) For stress relieved tempers (T3510, T3511, T4510, T4511, T6510, T6511), characteristics and properties other than those specified may differ somewhat from the corresponding characteristics and properties of material in the basic tempers.

8.2 Number of Specimens

9.

Heat Treatment

8.2.1 For material having a nominal weight of less than 1 lb/linear ft, one tension test specimen shall be taken for each 1,000 lb or fraction thereof in the lot.

9.1 Except as noted in 9.3, or otherwise specified in 9.2, producer or supplier heat treatment for the applicable tempers in Table 2 shall be in accordance with ML-H-6088.

8.2.2 For material having a nominal weight of 1 lb or more per linear foot, one tension test specimen shall be taken for each 1,000 ft or fraction thereof in the lot.

9.2 When specified, heat treatment of applicable tempers in Table 2 shall be in accordance with Practice B 597.

8.2.3 Other procedures for selecting samples may be employed if agreed upon between the producer or supplier and the purchaser.

9.3 Alloys 6061 and 6063 may be solution heat treated and quenched at the extrusion press in the production of T1, T4, T5, and T6-type tempers as applicable.

8.3 Geometry of test specimens and the location in the product from which they are taken shall be as specified in Test Methods B 557. 8.4 Test Methods — The tension tests shall be made in accordance with Test Methods B 557.

10.

10.1 Dimensions — Variations from the specified dimensions for the type of material ordered shall not exceed the permissible variations prescribed in the tables of ANSI H35.2 (see Table 3).

8.5 Retests — When there is evidence that the test specimen is defective or is not representative of the lot of material, retesting may be performed in accordance with Sections 8 and 9 of Test Methods B 557.

Dimensional Tolerances

10.1.1 Dimensional tolerances for sizes not covered in ANSI H35.2 shall be agreed upon between the

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TABLE 3 TABLES OF ANSI H35.2

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Table No. 10.1

10.2 10.3 10.4 10.5 10.6

10.7 10.8

10.9 10.10 10.11

12.2 When such inspection or witness of inspection and testing is agreed upon, the producer or supplier 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 or supplier’s operations.

Title Cross-Spectional Dimensions: Wire, Rod, Bar & Profiles Except for Profiles in T3510, T4510, T6510, T73510, T76510, and T8510 Tempers Length: Wire, Rod, Bar, and Profiles Straightness: Rod, Bar, and Profiles Twist: Bar and Profiles Flatness: Flat Surfaces Flatness: Flat Surfaces, Hollow Profiles Except for O, T3510, T4510, T6510, T73510, T76510, and T8510 Tempers Surface Roughness: Wire, Rod, Bar, and Profiles Contour (Curved Surfaces): Profiles Except for O, T3510, T4510, T6510, T73510, T76510, and T8510 Tempers Squareness of Cut Ends: Wire, Rod, Bar, and Profiles Corner and Fillet Radii: Bar and Profiles Angularity: Bar and Profiles Except for O, T3510, T4510, T6510, T73510, T76510, and T8510 Tempers

13.

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13.2 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. 13.3 Material in which defects are discovered subsequent to inspection may be rejected. 13.4 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.

General Quality

11.1 Unless otherwise specified, the extruded bar, rod, and profile 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 the producer and purchaser.

14.

15.

Identification Marking of Product

15.1 When specified in the contract or purchase order, all material shall be marked in accordance with Practice B 666. 15.2 The requirements specified in 15.1 are minimum; marking systems that involve added information, larger characters, and greater frequencies are acceptable under this specification and shall be agreed upon between the producer and purchaser.

Source Inspection

12.1 If the purchaser desires that his representative inspect or witness the inspection and testing of the material prior to shipment, such agreement shall be 275

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Certification

14.1 The producer or supplier shall 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.

11.2 Each bar, rod, or profile 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 or the supplier may use a system of statistical quality control for such examination.

12.

Retest and Rejection

13.1 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.

10.2 Sampling for Inspection — Examination for dimensional conformance shall be made to ensure conformance to the tolerance specified.

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made by the purchaser and the producer or supplier as part of the purchase contract.

producer and purchaser and shall be specified in the contract or purchase order.

11.

1998 SECTION II

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16.

1998 SECTION II

Packaging and Package Marking

number, alloy and temper, gross and net weights, and the producer’s name or trademark.

16.1 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 upon. The type of packing and gross weight of containers shall, unless otherwise agreed upon, be at the producer or supplier’s discretion, provided they are such as to ensure acceptance by common or other carriers for safe transportation at the lowest rate to the delivery point. 16.2 Each shipping container shall be marked with the purchase order number, material size, specification

16.3 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 level shall be as specified in the contract or order. Marking for shipment of such material shall be in accordance with Fed. Std. No. 123 for civil agencies and MIL-STD-129 for Military agencies.

17.

Keywords

17.1 aluminum alloy; extruded bars; extruded profiles; extruded rods

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ANNEXES

(Mandatory Information)

A1. BASIS FOR INCLUSION OF PROPERTY LIMITS

A2.2.3 The complete chemical composition limits are submitted.

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 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 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.

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 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: 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. ACCEPTANCE CRITERIA FOR INCLUSION OF NEW ALUMINUM AND ALUMINUM ALLOYS IN THIS SPECIFICATION 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. The Aluminum Association holds the Secretariat of ANSI H35 Committee and administers the criteria and procedures for registration. 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.

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).

A2.2.1 The designation submitted for inclusion does not utilize the same designation system as described in ANSI H35.1. A designation not in conflict with other designation systems or a trade name is acceptable.

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.

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.

NOTE A2.2 — Aluminum is specified as minimum for unalloyed aluminum and as a remainder for aluminum alloys.

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