ASTM B211/B211M-23

This document is not an ASTM standard and is intended only to provide the user of an ASTM standard an indication of what changes have been made to the previous version. Because
it may not be technically possible to adequately depict all changes accurately, ASTM recommends that users consult prior editions as appropriate. In all cases only the current version
of the standard as published by ASTM is to be considered the official document.
Designation: B211/B211M − 19 B211/B211M − 23
Standard Specification for
Aluminum and Aluminum-Alloy Rolled or Cold Finished Bar,
Rod, and Wire
This standard is issued under the fixed designation B211/B211M; 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 (´) indicates an editorial change since the last revision or reapproval.
This standard has been approved for use by agencies of the U.S. Department of Defense.
1. Scope*
1.1 This specification covers rolled or cold-finished bar, rod, and wire in alloys (Note 1) and tempers as shown in Table 2 [Table
3].
NOTE 1—Throughout this specification use of the term alloy in the general sense includes aluminum as well as aluminum alloy.
NOTE 2—The term cold finished is used to indicate the type of surface finish, sharpness of angles, and dimensional tolerances produced by drawing through
a die.
NOTE 3—See Specification B221 [B221M] for aluminum and aluminum-alloy extruded bars, rods, wire, shapes, and tubes; and Specification
B316/B316M for aluminum and aluminum-alloy rivet and cold-heading wire and rods.
1.2 Alloy and temper designations are in accordance with ANSI H35.1/H35.1M. The equivalent UNS alloy designations are those
of shall be Table 1 preceded by A9, for example, A91100 for aluminum 1100 in accordance with Practice E527.
1.3 For acceptance criteria for inclusion of new aluminum and aluminum alloys in this specification, see Annex A2.
1.4 This international standard was developed in accordance with internationally recognized principles on standardization
established in the Decision on Principles for the Development of International Standards, Guides and Recommendations issued
by the World Trade Organization Technical Barriers to Trade (TBT) Committee.
2. Referenced Documents
2.1 The following documents of the issue in effect on date of material purchase form a part of this specification to the extent
referenced herein:
2.2 ASTM Standards:
B221 Specification for Aluminum and Aluminum-Alloy Extruded Bars, Rods, Wire, Profiles, and Tubes
B221M Specification for Aluminum and Aluminum-Alloy Extruded Bars, Rods, Wire, Profiles, and Tubes (Metric)
B316/B316M Specification for Aluminum and Aluminum-Alloy Rivet and Cold-Heading Wire and Rods
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 Jan. 1, 2019Oct. 1, 2023. Published February 2019October 2023. Originally approved in 1946. Last previous edition approved in 20122019 as
ε1
B211 – 12B211 – 19. . DOI: 10.1520/B0211_B0211M-19.10.1520/B0211_B0211M-23.
For ASME Boiler and Pressure Vessel Code applications see related Specification SB-211 in Section II of that Code.
For referenced ASTM standards, visit the ASTM website, www.astm.org, or contact ASTM Customer Service at service@astm.org. For Annual Book of ASTM Standards
volume information, refer to the standard’s Document Summary page on the ASTM website.
*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
B211/B211M − 23
A,B,C,D
TABLE 1 Chemical Composition Limits
Other
E
Alloy Si Fe Cu Mn Mg Cr Ni Zn Ti Bi Pb Sn Elements Al, min
F
Each Total
G G
1100 0.95 Si + Fe 0.05–0.20 0.05 . . . . . . . . . 0.10 . . . . . . . . . . . . 0.05 0.15 99.00
2011 0.40 0.7 5.0–6.0 . . . . . . . . . . . . 0.30 . . . 0.20–0.6 0.20–0.6 . . . 0.05 0.15 rem
2111 0.40 0.7 5.0–6.0 . . . . . . . . . . . . 0.30 . . . 0.20–0.8 . . . 0.10–0.50 0.05 0.15 rem
2014 0.50–1.2 0.7 3.9–5.0 0.40–1.2 0.20–0.8 0.10 . . . 0.25 0.15 . . . . . . . . . 0.05 0.15 rem
2017 0.20–0.8 0.7 3.5–4.5 0.40–1.0 0.40–0.8 0.10 . . . 0.25 0.15 . . . . . . . . . 0.05 0.15 rem
2024 0.50 0.50 3.8–4.9 0.30–0.9 1.2–1.8 0.10 . . . 0.25 0.15 . . . . . . . . . 0.05 0.15 rem
H H
2219 0.20 0.30 5.8–6.8 0.20–0.40 0.02 . . . . . . 0.10 0.02–0.10 . . . . . . . . . 0.05 0.15 rem
3003 0.6 0.7 0.05–0.20 1.0–1.5 . . . . . . . . . 0.10 . . . . . . . . . . . . 0.05 0.15 rem
4032 11.0–13.5 1.0 0.50–1.3 . . . 0.8–1.3 0.10 0.5–1.3 0.25 . . . . . . . . . . . . 0.05 0.15 rem
5052 0.25 0.40 0.10 0.10 2.2–2.8 0.15–0.35 . . . 0.10 . . . . . . . . . . . . 0.05 0.15 rem
5056 0.30 0.40 0.10 0.05–0.20 4.5–5.6 0.05–0.20 . . . 0.10 . . . . . . . . . . . . 0.05 0.15 rem
5154 0.25 0.40 0.10 0.10 3.1–3.9 0.15–0.35 . . . 0.20 0.20 . . . . . . . . . 0.05 0.15 rem
6013 0.6–1.0 0.50 0.6–1.1 0.20–0.8 0.8–1.2 0.10 . . . 0.25 0.10 . . . . . . . . . 0.05 0.15 rem
6020 0.40–0.9 0.50 0.30–0.9 0.35 0.6–1.2 0.15 . . . 0.20 0.15 . . . 0.05 0.9–1.5 0.05 0.15 rem
6026 0.6–1.4 0.7 0.20–0.50 0.20–1.0 0.6–1.2 0.30 . . . 0.30 0.20 0.50–1.5 0.40 0.05 0.05 0.15 rem
6061 0.40–0.8 0.7 0.15–0.40 0.15 0.8–1.2 0.04–0.35 . . . 0.25 0.15 . . . . . . . . . 0.05 0.15 rem
6110 0.7–1.5 0.8 0.20–0.7 0.20–0.7 0.50–1.1 0.04–0.25 . . . 0.30 0.15 . . . . . . . . . 0.05 0.15 rem
6262 0.40–0.8 0.7 0.15–0.40 0.15 0.8–1.2 0.04–0.14 . . . 0.25 0.15 0.40–0.7 0.40–0.7 . . . 0.05 0.15 rem
6262A 0.40–0.8 0.7 0.15–0.40 0.15 0.8–1.2 0.04–0.14 . . . 0.25 0.10 0.40–0.9 . . . 0.40–1.0 0.05 0.15 rem
7075 0.40 0.50 1.2–2.0 0.30 2.1–2.9 0.18–0.28 . . . 5.1–6.1 0.20 . . . . . . . . . 0.05 0.15 rem
A
In case of any discrepancy in the values listed in this table when compared with those listed in the “Teal Sheets” (International Alloy Designations and Chemical
Composition Limits for Wrought Aluminum and Wrought Aluminum Alloys), the composition limits registered with The Aluminum Association and published in the “Teal
Sheets” shall be considered the controlling composition. The “Teal Sheets” are available at http://www.aluminum.org/tealsheets.
B
Limits are in mass percent maximum unless otherwise shown.
C
Analysis shall be made for the elements for which limits are shown in this table.
D
For purposes 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 figures used in expressing the specified limit, in accordance with the rounding-off method of Practice E29.
E
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.
F
Other Elements—Total: Total shall be the sum of unspecified metallic elements 0.010 % or more each, rounded to the second decimal before determining the sum.
G
The aluminum content is the difference between 100.00 % and the sum of all other metallic elements and silicon present in amounts of 0.010 % or more each, rounded
to the second decimal before determining the sum.
H
Vanadium 0.05–0.15 % zirconium 0.10–0.25 %. The total for other elements does not include vanadium and zirconium.
B557 Test Methods for Tension Testing Wrought and Cast Aluminum- and Magnesium-Alloy Products
B557M Test Methods for Tension Testing Wrought and Cast Aluminum- and Magnesium-Alloy Products (Metric)
B594 Practice for Ultrasonic Inspection of Aluminum-Alloy Wrought Products
B660 Practices for Packaging/Packing of Aluminum and Magnesium Products
B666/B666M Practice for Identification Marking of Aluminum and Magnesium Products
B881 Terminology Relating to Aluminum- and Magnesium-Alloy Products
B918/B918M Practice for Heat Treatment of Wrought Aluminum Alloys
B985 Practice for Sampling Aluminum Ingots, Billets, Castings and Finished or Semi-Finished Wrought Aluminum Products for
Compositional Analysis
E29 Practice for Using Significant Digits in Test Data to Determine Conformance with Specifications
E290 Test Methods for Bend Testing of Material for Ductility
E527 Practice for Numbering Metals and Alloys in the Unified Numbering System (UNS)
E607 Test Method for Atomic Emission Spectrometric Analysis Aluminum Alloys by the Point to Plane Technique Nitrogen
Atmosphere (Withdrawn 2011)
E716 Practices for Sampling and Sample Preparation of Aluminum and Aluminum Alloys for Determination of Chemical
Composition by Spark Atomic Emission Spectrometry
E1004 Test Method for Determining Electrical Conductivity Using the Electromagnetic (Eddy Current) Method
E1251 Test Method for Analysis of Aluminum and Aluminum Alloys by Spark Atomic Emission Spectrometry
E3061 Test Method for Analysis of Aluminum and Aluminum Alloys by Inductively Coupled Plasma Atomic Emission
Spectrometry (Performance Based Method)
G47 Test Method for Determining Susceptibility to Stress-Corrosion Cracking of 2XXX and 7XXX Aluminum Alloy Products
2.3 ANSI Standards:
H35.1/H35.1M Alloy and Temper Designation Systems for Aluminum
H35.2 [H35.2M] Dimensional Tolerances for Aluminum Mill Products
Available from American National Standards Institute (ANSI), 25 W. 43rd St., 4th Floor, New York, NY 10036, http://www.ansi.org.
B211/B211M − 23
A
TABLE 2 Mechanical Property Limits (US Customary)
Tensile Strength, ksi B B
Specified Diameter or
Yield Strength (0.2 % Elongation in 2 in. or
Temper
Thickness, in. offset), min, ksi 4× Diameter, min %
min max
Aluminum 1100
O 0.124 and under 11.0 15.5 . . . . . .
0.125 and over 11.0 15.5 3.0 25
H12 0.374 and under 14.0 . . . . . . . . .
H14 0.374 and under 16.0 . . . . . . . . .
H16 0.374 and under 19.0 . . . . . . . . .
H18 0.374 and under 22.0 . . . . . . . . .
H112 all 11.0 . . . 3.0 . . .
D D
F all . . . . . .
Alloy 2011
T3 0.125–1.500 45.0 . . . 38.0 10
1.501–2.000 43.0 . . . 34.0 12
2.001–3.500 42.0 . . . 30.0 12
E
T4 and T451 0.125–8.000 40.0 . . . 18.0 16
E
T6 and T651 0.375–6.500 54.0 . . . 40.0 10
T8 0.125–3.250 54.0 . . . 40.0 10
Alloy 2111
T8 0.500–3.500 52.0 . . . 38.0 10
F
Alloy 2014
O 0.124 and under . . . 35.0 . . . . . .
0.125–8.000 . . . 35.0 . . . 12
G E
T4, T42 , & T451 0.124 and under 55.0 . . . . . . . . .
H
0.125–8.000 55.0 . . . 32.0 16
G E
T6, T62 , & T651 0.124 and under 65.0 . . . . . . . . .
H
0.125–8.000 65.0 . . . 55.0 8
F
Alloy 2017
O 0.124 and under . . . 35.0 . . . . . .
0.125–8.000 . . . 35.0 . . . 16
G E
T4, T42 , & T451 0.124 and under 55.0 . . . . . . . . .
I
0.125–8.000 55.0 . . . 32.0 12
F
Alloy 2024
O 0.124 and under . . . 35.0 . . . . . .
0.125–8.000 . . . 35.0 . . . 16
T36 0.124 and under 69.0 . . . . . . . . .
0.125–0.375 69.0 . . . 52.0 10
J
T4 0.124 and under 62.0 . . . . . . . . .
J
0.125–0.499 62.0 . . . 45.0 10
H J
0.500–4.500 62.0 . . . 42.0 10
K
4.501–6.500 62.0 . . . 40.0 10
K
6.501–8.000 58.0 . . . 38.0 10
G
T42 0.124 and under 62.0 . . . . . . . . .
G
T42 0.125–1.000 62.0 . . . 40.0 10
H
1.001–6.500 62.0 . . . 40.0 10
E H
T351 0.500–6.500 62.0 . . . 45.0 10
6.501–8.000 62.0 . . . 45.0 9
T6 0.124 and under 62.0 . . . . . . . . .
H
0.125–6.500 62.0 . . . 50.0 5
G
T62 0.124 and under 60.0 . . . . . . . . .
H
0.125–6.500 60.0 . . . 46.0 5
E H
T851 0.500–6.500 66.0 . . . 58.0 5
Alloy 2219
E
T851 0.500–2.000 58.0 . . . 40.0 4
2.001–4.000 57.0 . . . 39.0 4
Alloy 3003
O all 14.0 19.0 5.0 25
H12 0.374 and under 17.0 . . . . . . . . .
H14 0.374 and under 20.0 . . . . . . . . .
H16 0.374 and under 24.0 . . . . . . . . .
H18 0.374 and under 27.0 . . . . . . . . .
H112 all 14.0 . . . 5.0 . . .
D D
F all . . . . . .
Alloy 4032
T86 0.375–0.750 51.0 . . . 46.0 4
Alloy 5052
O 0.124 and under . . . 32.0 . . . . . .
0.125 and over 25.0 32.0 9.5 25
H32 0.124 and under 31.0 . . . . . . . . .
0.125–0.374 31.0 . . . 23.0 . . .
H34 0.374 and under 34.0 . . . 26.0 . . .
H36 0.124 and under 37.0 . . . . . . . . .
0.125–0.374 37.0 . . . 29.0 . . .
H38 0.374 and under 39.0 . . . . . . . . .
D D
F all . . . . . .
B211/B211M − 23
TABLE 2 Continued
B B
Tensile Strength, ksi
Specified Diameter or
Yield Strength (0.2 % Elongation in 2 in. or
Temper
offset), min, ksi 4× Diameter, min %
Thickness, in.
min max
Alloy 5056
O 0.124 and under . . . 46.0 . . . . . .
0.125 and over . . . 46.0 . . . 20
H111 0.374 and under 44.0 . . . . . . . . .
H12 0.374 and under 46.0 . . . . . . . . .
H32 0.374 and under 44.0 . . . . . . . . .
H14 0.374 and under 52.0 . . . . . . . . .
H34 0.374 and under 50.0 . . . . . . . . .
H18 0.374 and under 58.0 . . . . . . . . .
H38 0.374 and under 55.0 . . . . . . . . .
H192 0.374 and under 60.0 . . . . . . . . .
H392 0.374 and under 58.0 . . . . . . . . .
Alloy 5154
O all 30.0 41.0 11.0 25
H32 0.374 and under 36.0 . . . . . . . . .
H34 0.374 and under 39.0 . . . . . . . . .
H36 0.374 and under 42.0 . . . . . . . . .
H38 0.374 and under 45.0 . . . . . . . . .
H112 all 30.0 . . . 11.0 . . .
Alloy 6013
E
T651 0.500–4.000 56.0 . . . 52.0 7
T8 0.750–1.500 58.0 . . . 56.0 8
1.501–5.500 57.0 . . . 55.0 7
Alloy 6020
T8 0.187–0.375 43.0 . . . 40.0 12
0.376–1.999 42.0 . . . 39.0 12
2.000–3.250 39.0 . . . 36.0 12
Alloy 6026
T6 0.200–3.000 54.0 . . . 44.0 6
T8 0.200–3.000 50.0 . . . 46.0 3
T9 0.200–3.000 52.0 . . . 48.0 3
F
Alloy 6061
O 0.124 and under . . . 22.0 . . . . . .
0.125–8.000 . . . 22.0 . . . 18
E
T4 & T451 0.124 and under 30.0 . . . . . . . . .
I
0.125–8.000 30.0 . . . 16.0 18
G I
T42 0.125–8.000 30.0 . . . 14.0 18
G E
T6, T62 , & T651 0.124 and under 42.0 . . . . . . . . .
I
0.125–8.000 42.0 . . . 35.0 10
T89 & T94 0.374 and under 54.0 . . . 47.0 . . .
Alloy 6110
T9 0.374 and under 65.0 . . . 63.0 2
Alloy 6262
E H
T6 & T651 0.125–8.000 42.0 . . . 35.0 10
T8 0.750–2.000 45.0 . . . 43.0 12
T9 0.125–2.000 52.0 . . . 48.0 5
2.001–3.000 50.0 . . . 46.0 5
F
Alloy 7075
O 0.124 and under . . . 40.0 . . . . . .
0.125–8.000 . . . 40.0 . . . 10
G
T6, T62 0.124 and under 77.0 . . . 66.0 . . .
L
0.125–4.000 77.0 . . . 66.0 7
E
T651 0.124 and under 77.0 . . . 66.0 . . .
L
0.125–4.000 77.0 . . . 66.0 7
4.001–6.000 75.0 . . . 64.0 7
6.001–7.000 73.0 . . . 62.0 7
E
T73 & T7351 0.124 and under 68.0 . . . . . . . . .
0.125–4.000 68.0 . . . 56.0 10
4.001–5.000 66.0 . . . 55.0 8
5.001–6.000 64.0 . . . 52.0 8
Temper Specified Diameter or Thickness, in Bend Diameter Factor, N
Alloy 2017
M
T4, T42, & T451 0.124 and under 3
I M
0.125–8.000 6
Alloy 2024
O 0.124 and under 1
T351, T4, T42 0.124 and under 3
0.125–6.500 6
Alloy 3003
O all 0
H12 0.374 and under 2
H14 0.374 and under 2
H16 0.374 and under 8
B211/B211M − 23
A
To determine conformance to this specification, each value for tensile strength and for yield strength shall be rounded to the nearest 0.1 ksi [1 MPa] and each value for
elongation to the nearest 0.5 %, both in accordance with the rounding-off method of Practice E29. The basis for establishment of tensile property limits is shown in Annex
A1.
B
The measurement of yield strength and elongation is not required for wire less than 0.125 in. [3.20 mm] in thickness or diameter.
C
Elongations in 50 mm applies to rectangular bar up through 12.5 mm thickness from which a standard rectangular tension test specimen is machined. The 5× diameter
s5.65 Ad requirements, where D and A are diameter and cross-sectional area of the specimen, respectively, apply to round specimens tested in fullsection or to standard
œ
or proportional, round-machined, tension test specimens.
D 1
There are no tensile requirements for material in the F temper but it usually can be expected that material 1 ⁄2 in. [40 mm] or less in thickness or diameter (except sections
over 4 in. [100 mm] in width) will have a strength about equivalent to the H14 or H34 temper. As size increases the strength decreases to nearly that of the O temper.
E
For stress-relieved tempers, characteristics and properties other than those specified may differ somewhat from the corresponding characteristics and properties of
material in the basic tempers.
F
Also available in the F temper for which no properties are specified or test results provided. Producers shall perform tension tests to confirm response to heat treatment
as required by Section 10.
G
Material in the T42 or T62 tempers is not available from the materials producers. These properties can usually be obtained by the user when material is properly solution
heat treated or solution and precipitation heat treated from the O or F temper. These properties also apply to samples of material in the O or F temper that are solution
heat treated or solution and precipitation heat treated by the producer to determine that the material will respond to proper heat treatment. Properties attained by the user,
however, may be lower than those listed if the material has been formed or otherwise cold or hot worked, particularly in the O temper, prior to solution heat treatment.
H
Properties listed for this full size increment are applicable to rod. Properties listed are also applicable to square, rectangular, hexagonal, or octagonal bar having a
2 2
maximum thickness of 4 in. [100 mm] and a maximum cross-sectional area of 36 in. [23 000 mm ].
I 2 2
For bar, maximum cross-sectional area is 50 in. [32 000 mm ].
J
Minimum yield strength for 2024-T4 wire and rod 0.125 in. [3.20 mm] and larger in thickness or diameter, produced in coil form for both straight length and coiled products,
is 40.0 ksi [275 MPa].
K
Properties listed for this size increment are applicable to rod only.
L
For rounds, maximum diameter is 4 in. [100 mm]; for square, hexagonal, or octagonal bar, maximum thickness is 3 ⁄2 in. [90 mm]; for rectangular bar, maximum thickness
is 3 in. [80 mm] with corresponding maximum width of 6 in. [150 mm]; for rectangular bar less than 3 in. [80 mm] in thickness, maximum width is 10 in. [250 mm].
M
Bend diameter factor values stated for this full size increment apply to T4 product only. Values listed also apply to T451 product in the 0.500–8.000 in. [12.20–200 mm]
size range.
2.4 Federal Standard:
Fed. Std. No. 123 Marking for Shipment (Civil Agencies)
2.5 Military Standard:
MIL-STD-129 Marking for Shipment and Storage
2.6 Aerospace Material Specification:
AMS 2772 Heat Treatment of Aluminum Alloy Raw Materials
2.7 The Aluminum Association:
International Alloy Designations and Chemical Composition Limits for Wrought Aluminum and Wrought Aluminum Alloys
(“Teal Sheets”)
Aluminum Standards & Data (AS&D)
Tempers for Aluminum and Aluminum Alloy Products (Yellow Sheets)
Tempers for Aluminum and Aluminum Alloy Products Metric Addition (Tan Sheets)
2.8 Other Standards:
CEN EN 14242 Aluminium and Aluminium Alloys–Chemical Analysis–Inductively Coupled Plasma Optical Emission Spectral
Analysis
3. Terminology
3.1 Definitions:
3.1.1 Refer to Terminology B881 for definitions of product terms in this specification.
3.1.2 flattened and slit wire—wire, n—Flattenedflattened wire which has been slit to obtain square edges.
3.2 Definitions of Terms Specific to This Standard:
3.2.1 capable of—of, adj—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. Ordering Information
4.1 Orders for material to this specification shall include the following information:
Available from Standardization Documents Order Desk, Bldg. 4 Section D, 700 Robbins Ave., Philadelphia, PA 19111-5094, Attn: NPODS.
Available from Society of Automotive Engineers (SAE), 400 Commonwealth Dr., Warrendale, PA 15096-0001.
Available from The Aluminum Association, Inc. 1400 Crystal Drive, Suite 430, Arlington, VA 22202, www.aluminum.org.
Available from European Committee for Standardization, Central Secretariat (CEN), rue de Stassart 36, B1050 Brussels, Belgium. http://www.cen.eu/esearch
B211/B211M − 23
A
TABLE 3 Mechanical Property Limits (Metric SI)
(See Table 2 for footnotes.)
B
Specified Diameter or Thickness,
Yield Strength (0.2 % offset),
B,C
Tensile Strength, MPa Elongation, min, %
MPa
mm
Temper
in 5× Diameter
over through min max min max in 50 mm
s5.65 Ad
œ
Aluminum 1100
O . . . 3.20 75 105 . . . . . . . . . . . .
3.20 . . . 75 105 20 . . . 25 22
H12 . . . 10.00 95 . . . . . . . . . . . . . . .
H14 . . . 10.00 110 . . . . . . . . . . . . . . .
H16 . . . 10.00 130 . . . . . . . . . . . . . . .
H18 . . . 10.00 150 . . . . . . . . . . . . . . .
H112 all 75 . . . 20 . . . . . . . . .
D D
F all . . . . . . . . . . . .
Alloy 2011
T3 3.20 40.00 310 . . . 260 . . . 10 9
40.00 50.00 295 . . . 235 . . . . . . 10
50.00 90.00 290 . . . 205 . . . . . . 12
E
T4 and T451 3.20 200.00 275 . . . 125 . . . 16 14
T6 and T651 10.00 160.00 370 . . . 275 . . . 10 9
T8 3.20 80.00 370 . . . 275 . . . 10 9
Alloy 2111
T8 12.70 88.90 360 . . . 260 . . . . . . 9
F
Alloy 2014
O . . . 3.20 . . . 240 . . . . . . . . . . . .
3.20 200.00 . . . 240 . . . . . . 12 10
G E
T4, T42 , & T451 . . . 3.20 380 . . . . . . . . . . . . . . .
H
3.20 200.00 380 . . . 220 . . . 16 14
G E
T6, T62 , & T651 . . . 3.20 450 . . . . . . . . . . . . . . .
H
3.20 200.00 450 . . . 380 . . . 8 7
F
Alloy 2017
O . . . 3.20 . . . 240 . . . . . . . . . . . .
3.20 200.00 . . . 240 . . . . . . 16 14
G E
T4, T42 , & T451 . . . 3.20 380 . . . . . . . . . . . . . . .
H,I
3.20 200.00 380 . . . 220 . . . 12 10
F
Alloy 2024
O . . . 3.20 . . . 240 . . . . . . . . . . . .
3.20 200.00 . . . 240 . . . . . . 16 14
T36 . . . 3.20 475 . . . . . . . . . . . . . . .
3.20 10.00 475 . . . 360 . . . 10 . . .
J
T4 . . . 3.20 425 . . . . . . . . . . . . . . .
J
3.20 12.50 425 . . . 310 . . . 10 . . .
H J
12.50 120.00 425 . . . 290 . . . . . . 9
K
120.00 160.00 425 . . . 275 . . . . . . 9
K
160.00 200.00 425 . . . 260 . . . . . . 9
G
T42 . . . 3.20 400 . . . . . . . . . . . . . . .
3.20 25.00 425 . . . 275 . . . 10 9
H
25.00 160.00 425 . . . 275 . . . . . . 9
E H
T351 12.50 160.00 425 . . . 310 . . . . . . 9
160.00 200.00 425 . . . 310 . . . . . . 8
T6 . . . 3.20 425 . . . . . . . . . . . . . . .
H
3.20 160.00 425 . . . 345 . . . 5 4
G
T62 . . . 3.20 415 . . . . . . . . . . . . . . .
H
3.20 160.00 415 . . . 315 . . . 5 4
E H
T851 12.50 160.00 455 . . . 400 . . . . . . 4
Alloy 2219
E
T851 12.50 50.00 400 . . . 275 . . . . . . 3
50.00 100.00 395 . . . 270 . . . . . . 3
Alloy 3003
O . . . 3.20 95 130 . . . . . . . . . . . .
3.20 . . . 95 130 35 . . . 25 22
H12 . . . 10.00 115 . . . . . . . . . . . . . . .
H14 . . . 10.00 140 . . . . . . . . . . . . . . .
H16 . . . 10.00 165 . . . . . . . . . . . . . . .
H18 . . . 10.00 185 . . . . . . . . . . . . . . .
H112 all 95 . . . 35 . . . . . . . . .
D D
F all . . . . . . . . . . . .
Alloy 4032
T86 10.00 20.00 350 . . . 315 . . . 4 3
Alloy 5052
O . . . 3.20 170 220 . . . . . . . . . . . .
3.20 . . . 170 220 65 . . . 25 22
H32 . . . 3.20 215 . . . . . . . . . . . . . . .
3.20 10.00 215 . . . 160 . . . . . . . . .
H34 . . . 3.20 235 . . . . . . . . . . . . . . .
3.20 10.00 235 . . . 180 . . . . . . . . .
B211/B211M − 23
TABLE 3 Continued
B
Specified Diameter or Thickness, Yield Strength (0.2 % offset),
B,C
Tensile Strength, MPa Elongation, min, %
MPa
mm
Temper
in 5× Diameter
over through min max min max in 50 mm
s5.65 Ad
œ
Alloy 5052 (Continued)
H36 . . . 3.20 255 . . . . . . . . . . . . . . .
3.20 10.00 255 . . . 200 . . . . . . . . .
D D
F all . . . . . . . . . . . .
Alloy 5056
O . . . 3.20 . . . 320 . . . . . . . . . . . .
3.20 . . . . . . 320 . . . . . . 20 18
H111 . . . 10.00 300 . . . . . . . . . . . . . . .
H12 . . . 10.00 315 . . . . . . . . . . . . . . .
H32 . . . 10.00 300 . . . . . . . . . . . . . . .
H14 . . . 10.00 360 . . . . . . . . . . . . . . .
H34 . . . 10.00 345 . . . . . . . . . . . . . . .
H18 . . . 10.00 400 . . . . . . . . . . . . . . .
H38 . . . 10.00 380 . . . . . . . . . . . . . . .
H192 . . . 10.00 415 . . . . . . . . . . . . . . .
H392 . . . 10.00 400 . . . . . . . . . . . . . . .
Alloy 5154
O . . . 3.20 205 285 . . . . . . . . . . . .
3.20 . . . 205 285 75 . . . 25 22
H32 . . . 10.00 250 . . . . . . . . . . . . . . .
H34 . . . 10.00 270 . . . . . . . . . . . . . . .
H36 . . . 10.00 290 . . . . . . . . . . . . . . .
H38 . . . 10.00 310 . . . . . . . . . . . . . . .
H112 all 205 . . . 75 . . . . . . . . .
Alloy 6013
E
T651 12.50 100.00 385 . . . 360 . . . . . . 6
T8 20.00 40.00 400 . . . 385 . . . . . . 7
40.00 140.00 395 . . . 380 . . . . . . 6
Alloy 6020
T8 5.00 10.00 295 . . . 275 . . . 12 . . .
10.00 50.00 290 . . . 270 . . . 12 10
50.00 80.00 270 . . . 250 . . . . . . 10
Alloy 6026
T6 5.00 80.00 370 . . . 300 . . . 6 8
T8 5.00 80.00 345 . . . 315 . . . 3 4
T9 5.00 80.00 360 . . . 330 . . . 3 4
F
Alloy 6061
O . . . 3.20 . . . 155 . . . . . . . . . . . .
3.20 200.00 . . . 155 . . . . . . 18 16
E
T4 & T451 . . . 3.20 205 . . . . . . . . . . . . . . .
I
3.20 200.00 205 . . . 110 . . . 18 16
G I
T42 3.20 200.00 205 . . . 95 . . . 18 16
G E
T6, T62 , & T651 . . . 3.20 290 . . . . . . . . . . . . . . .
I
3.20 200.00 290 . . . 240 . . . 10 9
T89 and T94 . . . 10.00 370 . . . 325 . . . . . . . . .
Alloy 6110
T9 . . . 10.00 450 . . . 435 . . . 2 . . .
Alloy 6262
E H
T6 and T651 3.20 200.00 290 . . . 240 . . . 10 9
T8 20.00 50.00 310 . . . 295 . . . 12 10
T9 3.20 50.00 360 . . . 330 . . . 5 4
50.00 80.00 345 . . . 315 . . . . . . 4
F
Alloy 7075
O . . . 3.20 . . . 275 . . . . . . . . . . . .
3.20 200.00 . . . 275 . . . . . . 10 9
G
T6, T62 . . . 3.20 530 . . . 455 . . . . . . . . .
L
3.20 100.00 530 . . . 455 . . . 7 6
E
T651 . . . 3.20 530 . . . 455 . . . . . . . . .
L
3.20 100.00 530 . . . 455 . . . 7 . . .
100.00 160.00 515 . . . 440 . . . 7 . . .
160.00 200.00 505 . . . 425 . . . 7 . . .
E
T73 and T7351 . . . 3.20 470 . . . . . . . . . . . . . . .
3.20 100.00 470 . . . 425 . . . 10 9
100.00 120.00 455 . . . 380 . . . 8 9
120.00 160.00 440 . . . 360 . . . . . . 7
B211/B211M − 23
Specified Diameter or Thickness, mm
Temper Bend Diameter Factor, N
over through
Alloy 2017
M
T4, T42, and T451 . . . 3.20 3
I M
3.20 200.00 6
Alloy 2024
O . . . 3.20 1
T351, T4, and T42 . . . 3.20 3
3.20 160.00 6
Alloy 3003
O all 0
H12 . . . 10.00 2
H14 . . . 10.00 2
H16 . . . 10.00 8
(See Table 2 for footnotes.)
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 pounds [kilograms],
4.1.3 Alloy (Section 7),
4.1.4 Temper (Section 9),
4.1.5 Product Form, rolled or cold finished bar, rolled or cold finished rod, or wire,
4.1.6 Geometry and Dimensions, Diameter for rounds; distance across flats for square-cornered squares, hexagons, or octagons;
width and depth for square-cornered rectangles (orders for squares, hexagons, octagons, or rectangles with rounded corners usually
require a drawing),
4.1.7 Length, and
4.1.8 Tensile property limits and dimensional tolerances for sized not covered in Table 2 [Table 3] and in ANSI H35.2 [H35.2M],
respectively.
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 B918/B918M is required (8.2),
4.2.2 Whether 7075-O material is required to develop requirements for T73 temper (see 10.1.2),
4.2.3 Whether bend testing is required for 2017, 2024, or 3003 (Section 12),
4.2.4 When specified finish of bar and rod is not required (Section 15),
4.2.5 Whether marking for identification is required (Section 16),
4.2.6 Whether
...