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ASTM B210M.pdf
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ASTM B210M.pdf
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Designation: B 210M – 05
METRIC
Standard Specification for
Aluminum and Aluminum-Alloy Drawn Seamless Tubes
[Metric]
1
This standard is issued under the fixed designation B 210M; 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.
1. Scope*
1.1 This specification covers aluminum and aluminum-alloy
drawn seamless tubes in straight lengths and coils for general
purpose and pressure applications in alloys (
Note 2), tempers,
and thicknesses shown in
Table 2. Coiled tubes are generally
available only as round tubes with a wall thickness not
exceeding 2.00 mm and only in nonheat-treatable alloys.
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.
1.3 Preferred metric sizes are in accordance with ANSI
B 32.5.
NOTE 1—See Specification B 483M for aluminum and aluminum-alloy
drawn tubes for general purpose applications, Specification
B 234M for
aluminum-alloy drawn seamless tubes for condensers and heat exchang-
ers, and Specification
B 241/B 241M for aluminum-alloy seamless pipe
and seamless extruded tube.
N
OTE 2—Throughout this specification use of the term alloy in the
general sense includes aluminum as well as aluminum alloy.
1.4 This specification is the metric counterpart of Specifi-
cation B 210.
1.5 For acceptance criteria for inclusion of new aluminum
and aluminum alloys in this specification, see
Annex A2.
1.6 The values stated in SI units are to be regarded as
standard. No other units of measure are included in this
standard.
1.7 This standard does not purport to address all of the
safety concerns, if any, associated with its use. It is the
responsibility of the user of this standard to establish appro-
priate safety and health practices and determine the applica-
bility of regulatory limitations prior to use.
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:
2
B 234M Specification for Aluminum and Aluminum-Alloy
Drawn Seamless Tubes for Condensers and Heat Exchang-
ers
B 241/B 241M Specification for Aluminum and Aluminum-
Alloy Seamless Pipe and Seamless Extruded Tube
B 483M Specification for Aluminum and Aluminum-Alloy
Drawn Tubes for General Purpose Applications
B 557M Test Methods of Tension Testing Wrought and Cast
Aluminum- and Magnesium-Alloy Products [Metric]
B 660 Practices for Packaging/Packing of Aluminum and
Magnesium Products
B 666/B 666M Practice for Identification Marking of Alu-
minum and Magnesium Products
B 881 Terminology Relating to Aluminium- and
Magnesium-Alloy Products
B 918 Practice for Heat Treatment of Wrought Aluminum
Alloys
E29 Practice for Using Significant Digits in Test Data to
Determine Conformance with Specifications
E34 Test Methods for Chemical Analysis of Aluminum and
Aluminum-Base Alloys
E55 Practice for Sampling Wrought Nonferrous Metals and
Alloys for Determination of Chemical Composition
E 215 Practice for Standardizing Equipment for Electro-
magnetic Examination of Seamless Aluminum-Alloy Tube
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
1
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 June 1, 2005. Published June 2005. Originally
approved in 1980. Last previous edition approved in 2002 as B 210M – 02.
2
For referenced ASTM standards, visit the ASTM website, www.astm.org, or
Standards volume information, refer to the standard’s Document Summary page on
the ASTM website.
1
*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.
Copyright by ASTM Int'l (all rights reserved);
Reproduction authorized per License Agreement with Kathe Hooper (ASTMIHS Account); Wed Jun 22 12:10:52 EDT 2005
Copyright ASTM International
Reproduced by IHS under license with ASTM
Not for Resale
No reproduction or networking permitted without license from IHS
--`,,`,``-`-`,,`,,`,`,,`---
E 716 Practices for Sampling Aluminum and Aluminum
Alloys for Spectrochemical Analysis
E 1004 Practice for Determining Electrical Conductivity
Using the Electromagnetic (Eddy-Current) Method
E 1251 Test Method for Optical Emission Spectrometric
Analysis of Aluminum and Aluminum Alloys by the Argon
Atmosphere, Point-to-Plane, Unipolar Self-Initiating Ca-
pacitor Discharge
2.3 ANSI Standards:
3
B 32.5 Preferred Metric Sizes For Tubular Metal Products
Other Than Pipe
H35.1M Alloy and Temper Designation Systems for Alu-
minum
H35.2M Dimensional Tolerances for Aluminum Mill Prod-
ucts
2.4 Military Standard:
4
MIL-STD-129 Marking for Shipment and Storage
2.5 AMS Specification:
5
AMS 2772 Heat Treatment of Aluminum Alloy Raw Mate-
rials
2.6 Federal Standard:
4
Fed. Std. No. 123 Marking for Shipment (Civil Agencies)
3. Terminology
3.1 Definitions: Refer to Terminology
B 881 for definitions
of product terms used in this specification.
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 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:
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 (Section
7),
4.1.4 Temper (Section
8),
3
Available from American National Standards Institute (ANSI), 25 W. 43rd St.,
4th Floor, New York, NY 10036.
4
Available from Standardization Documents Order Desk, Bldg. 4 Section D, 700
Robbins Ave., Philadelphia, PA 19111-5098.
5
Available from Society of Automotive Engineers (SAE), 400 Commonwealth
Dr., Warrendale, PA 15096-0001.
TABLE 1 Chemical Composition Limits
ABC
Alloy Silicon Iron Copper Manganese Magnesium Chromium Zinc Titanium
Other Elements
D
Aluminum,
min
Each Total
E
1060 0.25 0.35 0.05 0.03 0.03 ... 0.05 0.03 0.03
F
... 99.60 min
G
1100 0.95 Si + Fe 0.05–0.20 0.05 ... ... 0.10 ... 0.05 0.15 99.00 min
G
2011 0.40 0.7 5.0–6.0 ... ... ... 0.30 ... 0.05
H
0.15 remainder
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 remainder
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 remainder
3003 0.6 0.7 0.05–0.20 1.0–1.5 ... ... 0.10 ... 0.05 0.15 remainder
Alclad 3003
I
3102 0.40 0.7 0.10 0.05–0.40 ... ... 0.30 0.10 0.05 0.15 remainder
Alclad 3102
I
5005 0.30 0.7 0.20 0.20 0.50–1.1 0.10 0.25 ... 0.05 0.15 remainder
5050 0.40 0.7 0.20 0.10 1.1–1.8 0.10 0.25 ... 0.05 0.15 remainder
5052 0.25 0.40 0.10 0.10 2.2–2.8 0.15–0.35 0.10 ... 0.05 0.15 remainder
5083
5086
0.40
0.40
0.40
0.50
0.10
0.10
0.40–1.0
0.20–0.7
4.0–4.9
3.5–4.5
0.05–0.25
0.05–0.25
0.25
0.25
0.15
0.15
0.05
0.05
0.15
0.15
remainder
remainder
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 remainder
5456 0.25 0.40 0.10 0.50–1.0 4.7–5.5 0.05–0.20 0.25 0.20 0.05 0.15 remainder
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 remainder
6063 0.20–0.6 0.35 0.10 0.10 0.45–0.9 0.10 0.10 0.10 0.05 0.15 remainder
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 0.05
J
0.15 remainder
7072 cladding
K
0.7 Si + Fe 0.10 0.10 0.10 ... 0.8–1.3 ... 0.05 0.15 remainder
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 remainder
A
Limits are in weight percent maximum unless shown as a range or otherwise stated.
B
Analysis shall be made for the elements for which limits are shown in this table.
C
For purposes of determining conformance to these limits, an observed value or a calculated value obtained from analysis shall be rounded to the nearestunitinthe
last right-hand place of figures used in expressing the specified limit, in accordance with the rounding-off method of Practice
E29.
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.
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, roundedtothe
second decimal before determining the sum.
H
Bismuth and lead each 0.20 − 0.6 %.
I
Alloy clad with Alloy 7072.
J
Bismuth and lead each 0.40–0.7 %.
K
Composition of cladding alloy as applied during the course of manufacture. The samples from finished tube shall not be required to conform to these limits.
B210M–05
2
Copyright by ASTM Int'l (all rights reserved);
Reproduction authorized per License Agreement with Kathe Hooper (ASTMIHS Account); Wed Jun 22 12:10:52 EDT 2005
Copyright ASTM International
Reproduced by IHS under license with ASTM
Not for Resale
No reproduction or networking permitted without license from IHS
--`,,`,``-`-`,,`,,`,`,,`---
TABLE 2 Tensile Property Limits
A,B
Temper
Specified Wall Thickness
C
Tensile Strength, MPa
Yield Strength
D
(0.2 % offset), MPa
Elongation,
E
min, %
Over Through Min Max Min Max
Full-Section
Specimen in
50 mm
Cut-Out Specimen
in 50 mm
in 5 3 Diam-
eter
(5.65
=
A )
Aluminum 1060
F
O 0.25 12.50 60 95 15 ... ... ... ...
H12 0.25 12.50 70 ... 30 ... ... ... ...
H14 0.25 12.50 85 ... 70 ... ... ... ...
H18 0.25 12.50 110 ... 90 ... ... ... ...
H113
G
0.25 12.50 60 ... 15 ... ... ... ...
F All ... ... ... ... ... ... ...
Aluminum 1100
F
O 0.32 12.50 75 105 25 ... ... ... ...
H12 0.32 12.50 95 ... 75 ... ... ... ...
H14 0.32 12.50 110 ... 95 ... ... ... ...
H16 0.32 12.50 130 ... 115 ... ... ... ...
H18 0.32 12.50 150 ... 140 ... ... ... ...
H113
G
0.32 12.50 75 ... 25 ... ... ... ...
F All ... ... ... ... ... ... ...
Alloy 2011
T3 0.45 1.20 325 ... 275 ... ... ... ...
1.20 12.50 325 ... 275 ... 10 8 7
T4511 0.45 1.20 305 ... 170 ... ... ... ...
1.20 6.30 305 ... 170 ... 20 18 16
6.30 12.50 305 ... 170 ... 20 20 18
T8 0.45 12.50 400 ... 315 ... 10 8 7
Alloy 2014
O 0.45 12.50 ... 220 ... 110 ... ... ...
T4, T42
H
0.45 0.63 370 ... 205 ... 10 ... ...
0.63 1.20 370 ... 205 ... 12 10 ...
1.20 6.30 370 ... 205 ... 14 10 ...
6.30 12.50 370 ... 205 ... 16 12 10
T6, T62
H
0.45 0.63 450 ... 380 ... 7 ... ...
0.63 1.20 450 ... 380 ... 7 6 ...
1.20 6.30 450 ... 380 ... 8 7 ...
6.30 12.50 450 ... 380 ... 9 8 7
Alloy 2024
O 0.45 12.50 ... 220 ... 100 ... ... ...
T3 0.45 0.63 440 ... 290 ... 10 ... ...
0.63 1.20 440 ... 290 ... 12 10 ...
1.20 6.30 440 ... 290 ... 14 10 ...
6.30 12.50 440 ... 290 ... 16 12 10
T42
H
0.45 0.63 440 ... 275 ... 10 ... ...
0.63 1.20 440 ... 275 ... 12 10 ...
1.20 6.30 440 ... 275 ... 14 10 ...
6.30 12.50 440 ... 275 ... 16 12 10
Alloy 3003
F
O 0.25 0.63 95 130 35 ... ... ... ...
0.63 1.20 95 130 35 ... 30 20 ...
1.20 6.30 95 130 35 ... 35 25 ...
6.30 12.50 95 130 35 ... ... 30 27
H12 0.25 0.63 120 ... 85 ... ... ... ...
0.63 1.20 120 ... 85 ... ... ... ...
H14 ... 0.63 140 ... 115 ... 3 ... ...
0.63 1.20 140 ... 115 ... 5 3 ...
1.20 6.30 140 ... 115 ... 8 4 ...
6.30 12.50 140 ... 115 ... ... ... ...
H16 0.25 0.63 165 ... 145 ... ... ... ...
0.63 1.20 165 ... 145 ... 3 2 ...
1.20 6.30 165 ... 145 ... 5 4 ...
6.30 12.50 165 ... 145 ... ... ... ...
H18 ... 0.63 185 ... 165 ... 2 ... ...
0.63 1.20 185 ... 165 ... 3 2 ...
1.20 6.30 185 ... 165 ... 5 3 ...
6.30 12.50 185 ... 165 ... ... ... ...
H113
G
0.25 12.50 95 ... 35 ... ... ... ...
B210M–05
3
Copyright by ASTM Int'l (all rights reserved);
Reproduction authorized per License Agreement with Kathe Hooper (ASTMIHS Account); Wed Jun 22 12:10:52 EDT 2005
Copyright ASTM International
Reproduced by IHS under license with ASTM
Not for Resale
No reproduction or networking permitted without license from IHS
--`,,`,``-`-`,,`,,`,`,,`---
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