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  • ASTM
    B210-12 Standard Specification for Aluminum and Aluminum-Alloy Drawn Seamless Tubes
    Edition: 2012
    $103.58
    Unlimited Users per year

Description of ASTM-B210 2012

ASTM B210-12

Historical Standard: Standard Specification for Aluminum and Aluminum-Alloy Drawn Seamless Tubes




ASTM B210

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 0.083 in. and only in nonheat-treatable alloys.

1.2 Alloy and temper designations are in accordance with ANSI H35.1/H35.1(M). The equivalent Unified Numbering System alloy designations are those of Table 1 preceded by A9, for example, A91100 for aluminum designation 1100 in accordance with Practice E527.

Note 1—See Specification B483/B483M for aluminum-alloy drawn tubes for general purpose applications; Specification B234 for aluminum-alloy drawn seamless tubes for condensers and heat exchangers; and Specification B241/B241M for aluminum-alloy seamless pipe and seamless extruded tube.

Note 2—Throughout this specification, use of the term alloy in the general sense includes aluminum as well as aluminum alloy.

1.3 A complete metric companion to Specification B210 has been developedSpecification B210M; therefore, no metric equivalents are presented in this specification.

1.4 For acceptance criteria for inclusion of new aluminum and aluminum alloys in this specification, see Annex A2.

1.5 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 appropriate safety and health practices and determine the applicability of regulatory limitations prior to use.

TABLE 1 Chemical Composition LimitsA, B, C, D

Alloy Silicon Iron Copper Manganese Magnesium Chromium Zinc Titanium Bismuth Lead Other ElementsE Aluminum,
min
Each TotalF
1060 0.25 0.35 0.05 0.03 0.03 ... 0.05 0.03 0.03G ... 99.60 minH
1100 0.95 Si + Fe 0.050.20 0.05 ... ... 0.10 ... 0.05 0.15 99.00 minH
2011 0.40 0.7 5.06.0 ... ... ... 0.30 ... 0.200.6 0.200.6 0.05 0.15 remainder
2014 0.501.2 0.7 3.95.0 0.401.2 0.200.8 0.10 0.25 0.15 0.05 0.15 remainder
2024 0.50 0.50 3.84.9 0.300.9 1.21.8 0.10 0.25 0.15 0.05 0.15 remainder
3003 0.6 0.7 0.050.20 1.01.5 ... ... 0.10 ... 0.05 0.15 remainder
Alclad 3003I
3102 0.40 0.7 0.10 0.050.40 ... ... 0.30 0.10 0.05 0.15 remainder
Alclad 3102J
5005 0.30 0.7 0.20 0.20 0.501.1 0.10 0.25 ... 0.05 0.15 remainder
5050 0.40 0.7 0.20 0.10 1.11.8 0.10 0.25 ... 0.05 0.15 remainder
5052 0.25 0.40 0.10 0.10 2.22.8 0.150.35 0.10 ... 0.05 0.15 remainder
5083
5086
0.40
0.40
0.40
0.50
0.10
0.10
0.401.0
0.200.7
4.04.9
3.54.5
0.050.25
0.050.25
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 3.13.9 0.150.35 0.20 0.20 0.05 0.15 remainder
5456 0.25 0.40 0.10 0.501.0 4.75.5 0.050.20 0.25 0.20 0.05 0.15 remainder
6061 0.400.8 0.7 0.150.40 0.15 0.81.2 0.040.35 0.25 0.15 0.05 0.15 remainder
6063 0.200.6 0.35 0.10 0.10 0.450.9 0.10 0.10 0.10 0.05 0.15 remainder
6262 0.400.8 0.7 0.150.40 0.15 0.81.2 0.040.14 0.25 0.15 0.400.7 0.400.7 0.05 0.15 remainder
7072 cladding 0.7 Si + Fe 0.10 0.10 0.10 ... 0.81.3 ... 0.05 0.15 remainder
7075K 0.40 0.50 1.22.0 0.30 2.12.9 0.180.28 5.16.1 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 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.

D In case of a discrepancy in the values listed in Table 1 with those listed in the International Alloy Designations and Chemical Composition Limits for Wrought Aluminum and Wrought Aluminum Alloys (known as the Teal Sheets), 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.

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 elementsTotal shall be the sum of unspecified metallic elements 0.010 % or more, rounded to the second decimal before determining the sum.

G Vanadium 0.05 % max.

H 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.

I Alloy clad with Alloy 7072.

J 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.

K A Zr +Ti limit of 0.25 percent maximum may be used with this alloy designation for extruded and forged products only, but only when the supplier or producer and the purchaser have mutually so agreed. Agreement may be indicated, for example, by reference to a standard, by letter, by order note, or other means which allow the Zr +Ti limit.

TABLE 2 Tensile Property LimitsA,B

Temper Specified Wall
Thickness,C in.
Tensile Strength, ksi Yield StrengthD
(0.2 % offset),
min, ksi
Elongation in 2 in. or 4 × Diameter,E min, %
min max Full-Section
Specimen
Cut-Out
Specimen
Aluminum 1060F
O 0.0140.500 8.5 13.5 2.5 ... ...
H12 10.0 ... 4.0 ... ...
H14 12.0 ... 10.0 ... ...
H18 16.0 ... 13.0 ... ...
H113G 8.5 ... 2.5 ... ...
Aluminum 1100F
O 0.0100.500 11.0 15.5 3.5 ... ...
H12 14.0 ... 11.0 ... ...
H14 16.0 ... 14.0 ... ...
H16 19.0 ... 17.0 ... ...
H18 22.0 ... 20.0 ... ...
H113G 11.0 3.5
Alloy 2011
T3 0.0180.049 47.0 ... 40.0 ... ...
0.0500.500 47.0 ... 40.0 10 8
T4511 0.0180.049 44.0 ... 25.0 ...
...
...
...
0.0500.259 44.0 ... 25.0 20 18
0.2600.500 44.0 ... 25.0 20 20
T8 0.0180.500 58.0 ... 46.0 10 8
Alloy 2014
O 0.0180.500 ... 32.0 16.0 max ... ...
T4, T42H 0.0180.024 54.0 ... 30.0 10 ...
0.0250.049 54.0 ... 30.0 12 10
0.0500.259 54.0 ... 30.0 14 10
0.2600.500 54.0 ... 30.0 16 12
T6, T62H 0.0180.024 65.0 ... 55.0 7 ...
0.0250.049 65.0 ... 55.0 7 6
0.0500.259 65.0 ... 55.0 8 7
0.2600.500 65.0 ... 55.0 9 8
Alloy 2024
O 0.0180.500 ... 32.0 15.0 max ... ...
T3 0.0180.024 64.0 ... 42.0 10 ...
0.0250.049 64.0 ... 42.0 12 10
0.0500.259 64.0 ... 42.0 14 10
0.2600.500 64.0 ... 42.0 16 12
T42H 0.0180.024 64.0 ... 40.0 10 ...
0.0250.049 64.0 ... 40.0 12 10
0.0500.259 64.0 ... 40.0 14 10
0.2600.500 64.0 ... 40.0 16 12
Alloy 3003F
O 0.0100.024 14.0 19.0 5.0 ... ...
0.0250.049 14.0 19.0 5.0 30 20
0.0500.259 14.0 19.0 5.0 35 25
0.2600.500 14.0 19.0 5.0 ... 30
H12 0.0100.500 17.0 ... 12.0 ... ...
H14 0.0100.024 20.0 ... 17.0 3 ...
0.0250.049 20.0 ... 17.0 5 3
0.0500.259 20.0 ... 17.0 8 4
0.2600.500 20.0 ... 17.0 ... ...
H16 0.0100.024 24.0 ... 21.0 ... ...
0.0250.049 24.0 ... 21.0 3 2
0.0500.259 24.0 ... 21.0 5 4
0.2600.500 24.0 ... 21.0 ... ...
H18 0.0100.024 27.0 ... 24.0 2 ...
0.0250.049 27.0 ... 24.0 3 2
0.0500.259 27.0 ... 24.0 5 3
0.2600.500 27.0 ... 24.0 ... ...
H113G 0.0100.500 14.0 ... 5.0 ... ...
Alloy Alclad 3003F
O 0.0100.024 13.0 19.0 4.5 ... ...
0.0250.049 13.0 19.0 4.5 30 20
0.0500.259 13.0 19.0 4.5 35 25
0.2600.500 13.0 19.0 4.5 ... 30
H14 0.0100.024 19.0 ... 16.0 ... ...
0.0250.049 19.0 ... 16.0 5 3
0.0500.259 19.0 ... 16.0 8 4
0.2600.500 19.0 ... 16.0 ... ...
H18 0.0100.500 26.0 ... 23.0 ... ...
H113G 0.0100.500 13.0 ... 4.5 ... ...
Alloy 3102F
O 0.0180.049 12.0 17.0 4.0 30I 20I
0.0500.065 12.0 17.0 4.0 35 25
Alloy Alclad 3102F
O 0.0180.049 10.0 17.0 3.5 30I 20I
25
0.0500.065 10.0 17.0 3.5 35
Alloy 5005F
O 0.0180.500 15.0 21.0 5.0 ... ...
Alloy 5050F
O 0.0100.500 18.0 24.0 6.0 ... ...
H32 0.0100.500 22.0 ... 16.0 ... ...
H34 0.0100.500 25.0 ... 20.0 ... ...
H36 0.0100.500 27.0 ... 22.0 ... ...
H38 0.0100.500 29.0 ... 24.0 ... ...
Alloy 5052F
O 0.0100.450 25.0 35.0 10.0 ... ...
H32 0.0100.450 31.0 ... 23.0 ... ...
H34 0.0100.450 34.0 ... 26.0 ... ...
H36 0.0100.450 37.0 ... 29.0 ... ...
H38 0.0100.450 39.0 ... 24.0 ... ...
Alloy 5083F
O 0.0180.450 39.0 51.0 16.0 ... 14
Alloy 5086F
O 0.0100.450 35.0 46.0 14.0 ... ...
H32 0.0100.450 40.0 ... 28.0 ... ...
H34 0.0100.450 44.0 ... 34.0 ... ...
H36 0.0100.450 47.0 ... 38.0 ... ...
Alloy 5154F
O 0.0100.500 30.0 41.0 11.0 10 10
H34 0.0100.500 39.0 ... 29.0 5 5
H38 0.0100.250 45.0 ... 34.0 ... ...
Alloy 5456F
O 0.0180.450 41.0 53.0 19.0 ... 14
Alloy 6061
O 0.0180.500 ... 22.0 14.0 max 15 15
T4 0.0250.049 30.0 ... 16.0 16 14
0.0500.259 30.0 16.0 18 16
0.2600.500 30.0 ... 16.0 20 18
T42H 0.0250.049 30.0 ... 14.0 16 14
0.0500.259 30.0 ... 14.0 18 16
0.2600.500 30.0 ... 14.0 20 18
T6, T62H 0.0250.049 42.0 ... 35.0 10 8
0.0500.259 42.0 ... 35.0 12 10
0.2600.500 42.0 ... 35.0 14 12
Alloy 6063
O 0.0180.500 ... 19.0 ... ... ...
T4, T42H 0.0250.049 22.0 ... 10.0 16 14
0.0500.259 22.0 ... 10.0 18 16
0.2600.500 22.0 ... 10.0 20 18
T6, T62H 0.0250.049 33.0 ... 28.0 12 8
0.0500.259 33.0 ... 28.0 14 10
0.2600.500 33.0 ... 28.0 16 12
T83 0.0250.259 33.0 ... 30.0 5 ...
T831 0.0250.259 28.0 ... 25.0 5 ...
T832 0.0250.049 41.0 ... 36.0 8 5
0.0500.259 40.0 ... 35.0 8 5
Alloy 6262
T6, T62H 0.0250.049 42.0 ... 35.0 10 8
0.0500.259 42.0 ... 35.0 12 10
0.2600.500 42.0 ... 35.0 14 12
T9 0.0250.375 48.0 ... 44.0 5 4
Alloy 7075
O 0.0250.049 ... 40.0 21.0 maxJ 10 8
0.0500.500 ... 40.0 21.0 maxJ 12 10
T6, T62H 0.0250.259 77.0 ... 66.0 8 7
0.2600.500 77.0 ... 66.0 9 8
T73K 0.0250.259 66.0 ... 56.0 10 8
0.2600.500 66.0 ... 56.0 12 10

A See Annex A1.

B To determine conformance to this specification, each value for tensile strength and for yield strength shall be rounded to the nearest 0.1 ksi and each value for elongation to the nearest 0.5 % both in accordance with the rounding-off method of Practice E29.

C Coiled tube is generally available with a maximum wall thickness of 0.083 in. and only in nonheat-treatable alloys.

D Yield strength to be determined only on straight tube.

E Elongation of full-section and cut-out sheet-type specimens is measured in 2 in. of cut-out round specimens, in 4× specimen diameter.

F In this alloy tube other than round is produced only in the F (as drawn) and O tempers. Properties for F temper are not specified or guaranteed.

G Beginning with the 1982 issue the requirements for the H112 tempers were replaced by the H113 temper, applicable to other than round tube, which is fabricated by cold-forming annealed round tube and acquires some temper in this forming operation.

H Material in the T42 or T62 tempers is not available from the material producers.

I For specified wall thickness under 0.025 in., elongation is not required.

J Applicable only to round tube. The maximum yield strength for other-than-round tube shall be negotiated.

K Material in this temper exhibits improved resistance to stress corrosion compared to that of the T6 temper. The stress-corrosion resistance capability of individual lots is determined by testing the previously selected tension-test samples in accordance with the applicable electrical conductivity acceptance criteria of Table 3.

TABLE 3 Lot Acceptance Criteria for Resistance to Stress-Corrosion

Alloy and Temper Lot Acceptance Criteria Lot Acceptance Status
Electrical Conductivity, A, B %
IACS
Level of Mechanical Properties
7075T73 40.0 or greater per specified requirements acceptable
38.0 through 39.9 per specified requirements and yield strength does not exceed minimum by more than 11.9 ksi acceptable
38.0 through 39.9 per specified requirements but yield strength exceeds minimum by 12.0 ksi or more unacceptableC
less than 38.0 any level unacceptableC
A The electrical conductivity shall be determined in accordance with Practice E1004 in the locations noted below.
B For curved surfaces, the conductivity shall be measured on a machined flat spot; however, for small size tubes, a cut-out piece may be flattened and the conductivity determined.
C When material is found to be unacceptable, it shall be reprocessed (additional precipitation heat treatment or resolution heat treatment and precipitation heat treatment).
Wall Thickness, in. Location
up through 0.100 surface of tensile sample
0.101 and over subsurface after removal of
approximately 10 % of thickness.

Keywords

aluminum alloy; aluminum-alloy drawn seamless tubes


ICS Code

ICS Number Code 77.150.10 (Aluminium products)


DOI: 10.1520/B0210-12

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