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ASTM International - ASTM B221-12

Standard Specification for Aluminum and Aluminum-Alloy Extruded Bars, Rods, Wire, Profiles, and Tubes

inactive
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Organization: ASTM International
Publication Date: 15 January 2012
Status: inactive
Page Count: 14
ICS Code (Aluminium products): 77.150.10
scope:

1.1 This specification covers aluminum and aluminum-alloy extruded bars, rods, wire, profiles, and tubes in the aluminum alloys (Note 1) and tempers shown in Table 2.

Note 1-Throughout this specification, the use of the term alloy in the general sense includes aluminum as well as aluminum alloy.

Note 2-For rolled or cold-finished bar and rod refer to Specification B211, for drawn seamless tube used in pressure applications, Specification B210, for structural pipe and tube, Specification B429/B429M, and for seamless pipe and tube used in pressure applications, Specification B241/B241M.

Note 3-Structural pipe and tube produced in accordance with B221 is not intended for fluid-carrying applications involving pressure. Refer to either Specification B210 or B241/B241M, as appropriate, for seamless pipe and tube used in fluid-carrying applications involving pressure.

1.2 Alloy and temper designations are in accordance with ANSI H35.1/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 E527.

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

1.4 A complete metric companion to B221 has been developedB221M; therefore, no metric equivalents are presented in this specification.

TABLE 1 Chemical Composition Limits A,B,C

Note-In case of a discrepancy between the values listed in Table 2 and 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" should be considered the controlling composition. The "Teal Sheets" are available at http://www.aluminum.org/tealsheets.

AlloySiliconIronCopper Manga-
nese
Magne-
sium
ChromiumZincTitaniumVanadium Other Elements

D

Aluminum
EachTotal

E

1060 0.250.350.050.030.03...0.050.03 0.050.03...99.60 min

F

11000.95 Si + Fe0.05-0.200.05... ...0.10......0.05

G

0.1599.00 min

F

2014 0.50-1.20.73.9-5.00.40-1.20.20-0.80.100.250.15

H

...0.05

H

0.15remainder
2024 0.500.503.8-4.90.30-0.91.2-1.80.100.250.15

H

...0.05

H

0.15remainder
2219 0.200.305.8-6.80.20-0.400.02 ...0.100.02-0.100.05-0.150.05

I

0.15

I

remainder
3003 0.60.70.05-0.201.0-1.5... ...0.10......0.050.15remainder
Alclad 3003... 3003 Clad with 7072 alloy ..................... ...
3004 0.300.70.251.0-1.50.8-1.3...0.25......0.05 0.15remainder
3102 0.400.70.100.05-0.40... ...0.300.10...0.050.15remainder
5052 0.250.400.100.102.2-2.8 0.15-0.350.10......0.05 0.15remainder
5083 0.400.400.100.40-1.04.0-4.90.05-0.250.25 0.15...0.050.15remainder
5086 0.400.500.100.20-0.73.5-4.50.05-0.250.25 0.15...0.050.15remainder
5154 0.250.400.100.103.1-3.9 0.15-0.350.200.20...0.05

G

0.15remainder
5454 0.250.400.100.50-1.02.4-3.00.05-0.200.25 0.20...0.050.15remainder
5456 0.250.400.100.50-1.04.7-5.50.05-0.200.25 0.20...0.050.15remainder
6005 0.6-0.90.350.100.100.40-0.6 0.100.100.10...0.050.15remainder
6005A 0.50-0.90.350.300.50

J

0.40-0.70.30

J

0.200.10...0.050.15 remainder
6020

K

0.40-0.90.500.30-0.90.350.6-1.20.150.200.150.050.15remainder
6041

L

0.50-0.90.15-0.70.15-0.60.05-0.200.8-1.20.05-0.150.250.150.050.15remainder
6042

M

0.50-1.20.70.20-0.60.400.7-1.20.04-0.350.250.150.050.15remainder
6060 0.30-0.60.10-0.300.10 0.100.35-0.60.50.15 0.10...0.050.15remainder
6061

N

0.40-0.8 0.70.15-0.400.150.8-1.20.04-0.350.250.15...0.050.15 remainder
6063 0.20-0.60.350.100.100.45-0.90.100.100.10...0.05 0.15remainder
6064

O

0.40-0.80.70.15-0.400.150.8-1.20.05-0.140.250.150.050.15remainder
6066 0.9-1.80.500.7-1.20.6-1.10.8-1.40.400.250.20...0.05 0.15remainder
6070 1.0-1.70.500.15-0.400.40-1.00.50-1.20.100.250.15...0.05 0.15remainder
60820.7-1.30.500.100.40-1.00.6-1.20.250.200.10...0.050.15remainder
6105 0.6-1.00.350.100.150.45-0.8 0.100.100.10...0.050.15remainder
6162 0.40-0.80.500.200.100.7-1.10.100.250.10...0.05 0.15remainder
6262 0.40-0.80.70.15-0.400.150.8-1.20.04-0.140.25 0.15...0.05

P

0.15

P

remainder
6351 0.7-1.30.500.100.40-0.80.40-0.8...0.200.20...0.05 0.15remainder
63600.35-0.80.10-0.300.150.02-0.150.25-0.450.050.100.10...0.050.15remainder
6463 0.20-0.60.150.200.050.45-0.9...0.05......0.05 0.15remainder
65600.30-0.70.10-0.300.05-0.200.200.20-0.60.050.150.10...0.050.15remainder
7005 0.350.400.100.20-0.71.0-1.80.06-0.204.0-5.0 0.01-0.06...0.05

Q

0.15

Q

remainder
7072

R

0.7 Si + Fe0.100.100.10...0.8-1.3 ......remainder
7075 0.400.501.2-2.00.302.1-2.90.18-0.285.1-6.1 0.20

S

...0.05

S

0.15remainder
7116 0.150.300.50-1.10.050.8-1.4...4.2-5.2 0.050.050.05

T

0.15 remainder
7129 0.150.300.50-0.90.101.3-2.00.104.2-5.2 0.050.050.05

T

0.15 remainder
7178 0.400.501.6-2.40.302.4-3.10.18-0.286.3-7.3 0.20...0.050.15remainder

A Limits are in weight percent maximum unless shown as a range, or stated otherwise.

B Analysis shall be made for the elements for which limits are shown in this table.

C 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 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 nonconforming.

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

F 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.

G Be 0.0003 max for welding electrode, welding rod, and filler wire.

H Upon agreement between the purchaser and the producer or supplier, a Zr + Ti limit of 0.20 % max is permitted. Properties in Specification (Table 2) are not based on the Zirconium and Titanium algorithm.

I Zirconium, 0.10-0.25 %. The total for other elements does not include zirconium.

J Manganese plus chromium shall total 0.12-0.50.

K Lead 0.05 % max, Tin 0.9-1.5 %.

L Bismuth 0.30-0.9 %, Tin 0.35-1.2 %.

M Bismuth 0.20-0.8 % Lead 0.15-0.40 %.

N 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.

O Bismuth 0.50-0.7 %, Lead 0.20-0.40 %,

P Bismuth and lead shall be 0.40-0.7 % each.

Q Zirconium 0.08-0.20 %. The total for other elements does not include zirconium.

R Composition of cladding alloy applied during the course of manufacture. Samples from finished tube shall not be required to conform to these limits.

S Upon agreement between the purchaser and the producer or supplier, a Zr + Ti limit of 0.25 % max is permitted. Properties in Specification (Table 2) are not based on the Zirconium and Titanium algorithm.

T Gallium 0.03 % max.

TABLE 2 Mechanical Property LimitsA,B

Note-Strength values shown in parentheses are for information only.

TemperSpecified Section
or Wall
Thickness, in.
Area, in.

2

Tensile Strength,
ksi
Yield Strength
(0.2 % offset), ksi
Elongation in
2 in. or 4 ×
Diameter,
min, %

C

minmaxminmax
Aluminum 1060

D

Oallall8.514.02.5. . .25
H112allall8.5. . .2.5. . .25
Aluminum 1100

D

Oallall11.015.53.0. . .25
H112allall11.0. . .3.0. . .25
Alloy 2014

D

Oallall. . .30.0. . .18.012
T4
T4510

E

allall50.0. . .35.0. . .12
T4511

E

T42

F

allall50.0. . .29.0. . .12
T6

up through 0.499all60.0. . .53.0 . . .7
T6510

E

0.500-0.749all64.0. . .58.0. . .7
T6511

E


up through 2568.0. . .60.0. . .7
0.750 and overover 25 through 3268.0. . .58.0. . .6

up through 0.749all60.0. . .53.0. . .7
T62

F


up through 2560.0. . .53.0. . .7
0.750 and over
over 25 through 3260.0. . .53.0. . .6
Alloy 2024

D

Oallall. . .35.0. . .19.012

up through 0.249all57.0. . .42.0. . .12

G

T3
0.250-0.749all60.0. . .44.0. . .12

G

T3510

E

0.750-1.499all65.0. . .46.0. . .10
T3511

E


up through 2570.0. . .52.0

H

. . .10
1.500 and overover 25 through 3268.0. . .48.0

I

. . .8

up through 0.749all57.0. . .38.0. . .12
0.750-1.499all57.0. . .38.0. . .10
T42

F

1.500 and over
up through 2557.0. . .38.0. . .10
over 25 through 3257.0. . .38.0. . .8
T81
0.050-0.249all64.0. . .56.0. . .4
T8510

E

0.250-1.499all66.0. . .58.0. . .5
T8511

E

1.500 and overup through 3266.0. . .58.0. . .5
Alloy 2219

D

Oallall. . .32.0. . .18.012
T31
T3510

E


up through 0.499up through 2542.0. . .26.0. . .14
T3511

E

0.500-2.999up through 2545.0. . .27.0. . .14
T62

F


up through 0.999up through 2554.0. . .36.0. . .6
1.000 and overup through 2554.0. . .36.0. . .6
T81
T8510

E

up through 2.999up through 2558.0. . .42.0. . .6
T8511

E

Alloy 3003

D

Oallall14.019.05.0. . .25
H112allall14.0. . .5.0. . .25
Alloy Alclad 3003

D

Oallall13.018.04.5. . .25
H112allall13.0. . .4.5

J

. . .25
Alloy 3004

D

Oallall23.029.08.5. . .. . .
Alloy 3102
H112

K

0.028-0.050all11.018.04.0. . .25
Alloy 5052
Oallall25.035.010.0. . .. . .
Alloy 5083

D

Oup through 5.000

L

up through 3239.051.016.0. . .14
H111up through 5.000

L

up through 3240.0. . .24.0. . .12
H112up through 5.000

L

up through 3239.0. . .16.0. . .12
Alloy 5086

D

Oup through 5.000

L

up through 3235.046.014.0. . .14
H111up through 5.000

L

up through 3236.0. . .21.0. . .12
H112up through 5.000

L

up through 3235.0. . .14.0. . .12
Alloy 5154
Oallall30.041.011.0. . .. . .
H112allall30.0. . .11.0. . .. . .
Alloy 5454

D

Oup through 5.000

L

up through 3231.041.012.0. . .14
H111up through 5.000

L

up through 3233.0. . .19.0. . .12
H112up through 5.000

L

up through 3231.0. . .12.0. . .12
Alloy 5456

D

Oup through 5.000

L

up through 3241.053.019.0. . .14
H111up through 5.000

L

up through 3242.0. . .26.0. . .12
H112up through 5.000

L

up through 3241.0. . .19.0. . .12
Alloy 6005
T1up through 0.500all25.0. . .15.0. . .16
T5
up through 0.124all38.0. . .35.0. . .8
0.125-1.000all38.0. . .35.0. . .10
Alloy 6005A
T1up through 0.249all25.0. . .14.5. . .15
T5up through 0.249all38.0. . .31.0. . .7
0.250-0.999all38.0. . .31.0. . .9
T61up through 0.249all38.0. . .35.0. . .8
0.250-0.999all38.0. . .35.0. . .10
Alloy 6020
T65113.250-6.000all38.0. . .35.0. . .10
Alloy 6041
T6

M

0.400-2.000all45.0. . .40.0. . .10
T6511

M

0.400-2.000all45.0. . .40.0. . .10
Alloy 6042
T50.400-0.499all38.0. . .35.0. . .10
0.500-1.800all42.0. . .35.0. . .10
T55110.400-0.499all38.0. . .35.0. . .10
0.500-1.800all42.0. . .35.0. . .10
Alloy 6060
T51up through 0.125all22.0. . .16.0. . .8
T61up through 0.124
0.125-1.000
30.0
30.0
...
...
25.0
25.0
...
...
8
10
Alloy 6061

D

Oallall. . .22.0. . .16.016
T1up through 0.625all26.0. . .14.0. . .16
T4
T4510

E

allall26.0. . .16.0. . .16
T4511

E

T42

F

allall26.0. . .12.0. . .16
T51up through 0.625all35.0. . .30.0. . .8
T6, T62

F


T6510

E

up through 0.249all38.0. . .35.0. . .8
T6511

E

0.250 and overall38.0. . .35.0. . .10
Alloy 6063
Oallall. . .19.0. . .. . .18
T1
up through 0.500all17.0. . .9.0. . .12
0.501-1.000all16.0. . .8.0. . .12
T4, T42

F


up through 0.500all19.0. . .10.0. . .14
0.501-1.000all18.0. . .9.0. . .14
T5
up through 0.500all22.0. . .16.0. . .8
0.501-1.000all21.0. . .15.0. . .8
T52up through 1.000all22.030.016.025.08
T54
up through 0.124all33.0...30.0...8
0.125-0.499all33.0...30.0...10
T6, T62

F


up through 0.124all30.0. . .25.0. . .8
0.125-1.000all30.0. . .25.0. . .10
T65up through 0.182all36.0. . .33.0. . .8
Alloy 6064
T6

M

0.400-2.000all38.0. . .35.0. . .10
T6511

M

0.400-2.000all38.0. . .35.0. . .10
Alloy 6066
Oallall29.0. . .18.016
T4, T4510, T4511

E

allall40.0. . .25.0. . .14
T42

F

allall40.0. . .24.0. . .14
T6, T6510, T6511

E

allall50.0. . .45.0. . .8
T62

F

allall50.0. . .42.0. . .8
Alloy 6070
T6, T62up through 2.999up through 3248.0. . .45.0. . .6
Alloy 6082
T6,T6511
0.200-0.750all45.0...38.0...6
0.751-6.000all45.0....38.0....8
6.001-8.000all41.0...35.0...6
Alloy 6105
T1up through 0.500all25.0. . .15.0. . .16
T5
up through 0.124all38.0. . .35.0. . .8
0.125-1.000all38.0. . .35.0. . .10
Alloy 6162
T5, T5510,

E T5511E

up thru 1.000all37.0. . .34.0. . .7
T6, T6510,

E T6511E

up thru 0.249all38.0. . .35.0. . .8
0.250-0.499all38.0. . .35.0. . .10
Alloy 6262
T6
T6510

E
T6511E


allall38.0. . .35.0. . .10
Alloy 6351
T1up through 0.499up through 2026.0. . .13.0 . . .15
T11up through 0.749all26.0. . .16.0. . .16
T4up through 0.749all32.0. . .19.0. . .16
T5up through 0.249all38.0. . .35.0. . .8
0.250-1.000all38.0. . .35.0. . .10
T510.125-1.000all36.0. . .33.0. . .10
T54up through 0.500all30.0. . .20.0. . .10

up through 0.124all42.0. . .37.0. . .8
T60.125-0.749all42.0. . .37.0. . .10
Alloy 6360
T5up through 0.250all22.0. . .16.0. . .8
T6up through 0.120all30.0. . .25.0. . .8
0.121-0.250all30.0. . .25.0. . .10
Alloy 6463
T1up through 0.500up through 2017.0. . .9.0 . . .12
T5up through 0.500up through 2022.0. . .16.0. . .8
T6
up through 0.124up through 2030.0. . .25.0. . .8
0.125-0.500up through 2030.0. . .25.0. . .10
Alloy 6560
T50.090-0.125all22.0...16.0...8
T60.090-0.125all30.0...25.0...8
Alloy 7005
T53up through 0.750all50.0. . .44.0. . .10
Alloy 7075

D

Oallall. . .40.0. . .24.010

up through 0.249all78.0. . .70.0. . .7
0.250-0.499all81.0. . .73.0. . .7
T6, T62

F


0.500-1.499all81.0. . .72.0 . . .7
T6510

E

1.500-2.999all81.0. . .72.0. . .7
T6511

E

3.000-4.499
up through 2081.0. . .71.0. . .7
over 20 through 3278.0. . .70.0. . .6
4.500-5.000up through 3278.0. . .68.0. . .6
T73

0.062-0.249up through 2068.0. . .58.0. . .7
T73510

E

0.250-1.499up through 2570.0. . .61.0. . .8
T73511

E

1.500-2.999up through 2569.0. . .59.0. . .8
3.000-4.499up through 2068.0. . .57.0. . .7
over 20 through 3265.0. . .55.0. . .7

up through 0.049all73.0. . .63.0. . .7
T76
0.050-0.124all74.0. . .64.0. . .7
T76510

E

0.125-0.249up through 2074.0. . .64.0. . .7
T76511

E

0.250-0.499up through 2075.0. . .65.0. . .7
0.500-1.000up through 2075.0. . .65.0. . .7
1.001-2.000up through 2075.0. . .65.0. . .7
2.001-3.000up through 2074.0. . .64.0. . .7
3.001-4.000up through 2074.0. . .63.0. . .7
Alloy 7116
T50.125-0.500all48.0. . .42.0. . .8
Alloy 7129
T5, T6up through 0.500all55.0. . .49.0. . .9
Alloy 7178

D

Oallup through 32. . .40.0. . .24.010
up through 0.061up through 2082.0. . .76.0. . .. . .

0.062-0.249up through 2084.0. . .76.0. . .5
T6
0.250-1.499up through 2587.0. . .78.0. . .5
T6510

E

1.500-2.499
up through 2586.0. . .77.0. . .5
T6511

E

over 25 through 3284.0. . .75.0. . .5
2.500-2.999up through 3282.0. . .71.0. . .5

up through 0.061up through 2079.0. . .73.0. . .5
0.062-0.249up through 2082.0. . .74.0. . .5
0.250-1.499up through 2586.0. . .77.0. . .5
T62

F

1.500-2.499
up through 2586.0. . .77.0. . .5
over 25 through 3284.0. . .75.0. . .5
2.500-2.999up through 3282.0. . .71.0. . .5
T76

0.125-0.249up through 2076.0. . .66.0. . .7
T76510

E

0.250-0.499up through 2077.0. . .67.0. . .7
T76511

E

0.500-1.000up through 2077.0. . .67.0. . .7

A The basis for establishment of tensile property limits is shown in Annex A1.

B 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 E29.

C 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. See 8.1.1 and 8.1.2 for conditions under which measurements are not required.

D These alloys are also produced in the F temper for which no tensile properties are specified or guaranteed.

E For stress relieved tempers (T3510, T3511, T4510, T4511, T5510, T5511, T6510, T6511, T73510, T73511, T76510, T76511, T8510, T8511), characteristics and properties other than those specified may differ somewhat from the corresponding characteristics and properties of material in the basic tempers.

F Material in the T42 and T62 tempers is not available from the material producers.

G Minimum elongation for tube, 10 %.

H Minimum yield strength for tube, 48.0 ksi.

I Minimum yield strength for tube, 46.0 ksi.

J Yield strength is not applicable in tube.

K Only in tube form.

L Properties not applicable to extruded tube over 2.999 in wall thickness.

M Tentative; properties subject to revision.

abstract:

This specification covers extruded bars, rods, wires, profiles, and tubes made from aluminum and aluminum alloys. All the products should be produced by hot extrusion or similar methods. The... View More

Document History

December 1, 2020
Standard Specification for Aluminum and Aluminum-Alloy Extruded Bars, Rods, Wire, Profiles, and Tubes
1.1 This specification2 covers aluminum and aluminum-alloy extruded bars, rods, wire, profiles, and tubes in the aluminum alloys (Note 1) and tempers shown in Table 2. Note 1: Throughout this...
October 1, 2014
Standard Specification for Aluminum and Aluminum-Alloy Extruded Bars, Rods, Wire, Profiles, and Tubes
1.1 This specification2 covers aluminum and aluminum-alloy extruded bars, rods, wire, profiles, and tubes in the aluminum alloys (Note 1) and tempers shown in Table 2. Note 1: Throughout this...
April 1, 2013
Standard Specification for Aluminum and Aluminum-Alloy Extruded Bars, Rods, Wire, Profiles, and Tubes
1.1 This specification2 covers aluminum and aluminum-alloy extruded bars, rods, wire, profiles, and tubes in the aluminum alloys (Note 1) and tempers shown in Table 2. Note 1—Throughout this...
November 15, 2012
Standard Specification for Aluminum and Aluminum-Alloy Extruded Bars, Rods, Wire, Profiles, and Tubes
1.1 This specification2 covers aluminum and aluminum-alloy extruded bars, rods, wire, profiles, and tubes in the aluminum alloys (Note 1) and tempers shown in Table 2. Note 1—Throughout this...
ASTM B221-12
January 15, 2012
Standard Specification for Aluminum and Aluminum-Alloy Extruded Bars, Rods, Wire, Profiles, and Tubes
1.1 This specification covers aluminum and aluminum-alloy extruded bars, rods, wire, profiles, and tubes in the aluminum alloys (Note 1) and tempers shown in Table 2. Note 1—Throughout this...
August 8, 2008
Standard Specification for Aluminum and Aluminum-Alloy Extruded Bars, Rods, Wire, Profiles, and Tubes
1.1 This specification covers aluminum and aluminum-alloy extruded bar, rod, wire, profile, and tube in the aluminum alloys (Note 1) and tempers shown in Table 1. Note 1—Throughout this...
November 1, 2006
Standard Specification for Aluminum and Aluminum-Alloy Extruded Bars, Rods, Wire, Profiles, and Tubes
1.1 This specification covers aluminum and aluminum-alloy extruded bar, rod, wire, profile, and tube in the aluminum alloys (Note 0) and tempers shown in . Note 0 Throughout this specification, the...
October 1, 2005
Standard Specification for Aluminum and Aluminum-Alloy Extruded Bars, Rods, Wire, Profiles, and Tubes
1.1 This specification covers aluminum and aluminum-alloy extruded bar, rod, wire, profile, and tube in the aluminum alloys (Note 1) and tempers shown in Table 2. Note 1—Throughout this...
June 1, 2005
Standard Specification for Aluminum and Aluminum-Alloy Extruded Bars, Rods, Wire, Profiles, and Tubes
1.1 This specification covers aluminum and aluminum-alloy extruded bar, rod, wire, profile, and tube in the aluminum alloys (Note 1) and tempers shown in Table 2. Note 1—Throughout this...
October 5, 2004
Standard Specification for Aluminum and Aluminum-Alloy Extruded Bars, Rods, Wire, Profiles, and Tubes
1.1 This specification covers aluminum and aluminum-alloy extruded bar, rod, wire, profile, and tube in the aluminum alloys (Note 0) and tempers shown in Tabld 2. Note 1—Throughout this...
October 10, 2002
Standard Specification for Aluminum and Aluminum-Alloy Extruded Bars, Rods, Wire, Profiles, and Tubes
1.1 This specification covers aluminum and aluminum-alloy extruded bar, rod, wire, profile, and tube in the aluminum alloys (Note 1) and tempers shown in Table 2. Note 1—Throughout this...
May 10, 2000
Standard Specification for Aluminum and Aluminum-Alloy Extruded Bars, Rods, Wire, Profiles, and Tubes
1.1 This specification covers aluminum and aluminum-alloy extruded bar, rod, wire, profile, and tube in the aluminum alloys (Note 1) and tempers shown in Table 2. Note 1-Throughout this...
January 1, 1976
Standard Specification for Aluminum-Alloy Extruded Bars, Rods, Wire, Shapes, and Tubes
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