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  • ASTM
    B221-12 Standard Specification for Aluminum and Aluminum-Alloy Extruded Bars, Rods, Wire, Profiles, and Tubes
    Edition: 2012
    $113.57
    Unlimited Users per year

Description of ASTM-B221 2012

ASTM B221-12

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




ASTM B221

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.

Alloy Silicon Iron Copper Manga-
nese 		Magne-
sium 		Chromium Zinc Titanium Vanadium Other ElementsD Aluminum
Each TotalE
1060 0.25 0.35 0.05 0.03 0.03 ... 0.05 0.03 0.05 0.03 ... 99.60 minF
1100 0.95 Si + Fe 0.05–0.20 0.05 ... ... 0.10 ... ... 0.05G 0.15 99.00 minF
2014 0.50–1.2 0.7 3.9–5.0 0.40–1.2 0.20–0.8 0.10 0.25 0.15H ... 0.05H 0.15 remainder
2024 0.50 0.50 3.8–4.9 0.30–0.9 1.2–1.8 0.10 0.25 0.15H ... 0.05H 0.15 remainder
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 0.05I 0.15I remainder
3003 0.6 0.7 0.05–0.20 1.0–1.5 ... ... 0.10 ... ... 0.05 0.15 remainder
Alclad 3003 ... 3003 Clad with 7072 alloy ... ... ... ... ... ... ... ...
3004 0.30 0.7 0.25 1.0–1.5 0.8–1.3 ... 0.25 ... ... 0.05 0.15 remainder
3102 0.40 0.7 0.10 0.05–0.40 ... ... 0.30 0.10 ... 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 0.40 0.40 0.10 0.40–1.0 4.0–4.9 0.05–0.25 0.25 0.15 ... 0.05 0.15 remainder
5086 0.40 0.50 0.10 0.20–0.7 3.5–4.5 0.05–0.25 0.25 0.15 ... 0.05 0.15 remainder
5154 0.25 0.40 0.10 0.10 3.1–3.9 0.15–0.35 0.20 0.20 ... 0.05G 0.15 remainder
5454 0.25 0.40 0.10 0.50–1.0 2.4–3.0 0.05–0.20 0.25 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
6005 0.6–0.9 0.35 0.10 0.10 0.40–0.6 0.10 0.10 0.10 ... 0.05 0.15 remainder
6005A 0.50–0.9 0.35 0.30 0.50J 0.40–0.7 0.30J 0.20 0.10 ... 0.05 0.15 remainder
6020K 0.40-0.9 0.50 0.30-0.9 0.35 0.6-1.2 0.15 0.20 0.15 … 0.05 0.15 remainder
6041L 0.50-0.9 0.15-0.7 0.15-0.6 0.05-0.20 0.8-1.2 0.05-0.15 0.25 0.15 … 0.05 0.15 remainder
6042M 0.50-1.2 0.7 0.20-0.6 0.40 0.7-1.2 0.04-0.35 0.25 0.15 … 0.05 0.15 remainder
6060 0.30–0.6 0.10–0.30 0.10 0.10 0.35–0.6 0.5 0.15 0.10 ... 0.05 0.15 remainder
6061N 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
6064O 0.40-0.8 0.7 0.15-0.40 0.15 0.8-1.2 0.05-0.14 0.25 0.15 … 0.05 0.15 remainder
6066 0.9–1.8 0.50 0.7–1.2 0.6–1.1 0.8–1.4 0.40 0.25 0.20 ... 0.05 0.15 remainder
6070 1.0–1.7 0.50 0.15–0.40 0.40–1.0 0.50–1.2 0.10 0.25 0.15 ... 0.05 0.15 remainder
6082 0.7–1.3 0.50 0.10 0.40–1.0 0.6–1.2 0.25 0.20 0.10 ... 0.05 0.15 remainder
6105 0.6–1.0 0.35 0.10 0.15 0.45–0.8 0.10 0.10 0.10 ... 0.05 0.15 remainder
6162 0.40–0.8 0.50 0.20 0.10 0.7–1.1 0.10 0.25 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 ... 0.05P 0.15P remainder
6351 0.7–1.3 0.50 0.10 0.40–0.8 0.40–0.8 ... 0.20 0.20 ... 0.05 0.15 remainder
6360 0.35-0.8 0.10-0.30 0.15 0.02-0.15 0.25-0.45 0.05 0.10 0.10 ... 0.05 0.15 remainder
6463 0.20–0.6 0.15 0.20 0.05 0.45–0.9 ... 0.05 ... ... 0.05 0.15 remainder
6560 0.30–0.7 0.10–0.30 0.05–0.20 0.20 0.20–0.6 0.05 0.15 0.10 ... 0.05 0.15 remainder
7005 0.35 0.40 0.10 0.20–0.7 1.0–1.8 0.06–0.20 4.0–5.0 0.01–0.06 ... 0.05Q 0.15Q remainder
7072R 0.7 Si + Fe 0.10 0.10 0.10 ... 0.8–1.3 ... ... remainder
7075 0.40 0.50 1.2–2.0 0.30 2.1–2.9 0.18–0.28 5.1–6.1 0.20S ... 0.05S 0.15 remainder
7116 0.15 0.30 0.50–1.1 0.05 0.8–1.4 ... 4.2–5.2 0.05 0.05 0.05T 0.15 remainder
7129 0.15 0.30 0.50–0.9 0.10 1.3–2.0 0.10 4.2–5.2 0.05 0.05 0.05T 0.15 remainder
7178 0.40 0.50 1.6–2.4 0.30 2.4–3.1 0.18–0.28 6.3–7.3 0.20 ... 0.05 0.15 remainder

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.

Temper Specified 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
min max min max
Aluminum 1060D
O all all 8.5 14.0 2.5 . . . 25
H112 all all 8.5 . . . 2.5 . . . 25
Aluminum 1100D
O all all 11.0 15.5 3.0 . . . 25
H112 all all 11.0 . . . 3.0 . . . 25
Alloy 2014D
O all all . . . 30.0 . . . 18.0 12
T4

T4510E all all 50.0 . . . 35.0 . . . 12
T4511E
T42F all all 50.0 . . . 29.0 . . . 12
T6



up through 0.499 all 60.0 . . . 53.0 . . . 7
T6510E 0.500–0.749 all 64.0 . . . 58.0 . . . 7
T6511E

up through 25 68.0 . . . 60.0 . . . 7
0.750 and over over 25 through 32 68.0 . . . 58.0 . . . 6


up through 0.749 all 60.0 . . . 53.0 . . . 7
T62F

up through 25 60.0 . . . 53.0 . . . 7
0.750 and over
over 25 through 32 60.0 . . . 53.0 . . . 6
Alloy 2024D
O all all . . . 35.0 . . . 19.0 12


up through 0.249 all 57.0 . . . 42.0 . . . 12G
T3

0.250–0.749 all 60.0 . . . 44.0 . . . 12G
T3510E 0.750–1.499 all 65.0 . . . 46.0 . . . 10
T3511E

up through 25 70.0 . . . 52.0H . . . 10
1.500 and over over 25 through 32 68.0 . . . 48.0I . . . 8


up through 0.749 all 57.0 . . . 38.0 . . . 12
0.750–1.499 all 57.0 . . . 38.0 . . . 10
T42F 1.500 and over

up through 25 57.0 . . . 38.0 . . . 10
over 25 through 32 57.0 . . . 38.0 . . . 8
T81

0.050–0.249 all 64.0 . . . 56.0 . . . 4
T8510E 0.250–1.499 all 66.0 . . . 58.0 . . . 5
T8511E 1.500 and over up through 32 66.0 . . . 58.0 . . . 5
Alloy 2219D
O all all . . . 32.0 . . . 18.0 12
T31
T3510E

up through 0.499 up through 25 42.0 . . . 26.0 . . . 14
T3511E 0.500–2.999 up through 25 45.0 . . . 27.0 . . . 14
T62F

up through 0.999 up through 25 54.0 . . . 36.0 . . . 6
1.000 and over up through 25 54.0 . . . 36.0 . . . 6
T81

T8510E up through 2.999 up through 25 58.0 . . . 42.0 . . . 6
T8511E
Alloy 3003D
O all all 14.0 19.0 5.0 . . . 25
H112 all all 14.0 . . . 5.0 . . . 25
Alloy Alclad 3003D
O all all 13.0 18.0 4.5 . . . 25
H112 all all 13.0 . . . 4.5J . . . 25
Alloy 3004D
O all all 23.0 29.0 8.5 . . . . . .
Alloy 3102
H112K 0.028–0.050 all 11.0 18.0 4.0 . . . 25
Alloy 5052
O all all 25.0 35.0 10.0 . . . . . .
Alloy 5083D
O up through 5.000L up through 32 39.0 51.0 16.0 . . . 14
H111 up through 5.000L up through 32 40.0 . . . 24.0 . . . 12
H112 up through 5.000L up through 32 39.0 . . . 16.0 . . . 12
Alloy 5086D
O up through 5.000L up through 32 35.0 46.0 14.0 . . . 14
H111 up through 5.000L up through 32 36.0 . . . 21.0 . . . 12
H112 up through 5.000L up through 32 35.0 . . . 14.0 . . . 12
Alloy 5154
O all all 30.0 41.0 11.0 . . . . . .
H112 all all 30.0 . . . 11.0 . . . . . .
Alloy 5454D
O up through 5.000L up through 32 31.0 41.0 12.0 . . . 14
H111 up through 5.000L up through 32 33.0 . . . 19.0 . . . 12
H112 up through 5.000L up through 32 31.0 . . . 12.0 . . . 12
Alloy 5456D
O up through 5.000L up through 32 41.0 53.0 19.0 . . . 14
H111 up through 5.000L up through 32 42.0 . . . 26.0 . . . 12
H112 up through 5.000L up through 32 41.0 . . . 19.0 . . . 12
Alloy 6005
T1 up through 0.500 all 25.0 . . . 15.0 . . . 16
T5

up through 0.124 all 38.0 . . . 35.0 . . . 8
0.125–1.000 all 38.0 . . . 35.0 . . . 10
Alloy 6005A
T1 up through 0.249 all 25.0 . . . 14.5 . . . 15
T5 up through 0.249 all 38.0 . . . 31.0 . . . 7
0.250–0.999 all 38.0 . . . 31.0 . . . 9
T61 up through 0.249 all 38.0 . . . 35.0 . . . 8
0.250–0.999 all 38.0 . . . 35.0 . . . 10
Alloy 6020
T6511 3.250-6.000 all 38.0 . . . 35.0 . . . 10
Alloy 6041
T6M 0.400-2.000 all 45.0 . . . 40.0 . . . 10
T6511M 0.400-2.000 all 45.0 . . . 40.0 . . . 10
Alloy 6042
T5 0.400-0.499 all 38.0 . . . 35.0 . . . 10
0.500-1.800 all 42.0 . . . 35.0 . . . 10
T5511 0.400-0.499 all 38.0 . . . 35.0 . . . 10
0.500-1.800 all 42.0 . . . 35.0 . . . 10
Alloy 6060
T51 up through 0.125 all 22.0 . . . 16.0 . . . 8
T61 up through 0.124
0.125–1.000 		30.0
30.0 		...
... 		25.0
25.0 		...
... 		8
10
Alloy 6061D
O all all . . . 22.0 . . . 16.0 16
T1 up through 0.625 all 26.0 . . . 14.0 . . . 16
T4

T4510E all all 26.0 . . . 16.0 . . . 16
T4511E
T42F all all 26.0 . . . 12.0 . . . 16
T51 up through 0.625 all 35.0 . . . 30.0 . . . 8
T6, T62F

T6510E up through 0.249 all 38.0 . . . 35.0 . . . 8
T6511E 0.250 and over all 38.0 . . . 35.0 . . . 10
Alloy 6063
O all all . . . 19.0 . . . . . . 18
T1

up through 0.500 all 17.0 . . . 9.0 . . . 12
0.501–1.000 all 16.0 . . . 8.0 . . . 12
T4, T42F

up through 0.500 all 19.0 . . . 10.0 . . . 14
0.501–1.000 all 18.0 . . . 9.0 . . . 14
T5

up through 0.500 all 22.0 . . . 16.0 . . . 8
0.501–1.000 all 21.0 . . . 15.0 . . . 8
T52 up through 1.000 all 22.0 30.0 16.0 25.0 8
T54

up through 0.124 all 33.0 ... 30.0 ... 8
0.125–0.499 all 33.0 ... 30.0 ... 10
T6, T62F

up through 0.124 all 30.0 . . . 25.0 . . . 8
0.125–1.000 all 30.0 . . . 25.0 . . . 10
T65 up through 0.182 all 36.0 . . . 33.0 . . . 8
Alloy 6064
T6M 0.400-2.000 all 38.0 . . . 35.0 . . . 10
T6511M 0.400-2.000 all 38.0 . . . 35.0 . . . 10
Alloy 6066
O all all 29.0 . . . 18.0 16
T4, T4510, T4511E all all 40.0 . . . 25.0 . . . 14
T42F all all 40.0 . . . 24.0 . . . 14
T6, T6510, T6511E all all 50.0 . . . 45.0 . . . 8
T62F all all 50.0 . . . 42.0 . . . 8
Alloy 6070
T6, T62 up through 2.999 up through 32 48.0 . . . 45.0 . . . 6
Alloy 6082
T6,T6511

0.200–0.750 all 45.0 ... 38.0 ... 6
0.751–6.000 all 45.0 .... 38.0 .... 8
6.001–8.000 all 41.0 ... 35.0 ... 6
Alloy 6105
T1 up through 0.500 all 25.0 . . . 15.0 . . . 16
T5

up through 0.124 all 38.0 . . . 35.0 . . . 8
0.125–1.000 all 38.0 . . . 35.0 . . . 10
Alloy 6162
T5, T5510,E T5511E up thru 1.000 all 37.0 . . . 34.0 . . . 7
T6, T6510,E T6511E up thru 0.249 all 38.0 . . . 35.0 . . . 8
0.250–0.499 all 38.0 . . . 35.0 . . . 10
Alloy 6262
T6

T6510E
T6511E

all all 38.0 . . . 35.0 . . . 10
Alloy 6351
T1 up through 0.499 up through 20 26.0 . . . 13.0 . . . 15
T11 up through 0.749 all 26.0 . . . 16.0 . . . 16
T4 up through 0.749 all 32.0 . . . 19.0 . . . 16
T5 up through 0.249 all 38.0 . . . 35.0 . . . 8
0.250–1.000 all 38.0 . . . 35.0 . . . 10
T51 0.125–1.000 all 36.0 . . . 33.0 . . . 10
T54 up through 0.500 all 30.0 . . . 20.0 . . . 10


up through 0.124 all 42.0 . . . 37.0 . . . 8
T6 0.125–0.749 all 42.0 . . . 37.0 . . . 10
Alloy 6360
T5 up through 0.250 all 22.0 . . . 16.0 . . . 8
T6 up through 0.120 all 30.0 . . . 25.0 . . . 8
0.121–0.250 all 30.0 . . . 25.0 . . . 10
Alloy 6463
T1 up through 0.500 up through 20 17.0 . . . 9.0 . . . 12
T5 up through 0.500 up through 20 22.0 . . . 16.0 . . . 8
T6

up through 0.124 up through 20 30.0 . . . 25.0 . . . 8
0.125–0.500 up through 20 30.0 . . . 25.0 . . . 10
Alloy 6560
T5 0.090–0.125 all 22.0 ... 16.0 ... 8
T6 0.090–0.125 all 30.0 ... 25.0 ... 8
Alloy 7005
T53 up through 0.750 all 50.0 . . . 44.0 . . . 10
Alloy 7075D
O all all . . . 40.0 . . . 24.0 10


up through 0.249 all 78.0 . . . 70.0 . . . 7
0.250–0.499 all 81.0 . . . 73.0 . . . 7
T6, T62F

0.500–1.499 all 81.0 . . . 72.0 . . . 7
T6510E 1.500–2.999 all 81.0 . . . 72.0 . . . 7
T6511E 3.000–4.499

up through 20 81.0 . . . 71.0 . . . 7
over 20 through 32 78.0 . . . 70.0 . . . 6
4.500–5.000 up through 32 78.0 . . . 68.0 . . . 6
T73



0.062–0.249 up through 20 68.0 . . . 58.0 . . . 7
T73510E 0.250–1.499 up through 25 70.0 . . . 61.0 . . . 8
T73511E 1.500–2.999 up through 25 69.0 . . . 59.0 . . . 8
3.000–4.499 up through 20 68.0 . . . 57.0 . . . 7
over 20 through 32 65.0 . . . 55.0 . . . 7


up through 0.049 all 73.0 . . . 63.0 . . . 7
T76

0.050–0.124 all 74.0 . . . 64.0 . . . 7
T76510E 0.125–0.249 up through 20 74.0 . . . 64.0 . . . 7
T76511E 0.250–0.499 up through 20 75.0 . . . 65.0 . . . 7
0.500–1.000 up through 20 75.0 . . . 65.0 . . . 7
1.001–2.000 up through 20 75.0 . . . 65.0 . . . 7
2.001–3.000 up through 20 74.0 . . . 64.0 . . . 7
3.001–4.000 up through 20 74.0 . . . 63.0 . . . 7
Alloy 7116
T5 0.125–0.500 all 48.0 . . . 42.0 . . . 8
Alloy 7129
T5, T6 up through 0.500 all 55.0 . . . 49.0 . . . 9
Alloy 7178D
O all up through 32 . . . 40.0 . . . 24.0 10
up through 0.061 up through 20 82.0 . . . 76.0 . . . . . .


0.062–0.249 up through 20 84.0 . . . 76.0 . . . 5
T6

0.250–1.499 up through 25 87.0 . . . 78.0 . . . 5
T6510E 1.500–2.499

up through 25 86.0 . . . 77.0 . . . 5
T6511E over 25 through 32 84.0 . . . 75.0 . . . 5
2.500–2.999 up through 32 82.0 . . . 71.0 . . . 5


up through 0.061 up through 20 79.0 . . . 73.0 . . . 5
0.062–0.249 up through 20 82.0 . . . 74.0 . . . 5
0.250–1.499 up through 25 86.0 . . . 77.0 . . . 5
T62F
1.500–2.499

up through 25 86.0 . . . 77.0 . . . 5
over 25 through 32 84.0 . . . 75.0 . . . 5
2.500–2.999 up through 32 82.0 . . . 71.0 . . . 5
T76



0.125–0.249 up through 20 76.0 . . . 66.0 . . . 7
T76510E 0.250–0.499 up through 20 77.0 . . . 67.0 . . . 7
T76511E 0.500–1.000 up through 20 77.0 . . . 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.


Keywords

aluminum alloy; extruded bars; extruded profiles; extruded rods; extruded tubes; extruded wire; UNS A91100 (Wr. alum. alloy); UNS A92014 (Wr. alum. alloy, heat treatable); UNS A92024 (Wr. alum. alloy, heat treatable); UNS A92219 (Wr. alum. alloy, heat treatable); UNS A93003 (Wr. alum. alloy); UNS A93004 (Wr. alum. alloy); UNS A93102 (Wr. alum. alloy); UNS A95052 (Wr. alum. alloy); UNS A95083 (Wr. alum. alloy); UNS A95086 (Wr. alum. alloy); UNS A95154 (Wr. alum. alloy); UNS A95454 (Wr. alum. alloy); UNS A95456 (Wr. alum. alloy, non-heat treatable); UNS A96005 (Wr. alum. alloy, heat treatable); UNS A96061 (Wr. alum. alloy); UNS A96063 (Wr. alum. alloy); UNS A96066 (Wr. alum. alloy, heat treatable); UNS A96105 (Wr. alum. alloy, heat treatable); UNS A96262 (Wr. alum. alloy); Aluminum--specifications; Aluminum alloys (rod)--specifications; Aluminum alloys (tube)--specifications; Aluminum alloys (wire)--specifications; Extruded bars/rods/wire; UNS A91060 (Wr. alum. alloy); UNS A96351 (Wr. alum. alloy, heat treatable); UNS A96463 (Wr. alum. alloy, heat treatable); UNS A97005 (Wr. alum. alloy, heat treatable); UNS A97075 (Wr. alum. alloy, heat treatable); UNS A97178 (Wr. alum. alloy, heat treatable); UNS A97072 (Wr. alum. alloy)


ICS Code

ICS Number Code 77.150.10 (Aluminium products)


DOI: 10.1520/B0221-12

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