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ASTM B 221M : 2013

Superseded
Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

View Superseded by
superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

Standard Specification for Aluminum and Aluminum-Alloy Extruded Bars, Rods, Wire, Profiles, and Tubes (Metric)
Available format(s)

Hardcopy , PDF

Superseded date

11-11-2021

Language(s)

English

Published date

07-06-2013

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

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

TABLE 1 Chemical Composition Limits A,B,C
Note 1In case of a discrepancy between the values listed in Table 1 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

...

0.05

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

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

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.
DOthers 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.
EOther Elements—Total 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-.040 %,
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 Tensile Property LimitsA,B

Temper

Specified Section or Wall Thickness, mm

Area, mm2

Tensile Strength, MPa

Yield Strength (0.2 % offset), MPa

Elongation,C %, min

over

incl

over

incl

min

max

min

max

in 50 mm

in 5 ×
Diameter
Equation B0221M-13_1

Aluminum 1060

O

all

all

60

95

15

. . .

25

22

H112

all

all

60

. . .

15

. . .

25

22

FD

all

all

. . .

. . .

. . .

. . .

. . .

. . .

Aluminum 1100

O

all

all

75

105

20

. . .

25

22

H112

all

all

75

. . .

20

. . .

25

22

FD

all

all

. . .

. . .

. . .

. . .

. . .

. . .

Alloy 2014

O

all

all

. . .

205

. . .

125

12

10

T4

Equation B0221M-13_2

all

all

345

. . .

240

. . .

12

10

T4510E

T4511E

T42F

all

all

345

. . .

200

. . .

12

10

T6

Equation B0221M-13_3

Equation B0221M-13_4

. . .

12.50

all

415

. . .

365

. . .

7

6

T6510E

12.50

18.00

all

440

. . .

400

. . .

. . .

6

T6511E

18.00

. . .

. . .

16 000

470

. . .

415

. . .

. . .

6

18.00

. . .

16 000

20 000

470

. . .

400

. . .

. . .

5

T62F

Equation B0221M-13_5

. . .

18.00

all

. . .

415

. . .

365

. . .

7

6

18.00

. . .

. . .

16 000

415

. . .

365

. . .

. . .

6

18.00

. . .

16 000

20 000

415

. . .

365

. . .

. . .

5

FD

all

all

. . .

. . .

. . .

. . .

. . .

. . .

. . .

Alloy 2024

O

all

all

. . .

240

. . .

130

12

10

T3

Equation B0221M-13_6

. . .

6.30

all

395

. . .

290

. . .

12G

. . .

T3510E

Equation B0221M-13_7

6.30

18.00

all

415

. . .

305

. . .

12G

10G

T3511E

18.00

35.00

all

450

. . .

315

. . .

. . .

9

35.00

. . .

. . .

16 000

485

. . .

360H

. . .

. . .

9

35.00

. . .

16 000

20 000

470

. . .

330I

. . .

. . .

7

T42F

Equation B0221M-13_8

. . .

18.00

all

. . .

395

. . .

260

. . .

12

10

18.00

35.00

all

395

. . .

260

. . .

. . .

9

35.00

. . .

. . .

16 000

395

. . .

260

. . .

. . .

9

35.00

. . .

16 000

20 000

395

. . .

260

. . .

. . .

7

T81

Equation B0221M-13_9

Equation B0221M-13_10

1.20

6.30

all

440

. . .

385

. . .

4

. . .

T8510E

6.30

35.00

all

455

. . .

400

. . .

5

4

T8511E

35.00

. . .

. . .

20 000

455

. . .

400

. . .

. . .

4

FD

all

all

. . .

. . .

. . .

. . .

. . .

. . .

Alloy 2219

O

all

all

. . .

220

. . .

125

12

10

T31

Equation B0221M-13_11

Equation B0221M-13_12

. . .

12.50

. . .

16 000

290

. . .

180

. . .

14

12

T3510E

12.50

80.00

16 000

310

. . .

185

. . .

. . .

12

T62F

Equation B0221M-13_13

. . .

25.00

. . .

16 000

370

. . .

250

. . .

6

5

25.00

. . .

20 000

370

. . .

250

. . .

. . .

5

T81

Equation B0221M-13_14

T8510E

. . .

80.00

. . .

16 000

400

. . .

290

. . .

6

5

T8511E

FD

all

all

. . .

. . .

. . .

. . .

. . .

. . .

Alloy 3003

O

all

all

95

130

35

. . .

25

22

H112

all

all

95

. . .

35

. . .

25

22

FD

all

all

. . .

. . .

. . .

. . .

. . .

. . .

Alclad Alloy 3003

O

all

all

all

90

125

30

. . .

25

. . .

H112

all

90

. . .

30J

. . .

25

. . .

Alloy 3004

O

all

all

160

200

60

. . .

. . .

. . .

FD

all

all

. . .

. . .

. . .

. . .

. . .

. . .

Alloy 3102

H112K

0.70

1.30

all

75

125

30

. . .

25

. . .

Alloy 5052

O

all

all

170

240

70

. . .

. . .

. . .

Alloy 5083

O

. . .

130.00L

. . .

20 000

270

350

110

. . .

14

12

H111

. . .

130.00L

. . .

20 000

275

. . .

165

. . .

12

10

H112

. . .

130.00L

. . .

20 000

270

. . .

110

. . .

12

10

FD

all

all

. . .

. . .

. . .

. . .

. . .

. . .

Alloy 5086

O

. . .

130.00L

. . .

20 000

240

315

95

. . .

14

12

H111

. . .

130.00L

. . .

20 000

250

. . .

145

. . .

12

10

H112

. . .

130.00L

. . .

20 000

240

. . .

95

. . .

12

10

FD

all

all

. . .

. . .

. . .

. . .

. . .

. . .

Alloy 5154

O

all

all

205

285

75

. . .

. . .

. . .

H112

all

all

205

. . .

75

. . .

. . .

. . .

Alloy 5454

O

. . .

130.00L

. . .

20 000

215

285

85

. . .

14

12

H111

. . .

130.00L

. . .

20 000

230

. . .

130

. . .

12

10

H112

. . .

130.00L

. . .

20 000

215

. . .

85

. . .

12

10

FD

all

all

. . .

. . .

. . .

. . .

. . .

. . .

Alloy 5456

O

. . .

130.00L

. . .

20 000

285

365

130

. . .

14

12

H111

. . .

130.00L

. . .

20 000

290

. . .

180

. . .

12

10

H112

. . .

130.00L

. . .

20 000

285

. . .

130

. . .

12

10

FD

all

all

. . .

. . .

. . .

. . .

. . .

. . .

Alloy 6005

T1

. . .

12.50

all

170

. . .

105

. . .

16

14

T5

Equation B0221M-13_15

. . .

3.20

all

260

. . .

240

. . .

8

. . .

3.20

25.00

all

260

. . .

240

. . .

10

9

Alloy 6005A

T1

. . .

6.30

all

170

. . .

100

. . .

15

. . .

T5

. . .

6.30

all

260

. . .

215

. . .

7

. . .

6.30

25.00

all

260

. . .

215

. . .

9

8

T61

. . .

6.30

all

260

. . .

240

. . .

8

. . .

6.30

25.00

all

260

. . .

240

. . .

10

9

Alloy 6013

T6

5.00

12.50

all

340

. . .

315

. . .

8

. . .

12.50

20.00

all

340

. . .

315

. . .

. . .

7

20.00

50.00

all

340

. . .

310

. . .

. . .

7

T6511

5.00

12.50

all

340

. . .

315

. . .

8

. . .

12.50

20.00

all

340

. . .

315

. . .

. . .

7

20.00

50.00

all

340

. . .

310

. . .

. . .

7

Alloy 6020

T6511

80.00

160.00

all

260

. . .

240

. . .

. . .

9

Alloy 6041

T6M

10.00

50.00

all

310

. . .

275

. . .

10

9

T6511M

10.00

50.00

all

310

. . .

275

. . .

10

9

Alloy 6042

T5

10.00

12.50

all

260

. . .

240

. . .

10

. . .

12.50

50.00

all

290

. . .

240

. . .

. . .

9

T551

10.00

12.50

all

260

. . .

240

. . .

10

. . .

12.50

50.00

all

290

. . .

240

. . .

. . .

9

Alloy 6060

T51

. . .

3.20

all

150

. . .

110

. . .

8

. . .

T61

. . .

3.20

all

205

. . .

170

. . .

8

. . .

3.20

25.00

all

205

. . .

170

. . .

10

9

Alloy 6061

O

all

all

. . .

150

. . .

110

16

14

T1

. . .

16.00

all

180

. . .

95

. . .

16

14

T4

Equation B0221M-13_16

all

180

. . .

110

. . .

16

14

T4510E

all

T4511E

T42F

all

all

180

. . .

85

. . .

16

14

T51

. . .

16.00

all

240

. . .

205

. . .

8

7

T6, T62F

Equation B0221M-13_17

Equation B0221M-13_18

. . .

6.30

all

260

. . .

240

. . .

8

. . .

T6510E

6.30

. . .

all

260

. . .

240

. . .

10

9

T6511E

FD

all

all

. . .

. . .

. . .

. . .

. . .

. . .

Alloy 6063

O

all

all

. . .

130

. . .

. . .

18

16

T1

. . .

12.50

all

. . .

115

. . .

60

. . .

12

10

12.50

25.00

all

. . .

110

. . .

55

. . .

. . .

10

T4,T42F

. . .

12.50

all

130

. . .

70

. . .

14

12

12.50

25.00

all

125

. . .

60

. . .

. . .

12

T5

. . .

12.50

all

150

. . .

110

. . .

8

7

12.50

25.00

all

145

. . .

105

. . .

. . .

7

T52

. . .

25.00

all

150

205

110

170

8

7

T54

. . .

3.20

all

225

. . .

205

. . .

8

. . .

3.20

12.50

all

225

. . .

205

. . .

10

. . .

T6, T62K,F

. . .

3.20

all

205

. . .

170

. . .

8

. . .

3.20

25.00

all

205

. . .

170

. . .

10

9

T65

. . .

5.00

all

250

. . .

230

. . .

7

. . .

Alloy 6064

T6

5.00

80.00

all

290

. . .

260

. . .

10

9

T6511

5.00

80.00

all

290

. . .

260

. . .

10

9

Alloy 6066

O

all

all

. . .

200

. . .

125

16

14

T4

Equation B0221M-13_19

all

275

. . .

170

. . .

14

12

T4510E

all

T4511E

T42F

all

all

275

. . .

165

. . .

14

12

T6

Equation B0221M-13_20

all

345

. . .

310

. . .

8

7

T6510E

all

T6511E

T62F

all

all

345

. . .

290

. . .

8

7

Alloy 6070

T6, T62F

. . .

80.00

. . .

20 000

330

. . .

310

. . .

6

5

Alloy 6082

T6

5.00

20.00

all

310

...

260

...

6

8

T6511

20.00

150.00

all

310

...

260

...

8

150.00

200.00

all

280

...

240

...

8

Alloy 6105

T1

. . .

12.5

all

170

. . .

105

. . .

16

14

T5

. . .

3.20

all

250

. . .

240

. . .

8

. . .

3.20

25.00

all

250

. . .

240

. . .

10

9

Alloy 6162

T5,

Equation B0221M-13_21

. . .

25.00

all

255

. . .

235.

. . .

7

6

T5510E

T5511E

T6,

Equation B0221M-13_22

. . .

6.30

all

260

. . .

240

. . .

8

. . .

T6510E

6.30

12.50

all

260

. . .

240

. . .

10

9

T6511E

Alloy 6262

T6

Equation B0221M-13_23

T6510E

all

all

260

. . .

240

. . .

10

9

T6511E

Alloy 6351

T1

. . .

12.50

. . .

13 000

180

. . .

90

. . .

15

13

T11

. . .

20.00

all

180

. . .

110

. . .

16

14

T4

. . .

20.00

all

220

. . .

130

. . .

16

14

T5

. . .

6.30

all

260

. . .

240

. . .

8

. . .

6.30

25.00

all

260

. . .

240

. . .

10

9

T51

3.20

25.00

. . .

13 000

250

. . .

230

. . .

10

7

T54

. . .

12.50

. . .

13 000

205

. . .

140

. . .

10

9

T6

. . .

3.20

all

290

. . .

255

. . .

8

. . .

3.20

20.00

all

290

. . .

255

. . .

10

9

Alloy 6360

T5

. . .

6.30

all

150

. . .

110

. . .

8

. . .

T6

. . .

3.20

all

205

. . .

170

. . .

8

. . .

3.20

6.30

all

205

. . .

170

. . .

10

. . .

Alloy 6463

T1

. . .

12.50

. . .

13 000

115

. . .

60

. . .

12

10

T5

. . .

12.50

. . .

13 000

150

. . .

110

. . .

8

7

T6,T62F

. . .

3.20

. . .

13 000

205

. . .

170

. . .

8

. . .

3.20

12.50

. . .

13 000

205

. . .

170

. . .

10

9

Alloy 6560

T5

2.50

3.20

all

150

...

110

...

8

...

T6

2.50

3.20

all

205

...

170

...

8

...

Alloy 7005

T53

20.00

all

345

. . .

305

. . .

10

9

Alloy 7116

T5

3.20

12.50

all

330

. . .

290

. . .

8

7

Alloy 7129

T5, T6

. . .

12.50

all

380

. . .

340

. . .

9

8

Alloy 7075

O

all

all

. . .

275

. . .

165

10

9

T6

Equation B0221M-13_24

Equation B0221M-13_25

. . .

6.30

all

540

. . .

485

. . .

7

. . .

T62F

 6.30

12.50

all

560

. . .

505

. . .

7

6

T6510E

12.50

70.00

all

560

. . .

495

. . .

. . .

6

T6511E

70.00

110.00

. . .

13 000

560

. . .

490

. . .

. . .

6

70.00

110.00L

13 000

20 000

540

. . .

485

. . .

. . .

5

110.00

130.00L

. . .

20 000

540

. . .

470

. . .

. . .

5

T73

Equation B0221M-13_26

Equation B0221M-13_27

 1.60

6.30

. . .

13 000

470

. . .

400

. . .

7

. . .

T73510E

 6.30

35.00

. . .

16 000

485

. . .

420

. . .

8

7

T73511E

35.00

70.00

. . .

16 000

475

. . .

405

. . .

. . .

7

70.00

110.00L

. . .

13 000

470

. . .

395

. . .

. . .

6

70.00

110.00L

13 000

20 000

450

. . .

380

. . .

. . .

6

Equation B0221M-13_28

. . .

1.25

all

500

. . .

435

. . .

7

. . .

 1.25

3.20

all

510

. . .

440

. . .

7

. . .

T76

Equation B0221M-13_29

 3.20

6.30

. . .

13 000

510

. . .

440

. . .

7

. . .

T76510E

 6.30

12.50

. . .

13 000

515

. . .

450

. . .

7

6

T76511E

12.50

25.00

. . .

13 000

515

. . .

450

. . .

. . .

6

25.00

50.00

. . .

13 000

515

. . .

450

. . .

. . .

6

50.00

75.00

. . .

13 000

510

. . .

440

. . .

. . .

6

75.00

100.00

. . .

13 000

510

. . .

435

. . .

. . .

6

FD

all

all

. . .

. . .

. . .

. . .

. . .

. . .

Alloy 7178

O

all

. . .

20 000

. . .

275

. . .

165

10

9

Equation B0221M-13_30

. . .

1.60

all

565

. . .

525

. . .

. . .

. . .

 1.60

6.30

. . .

13 000

580

. . .

525

. . .

5

. . .

T6

Equation B0221M-13_31

 6.30

35.00

. . .

16 000

600

. . .

540

. . .

5

4

T6510E

35.00

60.00

. . .

16 000

595

. . .

530

. . .

. . .

4

T6511E

35.00

60.00

16 000

20 000

580

. . .

515

. . .

. . .

4

60.00

80.00

. . .

20 000

565

. . .

490

. . .

. . .

4

Equation B0221M-13_32

. . .

1.60

all

545

. . .

505

. . .

. . .

. . .

 1.60

6.30

. . .

13 000

565

. . .

510

. . .

5

. . .

 6.30

35.00

. . .

16 000

595

. . .

530

. . .

5

4

T62F

35.00

60.00

. . .

16 000

595

. . .

530

. . .

. . .

4

35.00

60.00

16 000

20 000

580

. . .

515

. . .

. . .

4

60.00

80.00

. . .

20 000

565

. . .

490

. . .

. . .

4

T76

Equation B0221M-13_33

Equation B0221M-13_34

 3.20

6.30

. . .

13 000

525

. . .

455

. . .

7

. . .

T76510E

 6.30

12.50

. . .

13 000

530

. . .

460

. . .

7

6

T76511E

12.50

25.00

. . .

13 000

530

. . .

460

. . .

. . .

6

FD

all

all

. . .

. . .

. . .

. . .

. . .

. . .

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 1 MPa for strength and the nearest 0.5 % for elongation, in accordance with the rounding-off method of Practice E29.
C Elongations in 50 mm apply for shapes tested in full section and for sheet-type specimens machined from material up through 12.5 mm in thickness having parallel surfaces. Elongations in 5× diameter (5.65

Equation B0221M-13_35
), where D and A are diameter and cross-sectional area of the specimen respectively, apply to round test specimens machined from thicknesses over 6.30. See 8.1.1 and 8.1.2 for conditions under which measurements are not required.
D No mechanical 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 offer 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 % in 50 mm and 9 % in 5× diameter.
H Minimum yield strength for tube, 330 MPa.
IMinimum yield strength for tube 315 MPa.
J Yield strength is not applicable to tube.
K Only in tube form.
L Properties not applicable to extruded tube over 70 mm wall thickness.
M Tentative—properties subject to revision.
Note 1Throughout this specification the use of the term alloy in the general sense includes aluminum as well as aluminum alloy.
Note 2For rolled or cold-finished bars and rods refer to Specification B211M, for drawn seamless tube used in pressure applications, Specification B210M, for structural pipe and tube, Specification B429/B429M, and for seamless pipe and tube used in pressure applications, Specification B241/B241M.
Note 3 Pipe and tube products listed in this specification are intended for general purpose applications. This specification may not address the manufacturing processes, integrity testing, and verification required for fluid-carrying applications involving pressure. See Specifications B210M and/or B241/B241M, as appropriate, for seamless pipe and tube used in fluid-carrying applications involving pressure. See Specification B234, as appropriate, for use in surface condensers, evaporators, and heat exchangers.

1.2Alloy 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.

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

1.4This specification is the metric counterpart of Specification B221.

1.5The values stated in SI are to be regarded as standard. No other units of measurement are included in this specification.

Committee
B 07
DocumentType
Standard
Pages
16
PublisherName
American Society for Testing and Materials
Status
Superseded
SupersededBy
Supersedes

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