Wrought aluminium and aluminium alloys — Cold-drawn rods/bars and tubes and wires — Part 2: Mechanical properties

This part of ISO 6363 specifies the mechanical properties of wrought aluminium and aluminium alloy rods/bars, tubes and wires for general engineering applications (except aeronautical rivets). It applies to products which are extruded and then cold drawn. It does not apply to: — products which are rolled and then cold drawn, including seam-welded tubes; — forging stock, wire for drawing stock; — drawn wires for aeronautical application, electrical or welding purposes.

Aluminium et alliages d'aluminium corroyés — Barres, tubes et fils étirés à froid — Partie 2: Caractéristiques mécaniques

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11-Jul-2012
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INTERNATIONAL ISO
STANDARD 6363-2
Second edition
2012-07-15
Wrought aluminium and aluminium
alloys — Cold-drawn rods/bars and
tubes and wires —
Part 2:
Mechanical properties
Aluminium et alliages d’aluminium corroyés — Barres, tubes et fils
étirés à froid —
Partie 2: Caractéristiques mécaniques
Reference number
ISO 6363-2:2012(E)
©
ISO 2012

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ISO 6363-2:2012(E)
COPYRIGHT PROTECTED DOCUMENT
© ISO 2012
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Published in Switzerland
ii © ISO 2012 – All rights reserved

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ISO 6363-2:2012(E)
Contents Page
Foreword .iv
1 Scope . 1
2 Normative references . 1
3 Terms and definitions . 1
4 Tensile testing . 1
5 Mechanical properties . 1
Annex A (normative) Rules for rounding .15
Annex B (normative) List of tempers used in Tables 1 and 2 .16
Bibliography .18
© ISO 2012 – All rights reserved iii

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ISO 6363-2:2012(E)
Foreword
ISO (the International Organization for Standardization) is a worldwide federation of national standards bodies
(ISO member bodies). The work of preparing International Standards is normally carried out through ISO
technical committees. Each member body interested in a subject for which a technical committee has been
established has the right to be represented on that committee. International organizations, governmental and
non–governmental, in liaison with ISO, also take part in the work. ISO collaborates closely with the International
Electrotechnical Commission (IEC) on all matters of electrotechnical standardization.
International Standards are drafted in accordance with the rules given in the ISO/IEC Directives, Part 2.
The main task of technical committees is to prepare International Standards. Draft International Standards
adopted by the technical committees are circulated to the member bodies for voting. Publication as an
International Standard requires approval by at least 75 % of the member bodies casting a vote.
Attention is drawn to the possibility that some of the elements of this document may be the subject of patent
rights. ISO shall not be held responsible for identifying any or all such patent rights.
ISO 6363-2 was prepared by Technical Committee ISO/TC 79, Light metals and their alloys, Subcommittee
SC 6, Wrought aluminium and aluminium alloys.
This second edition cancels and replaces the first edition (ISO 6363-2:1993) which has been technically revised.
ISO 6363 consists of the following parts, under the general title Wrought aluminium and aluminium alloys —
Cold-drawn rods/bars, tubes and wires:
— Part 1: Technical conditions for inspection and delivery
— Part 2: Mechanical properties
— Part 3: Drawn round bars and wires — Tolerances on form and dimensions (symmetric plus and minus
tolerances on diameter)
— Part 4: Drawn rectangular bars and wires — Tolerances on form and dimensions
— Part 5: Drawn square and hexagonal bars and wires — Tolerances on form and dimensions
— Part 6: Drawn round tubes — Tolerances on form and dimensions
iv © ISO 2012 – All rights reserved

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INTERNATIONAL STANDARD ISO 6363-2:2012(E)
Wrought aluminium and aluminium alloys — Cold-drawn rods/
bars and tubes and wires —
Part 2:
Mechanical properties
1 Scope
This part of ISO 6363 specifies the mechanical properties of wrought aluminium and aluminium alloy rods/bars,
tubes and wires for general engineering applications (except aeronautical rivets).
It applies to products which are extruded and then cold drawn.
It does not apply to:
— products which are rolled and then cold drawn, including seam-welded tubes;
— forging stock, wire for drawing stock;
— drawn wires for aeronautical application, electrical or welding purposes.
2 Normative references
The following referenced documents are indispensable for the application of this document. For dated
references, only the edition cited applies. For undated references, the latest edition of the referenced document
(including any amendments) applies.
ISO 6363-1, Wrought aluminium and aluminium alloys — Cold-drawn rods/bars, tubes and wires — Part 1:
Technical conditions for inspection and delivery
ISO 6892-1, Metallic materials — Tensile testing — Part 1: Method of test at room temperature
ASTM B557M, Standard Test Methods for Tension Testing Wrought and Cast Aluminum- and Magnesium-
Alloy Products
3 Terms and definitions
For the purposes of this document, the terms and definitions given in ISO 6363-1 apply.
4 Tensile testing
For the selection of the specimens and tensile testing, use ISO 6892-1 or ASTM B557M.
5 Mechanical properties
Values for mechanical properties of aluminium and aluminium alloys are given in Tables 1 and 2.
For elongation, two different gauge lengths are used. The choice of the gauge length for elongation
measurements (A or A ) is at the discretion of the producer, unless otherwise agreed.
50mm
NOTE A is the percentage elongation on a gauge length of 5,65 S · A is the percentage elongation on a gauge
50mm
o
length of 50 mm.
© ISO 2012 – All rights reserved 1

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ISO 6363-2:2012(E)
Test results shall be rounded in accordance with the rules given in Annex A.
Table 1 — Mechanical properties of rods/bars and wires
a
Alloy Temper Dimensions Tensile strength 0,2 % proof Elongation
stress

R R
m p0,2
min.
MPa MPa
min. max. min. max. A A
50mm
% %
1050 O D or S ≤ 3 60 100 – – – –
3 < D or S ≤ 100 60 100 20 – – 25
H14 D or S ≤ 10 95 – – – – –
H18 D or S ≤ 10 125 – – – – –
1050A O D or S ≤ 30 60 – 20 – 25 –
H14 D or S ≤ 30 100 – 70 – 6 5
H16 D ≤ 15 or S ≤ 5 120 160 105 – 4 3
H18 D or S ≤ 10 130 – 110 – 3 –
1070 O D or S ≤ 3 55 95 – – – –
3 < D or S ≤ 100 55 95 15 – – 25
H14 D or S ≤ 10 85 – – – – –
H18 D or S ≤ 10 120 – – – – –
1080A O D ≤ 20 – 80 – – – –
H14 D ≤ 18 90 – – – – –
H18 D ≤ 10 120 – – – – –
1098 O D ≤ 20 – 70 – – – –
H14 D ≤ 18 85 – – – – –
H18 D ≤ 10 115 – – – – –
1100 O D or S ≤ 3 75 110 – – – –
3 < D or S ≤ 100 75 110 20 – 22 25
b
H14 D or S ≤ 30 110 – 80 – 5 –
b
H18 D or S ≤ 10 150 – 130 – 3 –
1200 O D or S ≤ 3 75 110 – – – –
3 < D or S ≤ 30 75 110 30 – 20 25
30 < D or S ≤ 100 75 110 20 – – 25
H14 D or S ≤ 30 110 – 80 – 5 –
H16 D ≤ 15 or S ≤ 5 135 170 115 3 3
2007 T3 D or S ≤ 30 370 – 240 – 7 5
30 < D or S ≤ 80 340 – 220 – 6 –
T351 D or S ≤ 80 370 – 240 – 5 3
2011 T3 3 < D or S ≤ 38 310 – 260 – 9 10
38 < D or S ≤ 50 295 – 235 – 10 12
50 < D or S ≤ 80 280 – 205 – 10 14
T8 3 ≤ D or S ≤ 80 370 – 270 – 8 10
H13 D ≤ 18 155 225 – – – –
H18 D ≤ 10 240 – – – – –
2 © ISO 2012 – All rights reserved

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ISO 6363-2:2012(E)
Table 1 (continued)
a
Alloy Temper Dimensions Tensile strength 0,2 % proof Elongation
stress

R R
m p0,2
min.
MPa MPa
A
min. max. min. max. A
50mm
% %
2011A T3 D or S ≤ 40 320 – 270 – 10 8
40 < D or S ≤ 50 300 – 250 – 10 –
50 < D or S ≤ 80 280 – 210 – 10 –
T8 D or S ≤ 80 370 – 270 – 8 6
2014 O 3 ≤ D or S ≤ 100 – 245 – – – 12
T3 D or S ≤ 80 380 – 290 – 8 6
T351 D or S ≤ 80 380 – 290 – 6 4
T4 3 ≤ D or S ≤ 100 380 – 220 – 10 16
c
T42
T451
T6 3 ≤ D or S ≤ 100 450 – 380 – 7 8
d
T62
T651
2014A O D or S ≤ 80 – 240 – 125 12 10
H111
e
H13 D ≤ 18 210 280 – – – –
H18 D ≤ 10 295 – – – – –
T3 D or S ≤ 80 380 – 290 – 8 6
T351 D or S ≤ 80 380 – 290 – 6 4
T4 D or S ≤ 100 380 – 220 – 10 10
T451
T6 D or S ≤ 50 440 – 360 – 7 8
T651 D or S ≤ 100 450 – 380 – 7 8
2017 O D or S ≤ 3 – 245 – – – –
3 < D or S ≤ 100 – 245 – – – 16
H13 3 ≤ D or S ≤ 10 205 275 – – – –
T4 D or S ≤ 3 380 – – – – –
c
3 < D or S ≤ 100 380 – 225 – – 12
T42
2017A O D or S ≤ 80 – 240 – 125 12 10
H111
e
H13 D ≤ 18 210 300 – – – –
H18 D ≤ 10 315 – – – – –
T3 D or S ≤ 80 400 – 250 – 10 8
T351 D or S ≤ 80 400 – 250 – 8 6
T4 D or S ≤ 50 380 – 220 – 10 –
50 < D or S ≤ 100 390 – 235 – 10 –
T451
© ISO 2012 – All rights reserved 3

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ISO 6363-2:2012(E)
Table 1 (continued)
a
Alloy Temper Dimensions Tensile strength 0,2 % proof Elongation
stress

R R
m p0,2
min.
MPa MPa
A
min. max. min. max. A
50mm
% %
e
2117 H13 D or S ≤ 18 170 240 – – – –
H15 3 < D or S ≤ 10 195 245 – – – –
H18 D ≤ 18 260 – – – – –
T4 3 < D or S ≤ 10 265 – 125 – – 18
f
2024 O D or S ≤ 3 – 245 – – – –
3 < D or S ≤ 100 – 245 – – – 16
H111
e
H13 D ≤ 18 230 300 – – – –
H18 D ≤ 10 320 – – – – –
T3 D or S ≤ 10 425 – 310 – 10 8
10 < D or S ≤ 80 425 – 290 – 9 7
T351 12,5 < D or S ≤ 100 425 – 310 – 9 –
T4 D or S ≤ 3 425 – – – – –
3 < D or S ≤ 12 425 – 310 – 10 10
T451
12 < D or S ≤ 100 425 – 290 – 9 10
c
T42 D or S ≤ 3 430 – – – – –
3 < D or S ≤ 100 430 – 275 – – 10
T6 D or S ≤ 80 425 – 315 – 5 4
T651 D or S ≤ 80 425 – 315 – 4 3
d
T62 D or S ≤ 3 410 – – – – –
3 < D or S ≤ 100 410 – 315 – – 5
T8 D or S ≤ 80 455 – 400 – 4 3
T851 D or S ≤ 80 455 – 400 – 3 2
2030 T3 D or S ≤ 50 370 – 250 – 7 –
50 < D or S ≤ 100 340 – 210 – 7 –
T351 D or S ≤ 80 370 – 240 – 5 3
2219 T851 10 < D or S ≤ 50 400 – 275 – 3 –
50 < D or S ≤ 100 395 – 270 – 3 –
3003 O D or S ≤ 3 95 125 – – – –
3 < D or S ≤ 100 95 125 35 – 22 25
b b
H12 D or S ≤ 10 115 – 80 – 7 –
b b
H14 D or S ≤ 10 135 – 110 – 6 –
b b
H16 D ≤ 15 or S ≤ 5 160 – 130 – 3 –
b b
H18 D or S ≤ 10 180 – 145 – 2 –
3103 O D or S ≤ 50 95 – 35 – 22 19
H14 D or S ≤ 30 130 – 90 – 6 4
H16 D ≤ 15 or S ≤ 5 160 195 130 – 4 3
H18 D or S ≤ 10 160 – 130 – 4 3
4 © ISO 2012 – All rights reserved

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ISO 6363-2:2012(E)
Table 1 (continued)
a
Alloy Temper Dimensions Tensile strength 0,2 % proof Elongation
stress

R R
m p0,2
min.
MPa MPa
A
min. max. min. max. A
50mm
% %
5005 O D ≤ 80 or S ≤ 60 100 145 40 – 18 16
H111
H14 D ≤ 40 or S ≤ 10 140 – 110 – 6 4
H18 D ≤ 15 or S ≤ 2 185 – 155 – 4 2
5005A O D ≤ 80 or S ≤ 60 100 145 40 – 18 16
H111
H14 D ≤ 40 or S ≤ 10 140 – 110 – 6 4
H18 D ≤ 15 or S ≤ 2 185 – 155 – 4 2
5019 O D ≤ 80 or S ≤ 60 250 320 110 – 16 14
H111
H12 D ≤ 40 or S ≤ 25 270 350 180 – 8 7
H22
H32
H14 D ≤ 25 or S ≤ 10 300 – 210 – 4 3
H24
H34
5041 O D or S ≤ 25 225 – – – – 20
5050 O D or S ≤ 10 125 180 – – 25 22
H32 D or S ≤ 10 150 – – – – –
H34 D or S ≤ 10 170 – – – – –
H36 D or S ≤ 10 185 – – – – –
H38 D or S ≤ 10 200 – – – – –
5051A O D ≤ 20 – 195 – – – –
H12 D ≤ 18 170 220 – – – –
H14 D ≤ 18 195 245 – – – –
H18 D ≤ 10 245 – – – – –
5052 O D or S ≤ 3 170 220 – – – –
3 < D or S ≤ 100 170 220 65 – 22 25
H111
H32 3 < D or S ≤ 10 215 255 – – – –
H14 D or S ≤ 3 235 – – – – –
3 < D or S ≤ 30 235 – 180 – 5 –
H34 D or S ≤ 3 235 – – – – –
b
3 < D or S ≤ 30 235 – 180 – 6 –
H16 D or S ≤ 15 250 290 200 – 3 3
H26
H36
H18 D or S ≤ 10 270 – 220 – 2 –
b b
H38 D or S ≤ 10 270 – 220 – 2 –
© ISO 2012 – All rights reserved 5

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ISO 6363-2:2012(E)
Table 1 (continued)
a
Alloy Temper Dimensions Tensile strength 0,2 % proof Elongation
stress

R R
m p0,2
min.
MPa MPa
A
min. max. min. max. A
50mm
% %
5056 O D or S ≤ 3 – 315 – – – –
3 < D or S ≤ 100 250 320 110 – 16 20
H12 D or S ≤ 10 300 – – – – –
H32
H34 D or S ≤ 10 345 – – – – –
H38 D or S ≤ 10 380 – – – – –
5083 O D or S ≤ 3 275 355 – – – –
3 < D or S ≤ 100 275 355 110 – 14 14
H111 D or S ≤ 50 270 – 140 – 12 –
H12 D or S ≤ 30 300 – 200 – 4 –
5086 O D or S ≤ 50 240 – 95 – 16 –
H12 D or S ≤ 25 270 – 190 – 4 –
H32 D or S ≤ 25 270 – 190 – 5 –
5154 O D or S ≤ 10 205 285 75 – 20 16
H32 D or S ≤ 10 250 – – – – –
H34 D or S ≤ 10 270 – – – – –
H36 D or S ≤ 10 290 – – – – –
H38 D or S ≤ 10 310 – – – – –
5251 O D ≤ 80 or S ≤ 60 150 200 60 – 17 15
H111
H14 D ≤ 30 or S ≤ 5 200 240 160 – 5 4
H24
H34
H18 D ≤ 20 or S ≤ 3 240 – 200 2 2
H28
H38
5754 O D or S ≤ 50 180 – 80 – 16 –
H14 D or S ≤ 30 250 – 180 – 4 –
H34 D or S ≤ 30 250 – 180 – 5 –
H18 D or S ≤ 10 280 – 240 – 2 –
H38 D or S ≤ 10 280 – 240 – 3 –
g
6012 T4 D or S ≤ 80 200 – 100 – 10 8
g
T6 D or S ≤ 80 310 – 260 – 8 6
d
6056 H13 D ≤ 18 160 240 – – – –
H18 D ≤ 10 240 – – – – –
i
T39 D < 6 400 – – – – –
i
T39 D ≥ 6 360 – – – – –
T4 D ≤ 20 300 380 – – – –
T6 D ≤ 20 400 – – – – –
i
T89 D < 6 420 – – – – –
6 © ISO 2012 – All rights reserved

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ISO 6363-2:2012(E)
Table 1 (continued)
a
Alloy Temper Dimensions Tensile strength 0,2 % proof Elongation
stress

R R
m p0,2
min.
MPa MPa
A
min. max. min. max. A
50mm
% %
i
6060 T39 D ≥ 6 220 – – – – –
i
T39 D < 6 270 – – – – –
g
T4 D or S ≤ 80 130 – 65 – 15 13
g
T6 D or S ≤ 80 215 – 160 – 12 10
i
T89 D < 6 260 – – – – –
f
6061 O D or S ≤ 3 145 – – – – –
3 < D or S ≤ 100 145 – – – – 18
h
H13 3 ≤ D or S ≤ 10 155 205 – – – –
H18 D ≤ 10 210 – – – – –
T39 D < 6 310 – – – – –
6 ≤ D 260 – – – – –
T4 D or S ≤ 3 205 – – – – –
3 < D or S ≤ 100 205 – 110 – 16 18
c
T42 D or S ≤ 3 205 – – – – –
3 < D or S ≤ 100 205 – 95 – – 18
T6 D or S ≤ 3 290 – – – – –
d
3 < D or S ≤ 100 290 – 240 – 9 10
T62
i
T89 D < 6 300 – – – – –
i
6063 T39 D ≥ 6 230 – – – – –
i
T39 D < 6 280 – – – – –
g
T4 D or S ≤ 80 150 – 75 – 15 13
g
T6 D or S ≤ 80 220 – 190 – 10 8
g
T66 D or S ≤ 80 230 – 195 – 10 8
i
T89 D < 6 270 – – – – –
6063A O D or S ≤ 80 – 140 – – 15 13
H111
g
T4 D or S ≤ 80 150 – 90 – 16 14
g
T6 D or S ≤ 80 230 – 190 – 9 7
g
6065 T6 D ≤ 120 or S ≤ 85 290 – 240 – 10 8
g
T8 D ≤ 120 or S ≤ 85 345 – 315 – 4 3
g
T9 D ≤ 120 or S ≤ 85 360 – 330 – 4 3
6082 O D or S ≤ 80 – 160 – 110 15 –
h
H13 D ≤ 18 165 225 – – – –
H18 D ≤ 10 220 – – – – –
i
T39 D < 6 360 – – – – –
i
T39 6 ≤ D 310 – – – – –
T4 D or S ≤ 80 205 – 110 – 14 –
T6 D or S ≤ 80 310 – 255 – 10 –
T8 D or S ≤ 80 310 – 260 – 8 –
i
T89 D < 6 340 – – – – –
© ISO 2012 – All rights reserved 7

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ISO 6363-2:2012(E)
Table 1 (continued)
a
Alloy Temper Dimensions Tensile strength 0,2 % proof Elongation
stress

R R
m p0,2
min.
MPa MPa
A
min. max. min. max. A
50mm
% %
6181 T4 D or S ≤ 50 200 – 100 – 15 –
T6 D or S ≤ 50 280 – 240 – 8 –
6262 T6 D or S ≤ 100 290 – 240 – 8 7
g
T8 D or S ≤ 50 345 – 315 – 4 3
T9 D or S ≤ 50 360 – 330 – 4 5
50 < D or S ≤ 80 345 – 315 – 4 –
g
6262A T6 D ≤ 120 or S ≤ 85 290 – 240 – 10 8
g
T8 D ≤ 120 or S ≤ 85 345 – 315 – 4 3
g
T9 D ≤ 120 or S ≤ 85 360 – 330 – 4 3
7020 T5 D or S ≤ 50 350 – 280 – 10 –
T6
g
7022 T6 D or S ≤ 80 460 – 380 – 8 6
7049A T6 D ≤ 80 590 – 500 – 7 –
f
7075 O 3 ≤ D or S ≤ 100 – 275 – – – 10
h
H13 D ≤ 18 230 310 – – – –
H18 D ≤ 10 285 – – – – –
T6 3 ≤ D or S ≤ 100 520 – 460 – 6 7
d
T62
T651
T73 D or S ≤ 100 470 – 385 – 9 7
a
D (mm) = diameter for round bar.
S (mm) = width across flats for square and hexagonal bar, thickness for rectangular bar.
b
Guaranteed values agreed upon between the purchaser and the supplier where requested by the purchaser.
c
The mechanical properties of temper grade T42 shall be applied only where the material of temper grade O has been naturally
age-hardened after solution treatment by the purchaser. If the material is cold or hot worked prior to solution treatment by the purchaser,
its mechanical properties may be lower than the specified values.
d
The mechanical properties of temper grade T62 shall be applied only where the material of temper grade O has been artificially
age-hardened after solution treatment by the purchaser. If the material is cold or hot worked prior to solution treatment by the purchaser,
its mechanical properties may be lower than the specified values.
e
Mechanical properties shall be tested in T4 temper (alloys 2017A, 2117 and 2024) or T6 temper (alloy 2014A).Testing may also be
carri
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