ISO 6362-2:2014
(Main)Wrought aluminium and aluminium alloys — Extruded rods/bars, tubes and profiles — Part 2: Mechanical properties
Wrought aluminium and aluminium alloys — Extruded rods/bars, tubes and profiles — Part 2: Mechanical properties
ISO 6362-2:2014 specifies the mechanical properties of wrought aluminium and aluminium alloy extruded rods/bars, tubes, and profiles for general engineering applications. It applies to extruded products.
Aluminium et alliages d'aluminium corroyés — Barres, tubes et profilés filés — Partie 2: Caractéristiques mécaniques
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Standards Content (Sample)
INTERNATIONAL ISO
STANDARD 6362-2
Fourth edition
2014-09-15
Wrought aluminium and aluminium
alloys — Extruded rods/bars, tubes
and profiles —
Part 2:
Mechanical properties
Aluminium et alliages d’aluminium corroyés — Barres, tubes et
profilés filés —
Partie 2: Caractéristiques mécaniques
Reference number
ISO 6362-2:2014(E)
©
ISO 2014
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ISO 6362-2:2014(E)
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ii © ISO 2014 – All rights reserved
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ISO 6362-2:2014(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 .22
Annex B (normative) List of tempers used in Tables 1 to 3 .23
Bibliography .25
© ISO 2014 – All rights reserved iii
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ISO 6362-2:2014(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.
The procedures used to develop this document and those intended for its further maintenance are
described in the ISO/IEC Directives, Part 1. In particular the different approval criteria needed for the
different types of ISO documents should be noted. This document was drafted in accordance with the
editorial rules of the ISO/IEC Directives, Part 2 (see www.iso.org/directives).
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. Details of any
patent rights identified during the development of the document will be in the Introduction and/or on
the ISO list of patent declarations received (see www.iso.org/patents).
Any trade name used in this document is information given for the convenience of users and does not
constitute an endorsement.
For an explanation on the meaning of ISO specific terms and expressions related to conformity
assessment, as well as information about ISO’s adherence to the WTO principles in the Technical Barriers
to Trade (TBT) see the following URL: Foreword - Supplementary information
The committee responsible for this document is ISO/TC 79, Light metals and their alloys, Subcommittee
SC 6, Wrought aluminium and aluminium alloys.
This fourth edition cancels and replaces the third edition (ISO 6362-2:2012), which has been technically
revised.
ISO 6362 consists of the following parts, under the general title Wrought aluminium and aluminium
alloys — Extruded rods/bars, tubes and profiles:
— Part 1: Technical conditions for inspection and delivery
— Part 2: Mechanical properties
— Part 3: Extruded rectangular bars — Tolerances on shape and dimensions
— Part 4: Profiles — Tolerances on shape and dimensions
— Part 5: Round, square and hexagonal bars — Tolerances on shape and dimensions
— Part 6: Round, square, rectangular and hexagonal tubes — Tolerances on shape and dimensions
— Part 7: Chemical composition
iv © ISO 2014 – All rights reserved
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INTERNATIONAL STANDARD ISO 6362-2:2014(E)
Wrought aluminium and aluminium alloys — Extruded
rods/bars, tubes and profiles —
Part 2:
Mechanical properties
1 Scope
This part of ISO 6362 specifies the mechanical properties of wrought aluminium and aluminium alloy
extruded rods/bars, tubes, and profiles for general engineering applications.
It applies to extruded products.
2 Normative references
The following documents, in whole or in part, are normatively referenced in this document and are
indispensable for its application. For dated references, only the edition cited applies. For undated
references, the latest edition of the referenced document (including any amendments) applies.
ISO 6362-1, Wrought aluminium and aluminium alloys — Extruded rods/bars, tubes and profiles — 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 6362-1 apply.
4 Tensile testing
For the selection of the specimens and tensile testing, see ISO 6892-1 or ASTM B557M.
5 Mechanical properties
Values for mechanical properties of aluminium and aluminium alloys are given in Tables 1 to 3.
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
50mm
o
gauge length of 50 mm.
Test results shall be rounded in accordance with the rules given in Annex A.
© ISO 2014 – All rights reserved 1
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ISO 6362-2:2014(E)
Table 1 — Mechanical properties of rods/bars
a
Alloy Temper Dimensions Tensile 0,2 % proof Elongation
strength stress min.
R R
m p0,2
MPa MPa
A A
50mm
min. max. min. max.
% %
1070 H112 All 55 — 15 — — -
1070A H112 All 60 — 20 — 25 23
1060 H112 3 ≤ D or S ≤ 30 60 — 30 — — 25
1050 H112 All 65 — 20 — — —
H112 D < 35 or S < 30 65 — 20 — 25 23
1050A O
All 60 95 20 — 25 23
H111
b
1350 H112 All 60 — — — 25 23
D < 35 or S < 30 75 — 20 — 18 18
1100 H112
35 ≤ D or 30 ≤ S 75 — 20 — — —
D < 35 or S < 30 75 25 — 20 18
1200 H112 —
35 ≤ D or 30 ≤ S 75 20 — — —
T4 D or S ≤ 80 370 — 250 — 8 6
2007 T4510 80 < D or S ≤ 200 340 — 220 — 8 —
T4511 200 < D or S ≤ 250 330 — 210 — 7 —
3 ≤ D or S ≤ 40 310 — 260 — 10 10
T3 40 < D or S ≤ 50 295 — 235 — 10 12
50 < D or S ≤ 75 290 — 205 — 10 14
2011 T4 3 ≤ D or S ≤ 200 275 — 125 — 14 16
3 < D or S ≤ 75 310 — 230 — 8 10
T6
75 < D or S ≤ 160 295 — 195 — 6 8
T8 3 ≤ D or S ≤ 75 370 — 275 — 10 10
T4 D ≤ 200, S ≤ 60 275 — 125 — 14 12
2011A D ≤ 75, S ≤ 60 310 — 230 — 8 6
T6
75 < D ≤ 200 295 — 195 — 6 —
c
O All — 250 — 135 10 12
T4
2014 T4510 All 345 — 240 — 10 12
T4511
d
T42 All 345 — 205 — — 12
D or S ≤ 12 410 — 365 — — 7
12 < D or S ≤ 19 440 — 400 — 6 7
T6
19 < D or S, A ≤ 16 000 470 — 410 — 6 7
T6510
19 < D or S, 16 000 < A ≤ 20 000 470 — 400 — 6 6
T6511
19 < D or S, 20 000 < A ≤ 25 000 450 — 380 — 6 6
19 < D or S, 25 000 < A ≤ 30 000 430 — 365 — 6 6
D or S ≤ 19 410 — 365 — — 7
e
T62 19 < D or S, A ≤ 16 000 410 — 365 — — 7
19 < D or S, 16 000 < A ≤ 20 000 410 — 365 — — 6
2 © ISO 2014 – All rights reserved
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ISO 6362-2:2014(E)
Table 1 (continued)
a
Alloy Temper Dimensions Tensile 0,2 % proof Elongation
strength stress min.
R R
m p0,2
MPa MPa
A A
50mm
min. max. min. max.
% %
O 10 < D or S ≤ 200 — 250 — 135 10 12
T4,
T4510 10 < D or S ≤ 200 345 — 240 — 10 12
2014A T4511
T6 12,5 < D or S ≤ 100 440 — 400 — 6 —
T6510 100 < D or S ≤ 120 430 — 350 — 6 —
T6511 120 < D or S ≤ 200 430 — 350 — 6 —
c
O All 245 125 —- 16
2017 T4 A ≤ 70 000 345 215 — 12
d
T42 70 000 < A ≤ 100 000 345 195 — 12
O 10 < D or S ≤ 100 — 250 — 150 10 —
T4
2017A 10 < D or S ≤ 80 390 — 265 — 10 —
T4510
80 < D or S ≤ 200 360 — 220 — 7 —
T4511
c
O All — 245 — 125 10 12
D or S ≤ 6 390 — 295 — — 12
6 < D or S ≤ 19 410 — 300 — 10 12
T3510
19 < D or S ≤ 38 450 — 310 — 8 10
T3511
38 < D or S, A ≤ 16 000 480 — 365 — 7 10
38 < D or S, 16 000 < A ≤ 20 000 470 — 335 — 7 8
D or S ≤ 6 390 — 295 — — 12
6 < D or S ≤ 19 410 — 305 — — 12
19 < D or S ≤ 38 450 — 315 — — 10
38 < D or S ≤ 100, A ≤ 16 000 480 — 365 — 8 10
T3
2024 38 < D or S ≤ 100, 16 000 < A ≤ 20 000 470 — 335 — 8 8
T4
38 < D or S ≤ 100, 20 000 < A ≤ 30 000 460 — 315 — 8 8
100 < D or S ≤ 200, A ≤ 16 000 480 — 365 — 6 10
100 < D or S ≤ 200, 16 000 < A ≤ 20 000 470 — 335 — 6 8
100 < D or S ≤ 200, 20 000 < A ≤ 30 000 460 — 315 — 6 8
D or S ≤ 19 390 — 265 — — 12
19 < D or S ≤ 38 390 — 265 — — 10
d
T42
38 < D or S, A ≤ 16 000 390 — 265 — — 10
38 < D or S, 16 000 < A ≤ 20 000 390 — 265 — — 8
T8510
T8511 10 < D or S ≤ 150 455 — 400 — 4 —
T81
T4 D or S ≤ 80 370 — 250 — 8 6
2030 T4510 80 < D or S ≤ 200 340 — 220 — 8 —
T4511 200 < D or S ≤ 250 330 — 210 — 7 —
© ISO 2014 – All rights reserved 3
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ISO 6362-2:2014(E)
Table 1 (continued)
a
Alloy Temper Dimensions Tensile 0,2 % proof Elongation
strength stress min.
R R
m p0,2
MPa MPa
A A
50mm
min. max. min. max.
% %
3102 H112 All 80 — 30 — 25 23
H112 All 95 — 35 — — —
3003 O
All 95 135 35 — 25 20
H111
H112 All 95 — 35 — 25 20
3103 O
All 95 135 35 — 25 20
H111
H112 All 100 — 40 — 18 16
5005
O
5005A
D ≤ 80, S ≤ 60 100 150 40 — 18 16
H111
H112 D or S ≤ 200 250 — 110 — 14 12
5019 O
D or S ≤ 200 250 320 110 — 15 13
H111
5049 H112 All 180 — 80 — 15 13
H112 All 150 — 50 — 16 14
5051A O
All 150 200 50 — 18 16
H111
H112 All 160 — 60 — 16 14
5251 O
All 160 220 60 — 17 15
H111
H112 All 175 — 70 — — —
5052
O All 175 245 70 — — 20
H112 D or S ≤ 200 200 — 85 — 16 14
5154A O
D or S ≤ 200 200 275 85 — 18 16
H111
H112 All 215 — 100 — — 12
5454 O
D or S ≤ 200 200 275 85 — 18 16
H111
D or S ≤ 150 180 — 80 — 14 12
H112
150 < D or S ≤ 250 180 — 70 — 13 —
5754
O
D or S ≤ 150 180 250 80 — 17 15
H111
A ≤ 30 000 245 — 100 — — —
5056 H112 30 000 < A ≤ 70 000 225 — 80 — — —
70 000 < A ≤ 100 000 215 — 70 — — —
H112 D or S ≤ 130, A ≤ 20 000 275 — 140 — 12 12
5083
O D or S ≤ 130, A ≤ 20 000 275 355 110 — — 14
H112 D or S ≤ 250 240 — 95 — 12 10
5086
O D or S ≤ 200 240 320 95 — 18 15
4 © ISO 2014 – All rights reserved
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ISO 6362-2:2014(E)
Table 1 (continued)
a
Alloy Temper Dimensions Tensile 0,2 % proof Elongation
strength stress min.
R R
m p0,2
MPa MPa
A A
50mm
min. max. min. max.
% %
3 ≤ D or S ≤ 7 195 — 165 — — 10
f
T6 7 < D or S ≤ 17 195 — 165 — — 12
6101
17 < D or S ≤ 30 175 — 145 — — 14
T7 3 ≤ D or S ≤ 17 135 — 110 — — 10
f
6101A T6 D or S ≤ 150 200 — 170 — 10 8
f,g
T6 S ≤ 15 215 — 160 — 8 6
6101B
f,h
T7 S ≤ 15 170 — 120 — 12 10
D or S ≤ 25 270 — 225 — 10 8
6005
f
T6 25 < D or S ≤ 50 270 — 225 — 8 —
6005A
50 < D or S ≤ 100 260 — 215 — 8 —
D or S ≤ 6 245 — 205 — — 8
T5
6005C 6 < D or S ≤ 12 225 — 175 — — 8
f
T6 D or S ≤ 6 265 — 235 — — 8
f
T5 D or S ≤ 120 380 — 360 — 10 8
6110A
f
T6 D ≤ 120 or S ≤ 150 410 — 380 — 10 8
f
T6
D or S ≤ 150 310 — 260 — 8 6
f
6012 T6510
150 < D or S ≤ 200 260 — 200 — 8 —
f
T6511
f
T6
D or S ≤ 150 310 — 260 — 8 6
f
6018 T6510
150 < D or S ≤ 200 260 — 200 — 8 —
f
T6511
f
T6
f
6023 T6510 D or S ≤ 150 320 — 270 — 10 8
f
T6511
O
D or S ≤ 200 — 160 — 110 14 12
H111
f
T4 D or S ≤ 200 205 — 110 — 14 12
D or S ≤ 20 295 — 250 — 8 6
6351
20 < D or S ≤ 75 300 — 255 — 8 —
f
T6 75 < D or S ≤ 150 310 — 260 — 8 —
150 < D or S ≤ 200 280 — 240 — 6 —
200 < D or S ≤ 250 270 — 200 — 6 —
f
T4 D or S ≤ 150 120 — 60 — 16 14
T5 D or S ≤ 150 160 — 120 — 8 6
f
6060 T6 D or S ≤ 100 190 — 150 — 10 8
f
T64 D or S ≤ 50 180 — 120 — 12 10
f
T66 D or S ≤ 150 215 — 160 — 8 6
© ISO 2014 – All rights reserved 5
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ISO 6362-2:2014(E)
Table 1 (continued)
a
Alloy Temper Dimensions Tensile 0,2 % proof Elongation
strength stress min.
R R
m p0,2
MPa MPa
A A
50mm
min. max. min. max.
% %
f
T4 D or S ≤ 150 110 — 50 — 16 14
T5 D or S ≤ 150 150 — 110 — 8 6
6360
f
T6 D or S ≤ 150 185 — 140 — 8 6
f
T66 D or S ≤ 150 195 — 150 — 8 6
c
O All — 145 — 110 — 16
f
T4
All 180 — 110 — 14 16
T4511
d
6061 T42 All 175 — 85 — — 16
f
T6
D or S ≤ 6 260 — 240 — 7 8
e
T62
6 < D or S 260 — 240 — 9 10
T6511
O
D or S ≤ 100 — 170 — 120 14 12
H111
f
6261 T4 D or S ≤ 100 180 — 100 — 14 12
D or S ≤ 20 290 — 245 — 8 7
f
T6
20 < D or S ≤ 100 290 — 245 — 8 —
f
6262 T6 D or S ≤ 200 260 — 240 — 10 8
f
6262A T6 D ≤ 220 or S ≤ 155 260 — 240 — 10 8
O
D or S ≤ 200 — 130 — — 18 16
H111
D or S ≤ 12 120 — 60 — — 12
T1
12 < D or S ≤ 25 110 — 55 — — 12
D or S ≤ 150 130 — 65 — 14 12
f
6063 T4
150 < D or S ≤ 200 120 — 65 — 12 —
D or S ≤ 12 150 — 110 — 7 8
T5
12 < D or S ≤ 25 145 — 105 — 7 8
D or S ≤ 3 205 — 170 — — 8
f
T6
3 < D or S ≤ 25 205 — 170 — 9 10
f
T66 D or S ≤ 200 245 — 200 — 10 8
O
D or S ≤ 200 — 150 — — 16 14
H111
D or S ≤ 150 150 — 90 — 12 10
f
6063A T4
150 < D or S ≤ 200 140 — 90 — 10 —
T5 D or S ≤ 200 200 — 160 — 7 5
D or S ≤ 150 230 — 190 — 7 5
f
T6
150 < D or S ≤ 200 220 — 160 — 7 —
f
T4 D or S ≤ 150 125 — 75 — 14 12
6463 T5 D or S ≤ 150 150 — 110 — 8 6
f
T6 D or S ≤ 150 195 — 160 — 10 8
6 © ISO 2014 – All rights reserved
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ISO 6362-2:2014(E)
Table 1 (continued)
a
Alloy Temper Dimensions Tensile 0,2 % proof Elongation
strength stress min.
R R
m p0,2
MPa MPa
A A
50mm
min. max. min. max.
% %
f
6065 T6 D ≤ 220 or S ≤ 155 260 — 240 — 10 8
f
6081 T6 D or S ≤ 250 275 — 240 — 8 6
O
D or S ≤ 200 — 160 — 110 14 12
H111
f
6082 T4 10 ≤ D or S ≤ 80 205 — 110 — 14 14
10 ≤ D ≤ 60 or 10 ≤ S ≤ 50 310 — 260 — 8 7
f
T6
60 < D ≤ 150 or 50 < S ≤ 150 300 — 240 — 8 —
f
T4 D ≤ 220 or S ≤ 155 205 — 110 — 12 10
9 < D or S ≤ 100 360 — 330 — 9 7
6182
f,i
T6 100 < D or S ≤ 150 330 — 300 — 8 6
150 < D or S ≤ 220 280 — 240 — 6 4
D or S ≤ 12 285 — 245 — — 10
T5
12 < D or S ≤ 25 275 — 235 — — 10
7003
D or S ≤ 50 350 — 290 — 10 8
f
T6
50 < D or S ≤ 150 340 — 280 — 10 8
O All — 245 — 145 — 12
j
7204 T4 All 315 — 195 — — 11
T6 All 335 — 275 — — 10
D or S ≤ 50 350 — 290 — 10 8
f
7005 T6
50 < D or S ≤ 200 340 — 270 — 10 —
f
7108 T6 D or S ≤ 100 310 — 260 — 10 8
f
T6 D or S ≤ 200 310 — 260 — 12 10
7108A D or S ≤ 50 350 — 290 — 10 8
f
T66
50 < D or S ≤ 200 340 — 275 — 10 —
D or S ≤ 50 350 — 290 — 10 8
f
7020 T6
50 < D or S ≤ 200 340 — 275 — 10 —
f
7021 T6 D or S ≤ 40 410 — 350 — 10 8
f
T6
D or S ≤ 80 490 — 420 — 7 5
f
7022 T6510
80 < D or S ≤ 200 470 — 400 — 7 —
f
T6511
D or S ≤ 100 610 — 530 — 5 4
T6
100 < D or S ≤ 125 560 — 500 — 5 —
7049A T6510
125 < D or S ≤ 150 520 — 430 — 5 —
T6511
150 < D or S ≤ 180 450 — 400 — 3 —
T73511 D or S ≤ 125, A ≤ 20 000 485 — 415 — 7 8
7050 T74511 D or S ≤ 76 505 — 435 — — 7
T76510 D or S ≤ 127 545 — 475 — — 7
© ISO 2014 – All rights reserved 7
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ISO 6362-2:2014(E)
Table 1 (continued)
a
Alloy Temper Dimensions Tensile 0,2 % proof Elongation
strength stress min.
R R
m p0,2
MPa MPa
A A
50mm
min. max. min. max.
% %
c
O A ≤ 20 000 — 275 — 165 9 10
D or S ≤ 6 540 — 480 — — 7
T6, 6 ≤ D or S ≤ 75 560 — 500 — 6 7
e
T62 75 < D or S ≤ 110, A ≤ 13 000 560 — 490 — 5 7
T6510 75 < D or S ≤ 110, 13 000 < A ≤ 20 000 540 — 480 — 5 7
T6511 110 < D or S ≤ 130, A ≤ 20 000 540 — 470 — 5 6
130 < D or S ≤ 150 500 — 440 — 5 —
7075 10 < D or S ≤ 25 485 — 420 — 7 —
25 < D or S ≤ 50 475 — 405 — 7 —
k
T73
50 < D or S ≤ 70 475 — 405 — 7 —
70 < D or S ≤ 100 470 — 390 — 6 —
D or S ≤ 25 485 — 420 — 7 5
k
T73510 25 < D or S ≤ 75 475 — 405 — 7 —
k
T73511 75 < D or S ≤ 100 470 — 390 — 6 —
100 < D or S ≤ 150 440 — 360 — 6 —
a
D (mm) = diameter for round bar.
S (mm) = width across flats for square and hexagonal bar, thickness for rectangular bar.
2
A (mm ) = cross-section area.
b
Electrical conductivity γ ≥ 35,4 MS/m.
c
The material of temper grade O shall be a basis for materials of temper grades T42 or T62. When requested by the pur-
chaser, the capability to achieve T42 or T62 properties after appropriate heat treatment is demonstrated.
d
The mechanical properties of temper grade T42 shall be applied only when 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 can be lower than the specified values.
e
The mechanical properties of temper grade T62 shall be applied only when 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 can be lower than the specified values.
f
Applicable for those after extrusion followed by controlled cooling at a rate rapid enough to hold constituents in solu-
tion.
g
Electrical conductivity γ ≥ 30 MS/m.
h
Electrical conductivity γ ≥ 32 MS/m.
i
Properties obtained by the user, however, can be lower than those listed if the material has been formed or otherwise
cold or hot worked, particularly in the annealed temper, prior to normal solution heat treatment.
j
The mechanical properties of temper grade T4 are the values specified, based on reference values obtained by 1 month
of natural ageing at room temperature (approximately 20 °C) after solution treatment.
In the case of the tensile test made before completion of 1 month of natural ageing, the tensile performance of temper
grade T4 can be deemed as guaranteed if the test result of the test piece which has been artificially aged after solution
treatment is confirmed to satisfy the tensile performance of temper grade T6.
k
For materials of thickness 20 mm or above, see EN 755–1, with respect to stress corrosion cracking resistance.
8 © ISO 2014 – All rights reserved
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ISO 6362-2:2014(E)
Table 2 — Mechanical properties of tubes
a
Alloy Temper Dimensions Tensile 0,2 % proof Elongation
strength stress min.
R R
m p0,2
MPa MPa
A A
50mm
min. max. min. max.
% %
1070 H112 All 55 — 15 — — —
1050 H112 All 65 — 20 — — —
H112 All 60 — 20 — 25 23
1050A
O,H111 All 60 95 20 — 25 23
1350 H112 All 60 — — — 25 23
1100,
H112 All 75 — 20 — — 25
1200
T4
2007 T4510 t ≤ 25 370 — 250 — 8 6
T4511
2011,
T6 t ≤ 25 310 — 230 — 6 4
2011A
b
O All — 245 — 125 — 12
T4 All 345 — 245 — — 12
c
T42 All 345 — 205 — — 12
T4510
2014 t ≤ 20 370 — 230 — 11 10
T4511
t ≤ 12 410 — 365 — — 7
12 < t ≤ 19 440 — 400 — — 7
19 < t, A ≤ 16 000 470 — 410 — — 7
T6
19 < t, 16 000 < A ≤ 20 000 470 — 400 — — 6
19 < t, 20 000 < A ≤ 25 000 450 — 380 — — 6
19 < t, 25 000 < A ≤ 30 000 430 — 365 — — 6
t ≤ 19 410 — 365 — — 7
d
T62 19 < t, A ≤ 16 000 410 — 365 — — 7
19 < t, 16 000 < A ≤ 20 000 410 — 365 — — 6
T6510 t ≤ 10 415 — 370 — 7 5
T6511 10 < t ≤ 40 450 — 400 — 6 4
O
t ≤ 20 — 250 — 135 12 10
H111
T4
T4510 t ≤ 20 370 — 230 — 11 10
2014A
T4511
T6
t ≤ 10 415 — 370 — 7 5
T6510
10 < t ≤ 40 450 — 400 — 6 4
T6511
b
O All — 245 — 125 — 16
2017 T4 A ≤ 70 000 345 — 215 — — 12
c
T42 70 000 < A ≤ 100 000 335 — 195 — — 12
© ISO 2014 – All rights reserved 9
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ISO 6362-2:2014(E)
Table 2 (continued)
a
Alloy Temper Dimensions Tensile 0,2 % proof Elongation
strength stress min.
R R
m p0,2
MPa MPa
A A
50mm
min. max. min. max.
% %
O
t ≤ 20 — 250 — 135 12 10
H111
2017A T4
t ≤ 10 380 — 260 — 12 10
T4510
10 < t ≤ 75 400 — 270 — 10 8
T4511
b
O All — 245 — 125 — 12
T3
T3510 t ≤ 30 420 — 290 — 8 6
T3511
t ≤ 6 390 — 295 — — 10
6 < t ≤ 19 410 — 305 — — 10
19 < t ≤ 38 450 — 315 — — 10
2024 T4
38 < t, A ≤ 16 000 480 — 335 — — 10
38 < t, 16 000 < A ≤ 20 000 470 — 315 — — 8
38 < t, 20 000 < A ≤ 30 000 460 — 315 — — 8
t ≤ 19 390 — 265 — — 12
19 < t ≤ 38 390 — 265 — — 10
c
T42
38 < t, A ≤ 16 000 390 — 265 — — 10
38 < t, 16 000 < A ≤ 20 000 390 — 265 — — 8
T8
T8510 t ≤ 30 455 — 380 — 5 4
T8511
T4
2030 T4510 t ≤ 25 370 — 250 — 8 6
T4511
3102 H112 All 80 — 30 — 25 23
3003,
H112 All 95 — 35 — — —
3203
H112 All 95 — 35 — 25 20
3103 O
All 95 135 35 — 25 20
H111
H112 All 100 — 40 — 18 16
5005,
O
5005A
t ≤ 20 100 150 40 — 20 18
H111
H112 t ≤ 30 250 — 110 — 14 12
5019 O
t ≤ 30 250 320 110 — 15 13
H111
5049 H112 All 180 — 80 — 15 13
10 © ISO 2014 – All rights reserved
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ISO 6362-2:2014(E)
Table 2 (continued)
a
Alloy Temper Dimensions Tensile 0,2 % proof Elongation
strength stress min.
R R
m p0,2
MPa MPa
A A
50mm
min. max. min. max.
% %
H112 All 150 — 60 — 16 14
5051A O
All 150 200 60 — 18 16
H111
H112 All 160 — 60 — 16 14
5251 O
All 160 220 60 — 17 15
H111
H112 All 175 — 70 — — —
5052
O All 175 245 70 — — 20
H112 All 205 — 75 — — —
5154
O All 205 285 75 — — —
H112 t ≤ 25 200 — 85 — 16 14
5154A O
t ≤ 25 200 275 85 — 18 16
H111
H112 t ≤ 130, A ≤ 20 000 215 — 85 — — 12
5454
O t ≤ 130, A ≤ 20 000 215 285 85 — — 14
H112 t ≤ 25 180 — 80 — 14 12
5754 O
t ≤ 25 180 250 80 — 17 15
H111
A ≤ 30 000 245 — 100 — — —
5056 H112 30 000 < A ≤ 70 000 225 — 80 — — —
70 000 < A ≤ 100 000 215 — 70 — — —
H112 A ≤ 20 000 275 — 110 — — 12
5083
O A ≤ 20 000 275 355 110 — — 14
H112 All 240 — 95 — 12 10
5086 O
All 240 320 95 — 18 15
H111
3 ≤ t ≤ 12 195 — 165 — — 10
e
6101 T6
12 < t ≤ 16 175 — 145 — — 14
e
6101A T6 t ≤ 25 200 — 170 — 10 8
e,f
T6 t ≤ 15 215 — 160 — 8 6
6101B
e,g
T7 t ≤ 15 170 — 120 — 12 10
6005, t ≤ 5 270 — 225 — 8 6
e
T6
6005A 5 < t ≤ 10 260 — 215 — 8 6
t ≤ 6 245 — 205 — — 8
T5
6005C 6 < t ≤ 12 225 — 175 — — 8
e
T6 t ≤ 6 265 — 235 — — 8
T4 t ≤ 10 180 — 90 — 15 13
6008 t ≤ 5 270 — 225 — 8 6
e
T6
5 < t ≤ 10 260 — 215 — 8 6
© ISO 2014 – All rights reserved 11
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ISO 6362-2:2014(E)
Table 2 (continued)
a
Alloy Temper Dimensions Tensile 0,2 % proof Elongation
strength stress min.
R R
m p0,2
MPa MPa
A A
50mm
min. max. min. max.
% %
e
T4 t ≤ 25 320 — 220 — 16 14
6110A
e
T6 t ≤ 25 380 — 360 — 10 8
e
T6
e
6012 T6510 t ≤ 30 310 — 260 — 8 6
e
T6511
e
T4 t ≤ 10 140 — 70 — 15 13
6014 t ≤ 5 250 — 200 — 8 6
e
T6
5 < t ≤ 10 225 — 180 — 8 6
e
T6
e
6018 T6510 t ≤ 30 310 — 260 — 8 6
e
T6511
O
t ≤ 25 — 160 — 110 14 12
H111
e
6351 T4 t ≤ 25 205 — 110 — 14 12
t ≤ 5 290 — 250 — 8 6
e
T6
5 < t ≤ 25 300 — 255 — 10 8
e
T4 t ≤ 15 120 — 60 — 16 14
T5 t ≤ 15 160 — 120 — 8 6
e
6060 T6 t ≤ 15 190 — 150 — 8 6
e
T64 t ≤ 15 180 — 120 — 12 10
e
T66 t ≤ 15 215 — 160 — 8 6
e
T4 t ≤ 15 110 — 50 — 16 14
T5 t ≤ 15 150 — 120 — 8 6
6360
e
T6 t ≤ 15 185 — 140 — 8 6
e
T66 t ≤ 15 195 — 150 — 8 6
O All — 145 — 110 — 16
e
T4 All 175 — 110 — — 16
c
6061 T42 All 175 — 85 — — 16
e
T6 t ≤ 6 265 — 245 — — 8
d
T62 6 < t 265 — 245 — — 10
O
t ≤ 10 — 170 — 120 14 12
H111
e
T4 t ≤ 10 180 — 100 — 14 12
6261 t ≤ 5 270 — 230 — 8 7
T5
5 < t ≤ 10 260 — 220 — 9 8
t ≤ 5 290 — 245 — 8 7
e
T6
5 < t ≤ 10 290 — 245 — 9 8
e
6262 T6 t ≤ 25 260 — 240 — 10 8
12 © ISO 2014 – All rights reserved
---------------------- Page: 16 ----------------------
ISO 6362-2:2014(E)
Table 2 (continued)
a
Alloy Temper Dimensions Tensile 0,2 % proof Elongation
strength stress min.
R R
m p0,2
MPa MPa
A A
50mm
min. max. min. max.
% %
O
t ≤ 25 — 130 — — 18 16
H111
t ≤ 12 120 — 60 — — 12
T1
12 < t ≤ 25 110 — 55 — — 12
t ≤ 10 130 — 65 — 14 12
e
6063 T4
10 < t ≤ 25 120 — 65 — 12 10
t ≤ 12 155 — 110 — — 8
T5
12 < t ≤ 25 145 — 110 — — 8
t ≤ 3 205 — 175 — — 8
e
T6
3 < t ≤ 25 205 — 175 — — 10
e
T66 t ≤ 25 245 — 200 — 10 8
O
t ≤ 25 — 150 — — 16 14
H111
t ≤ 10 150 — 90 — 12 10
e
6063A T4
10 < t ≤ 25 140 — 90 — 10 8
T5 t ≤ 25 200 — 160 — 7 5
e
T6 t ≤ 25 230 — 190 — 7 5
e
6463 T6 t ≤ 25 195 — 160 — 10 8
e
6081 T6 t ≤ 25 275 — 240 — 8 6
O
t ≤ 25 — 160 — 110 14 12
H111
e
6082 T4 t ≤ 25 205 — 110 — 14 12
t ≤ 5 290 — 250 — 8 6
e
T6
5 < t ≤ 25 310 — 260 — 10 8
≤ 12 285 — 245 — — 10
T5
12 < t ≤ 25 275 — 235 — — 10
7003
t ≤ 10 350 — 290 — 10 8
e
T6
10 < t ≤ 25 340 — 280 — 10 8
O 1,6 ≤ t ≤ 12 — 245 — 145 — 12
h
T4 1,6 ≤ t ≤ 12 315 — 195 — — 11
7204
1,6 ≤ t ≤ 6 325 — 235 — — 10
T6
6 < t ≤ 12 335 — 255 — -— 10
e
7005 T6 t ≤ 15 350 — 290 — 10 8
e
7108 T6 t ≤ 20 310 — 260 — 10 8
e
T6 t ≤ 20 310 260 12 10
7108A
e
T66 t ≤ 20 350 290 10 8
e
7020 T6 t ≤ 15 350 — 290 — 10 8
e
7021 T6 t ≤ 10 410 — 350 — 10 8
© ISO 2014 – All rights reserved 13
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ISO 6362-2:2014(E)
Table 2 (continued)
a
Alloy Temper Dimensions Tensile 0,2 % proof Elongation
strength stress min.
R R
m p0,2
MPa MPa
A A
50mm
min. max. min. max.
% %
e
T6
e
7022 T6510 t ≤ 30 490 — 420 — 7 5
e
T6511
T6
7049A T6510 t ≤ 30 610 — 530 — 5 4
T6511
T73511 t or D ≤ 125, A ≤ 20 000 485 — 415 — 7 8
7050 T74511 t ≤ 76 505 — 435 — — 7
T76510 t or D ≤ 127 545 — 475 — — 7
b
O All — 275 — 165 — 10
T6 t ≤ 6 540 — 480 — — 7
d
T62 6 < t ≤ 75 560 — 500 — — 7
t ≤ 5 540 — 485 — 8 6
T6510
7075 5 < t ≤ 10 560 — 505 — 7 5
T6511
10 < t ≤ 50 560 — 495 — 6 4
i
T73 t ≤ 5 470 — 400 — 7 5
i
T73510 5 < t ≤ 25 485 — 420 — 8 6
i
T73511 25 < t ≤ 50 475 — 405 — 8 —
a
t (mm) = wall thickness.
D (mm) = outside diameter.
2
A (mm ) = cross-section area.
b
The material of temper grade O shall be a basis for materials of temper grades T42 or T62. When requested by the pur-
chaser, the capability to achieve T42 and T62 properties after appropriate heat treatment is demonstrated.
c
The mechanical properties of temper grade T42 shall be applied only when 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 can be lower than the specified values.
d
The mechanical properties of temper grade T62 shall be applied only when 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 can be lower than the specified values.
e
Applicable for those after extrusion followed by controlled cooling at a rate rapid enough to hold constituents in solu-
tion.
f
Electrical conductivity γ ≥ 30 MS/m.
g
Electrical conductivity γ ≥ 32 MS/m.
h
The mechanical properties of temper grade T4 are the values specified, based on reference values obtained by 1 month
of natural ageing at room temperature (approximately 20 °C) after solution treatment.
In the case of the tensile test made before completion of 1 month of natural ageing, the tensile performance of temper
grade T4 can be deemed as guaranteed if the test result of the test piece which has been artificially aged after solution
treatment is confirmed to satisfy the tensile performance of temper grade T6.
i
For materials of thickness 20 mm or above, see EN 755–1, with respect to stress corrosion cracking resistance.
14 © ISO 2014 – All rights reserved
---------------------- Page: 18 ----------------------
ISO 6362-2:2014(E)
Table 3 — Mechanical properties of profiles
a
Alloy Temper Dimensions Tensile 0,2 % proof Elongation
strength stress min.
R R
m p0,2
MPa MPa
A A
50mm
min. max. min. max.
% %
1070 H112 All 55 — 15 — — —
1070A H112 All 60 20 25 23
1060 H112 3 ≤ t ≤ 30 60 — 30 — — 25
1050 H112 All 65 — 20 — — —
1050A H112 All 60 — 20 — 25 23
b
1350 H112 All 60 — — — 25 23
1100,
H112 All 75 — 20 — — —
1200
T4
2007 T4510 t ≤ 30 370 — 250 — 8 6
T4511
d
O All — 245 — 125 — 12
T4 All 345 — 245 — — 12
e
T42 All 345 — 205 — — 12
T4510 t ≤ 25 370 — 230 — 11 10
c
2014
T4511 25 < t ≤ 75 410 — 270 — 10 —
t ≤ 15 415 — 365 — 6 7
15 < t ≤ 30 440 — 400 — 6 7
30 < t, A ≤ 16 000 470 — 410 — 5 7
T6
30 < t, 16 000 < A ≤ 20 000 470 — 400 — 5 6
30 < t, 20 000 < A ≤
...
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