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Brief Introduction

The Aluminum Association established the alloy description system in 1954. When the system was first implemented, it listed 75 chemical compositions — today, there are more than 530 registered active chemical elements, and this number continues to grow.

The aluminum series names elements with four numerical digits where the first digit represents the principal alloying element, the second digit indicates a modification of a specific alloy, and the third and fourth digits are arbitrary numbers assigned to specific alloys in the series.

Ingots A5/A7/A8

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Tubes

Plates & Laminates

Coils

Profile


1xxx – 99.00 Minimum Aluminum

It’s impossible for aluminum to be 100% pure, but aluminum in this wrought series category contains at least 99% aluminum. For all intents and purposes, 1xxx alloys are considered pure aluminum. Notably, this alloy is the exception to the wrought series naming rule — in 1xxx alloy names, the last two digits stand for the minimum percentage of aluminum above 99. For example, Alloy 1350 consists of at least 99.50% aluminum.

Pure aluminum has great corrosion resistance and workability, plus high electrical and thermal conductivity. For this reason, this alloy is often used for electrical and chemical applications. Pure aluminum is not very strong and is seldom used for structural applications, but strain hardening can moderately increase material strength.

Lega Si Fe Cu Mn Mg Cr Zn V Ti Bi Ga Pb Zr Altro Cad Altro Tot. Altri min.
1050 0,25 0,4 0,05 0,05 0,05 / 0,07 / 0,05 / / / / 0,03 / 99,5
1060 0,25 0,35 0,05 0,03 0,03 0,03 0,05 0,05 0,03 0,03 0,03 0,03 0,03 0,03 / 99,6
1070 0,2 0,25 0,03 0,03 0,03 / 0,07 / 0,03 / / / / 0,03 / 99,7
1080 0,15 0,15 0,03 0,02 0,02 / 0,06 / 0,02 / / / / 0,2 / 99,8
1100 0,95 / 0,05 0,05 / / 0,1 / / / / / / 0,05 0,15 99
Si+Fe 0,2
1200 1 / 0,05 0,05 / / 0,1 / / / / / / 0,05 0,15 99
Si+Fe
1250 0,2 0,4 0,1 0,01 0,01 0,01 0,05 / / / / / / 0,03 / 99,5
1350 0,1 0,4 0,05 0,01 / 0,01 0,05 / / / / / / 0,03 0,1 99,5


2xxx – Copper

This wrought series alloy offers high strength and performance over a wide range of temperatures and is regularly used in aerospace applications. One well-known aircraft aluminum alloy is Alloy 2024. However, some copper aluminum alloys are susceptible to heat and stress corrosion cracking and are considered non-weldable, whereas other 2xxx alloys can be welded using the right methods. 2xxx decreases the elongation and tensile strength of aluminum and doesn’t offer as good corrosion resistance as other alloys in the wrought series.

Lega Si Fe Cu Mn Mg Cr Zn V Ti Bi Ga Pb Zr Altro Cad Altro Tot. Altri min.
2007 0,8 0,8 3,3 0,5 0,4 0,1 / 0,2 0,2 0,2 / 0,8 / 0,1 0,3 /
4,6 1 1,8 Sn 1,5
2011 0,4 0,7 5 / / / 0,3 / / 0,2 / 0,2 / 0,05 0,15 /
6 0,6 0,4
2014 0,2 0,7 3,9 0,4 0,2 0,1 0,25 / 0,15 / / / / 0,05 0,15 /
1,2 5 1,2 0,8
2017A 0,2 0,7 3,5 0,4 0,1 1 0,25 / / / / / / 0,05 0,15 /
0,8 4,5 1
2017B 0,8 0 2,2 0,2 0,2 0,1 0,25 / / / / / / 0,05 0,15 /
3 0,5
2618 0,15 0,9 1,8 0,25 1,2 / 0,1 / 0,2 / / / / 0,05 0,15 /
0,25 1,4 2,7 1,8
2219 0,2 0,3 5,8 0,2 0,02 / 0,1 0,05 0,02 / / / / 0,05 0,15 /
6,8 0,4 0,2 0,1
2024 0,5 0,5 3,8 0,3 1,2 0,1 0,25 / 0,15 / / / / 0,05 0,15 /
4,9 0,9 1,8
2030 0,8 0,7 6,5 0,2 0,5 0,1 0,5 / 0,2 0,2 / 0,8 / 0,05 0,15 /
4,5 1 1,3 1,5

3xxx — Manganese

3xxx aluminum alloys were first used only in pots and pans, but are now widely used in heat exchanger components for vehicles and power plants. With good temperature stability and corrosion resistance, alloys in this category are suitable for use in extreme conditions. 3xxx also allows for good formability and workability. 3003 is a popular manganese alloy used for moderate strength applications that require complex shapes.

Lega Si Fe Cu Mn Mg Cr Zn V Ti Bi Ga Pb Zr Altro Cad Altro Tot. Altri min.
3003 0,6 0,7 0,05 1 / / 0,1 / / / / / / 0,05 0,15 /
0,2 1,5
3103 0,5 0,7 0,1 0,9 0,3 0,1 0,2 / / / / / / 0,05 0,15 /
1,5
3004 0,3 0,7 0,25 1 0,8 / 0,2 / / / / / / 0,05 0,15 /
1,5 1,3
3104 0,6 0,8 0,05 0,8 0,8 / 0,25 0,1 0,1 / / / / 0,05 0,15 /
0,25 1,4 1,3
3005 0,6 0,7 0,6 1 0,2 0,25 0,3 / 0,1 / / / / 0,05 0,15 /
1,5
3105 0,6 0,7 0,3 0,3 0,2 0,2 0,4 / 0,1 / / / / 0,05 0,15 /
0,8 0,8

4xxx — Silicon

Silicon reduces aluminum’s melting point and improves its fluidity when molten. For this reason, 4xxx alloys are often used in fusion welding wire and as brazing alloys. Silicon on its own is non-heat-treatable, but a number of 4xxx alloys respond well to heat treatments thanks to added copper or magnesium.

5xxx — Magnesium
 

Aluminum alloys in this category are easily weldable and widely used for applications in shipbuilding, transportation, bridge building, and construction. 5xxx alloys offer good corrosion resistance in marine environments and have the highest strength of all non-heat-treatable alloys. However, 5xxx alloys with more than 3 to 3.5% magnesium are not recommended for elevated temperature service above 65.6°C (150°F) due to the possibility of stress corrosion cracking.

Lega Si Fe Cu Mn Mg Cr Zn V Ti Bi Ga Pb Zr Altro Cad Altro Tot. Altri min.
5005 0,3 0,7 0,2 0,2 0,5 0,1 0,25 / / / / / / 0,05 0,15 /
1,1
5050 0,4 0,7 0,2 0,1 1,1 0,1 0,25 / / / / / / 0,05 0,15 /
1,8
5150 0,08 0,1 0,1 0,03 1,3 / 0,1 / 0,06 / / / / 0,03 0,1 /
1,7
5251 0,4 0,5 0,15 0,1 1,7 0,15 0,15 / 0,15 / / / / 0,05 0,15 /
0,5 1,4
5052 0,25 0,4 0,1 0,1 2,2 0,15 0,1 / / / / / / 0,05 0,15 /
2,8 0,35
5154A 0,5 0,5 0,1 0,1 3,1 0,25 0,2 / 0,2 / / / / 0,05 0,15 /
0,5 3,9
5154B 0,35 0,45 0,05 0,15 3,2 0,1 0,15 / 0,15 / / / / 0,05 0,15 /
0,45 3,8
5454 0,25 0,4 0,1 0,5 2,4 0,05 0,25 / 0,2 / / / / 0,05 0,15 /
1 3 0,2
5754 0,4 4 0,1 0,5 2,6 0,3 0,2 / 0,15 / / / / 0,05 0,15 /
3,6
5056 0,3 0,4 0,1 0,05 4,5 / 0,1 / / / / / / 0,05 0,15 /
0,24 5,6
5456 0,25 0,4 0,1 0,5 4,7 0,05 0,25 / 0,2 / / / / 0,05 0,15 /
1 5,5 0,2
5556 0,25 0,4 0,1 0,5 4,7 0,05 0,25 / 0,05 / / / / 0,05 0,15 /
5,5 0,2 0,2
5182 0,2 0,35 0,15 0,2 4 0,1 0,25 / 0,1 / / / / 0,05 0,15 /
0,5 5
5083 0,4 4 0,1 0,4 4 0,25 0,25 / 0,15 / / / / 0,05 0,15 /
1 4,9 0,25
5086 0,4 0,5 0,1 0,2 3,5 0,05 0,25 / 0,15 / / / / 0,05 0,15 /
0,7 4,5 0,25

6xxx — Magnesium and Silicon
 

6xxx alloys usually consist of around 1.0% magnesium and silicon each, which produces magnesium-silicide. Magnesium-silicide can support solution heat treatments that improve strength, formability, and corrosion resistance. This wrought series number is used throughout the welding fabrication industry, primarily incorporated into structural components and extrusions.

These alloys are sensitive to solidification cracks, which means they should not be welded without filler materials — oftentimes, 6xxx is welded with 4xxx or 5xxx filler materials to increase weldability. A major magnesium-silicide alloy is 6061, which is one of the most versatile heat treatable aluminum alloys.

Lega Si Fe Cu Mn Mg Cr Zn V Ti Bi Ga Pb Zr Altro Cad Altro Tot. Altri min.
6101 0,3 0,5 0,1 0,03 0,35 0,03 0,1 / / / / / / 0,03 0,1 /
0,7 0,8
6005 0,5 0,35 0,3 0,5 0,4 0,3 0,2 / 0,1 / / / / 0,05 0,15 /
0,9 0,7
6105 0,6 0,35 0,1 0,1 0,45 0,1 0,1 / 0,1 / / / / 0,05 0,15 /
1 0,8
6060 0,3 0,1 0,1 0,1 0,35 0,05 0,15 / 0,1 / / / / 0,05 0,15 /
0,6 0,3 0,6
6012 0,6 0,5 0,1 0,4 0,6 0,3 0,3 / 0,2 0,7 / 0,4 / 0,05 0,15 /
1,4 1 1,2 2
6026 0,6 0,7 0,2 0,2 0,6 0,3 0,3 / 0,2 0,5 / 0,4 / 0,05 0,15 /
1,4 0,5 1 1,2 1,5
6061 0,4 0,7 0,15 0,15 0,8 0,04 0,25 / 0,15 / / / / 0,05 0,15 /
0,8 0,4 1,2 0,35
6282 0,4 0,7 0,15 0,15 0,8 0,04 0,25 / 0,15 0,4 / 0,4 / 0,05 0,15 /
0,8 0,4 1,2 0,14 0,7 0,7
6063 0,2 0,35 0,1 0,1 0,45 0,1 0,1 / 0,1 / / / / 0,05 0,15 /
0,6 0,9
6763 0,2 0,08 0,04 0,03 0,45 / 0,03 / / / / / / 0,03 0,1 /
0,6 0,16 0,9
6082 0,7 0,5 0,1 0,4 0,6 0,25 0,2 / 0,1 / / / / 0,05 0,15 /
1,3 1 1,2

7xxx — Zinc

This wrought series number contains some of the highest strength aluminum alloys that are best-suited for high-performance applications in competitive sporting equipment or the aircraft and aerospace industries. Zinc additions range from 0.8 to 12% in 7xxx alloys and can be coupled with smaller percentages of magnesium, copper, and chromium for heat treatability.

Like 2xxx, 7xxx contains alloys both suitable and non-suitable for welding — one commonly welded alloy is 7005, which is primarily used with 5xxx alloy fillers. One of the highest-strength aluminum alloys available is 7075, which is often used in air-frame structures and for other high-stress applications.

It’s important to note which aluminum alloys are heat treatable and which are non-heat-treatable. This will help product teams determine appropriate applications for specific aluminum alloys, and protect components from high temperatures when necessary.

  • 2xxx, 6xxx, and 7xxx series alloys are heat treatable.
  • 1xxx, 3xxx, and 5xxx series wrought aluminum alloys are non-heat-treatable and only allow for strain hardening.
  • 4xxx series contains some heat-treatable alloys, but mostly non-heat-treatable alloys. However, most 4xxx non-heat-treatable alloys can respond to heat treatments when mixed with other heat-treatable alloys.
Lega Si Fe Cu Mn Mg Cr Zn V Ti Bi Ga Pb Zr Altro Cad Altro Tot. Altri min.
7003 0,3 0,35 0,2 0,3 0,5 0,2 5 / 0,2 / / / / 0,5 0,15 /
1 6,5
7010 0,12 0,15 1,5 0,1 2,1 0,05 5,7 / / / / / / 0,5 0,15 /
2 2,6 6,7
7012 0,15 0,25 0,8 0,08 1,8 0,04 5,8 / 0,04 / / / / 0,5 0,15 /
1,2 0,15 1,2 6,5 0,08
7017 0,35 0,45 0,2 0,05 2 0,35 4 / 0,15 / / / / 0,5 0,15 /
0,5 3 5,2
7020 0,35 0,4 0,2 0,05 1 0,1 4 / / / / / / 0,5 0,15 /
0,5 1,4 0,35 5
7075 0,4 0,5 1,2 0,3 2,1 0,18 5,1 / 0,2 / / / / 0,5 0,15 /
2 2,9 0,28 6,1
7079 0,3 0,4 0,4 0,1 2,9 0,1 3,8 / 0,1 / / / / 0,5 0,15 /
0,8 0,2 3,7 0,25 4,8

Understanding Aluminum Alloys and Tempers

Tempers indicate whether an aluminum alloy has undergone any processing to increase mechanical properties like tensile strength, hardness, or heat resistance. Tempers are shown in the wrought aluminum series as a tagged-on letter after an alloy number, e.g. 3003-H.

Strained-Hardened Tempers (-H)
 

The addition of an “-H” after alloys 1xxx, 3xxx, 5xxx, and sometimes 4xxx indicates that the alloy has been strained-hardened since they cannot be heat treated. The number immediately following the H indicates its processing:

  • H1 — Strain-hardened
  • H2 — Strain-hardened and partially annealed
  • H3 — Strain-hardened and stabilized
  • H4 — Strain-hardened and lacquered or painted

Strained hardened aluminum alloys are followed by two numbers, where the second number indicates a scale designation ranging from 0 (fully annealed, softest) to 8 (hardest). For example, Aluminum 5052-H32 has been strained-hardened plus stabilized and is relatively soft.

Thermal and Heat-Treated Tempers (-T)

The addition of a “-T” after alloys 2xxx, 6xxx, 7xxx, and some 4xxx indicates that the alloy has been heat-treated, rapidly cooled or quenched, or precipitation hardened. The number following the T indicates which thermal process it has undergone.

  • T1 — Cooled from an elevated temperature and naturally aged
  • T2 — Cooled from an elevated temperature, cold-worked, and naturally aged
  • T3 — Solution heat-treated, cold-worked, and naturally aged
  • T4 — Solution heat-treated and naturally aged
  • T5 — Cooled from an elevated temperature and artificially aged
  • T6 — Solution heat-treated and artificially aged
  • T7 — Solution heat-treated and stabilized
  • T8 — Solution heat-treated, cold-worked, and artificially aged
  • T9 — Solution heat-treated, artificially aged, and cold-worked
  • T10 — Cooled from elevated temperature, cold-worked, and artificially aged

Precipitation hardened or heat-treated alloys sometimes contain an additional digit, which indicates specific end properties such as stress relief by stretch (-T51) or compression (-T52).


Global aluminum alloy grade cross-reference chart

 
 

EN USA China UK Japan France Germany India Russia ISO
EN AW-1050A/Al99.5 1050A(L3) A1050 19500 A99.5
EN AW-1060/ 1060(L2) A1060 19600 A6 A99.6
A99.6
1070 A1070 19700 A7
EN AW-1070A/ 1070A A99.7
Al99.7
EN AW-1100/ 1100(L5-1) 1100/AIN00 A99.0CU
A99.0CU
EN AW-1200/ 1200(L5) A1200 19000 A0 99
Al99.0
EN AW-1350/ 1350 A5E E-Al99.5
E-Al99.5
EN AW-1370/ 1370 E-Al99.7
E-AI99.7
1A30(L4-1) AlN30 A99.3
EN AW-1050A/ 1050 1A50(LB2) 1050(1B) 1050 1050A A199.50 A5
Al99.5
1A80 1080(1A) A1080 1080A A199.90
EN AW-1080A/ 1A80A 19800 A8 99.8(A)
Al99.8(A)
EN AW-1085/ 1A85(LG1) A1085 485
Al99.85
EN AW-1090/ 1A90(LG2) AIN90
A99.90
1A95 A95
1A97(LG4) A199.98R A97
1199 1A99 A199.99R
EN AW-1199/ 1A999(LG5) AIN99 A99
A99.99
EN AW-11098/
Al99.98
A85
EN AW-1350/
Al99.5(A)
EN USA China UK Japan France Germany India Russia ISO
2036 2A01(LY1) A2117 2117 AlCu2.5Mg0.5 22500 д18n/1180 AlCu2.5Mg
2A02(LY2) Bд17/1170
2A06(LY6) д19/1190
2A80 2N01
2A10(LY11) B65/1165
2A11(LY11) HF15 A2017 2017S AlCuMg1 24534 д1/1110 Al Cu4MgSi
2B11(LY8) A2017A д1n/1111 AlCu5MgSi(A)
EN AW-2024/ 2124 2A12(LY12) A2024 2024 AlCuMg2 24530 д16/1160 AlCu4MgSi1
AlCu4Mg1
2B12(LY9) A2024 д16/1160
EN AW-2014/ 2014 2A14(LD10) A2014 AlCuSiMn 24345 AK8/1380 AlCu4MgSi
AICu4Mg
EN AW-2019/ 2A16(LY16) A2219 д20/1201 AlCu6Mn
AlCu6Mn
2319 2B16(LY16-1) ~A2219 ~д20/1201 ~AlCu6Mn
2A17(LY17) 1210
EN AW-2319/ 2A20(LY20) A2319 ~CB-1201
AlCu6Mn(A)
2A21(214) A2018
2A70(LD7) A2618 AK4-1/1141
2A80(LD8) A2NO1 AK4/1140
AK2 2218 2A90(LD9) A2018 AK2/1120
EN AW-2011/ 2011 A2011 ~1д/1110 AlCu6BiPb
AICu6BiPb
EN AW-2014/ 2014 42014 24345 AK8/1380 AlCu4SiMg
AlCu4SiMg
EN AW-2014/ 2014A A2014A AlCu4SiMg(A)
AlCu4SiMq(A)
2017 42017 д1/1110 AlCu4MgSi
EN AW-2017A/ 2017A A2017A 24534 AK21/1120 AlCu4MgSi(A)
AlCu4MgSi(A)
EN AW-2024/ 2024 42024 24530 д16/1160 AlCu4Mg1
AlCu4Mg1
EN AW-2124/ 2124 д16n/1161
AlCu4Mg1(A)
EN AW-2117/ 2117 A2117 AlCu2.5Mg
AlCu2.5Mg
EN AW-2214/ 2214 ~AK8/1380
AlCu4SiMg(B)
2218 A2218
EN AW-2219/ 2219(LY19.147) 42219 д20/1201 AlCu6Mn
AlCu6Mn
2618 A2618 AK4-1/1141
EN AW-2001/
AlCu5.5MgMn
EN AW-2007/
AlCu4PbMgMn
EN AW-2030/ A2030
AlCu4PbMg
EN AW-2031/ 22588 AK4/1140
AlCu2.5NIiMg
EN AW-2618/ A2618
AlCu2Mg1.5Ni
EN USA China UK Japan France Germany India Russia ISO
EN AW-3003/ 3421(LF21) A3003 AMu/1400 AlMn1Cu
AlMn1Cu
EN AW-3003/ 3003 A3003 31000 AMu/1400 AlMn1Cu
AlMn1Cu
EN AW-3004/ 3004 A3004 31500 AMu2/1511 AlMn1Mg1
AIMn1Mg1
EN AW-3005/ 3o05 A3005 MM/1403 AlMn1Mg1.5
AlMn1Mg0.5
EN AW-3103/ 3103 A3103 31000 AlMn1
AlMn1
EN AW-3105/ 3105 A3105 AlMn0.5Mg0.5
AIMn0.5Mg0.5
EN AW-3017/
AlMg1Cu0.3
EN AW-3102/
AlMn0.2
EN AW-3104/ A3104
AlMn1Mg1Cu
EN AW-3207/
AlMn0.6
EN USA China UK Japan France Germany India Russia ISO
EN AW-4043A/ 4A01(LT1) A4043 43000 AlSi5
AISi5(A)
EN AW-4032/ 4A11(LD11) A4032
AISi2.5MgCuNi
EN AW-4343/ 4A13(LT13) BA4343
AlSi7.5
EN AW-4047A/ 4A17(LT17) A4047 46000 AlSi12
AISi12(A)
EN AW-4004/ 4004 BA4004
AlSi10Mg1.5
EN AW-4032/ 4032 44032
AISi2.5MgCuNi
4043 44043 AlSi5
EN AW-4043A/ 40434 AlSi5(A)
AlSi5(A)
4047 A4047 AlSi12
EN AW-4047A/ 4047A AISi12(A)
AlSi12(A)
EN AW-4006A/
AlSi1Fe
EN AW-4007/
AISi1.5Mn
EN AW-4014/
AlSi2
EN AW-4015/
AlSi2Mn
EN AW-4045/ 44045
AlSi10
EN AW-4046/
AlSi10Mg
EN AW-4104/ A4104
AISi10MgBi
EN USA China UK Japan France Germany India Russia ISO
EN AW-5052/AlMn2.5 5052 5A02(LF2) NS4 A5052 5052 A1Mg2.5 AMr2/1520 AlMg2.5
EN AW-5154/ 5A03(LF3) NS5 A5154 AMr3/1530 AlMg3.5
AlMn3.5(A)
~EN AW-5019/ 5056 5A05(LF5) NB6 A5056 A1Mg5 ~AMr5/1550 AlMg5Mn1
AIMg5
5B05(LF10) A5056 55000 AMr5n/1551 AlMg5Cr
5A06(LF6) AMr6/1560
EN AW-5556A/ 5456 5A30(LF16, 2103) NG61 5556 5957 55380
AIMgMn
EN AW-5051A/ 5A66(LT66(LT66)
AlMg2(B)
EN AW-5005/ 5005 A.5005 51000-A AMr1/1510 AlMg1(B)
AIMg1(B)
EN AW-5019/ 5019 AMr5/1550
AlMg5
EN AW-5050/ 5050 AlMg1.5(C)
AlMg1.5©
EN AW-5052/ 5052 A5052 AMr2/1520 AlMg2.5
AlMg2.5
EN AW-5056A/ 5056(LF5-1) A45056 AMr5/1550 AlMg5Cr
AlMg5
EN AW-5082/ 5082 A5082
AlMg4.5
EN AW-5083/ 5083(LF4) A5083 54300 AlMg4.5Mn0.7
AlMg4.5Mn0.7
EN AW-5086/ 5086 45086 AMr4/1540 AlMg4
AlMg4
5154 A5154 AMr3/1530 AlMg3.5
EN AW-5154A/ 5154A 53000 AlMg3.5(A)
AIMg3.5(A)
EN AW-5182/ 5182 A5182
AIMg4.5Mn0.4
EN AW-5183/ 5183 AlMr4.5
AlMg4.5Mn0.7
EN AW-5251/ 5251 52000 AMr2/1520 AlMg2
AlMg2
EN AW-5356/ 5356 45356 AlMg5Cr(A)
AlMgCr(A)
EN AW-5454/ 5454 A5454 AlMg3Mn
AIMg3Mn
~EN AW-5456A/ 5456 ~AMr5/1550 AlMg5Mn1
AlMg5Mn1
EN AW-5554/ 5554 45554 AlMg3Mn(A)
AlMg3Mn(A)
EN AW-5754/ 5754 AMr3/1530 AlMg3
AIMg3
EN AW-5556A/ 55380
AlMg5Mn
EN AW-5654/ A5654
AlMg3.5Cr
EN USA China UK Japan France Germany India Russia ISO
6A02(LD2) A6165 AB/1340
6B02(LD2-1) A6151
EN AW-6005/AISiMg 6005 AlSiMg
EN AW-6005/AISiMg(A) 6005A AlSiMg(A)
EN AW-6082/AISiMgMn 6082 64430 Aд35/1350 AlSiMgMn
EN AW-6181/AISi1Mg0.8 6181 AISi1Mg0.8
EN AW-6351/AlSiMg0.5Mn 6351 AB/1340 AlSiMg0.5Mn
EN AW-6060/AlMgSi 6060 AlSiMg
EN AW-6061/AlMg1SiCu 6061(LD30) A6061 65032 Aд33/1330 AlSi1MgCu
ENAW-6063/AlMg0.7Si 6063(LD31) A6063 63400 Aд31/1310 AlMg0.7Si
EN AW-6063A/AlMg0.7Si(A) 6063A AlMg0.7Si(A)
EN AW-6101A/E-AlMgSi 6101 A6101 E-AlMgSi
EN AW-6101A/E-AlMgSi(A) 6101A E-AlMgSi(A)
EN AW-6102A/E-AIMgSiPb
EN AW-6081/AlSi0.9MgMn
EN AW-6262/AIMg1SiPb AlMg1SiPb
EN AW-6401/Al99.9MgSi
EN AW-6463/AlMg0.7Si(B)
EN USA China UK Japan France Germany India Russia ISO
EN AW-7072/ 7A01(LB1) A7072 Aц1
AlZn1
EN AW-7010/ 7A03(LC3) B94/1950
AlZn6MgCu
EN AW-7005/ 7A05(705) A7N01 74530 AдM AlZn4.5Mg1.5Mn
AlZn4.5Mg1.5M
EN AW-7075/ 7175 7A09(LC9) A7075 7075 AlZnMgCu1.5 76528 B95/1950 Azn5.5MgCu
AlZn5.5MgCu
7A10(LC10)
7A52(LC52.5210) 1925
EN AW-7003/ 7003(LC12) A7003
AlZn6Mg0.8Zr
EN AW-7005/ 7005 A7N01 74530 Alzn4.5Mg1.5Mn
AlZn4.5Mg1.5M
EN AW-7010/ 7010 Alzn6MgCu
AlZn6MgCu
EN AW-7020/ 7020 ≈1925c AlZn4.5Mg1
AlZn4.5Mg1
EN AW-7022/ 7022
AlZn5Mg3Cu
EN AW-7050/ 7050 47050 Alzn6CuMgzr
AlZn6CuMgZr
EN AW-7075/ 7075 A7075 76528 B95/1950 Alzn5.5MgCu
AlZn5.5MgCu
EN AW-7075/ 7475 Alzn5.5MgCu(A)
AlZn5.5MgCu
EN AW-7012/
AlZn6Mg2Cu
EN AW-7049A/ Alzn8MgCu
AlZn8MgCu
EN AW-7178/ Alzn7MgCu
AlZn7MgCu

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