Technical Specification

TEMPER DESIGNATION TABLE
India or UK USA or Canada ISO Temper Description of Designation
O O O Annealed
M F F As fabricated, as manufactured or as cast
- T3 TD Solution heat-treated, and cold worked
W T4 TB Solution heat-treated, naturally aged and amenable to artificial agenig
P T5 TE Artificially aged or precipetation heat-treated
WP T6 TF Solution heat-treated and precipetation heat-treated
H-21 H-1 H-2A H1 Strain hardened to specified strength
H-22 H-32 H-2B H3B 1/4 Hard Stabilized
H-24 H-34 H-2D H3D 1/2 Hard Stabilized
H-26 H-36 H-2F H3F 3/4 Hard Stabilized
H-28 H-38 H-2H H3H Fully Hard, Stabilized

INDIA

U.S.A.
(A.A)
BRITAIN
(B.S.)
CANADA GERMANY
(DIN)
RUSSIA I.S.O FRENCH
ND
NEW I.S. OLD I.S.
Series Main Alloy Effect on Alloying Elements
1000 Non (99% Alum.) Unalloyed aluminuim is highly corrosain resistant, low stregth, Workable, Conductive, Non-heat-treatable.
19501 1E 1050(E.C.) 1E C 15 E-Al 99.5 - - -
19500 1B 1050 1B 1S A-99.5 - Al-99.5 1050A
19600 - 1060 - - - - - -
19700 - 1070 - - Al-99.7 - Al-99.7 -
19800 1A 1080 1A - - - Al-99.8 -
19000 1C 1100 1C 2S Al-99.0 AD Al-99.0 1200
Series Main Alloy Effect on Alloying Elements
2000 Copper Based Goves Strength, hardness, machinability, Heat-treatable
- - 2011 FC1 28S Al-Cu-Bi-Pb - Al-Cu-6 Bi Pb 2011
24345 H15 2014 H15 B26S Al-Cu-Si AK - -
24534 H14 2017 H14 17S/16S - D1 Al-Cu-4Mg Si -
- - 2024 - 24S Al-Cu-Mg.2 - Al-Cu-4Mg 1 2024
Series Main Alloy Effect on Alloying Elements
3000 Manganese Based Adds moderate strength, good workability, non-heat-teatable
31000 N3 3003 N3 3S Al-Mn A-Mn Al-Mn 1 3003
Series Main Alloy Effect on Alloying Elements
4000
43000 N21 4043 N21 33S Al-Si-5 AK Al-SI5 4043
46000 N2 4047 N2 35S - - - -
Series Main Alloy Effect on Alloying Elements
5000 Magnesium Based Moderate to high strength, Corrosion resistant, Non-heat-treatable
51000 - 5005 - B57S - - Al-Mg-1 -
52000 N4 5052 N4 M57S Al-Mg.2 A-Mg Al-Mg-2.5 5051
53000 N5 5086 N5 54S - A.Mg-3 Al-Mg-4 -
54300 N8 5083 N8 D54S Al-Mg-4.5 Mn - Al-Mg-4.5 Mn 5083
55000 N6 5056 N6 A56S Al-Mg.5 - Al-Mg.5 5356
Series Main Alloy Effect on Alloying Elements
6000 Magnesium & Silicon Based Increase strength, formability, corrosion resistant, Heat-Treatable
65032 H20 6061 H20 65S Al-Mg-Si Cu - Al-Mg-1Si Cu -
63400 H9 6063 H9 50S Al-Mg-s- 0.5 - Al-Mg-Si -
64430 H30 6351 H30 B51S Al-Mg-Si 1 AV Al-Si-1 Mg 6081
64423 H11 6066 H11 C62S - - - -
62400 - 6005 - C51S - - - -
63401 91E 6101 91E D50S E.Al.Mg.Si 0.5 - - -
64401 - 6201 - - - - - -
Series Main Alloy Effect on Alloying Elements
7000 Zinc Based For Greatest strength, Heat-Treatable
74530 - 7039 - D74S Al-Zn-Mg. 1 - - 3004
76528 H17 7075 DTD
5124
75S Al-Zn-Mg Cu 1.5 - Al-Zn 6 Mg Cu 7075

Aluminium Alloy: Chemical Composition Limits (Percent)

Alloy (ISS) Equivalent alloy (AA) Copper Magnesium Silicon Iron Manganese Other (Total) Remarks
Old New USA Min. Max. Min. Max. Min. Max. Max. Min. Max. Ma.
1 C 19000 1100 - 0.10 - - - 0.5 0.6 - 0.1 0.1 Aluminium 99.0 % Min
1200 - 0.05 - - Si + Fe 1, 0 - 0.05 0.1 Aluminium 99.0 % Min
1 B 19500 1050 - 0.05 - - - 0.25 0.4 - 0.05 0.1 Aluminium 99.5 % Min
1 E 19501 - - 0.04 - - - 0.15 0.35 - 0.03 0.1 Aluminium 99.5 % Min
- 1350 - 0.05 - - - 0.10 0.40 - 0.01 0.1 Aluminium 99.5 % Min
19600 1060 - 0.05 - - - 0.25 0.35 - 0.03 0.1 Aluminium 99.6 % Min
19700 1070 - 0.03 - - - 0.20 0.25 - 0.03 0.1 Aluminium 99.7 % Min
H15 24345 2014 3.8 5.0 0.2 0.8 0.5 1.20 1.7 0.3 1.2 0.5 -
H4 24534 2017 3.5 4.7 0.4 1.2 0.2 0.7 0.7 0.4 1.2 0.5 -
N3 31000 3003 - 0.1 - 0.1 - 0.6 0.7 1.0 1.5 0.4 -
N21 43000 4043 - 0.1 - 0.2 4.5 6.0 0.6 - 0.5 0.2 -
N2 46000 4047 - 0.1 - 0.2 10.0 13.0 0.6 - 0.5 0.2 -
N4 52000 5052 - 0.1 1.7 2.6 - 0.6 0.5 - 0.5 0.4 Cr + Mn = 0.5 %
N5 53000 5086 - 0.1 2.8 4.0 - 0.6 0.5 - 0.5 0.4 Cr + Mn = 0.5 %
N6 55000 5056 - 0.1 4.5 5.6 - 0.6 0.7 - 0.5 0.4 Cromium upto 0.25 %
N8 54300 5083 - 0.1 4.0 4.9 - 0.4 0.7 0.5 1.0 0.4 Cromium upto 0.25 %
H20 65032 - 0.15 0.4 0.7 1.2 0.4 0.8 0.7 0.2 0.8 0.4 **Cr = 0.15 - 0.35 %
- - 6061 0.15 0.4 0.8 1.2 0.4 0.8 0.7 - 0.15 0.4 Chromium 0.04 - 0.35 %
H9 63400 6063 - 0.1 0.4 0.9 0.3 0.7 0.6 - 0.3 0.4 -
- - 6066 0.7 1.2 0.8 1.4 0.9 1.8 0.7 0.6 1.1 0.4 -
- 64423 - 0.5 1.0 0.5 1.3 0.7 1.3 0.8 - 1.0 - -
91E 63401 6101 - 0.05 0.4 0.9 0.3 0.7 0.5 - 0.03 0.1 -
- 64401 6201 - 0.1 0.6 0.9 0.5 0.9 0.5 - 0.03 0.1 -
H30 64430 6351 - 0.1 0.4 1.2 0.6 1.3 0.6 0.4 1.0 0.3 -
- - 6082 - 0.1 0.6 1.2 0.7 1.3 0.5 0.4 1.0 0.3 Chromium upto 0.25 %
- 74530 7039 - 0.2 1.0 1.5 - 0.4 0.7 0.2 0.7 0.4 Zinc 4.0 - 5.0 %
H17 76528 7075 1.2 2.0 2.1 2.9 - 0.5 0.5 - 0.3 0.2 Zinc 5.1 - 6.1 %
- - - - - - - - - - - - - Chromium 0.18 - 0.28 %

* Titanium and/or other grain refining elements
** Either Mn or Cr shall be present