SAE 6063 Aluminium Alloys

Material group: Nonferrous Alloys / Aluminium Alloys
Country / Standard: United States / SAE
Indicative price:

Data updates

Latest Update: 2023-05
Total number of updates: 9
Update History

This material has 463 properties — only a subset is shown here.

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SAE 6063 Chemical Composition

CRITERIA
VALUE
UNIT
CAS NUMBER
CRITERIA
Al
VALUE
Remainder
UNIT
%
CAS NUMBER
7429-90-5
CRITERIA
Cr
VALUE
≤ 0.1
UNIT
%
CAS NUMBER
7440-47-3
CRITERIA
Cu
VALUE
≤ 0.1
UNIT
%
CAS NUMBER
7440-50-8
CRITERIA
Fe
VALUE
val1
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UNIT
%
CAS NUMBER
7439-89-6
CRITERIA
Mg
VALUE
val1
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UNIT
%
CAS NUMBER
7439-95-4
CRITERIA
Mn
VALUE
val1
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UNIT
%
CAS NUMBER
7439-96-5
CRITERIA
Other each
VALUE
val1
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UNIT
%
CAS NUMBER
CRITERIA
Other total
VALUE
val1
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UNIT
%
CAS NUMBER
CRITERIA
Si
VALUE
val1
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UNIT
%
CAS NUMBER
7440-21-3
CRITERIA
Ti
VALUE
val1
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UNIT
%
CAS NUMBER
7440-32-6
CRITERIA
Zn
VALUE
val1
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UNIT
%
CAS NUMBER
7440-66-6

SAE J454: 1991 / General Data on Wrought Aluminum Alloys

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SAE 6063 Physical Properties


Temperature

PROPERTY / VALUE
Modulus of Elasticity
69 — 79 GPa
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Electrical Resistivity
0.031 — 0.043 Ω∙mm²/m
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Density
val1
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kg/dm³
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Electrical Conductivity
val1
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S/m
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Melting Temperature
val1
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°C
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Thermal Conductivity
193 — 217.784 W/(m∙°C)
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Poisson Coefficient
val1
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This material has 463 properties — only a subset is shown here.

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SAE 6063 Heat Treatments


  • Solution heat treating at 529°C for all forms.
    Solution heat treating soaking times and maximum quench delay times is on specifications.
    For all forms (aging treatment is mandatory): Starting temper is AQ or W, final temper is T4 or T42 (sometimes used to designate final tempers), aging at room temperatures. For all forms (aging treatment is preferred): Starting temper is T4, final temper is T6 (sometimes used to designate final tempers), aging at 177°C for 8-10h. For all forms (aging treatment is alternate): Starting temper is T42, final temper is T62 (sometimes used to designate final tempers), aging at 160°C for 18-34h. When temper before furnace aging is AQ, W, T4 or T42, the furnace aging treatment may be started immediately after quenching or at any time thereafter.
    Full anneal: At 399-427°C, soaking time is minimum 1h (soak times listed are for up to 13 mm maximum thickness. Add 0.5 hour for each additional 13 mm of product or nested stack thickness or fraction thereof over 13 mm), cooling in furnace (furnace cool at 28°C degrees per hour maximum, to 260°C, air cool to room temperature or furnace cool at 28°C degrees per hour maximum, to 232°C, hold at 232°C for 6 hours, furnace or air cool to room temperature). Stress relief: At 333-349°C, soaking time is minimum 0.5h (soak times listed are for up to 13 mm maximum thickness. Add 0.5 hour for each additional 13 mm of product or nested stack thickness or fraction thereof over 13 mm), cooling in air.
  • Typical heat treatment:
    Solution heat treatment (T1), extrusions, tube: By suitable control of extrusion temperature, product may be quenched directly from extrusion press to provide specified properties for this temper;
    Solution heat treatment (T4), extrusions, tube: At 515 - 525°C; by suitable control of extrusion temperature, product may be quenched directly from extrusion press to provide specified properties for this temper
    Some products may be adequately quenched in air blast at room temperature.
    Material should be quenched in water or by high velocity fans from the solution heat-treating temperature as rapidly as possible and with minimum delay after removal from the furnace. Unless otherwise indicated, when material is quenched by total immersion in water, the water should be at room temperature and suitably cooled to remain below 35°C during the quench cycle. The use of high velocity, high volume jets of cold water is also effective for some material.
    Precipitation heat treatment (T5), extrusions, tube: At 175 - 185°C, 3 h (An alternate treatment comprised of 1 - 2 h at 200 - 210°C may be used);
    Precipitation heat treatment (T6), extrusions, tube: At 170 - 180°C, 8 h (An alternate treatment comprised of 6 h at 175 - 185°C may be used); the time at temperature will depend on the time required for load to reach temperature. The times shown are based on rapid heating with soaking time measured from the time the load reaches the 10°C range listed or selected.

SAE 6063 Mechanical Properties


Temperature

PROPERTY / VALUE
Tensile Strength
110 — 240 MPa
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Brinell Hardness (HB)
≥ 60
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Elongation, A
≥ 8 %
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Shear Strength
val1
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MPa
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Yield Strength, Rp0.2
val1
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MPa
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SAE 6063 International Equivalent Materials


Showing 15 of 105 results.

MATERIAL
STANDARD
COUNTRY / PRODUCER
EQUIVALENCE CATEGORY
MATERIAL
STANDARD
UNS
COUNTRY / PRODUCER
United States
EQUIVALENCE CATEGORY
Official
MATERIAL
STANDARD
AA
COUNTRY / PRODUCER
United States
EQUIVALENCE CATEGORY
Composition 100%
MATERIAL
STANDARD
B.S.
COUNTRY / PRODUCER
United Kingdom
EQUIVALENCE CATEGORY
Composition 100%
MATERIAL
STANDARD
EN
COUNTRY / PRODUCER
European Union
EQUIVALENCE CATEGORY
Composition 100%
MATERIAL
STANDARD
EN
COUNTRY / PRODUCER
European Union
EQUIVALENCE CATEGORY
Composition 100%
MATERIAL
STANDARD
GB
COUNTRY / PRODUCER
China
EQUIVALENCE CATEGORY
Official
MATERIAL
STANDARD
ASME
COUNTRY / PRODUCER
United States
EQUIVALENCE CATEGORY
Composition 100%
MATERIAL
STANDARD
B.S.
COUNTRY / PRODUCER
United Kingdom
EQUIVALENCE CATEGORY
Composition 100%
MATERIAL
STANDARD
B.S.
COUNTRY / PRODUCER
United Kingdom
EQUIVALENCE CATEGORY
Composition 100%
MATERIAL
STANDARD
B.S.
COUNTRY / PRODUCER
United Kingdom
EQUIVALENCE CATEGORY
Composition 100%
MATERIAL
STANDARD
GOST
COUNTRY / PRODUCER
Russia
EQUIVALENCE CATEGORY
Composition 100%
MATERIAL
STANDARD
ISO
COUNTRY / PRODUCER
International
EQUIVALENCE CATEGORY
Composition 100%
MATERIAL
STANDARD
JIS
COUNTRY / PRODUCER
Japan
EQUIVALENCE CATEGORY
Composition 100%
MATERIAL
STANDARD
JIS
COUNTRY / PRODUCER
Japan
EQUIVALENCE CATEGORY
Composition 100%
MATERIAL
STANDARD
JIS
COUNTRY / PRODUCER
Japan
EQUIVALENCE CATEGORY
Composition 100%

Equivalence categories reflect chemical-composition and mechanical-property comparison — always verify suitability against the governing specification for your application.

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  • 105Cross References

  • 33Composition
  • 82Mechanical Properties
  • 29Physical Properties
  • 3Heat Treatment
  • -Metallography
  • -Machinability

  • 50Stress-Strain
  • 13Formability
  • 49Fatigue
  • 6Fracture
  • 6Creep

  • 2Joints
  • -Coatings
  • -Dimensions
  • -Tribology

  • -Corrosion
  • 30Ageing
  • -Weatherability
  • -Irradiation

  • 55Total Suppliers