SAE 7050 Aluminium Alloys

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

Data updates

Latest Update: 2024-08
Total number of updates: 29
Update History

This material has 1911 properties — only a subset is shown here.

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SAE 7050 Chemical Composition

CRITERIA
VALUE
UNIT
CAS NUMBER
CRITERIA
Al
VALUE
Remainder
UNIT
%
CAS NUMBER
7429-90-5
CRITERIA
Cr
VALUE
≤ 0.04
UNIT
%
CAS NUMBER
7440-47-3
CRITERIA
Cu
VALUE
2.0 – 2.6
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
CRITERIA
Zr
VALUE
val1
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UNIT
%
CAS NUMBER
7440-67-7

SAE AMS 4341H: 2024 / Aluminum Alloy, Extrusions 6.2Zn - 2.3Cu - 2.2Mg - 0.12Zr (7050-T73511) Solution Heat Treated, Stress Relieved by Stretching, Straightened, and Overaged

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SAE 7050 Physical Properties


Temperature

PROPERTY / VALUE
Compression Modulus
72 — 74 GPa
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Modulus of Elasticity
69 — 79 GPa
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Density
val1
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kg/dm³
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Thermal Conductivity
val1
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W/(m∙°C)
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Electrical Resistivity
≤ 0.0466 Ω∙mm²/m
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Electrical Conductivity
val1
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S/m
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Poisson Coefficient
val1
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Shear Modulus
val1
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GPa
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This material has 1911 properties — only a subset is shown here.

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SAE 7050 Heat Treatments


  • Overaging heat treatment: recommended practice is heating to 121°C ± 3 (250°F ± 5), holding at heat for not less than 4 hours, further heating to 174°C ± 6 (345°F ± 10), holding at heat for not less than 8 hours, and cooling in air.
  • Solution heat treating at 471°C for forgings. Solution heat treating at 477°C for all others ), (to avoid stress corrosion cracking of thick 7049 parts, delay between quenching and start of aging should not exceed 72h); (solution heat treat temperatures as low as 466°C may be used to control recrystallization and surface cracking problems); (eutectic melting may occur at the specified temperature if the raw material was not properly homogenized or worked).
    Solution heat treating soaking times and maximum quench delay times is on specifications.
    Limits for quenching in polymer solutions for sheets, plates, bars: for thickness 2.03 mm polymer concentration is 40% max (±2); for thickness 6.35 mm polymer concentration is 34% max (±2); for thickness 9.52 mm polymer concentration is 28% max (±2); for thickness 12.70 mm polymer concentration is 22% max (±2); for thickness 25.40 mm polymer concentration is 16% max (±2). Limits for quenching in polymer solutions for forgings: for thickness 25.40 mm polymer concentration is 28-32% max (±2); for thickness 50.80 mm polymer concentration is 24-28% max (±2); for thickness 76.20 mm polymer concentration is 18-22% max (±2); for thickness 101.50 mm polymer concentration is 13-17% max (±2). Limits for quenching in polymer solutions for extrusions: for thickness 6.35 mm polymer concentration is 28% max (±2); for thickness 9.52 mm polymer concentration is 22% max (±2).
    Aging treatment is mandatory. For rivets: Starting temper is AQ or W, final temper is T73 (sometimes used to designate final tempers), 1st step: aging at 121°C for 4min, 2nd step: aging at 179°C for 8min. For plates, extruded bars and shapes: Starting temper is AQ or W, final temper is T73 (sometimes used to designate final tempers), 1st step: aging at 121°C for 6-8h, 2nd step: aging at 177°C for 11.5-12.5h. For plates: Starting temper is AQ or W, final temper is T76 (sometimes used to designate final tempers), 1st step: aging at 121°C for 6-8h, 2nd step: aging at 177°C for 6.5-7h. For all forms, except plates, extruded bars and shapes: Starting temper is AQ or W, final temper is T76 (sometimes used to designate final tempers), 1st step: aging at 121°C for 6-8h, 2nd step: aging at 177°C for 3.5-4.5h. For all forms: Starting temper is AQ or W, final temper is T74 (sometimes used to designate final tempers), 1st step: aging at 121°C for 6-8h, 2nd step: aging at 177°C for 6-8h.
    Full anneal: At 399-427°C, soaking time is minimum 2h (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 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 2h (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.

SAE 7050 Mechanical Properties


Temperature

PROPERTY / VALUE
Tensile Strength
≥ 71 MPa
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Brinell Hardness (HB)
≥ 135
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Compression Yield Strength
val1
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MPa
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Elongation, A
≥ 1.5 %
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Yield Strength, Rp0.2
val1
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MPa
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SAE 7050 International Equivalent Materials


Showing 15 of 143 results.

MATERIAL
STANDARD
COUNTRY / PRODUCER
EQUIVALENCE CATEGORY
MATERIAL
STANDARD
UNS
COUNTRY / PRODUCER
United States
EQUIVALENCE CATEGORY
Official
MATERIAL
STANDARD
GB
COUNTRY / PRODUCER
China
EQUIVALENCE CATEGORY
Official
MATERIAL
STANDARD
AA
COUNTRY / PRODUCER
United States
EQUIVALENCE CATEGORY
Composition 100%
MATERIAL
STANDARD
EN
COUNTRY / PRODUCER
European Union
EQUIVALENCE CATEGORY
Composition 100%
STANDARD
EN
COUNTRY / PRODUCER
European Union
EQUIVALENCE CATEGORY
Composition 100%
MATERIAL
STANDARD
WL
COUNTRY / PRODUCER
Germany
EQUIVALENCE CATEGORY
Official
MATERIAL
STANDARD
ASTM
COUNTRY / PRODUCER
United States
EQUIVALENCE CATEGORY
Composition 100%
MATERIAL
STANDARD
ASTM
COUNTRY / PRODUCER
United States
EQUIVALENCE CATEGORY
Composition 100%
MATERIAL
STANDARD
ISO
COUNTRY / PRODUCER
International
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%
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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  • 143Cross References

  • 108Composition
  • 883Mechanical Properties
  • 81Physical Properties
  • 5Heat Treatment
  • 2Metallography
  • -Machinability

  • 389Stress-Strain
  • 27Formability
  • 113Fatigue
  • 99Fracture
  • 2Creep

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

  • -Corrosion
  • 10Ageing
  • -Weatherability
  • -Irradiation

  • 49Total Suppliers