SAE 5914 Nickel Alloys

Material group: Nonferrous Alloys / Nickel Alloys
Country / Standard: United States / SAE

Data updates

Latest Update: 2025-01
Total number of updates: 3
Update History
2024-12 2019-06

This material has 76 properties — only a subset is shown here.

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SAE 5914 Chemical Composition

CRITERIA
VALUE
UNIT
CAS NUMBER
CRITERIA
Al
VALUE
0.20 – 0.80
UNIT
%
CAS NUMBER
7429-90-5
CRITERIA
B
VALUE
≤ 0.006
UNIT
%
CAS NUMBER
7440-42-8
CRITERIA
Bi
VALUE
0.00003%
UNIT
%
CAS NUMBER
7440-69-9
CRITERIA
C
VALUE
val1
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UNIT
%
CAS NUMBER
7440-44-0
CRITERIA
Co
VALUE
val1
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UNIT
%
CAS NUMBER
7440-48-4
CRITERIA
Cr
VALUE
val1
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UNIT
%
CAS NUMBER
7440-47-3
CRITERIA
Cu
VALUE
val1
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UNIT
%
CAS NUMBER
7440-50-8
CRITERIA
Fe
VALUE
val1
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UNIT
%
CAS NUMBER
7439-89-6
CRITERIA
Mn
VALUE
val1
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UNIT
%
CAS NUMBER
7439-96-5
CRITERIA
Mo
VALUE
val1
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UNIT
%
CAS NUMBER
7439-98-7
CRITERIA
N
VALUE
val1
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UNIT
%
CAS NUMBER
7727-37-9; 17778-88-0
CRITERIA
Nb
VALUE
val1
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UNIT
%
CAS NUMBER
7440-03-1
CRITERIA
Ni
VALUE
val1
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UNIT
%
CAS NUMBER
7440-02-0
CRITERIA
P
VALUE
val1
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UNIT
%
CAS NUMBER
7723-14-0
CRITERIA
Pb
VALUE
val1
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UNIT
%
CAS NUMBER
7439-92-1
CRITERIA
S
VALUE
val1
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UNIT
%
CAS NUMBER
7704-34-9
CRITERIA
Se
VALUE
val1
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UNIT
%
CAS NUMBER
7782-49-2
CRITERIA
Si
VALUE
val1
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UNIT
%
CAS NUMBER
7440-21-3
CRITERIA
Ta
VALUE
val1
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UNIT
%
CAS NUMBER
7440-25-7
CRITERIA
Ti
VALUE
val1
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UNIT
%
CAS NUMBER
7440-32-6

SAE AMS 5914C: 2024 / Nickel Alloy, Corrosion and Heat Resistant, Sheet, Strip, and Foil 52.5Ni - 19Cr - 3.0Mo - 5.0Cb (Nb) - 0.90Ti - 0.50Al - 18Fe Consumable Electrode or Vacuum Induction Melted, Precision Cold Rolled, Solution Heat Treated (Alloy 718 SPF)

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SAE 5914 Physical Properties


Temperature

PROPERTY / VALUE
Modulus of Elasticity
185 — 205 GPa
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Density
7.9 — 8.8 kg/dm³
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Poisson Coefficient
0.32 — 0.34
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This material has 76 properties — only a subset is shown here.

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SAE 5914 Heat Treatments


  • Solution heat treated
    Heating in the protective atmosphere (hydrogen or argon gas with a dew point of -51°C (-60°F) or lower or a vacuum) to a temperature within the range of 941°C-996°C (1725-1825°F), holding at the selected temperature within ± 14°C (± 25°F) for a time commensurate with product thickness, and cooling at a rate equivalent to an air cool or faster.
    Precipitation heat treatment:
    Heating to 718°C ± 8°C (1325°F ± 15°F), holding at heat for 8 hours ± 0.5, cooling at a rate of 56°C (100°F) per hour to 621°C ± 8°C (1150°F ± 15°F), holding at 621°C ± 8°C (1150°F ± 15°F) for 8 hours ± 0.5, and cooling at a rate equivalent to an air cool or faster. Instead of the 56°C (100°F) per hour cooling rate to 621°C ± 8°C (1150°F ± 15°F), product may be furnace cooled at any rate provided the time at 621°C ± 8°C (1150°F ± 15°F) is adjusted to give a total precipitation heat treatment time of 18h minimum. After being re-solution heat treated by heating to 954°C ± 14°C (1750°F ± 25°F), holding at heat for a time commensurate with product cross-section, and cooling at a rate equivalent to an air cool or faster and precipitation heat treated as above.

SAE 5914 Mechanical Properties


Temperature

PROPERTY / VALUE
Tensile Strength
≥ 1034 MPa
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Elongation, A
≥ 12 %
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Yield Strength, Rp0.2
val1
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MPa
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Grain Size
val1
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Rockwell Hardness (HR)
val1
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Vickers Hardness (HV)
val1
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SAE 5914 International Equivalent Materials


Showing 3 of 3 results.

MATERIAL
STANDARD
COUNTRY / PRODUCER
EQUIVALENCE CATEGORY
MATERIAL
STANDARD
UNS
COUNTRY / PRODUCER
United States
EQUIVALENCE CATEGORY
Official
STANDARD
PROPRIETARY
COUNTRY / PRODUCER
EQUIVALENCE CATEGORY
Official
MATERIAL
STANDARD
SAE
COUNTRY / PRODUCER
United States
EQUIVALENCE CATEGORY
Implicit

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  • 3Cross References

  • 20Composition
  • 29Mechanical Properties
  • 3Physical Properties
  • 1Heat Treatment
  • -Metallography
  • -Machinability

  • -Stress-Strain
  • -Formability
  • -Fatigue
  • -Fracture
  • 1Creep

  • -Joints
  • -Coatings
  • 17Dimensions
  • -Tribology

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

  • 2Total Suppliers