Alloy A286 Nickel Sheet, Coil & Bar - AMS 5525, 5858, 5731, 5732, 5737
Incoloy Alloy® A286 is an iron-based superalloy useful for applications requiring high strength and corrosion resistance up to 1300˚F (704˚C) and for lower stress applications at higher temperatures. The mechanical properties of this alloy are developed by suitable solution annealing and precipitation hardening treatments. Alloy A286 is non-magnetic.
This alloy has excellent high temperature oxidation resistance and is designed to maximize creep and stress rupture properties, with some reduction in strength. A-286 material can attain high strength levels when aged after cold work, and has wide application in high temperature fasteners and springs.
Standard Inventory Specifications
- UNS S66286
- AMS 5525
- AMS 5858
- AMS 5731
- AMS 5732
- AMS 5737
- ASTM A 453
- ASTM A 638
- ASME SA 453
- ASME SA 638
- EN 1.4980
- DIN EN 10204 3.1
- RR SABRe Edition 2
- DFARS Compliant
Common Trade Names
- Incoloy Alloy A286 (® Special Metals)
- Pyromet Alloy A-286 (® Carpenter Technology)
- ATI A286 (™ Allegheny Technologies)
Common Apllications of Alloy A286 Nickel
- Jet engine components
- Automotive applications
- Offshore oil and gas applications
- Moderate corrosion applications in aqueous solutions
- Non-magnetic cryogenic equipment
Inventory Size Range
- Sheet : 0.016" - 0.130"
- Bar : 0.250" - 6.000"
Please contact us for more details.
The technical data provided is for information only and not for design purposes. It is not warranted or guaranteed.
Alloy A286 Chemical Composition
|Element||Percent by Weight|
|Chromium||13.50 - 16.00|
|Nickel||24.00 - 27.00|
|Molybdenum||1.00 - 1.50|
|Titanium||1.90 - 2.35|
|Vanadium||0.10 - 0.50|
|Boron||0.003 - 0.010|
Resistance to Corrosion and Oxidation
Type A286 alloy content is similar in chromium, nickel, and molybdenum to some of the austenitic stainless steels. Consequently, this alloy possesses a level of aqueous corrosion resistance comparable to that of the austenitic stainless steels. In elevated temperature service, the level of corrosion resistance to atmospheres such as those encountered in jet engine applications is excellent to at least 1300°F (704°C). Oxidation resistance is high for continuous service up to 1500°F (816°C) and intermittent service up to 1800°F (982°C).
Alloy A286 Physical Properties
|Solution Treated||Solution Treated and Aged|
|Density||0.286 lb./in3 (7.92 g/cm3)||0.287 lb./in3 (7.94 g/cm3)|
|Melting Range||2500 - 2600 °F||1370 - 1430 °C|
|Temperature Range||Linear Coefficients of Thermal Expansion · 10-6|
|21 - 93||70 - 200||16.5||9.17|
|21 - 204||70 - 400||16.8||9.35|
|21 - 316||70 - 600||17.0||9.47|
|21 - 427||70 - 800||17.4||9.64|
|21 - 538||70 - 1000||17.6||9.78|
|21 - 649||70 - 1200||17.8||9.88|
|21 - 760||70 - 1400||18.6||10.32|
420 Joules/kg °K (Btu/lb/°F)
Mechanical Properties and Yield Strength of Alloy A286
Type A286 alloy is formed most easily in the solution treated condition. Typical room temperature tensile properties of material solution treated at 1800°F (982°C) are shown below.
- Yield Strength: 40,000 psi (275 MPa)
- Ultimate Tensile Strength: 90,000 psi (620 MPa)
- Elongation: 40%