Alloy A-286
About Alloy A-286
What is Alloy A-286?
Alloy A-286 is an iron-nickel-chromium alloy with additions of molybdenum and titanium.
Alloy A-286 also referred to as the UNS S66286/W.Nr. 1.4980 alloy.
The high strength and excellent fabrication characteristics of alloy A-286 make the alloy useful for various components of aircraft and industrial gas turbines.
It is also used for fastener applications in automotive engine and manifold components subject to high levels of heat and stress and in the offshore oil and gas industry.
Alloys A-286 is available in all standard mill forms including pipe, rod, bar, plate, sheet, strip and foil products.
Alloy A-286 Standards
SAE AMS 5858
-Plate, Sheet, Strip & Foil
ASTM A638
-Rod & Bar
Alloy A-286 Chemical Composition
Alloy A-286 Data Sheet
Alloy A-286 Equivalent Grades
| STANDARD | WERKSTOFF NR. | UNS | GOST | AFNOR | JIS | BS | EN | OR |
| Alloy A-286 | 1.4980 | S66286 | – | – | – | – | – | – |
Alloy A-286 Mechanical Properties
| Density | Melting Point | Tensile Strength | Yield Strength (0.2%Offset) | Elongation |
| 7.94 g/cm3 | 1430 °C (2600 °F) | 550-1300Mpa | 350-750Mpa2 | 25% |
Alloy A-286 Applications
Alloy A-286 Related Resources
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