TECHNICAL INFORMATION FOR A286 PER AMS 5895
A286, as per the specifications of AMS 5895, is a corrosion- and heat-resistant alloy that achieves its hardness through precipitation. It is supplied in the form of bars, wire, forgings, tubing, and rings. The alloy is melt-cast as a consumable electrode and then solution heat-treated at 1750°F (954°C) for the purpose of offering strength and structural stability in tough environments.
A286 alloy composition: The alloy composition is based on iron, nickel, and chromium, with the addition of molybdenum, titanium, boron, and vanadium for the purpose of improving its mechanical properties at high temperatures.
Is A286 a Stainless Steel?
Some companies list A286 under Nickel and some companies list A286 under Stainless Steel. Ultimately, It is an iron-nickel-chromium alloy with additions of molybdenum and titanium making it a super alloy that is in between those categories. As one of the austenitic alloys it maintains good strength and oxidation resistance at temperatures up to 1300ºF. Due to its high strength and excellent fabrication characteristics it performs like a Nickel alloy but has a similar density to that of Stainless Steel. Because of these characteristics, A286 is one of the most popular high temperature alloys.
Applications of AMS 5895
Because of its strength and corrosion resistance, A286 per AMS 5895 is commonly used in demanding industries, including:
- Aerospace engine components
- Turbine hardware
- High-temperature fasteners
- Cryogenic structural components
- Industrial gas turbine systems
A286 STAINLESS STEEL SPECIFICATIONS
SHEET & PLATE
Flat products for structural, high-temperature, and corrosion-resistant applications.
BARS & FORGINGS
Semi-finished and forged shapes for critical components requiring toughness and high-temperature performance.
GE SPECIFICATIONS
Engineered for General Electric aerospace components.
ROLLS ROYCE SPECIFICATIONS
Certified to Rolls-Royce standards for turbine and high-temperature parts.
PRATT & WHITNEY SPECIFICATIONS
Engineered for Pratt & Whitney engine and structural applications.
SAFRAN SPECIFICATIONS
Manufacturer-specific superalloy components for aerospace applications.
Certified Material for Critical Service
A286 Stainless Steel is specified under multiple aerospace standards including AMS 5525, AMS 5726, AMS 5731–5737, AMS 5853, AMS 5895, and various GE, Rolls Royce, Pratt & Whitney, and Safran specifications. This ensures reliability, traceability, and suitability for critical high-temperature and high-strength applications.