Inconel 718 UNS N07718 Nickel Alloy Sheet Plate AMS 5596 for Aerospace Gas Turbine Engine Components

We supply premium Inconel 718 nickel-chromium superalloy sheet and plate in full compliance with AMS 5596 and ASTM B670 standards. Our products undergo strict solution heat treatment per AMS 5662, ensuring excellent mechanical properties and structural integrity for demanding aerospace and high-temperature applications.

• Excellent High Temperature Strength: Maintains mechanical properties up to 700°C (1300°F), making it ideal for gas turbine and jet engine components.
• Outstanding Oxidation & Corrosion Resistance: Performs reliably in harsh oxidizing and reducing environments, including chemical processing and marine applications.
• Precipitation Hardenable: Achieves high strength through gamma prime and gamma double prime phase strengthening without pre-heat treatment distortion.
• Weldable & Fabrication Friendly: Good weldability with both manual and automated welding processes, allowing complex part fabrication.
• Mill Test Certificate (MTC): Every shipment includes full traceability documentation per EN 10204 3.1 or 3.2 requirements.

• Aerospace compressor blades, turbine discs, and structural components
• Gas turbine hot-section parts (combustors, casings, afterburners)
• Oil & gas downhole tools, hangers, and wellhead components
• Nuclear reactor core components and cryogenic storage tanks
• High-temperature fasteners, springs, and bolting for industrial furnaces

• 20+ years specializing in nickel-based superalloys
• In-house spectrographic and mechanical testing laboratory
• Flexible order quantities: from trial samples to container loads
• Fast global shipping via DHL, FedEx, sea freight, or air freight