INCONEL 718
ITN07763.07 is an engineering material specification associated with Inconel 718 (UNS N07718), a precipitation-hardenable nickel-chromium superalloy widely used in aerospace propulsion systems and high-temperature industrial applications. Materials produced to this specification are intended for components that must operate under high mechanical stress, elevated temperatures, and aggressive environments.
Product Forms & Size Range
- Excellent strength at elevated temperatures
- Superior fatigue and creep resistance
- Strong oxidation and corrosion resistance
- Good fabrication and weldability characteristics
- Stable performance under thermal cycling and mechanical stress
Typical Applications of ITN07763.07
Materials produced to ITN07763.07 are commonly used in:
- Aerospace turbine engine components
- Gas turbine shafts and rotors
- High-temperature structural hardware
- Fasteners and critical mechanical parts
- Equipment operating in corrosive or high-pressure environments
Related Specifications
SHEET & PLATE
Sheets and plates for high-temperature aerospace and industrial applications.
BARS & FORGINGS
Bars and forgings designed for high-strength, creep, and fatigue-resistant components.
Full INCONEL 718 Specifications List
Looking for the complete list of INCONEL 718 specifications used across aerospace and industrial standards? Click the button below to view the full specification list, including standards from major organizations and manufacturers.
Certified Material for Critical Service
All INCONEL 718 supplied by Fighter Jet Metals includes:
- Full test reports with heat numbers and traceability.
- Dual certifications with AMS and OEM standards when applicable.
- Compliance with AMS, Boeing, GE, and Pratt & Whitney specifications.
- NADCAP-certified heat treatment and SAE aerospace-approved quality systems.
Our INCONEL 718 products are designed for mission-critical aerospace and industrial operations where reliability and compliance are paramount.