INCONEL 718 per GE B50A915
GE B50A915 is a General Electric aerospace material specification associated with Inconel 718 (UNS N07718), a precipitation-hardenable nickel-chromium superalloy widely used in high-performance turbine and aerospace components. The specification defines requirements for materials intended to operate under extreme mechanical stress, elevated temperatures, and corrosive environments, conditions commonly encountered in modern aircraft engines and industrial gas turbines.
Key Properties of GE B50A915
- Excellent high-temperature tensile strength
- Superior fatigue and creep resistance
- Strong oxidation and corrosion resistance
- Good weldability and fabrication characteristics
- Reliable performance under thermal cycling and mechanical stress
Typical Applications of GE B50A915
Materials conforming to GE B50A915 are commonly used in:
- Aircraft turbine engine components
- Gas turbine rotors and shafts
- High-temperature structural hardware
- Fasteners and critical mechanical parts
- Equipment exposed to corrosive or high-temperature environments
More GE Aviation Specifications
GE AVIATION
Engine components requiring high-temperature strength and durability.
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.