The AS1895/7-125 Coupling is a precision component made from Nickel Alloy 718, offering excellent corrosion resistance. With a housing bore of 1.208" and accommodating a 1.125" shaft, it ensures a secure fit for CF34-10E/8C/8E engines, making it ideal for critical aviation applications.
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Overview
The AS1895/7-125 Coupling is a precision-engineered component designed for optimal performance in aviation applications. Constructed from high-quality Nickel Alloy 718, this coupling features a passivated surface treatment that enhances corrosion resistance and durability. With a housing bore diameter of 1.208 inches and an accommodated shaft diameter of 1.125 inches, it ensures a secure fit for various assemblies. This coupling is fabricated using solid construction methods, making it a reliable choice for critical applications in CF34-10E/8C/8E engines.
Features & Benefits
Features
Constructed from Nickel Alloy 718 for superior strength and durability.
Passivated surface treatment for enhanced corrosion resistance.
Housing bore diameter of 1.208 inches and accommodated shaft diameter of 1.125 inches for secure fitting.
Solid fabrication method ensures reliability in demanding environments.
Benefits
Provides long-lasting performance in aviation applications.
Enhances safety and reliability through secure connections.
Resists corrosion, extending the lifespan of the coupling.
Meets stringent industry standards for quality and performance.
Technical Information
ATA Number
72,
75
ATA Chapter
Engine Turbine / Turbo Prop Ducted Fan / Unducted Fan
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