Size (CM): 94*64*20

Weright (KG): 18

856A1870G01 is a precision aviation engine tool, specifically a compressor blade installation/removal fixture engineered for commercial turbofan engines (e.g., CFM56, PW4000 series). It plays a critical role in safely handling and positioning compressor blades during engine assembly, overhaul, or repair, ensuring accurate alignment with rotor disks and preventing blade damage.

Crafted from aerospace-grade high-strength alloy with a wear-resistant coating, it withstands mechanical stress and extreme engine bay temperatures (-40℃ to 150℃) while maintaining dimensional stability. Its precision-machined clamping surfaces and ergonomic design enable secure blade grip and controlled manipulation, adhering to strict OEM specifications and SAE AS9100 standards.

Compact and lightweight, it enhances maneuverability in confined spaces, streamlines maintenance workflows, and reduces human error. This fixture is indispensable for preserving compressor efficiency, engine performance, and operational reliability—critical for ensuring safe, long-term flight operations of commercial and regional aircraft.