956A8018P12
Screw head
Size (CM): 23*18*11
Weright (KG): 1
956A8018P12 is a precision aviation maintenance tool, specifically a high-accuracy turbine blade tip clearance gauge designed for commercial turbofan engines (e.g., CFM56-7B/5C, V2500-E5 series) in MRO, assembly, and overhaul workflows. It precisely measures the critical gap between turbine blade tips and engine casings, ensuring optimal airflow efficiency, minimizing energy loss, and preventing catastrophic blade-casing contact during engine operation.
Crafted from aerospace-grade wear-resistant alloy with a calibrated, corrosion-resistant probe, it withstands extreme engine bay temperatures (up to 1,350°F) and mechanical stress while maintaining sub-millimeter measurement precision. Compliant with OEM specifications and SAE AS9100 standards, its ergonomic grip and compact design enhance maneuverability in confined engine compartments.
Lightweight and easy to operate, it streamlines inspection processes, reduces maintenance downtime, and ensures consistent engine performance. This tool is indispensable for upholding airworthiness compliance, preserving turbine efficiency, and safeguarding long-term operational safety of commercial and regional aircraft.

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