956A8018P10
Double threaded screw
Size (CM): 23*18*11
Weright (KG): 1
956A8018P05 is a precision aviation maintenance tool, specifically a turbine blade tip clearance gauge engineered for commercial turbofan engines (e.g., CFM56-5B/7B, V2500-A5 series) during assembly, overhaul, and MRO operations. It delivers accurate measurement of the critical gap between turbine blade tips and engine casings, ensuring optimal airflow dynamics, minimizing energy loss, and preventing catastrophic blade-casing contact.
Crafted from aerospace-grade wear-resistant alloy with a calibrated, high-precision probe, it withstands extreme engine bay temperatures (up to 1,300°F) and mechanical stress while maintaining sub-millimeter measurement accuracy. Compliant with OEM specifications and SAE AS9100 standards, its ergonomic design enhances maneuverability in confined engine compartments.
Compact and lightweight, it streamlines maintenance workflows, reduces inspection downtime, and ensures consistent engine performance. This tool is indispensable for preserving turbine efficiency, adhering to airworthiness regulations, and safeguarding long-term operational safety of commercial and regional aircraft.

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