956A8492G02 is a precision-engineered aerospace engine high-pressure compressor (HPC) stator vane, compliant with AS9100D quality standards and FAA/EASA regulations, designed for CFM56 and IAE V2500 turbofan engines. It guides the flow of compressed air between HPC rotor stages, adjusting the air flow angle to match the rotor blades' operating state, which is critical for reducing air turbulence, improving compression efficiency, and maintaining stable air pressure output for the engine's combustion system.

Made from a high-strength, heat-resistant titanium alloy, it withstands operating temperatures up to 580°C and continuous air flow impact. Weighing 0.14kg with a precision-machined mounting structure, it enables fast installation and alignment checks during HPC MRO overhauls. FAA Part 25 certified, it is a key component for HPC performance and engine operational efficiency.