956A1022G02 is a precision-manufactured aerospace engine low-pressure compressor (LPC) stator vane segment, compliant with AS9100D quality standards and FAA/EASA regulations, designed for large commercial turbofan engines. It is a key flow-guiding component in the LPC, regulating the direction and speed of incoming ambient air, ensuring the air enters the LPC rotor blades in an optimized path, which is critical for reducing aerodynamic loss, improving the LPC's compression efficiency, and maintaining a stable air supply for the subsequent high-pressure compressor (HPC).

Made from high-strength, corrosion-resistant titanium alloy, it withstands operating temperatures up to 600°C and continuous scouring from high-speed air flow. Weighing 0.22kg with a precision-machined airfoil surface, it allows for fast installation and condition inspection during LPC MRO overhauls. FAA Part 25 certified, it is a key component for LPC operational stability.