956A6323G01 is a precision-engineered aerospace engine low-pressure turbine (LPT) blade retainer, compliant with AS9100D quality standards and FAA/EASA regulations, designed for CFM56 series turbofan engines. It secures the LPT blades in the turbine disk slots, preventing displacement or loosening under the impact of the expanded exhaust gas passing through the turbine, which is critical for maintaining the regular air flow path of the LPT, ensuring stable energy conversion efficiency, and avoiding damage to the turbine caused by detached blades.

Made from a heat-resistant, high-strength nickel-based superalloy, it withstands operating temperatures up to 980°C and continuous mechanical stress. Weighing 0.19kg with a precision-locking structure, it allows for fast installation and position verification during LPT MRO overhauls. FAA Part 25 certified, it is a key component for LPT performance and engine operational safety.