2C81444G02
FIXTURE, GRIND - HPT STATOR
2C81444G02 is a precision-engineered aerospace engine low-pressure turbine (LPT) seal segment, compliant with AS9100D quality standards and FAA/EASA regulations, optimized for CFM56-5B/7 and IAE V2500 turbofan engines. It forms a circumferential airtight barrier between the LPT rotor and casing, minimizing hot exhaust gas leakage, improving turbine expansion efficiency, and reducing unnecessary fuel consumption across all engine operating conditions.
Crafted from heat-resistant nickel-based alloy with a wear-resistant coating, it operates stably at temperatures up to 850°C and withstands high-frequency rotational vibration. Weighing 0.15kg with a segmented design, it enables tool-free installation and rapid replacement during LPT MRO overhauls. FAA Part 25 certified, it is a key component for sustaining turbine performance and engine fuel efficiency.

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