956A8675G05
FIXTURE, INSTALL - PLATFORM FRONT SHROUD
Size (CM): 38.5*23.5*16
Weright (KG): 3.5
956A8675G05 is a precision aviation engine component, specifically a turbine stator vane segment engineered for commercial turbofan engines (e.g., CFM56 or PW1000G series). It plays a critical role in directing airflow through the engine core, optimizing combustion efficiency and reducing turbine wear by maintaining stable, uniform gas flow during high-temperature operation.
Crafted from aerospace-grade single-crystal superalloy with thermal barrier coating, it withstands extreme temperatures (up to 1,900°F) and mechanical stress without deformation. Its precision-machined aerodynamic profile adheres to strict engine manufacturer specifications and aerospace standards (e.g., AS9100).
Compact and fully compatible with OEM assembly requirements, it simplifies engine overhaul and replacement workflows. This component is indispensable for preserving engine performance, fuel efficiency, and operational reliability—critical for ensuring long-term airworthiness and safe flight operations for commercial and regional aircraft.

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