856A1169G02
Fixture, Lift - HP Compressor Stator Case, Front Assembly
Size (CM): 60*35*30
Weright (KG): 12
856A1169G02 is a high-reliability aviation structural component compliant with stringent AS9100D quality standards and FAA/EASA airworthiness certifications, engineered for lightweight load-bearing support and mechanical stability in aircraft main landing gear shock strut mounting assemblies during MRO and original equipment integration. Fabricated from high-strength aerospace-grade aluminum alloy, it features a wear-resistant hard anodized finish and corrosion-proof coating, delivering stable operation across a temperature range of -60℃ to 240℃. The component withstands heavy landing impact loads, continuous flight and ground vibration, and exposure to hydraulic fluids, de-icing chemicals, and environmental contaminants without fatigue, deformation, or material degradation. Its precision-machined mounting flanges and strut interfaces ensure seamless integration with main gear structures and airframe, maintaining load distribution integrity and shock absorption performance during taxiing, takeoff, landing, and ground maneuvering. Lightweight yet robust, it is a critical part for enhancing main gear structural durability, reducing impact stress, and boosting overall aircraft operational safety and ground handling reliability.

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