Size (CM)：48*48*19
Weight (KG)：6.5

856A2318G01 is a high-reliability aviation mechanical component compliant with AS9100D standards and FAA/EASA airworthiness regulations, engineered for structural bracing and load stabilization in aircraft wing flap actuation systems during MRO and assembly. Fabricated from high-strength corrosion-resistant alloy steel with wear-resistant manganese phosphate plating, it withstands extreme temperatures ranging from -55℃ to 215℃, resisting aerodynamic stress, mechanical fatigue and hydraulic fluid erosion without structural deformation. Its precision-machined mounting slots ensure seamless, stable integration with flap drive mechanisms, eliminating misalignment risks during takeoff, landing and low-speed flight phases. Compact and robust, it optimizes wing control efficiency and serves as a critical part for aircraft operational reliability and flight safety.