Size (CM)：38*23*16

Weight (KG)：0.8

856A2663G01 is a high-strength aviation structural component adhering to stringent AS9100D standards and FAA/EASA airworthiness regulations, engineered for load distribution and motion guidance in aircraft wing slat drive systems during MRO and assembly. Fabricated from corrosion-resistant high-tensile aluminum alloy with a wear-resistant hard anodized coating, it delivers stable performance across -60℃ to 230℃, withstanding aerodynamic load cycling, vibration-induced fatigue and aviation fluid erosion without structural distortion. Its precision-machined guide slots ensure smooth slat deployment and retraction, eliminating jamming risks during takeoff, low-speed cruise and landing phases. Compact yet robust, it is a critical part for aircraft lift control system reliability and overall operational safety.