Size (CM)：16.5*12*6
Weight (KG)：0.4

856A2632G01 is a high-strength aviation structural component that adheres to AS9100D standards and FAA/EASA airworthiness regulations, designed for load-bearing reinforcement and alignment maintenance in aircraft wing trailing-edge flap assemblies during MRO and assembly. Crafted from corrosion-resistant high-tensile aluminum alloy with a wear-resistant hard anodized coating, it maintains stable performance across -60℃ to 230℃, withstanding aerodynamic load cycling, vibration-induced fatigue and aviation fluid erosion without structural distortion. Its precision-machined guide rails ensure seamless, synchronized flap movement, eliminating jamming risks during takeoff, low-speed cruise and landing phases. Compact yet robust, it optimizes flap system reliability and acts as a critical part for aircraft lift control and operational safety.