Size (CM)：16.5*12*6
Weight (KG)：0.25

856A3108G01 is a high-reliability aviation mechanical component compliant with AS9100D standards and FAA/EASA regulations, engineered for load-bearing and positioning in aircraft rudder control linkage systems during MRO and assembly. Fabricated from high-strength corrosion-resistant titanium alloy with a fatigue-resistant coating, it withstands extreme temperatures ranging from -60℃ to 215℃, resisting aerodynamic stress, mechanical vibration and aviation fluid erosion without structural deformation. Its precision-machined pivot interfaces ensure seamless, stable articulation with rudder drive components, eliminating jamming risks during course correction, crosswind operations and turbulence response. Compact yet robust, it fits confined tail compartments, streamlines maintenance workflows, and serves as a critical part for aircraft flight control stability and operational safety.