Size (CM): 59.5*49.5*20
Weight (KG): 20.5

856A1491G02 is a high-precision aviation structural component compliant with AS9100D standards and FAA/EASA regulations, engineered for load-bearing and linkage functions in aircraft rudder control systems during MRO and assembly. Fabricated from high-strength corrosion-resistant titanium alloy with fatigue-resistant coating, it withstands extreme temperatures from -60℃ to 215℃, resisting aerodynamic stress, mechanical vibration and aviation fluid erosion without structural deformation. Its precision-machined connection slots ensure seamless, stable fitting with rudder actuators and linkages, eliminating loosening risks during critical flight maneuvers. Compact yet robust, it optimizes tail compartment space utilization and serves as a critical part for aircraft flight control stability and operational safety.