Size (CM)：38.5*23.5*16
Weight (KG)：3.5

856A1612G01 is a high-precision aviation structural component compliant with AS9100D standards and FAA/EASA regulations, engineered for load-bearing linkage in aircraft horizontal stabilizer 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 220℃, resisting aerodynamic stress, mechanical vibration and aviation fluid erosion without structural deformation. Its precision-machined connection interfaces ensure seamless, stable fitting with stabilizer actuators and brackets, 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.