Size (CM)：21*17*9
Weight (KG)：0.67

856A2796 is a high-strength aviation structural component compliant with rigorous AS9100D standards and FAA/EASA airworthiness regulations, engineered for load distribution and structural reinforcement in aircraft wing flap drive assemblies during MRO and assembly. Fabricated from corrosion-resistant high-tensile aluminum alloy with a wear-resistant hard anodized coating, it operates stably across -60℃ to 230℃, withstanding aerodynamic load cycling, vibration-induced fatigue and aviation fluid erosion without structural distortion. Its precision-machined connection interfaces ensure seamless integration with flap actuators and wing frames, eliminating disengagement risks during takeoff, low-speed cruise and landing phases. Compact yet robust, it is a critical part for aircraft lift control system reliability and operational safety.