Size (CM): 16.5*12*6
Weight (KG): 0.25

856A2794G01 is a high-strength aviation structural component compliant with AS9100D standards and FAA/EASA airworthiness regulations, engineered for load distribution and structural reinforcement in aircraft wing-fuselage junction assemblies during MRO and assembly. Fabricated from corrosion-resistant high-tensile steel alloy with a wear-resistant zinc-rich coating, it operates stably across extreme temperatures from -60℃ to 240℃, resisting aerodynamic shear stress, continuous vibration fatigue and aviation fluid corrosion without structural deformation. Its precision-machined fastener holes ensure seamless, rigid integration with wing spars and fuselage frames, eliminating structural loosening risks during takeoff, high-speed cruise and turbulent flight. Compact yet robust, it enhances airframe structural integrity and serves as a critical part for aircraft flight safety and operational reliability.