Size (CM): 47*47*21
Weight (KG): 8.5

856A1199P01 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 main landing gear bracing assemblies during MRO and assembly. Fabricated from corrosion-resistant high-tensile steel alloy with a fatigue-resistant cadmium plating, it operates stably across extreme temperatures from -60℃ to 260℃, resisting landing impact loads, retraction cycle fatigue and aviation fluid erosion without structural deformation. Its precision-machined load-bearing joints ensure seamless integration with gear struts and fuselage hardpoints, eliminating loosening risks during taxiing, takeoff roll and rough-field landing phases. Compact yet robust, it enhances landing gear structural integrity and serves as a critical part for aircraft ground operational safety.