Size (CM)：20.5*14*8
Weight (KG)：0.88

856A1336G02 is a high-strength aviation structural component that complies with AS9100D standards and FAA/EASA airworthiness regulations. Engineered for load-bearing reinforcement and vibration damping in aircraft landing gear retraction mechanisms during MRO and assembly, it is fabricated from corrosion-resistant high-tensile steel alloy with a fatigue-resistant zinc-nickel plating. It operates stably across a wide temperature range of -60℃ to 250℃, withstanding landing impact loads, retraction cycle fatigue and aviation fluid erosion without structural deformation. Its precision-machined mounting lugs ensure seamless, rigid integration with gear struts and fuselage brackets, eliminating loosening risks during takeoff, cruise and rough-landing phases. Compact yet robust, it enhances landing gear structural integrity and serves as a critical part for aircraft ground operational safety.