Size (CM): 17*12*6

Weright (KG): 0.25

856A1213G01 is a high-strength aviation structural component that complies with stringent AS9100D standards and FAA/EASA airworthiness regulations, engineered for load-bearing support and structural stability in aircraft engine mounting assemblies during MRO and assembly. Fabricated from corrosion-resistant high-tensile steel alloy with a fatigue-resistant anti-corrosion plating, it operates stably across a wide temperature range of -60℃ to 300℃, withstanding engine vibration, thermal expansion stress and aviation fluid erosion without structural deformation. Its precision-machined mounting holes ensure seamless integration with engine frames and fuselage structures, eliminating loosening risks during takeoff, cruise and landing phases. Compact yet robust, it is a critical part for enhancing engine system reliability and aircraft operational safety.