Size (CM): 166*166*228

Weright (KG): 805.5

856A2713G07 is a precision-manufactured aerospace engine fan frame strut component, compliant with AS9100D quality standards and FAA/EASA regulations, designed for large commercial turbofan engines. It is a core load-bearing and flow-guiding structure in the engine fan section, supporting the fan hub and guiding the incoming air to flow stably into the low-pressure compressor, which is critical for maintaining the fan's operational stability, reducing aerodynamic resistance of the air flow, and ensuring the continuous and stable air supply for the subsequent engine sections.

Made from high-strength, lightweight titanium alloy with surface anti-corrosion treatment, it withstands operating temperatures from -50°C to 190°C and continuous aerodynamic load. Weighing 1.4kg with a precision-machined airfoil structure, it allows for fast installation and alignment inspection during fan section MRO overhauls. FAA Part 25 certified, it is a key component for engine fan section operational safety.