8C2666G02 is a precision-manufactured aerospace component, compliant with AS9100D quality standards and FAA/EASA regulations, designed for large commercial turbofan engines, acting as an engine fuel system flow control valve bracketIt is a core load-bearing and positioning structure for the fuel flow control valve, fixing the valve in the designated position of the engine's fuel supply section, which is critical for maintaining the stability of the valve's installation position, avoiding displacement caused by engine vibration, and ensuring the valve can accurately adjust the fuel supply volume according to the engine's working conditions.

Made from high-strength, corrosion-resistant aluminum alloy with surface anti-corrosion treatment, it withstands operating temperatures from -55°C to 180°C and long-term mechanical load. Weighing 0.42kg, it allows fast inspection and fitting testing during fuel system MRO overhauls. FAA Part 25 certified, it is a key component for fuel system operational stability.