956A3111G01 is a high-precision aerospace engine component adhering to AS9100D standards and FAA/EASA regulations, mainly applied to aircraft turbine engine combustion systems. It functions as a heat-resistant alloy nozzle insert, responsible for guiding and atomizing fuel before injection into the combustion chamber. Forged from MA956 oxide dispersion - strengthened alloy, it endures temperatures up to 1200°C, resisting oxidation and creep even under extreme heat. Its precision - drilled flow channels ensure uniform fuel atomization, boosting combustion efficiency and reducing emissions. With an anti - wear coating, it withstands long-term fuel erosion and mechanical vibration without deformation. Compact and lightweight, it fits seamlessly into engine combustion chambers, maintaining stable performance to support reliable engine operation and enhance overall flight safety.