956A1228G04 is a precision-manufactured aerospace engine high-pressure fuel manifold, compliant with AS9100D quality standards and FAA/EASA regulations, optimized for CFM56 and IAE V2500 turbofan engines. It distributes pressurized fuel evenly to each fuel injector nozzle in the combustion system, ensuring consistent fuel supply for stable, efficient combustion, and supporting balanced thrust output across idle, climb, cruise, and takeoff phases.

Made from corrosion-resistant stainless steel with precision-machined fuel distribution ports, it withstands fuel pressures up to 6,200 psi and operating temperatures from -55°C to 160°C. Weighing 1.2kg with a modular welded structure and threaded connection interfaces, it enables fast inspection and replacement during fuel system MRO overhauls. FAA Part 25 certified, it is a core component for fuel system stability and engine performance.