956A7629G01 is a precision-engineered aerospace engine high-pressure fuel manifold, compliant with AS9100D quality standards and FAA/EASA regulations, optimized for CFM56-5B/7 and IAE V2500 turbofan engines. It evenly distributes pressurized fuel to individual injectors, ensuring consistent fuel-air mixing in the combustion chamber, which is critical for stable combustion, reduced emissions, and optimal thrust output across idle, cruise, and takeoff phases.

Constructed from corrosion-resistant titanium alloy with precision-machined fuel passages, it withstands operating pressures up to 6,000 psi and temperatures ranging from -55°C to 150°C. Weighing 0.85kg with a modular bolt-on design, it enables fast disassembly and replacement during fuel system MRO services. FAA Part 25 certified, it is a core component for fuel delivery accuracy and engine operational reliability.