856A4002G01
FUEL NOZZLE, MANIFOLD LEAK CHECK
Size (CM): 99*99*15
Weright (KG): 13.6
856A4002G01 is a precision aerospace engine tool, a dedicated alignment fixture for turbine rotor stages, tailored for turbofan engines like CFM56 and V2500. It ensures accurate stacking, pitch, and axial positioning of rotor blades and disks during assembly/overhaul, critical for balanced rotation, reduced vibration, and optimal airflow through the turbine section.
Made from high-strength aerospace alloy with wear-resistant finish, it maintains dimensional stability under high mechanical stress and engine bay temperatures, adhering to SAE AS9100 and OEM specs. Its precision locating pins, clamping jaws, and quick-lock design minimize human error and streamline workflow.
Compact and easy to operate, it shortens overhaul time, boosts assembly consistency, and safeguards engine performance, fuel efficiency, and long-term reliability—vital for commercial aircraft airworthiness and safe flight operations.

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