9C1140G01 is a precision-manufactured aerospace engine thrust reverser locking linkage component, compliant with AS9100D quality standards and FAA/EASA regulations, designed for large commercial turbofan engines.It serves as the foundational safety structure in the thrust reverser system, locking the thrust reverser cascade vanes in the retracted position during normal flight, and releasing the lock precisely when reverse thrust is engaged. This is critical for preventing accidental reverser deployment that would disrupt flight stability, and ensuring the reverser delivers consistent deceleration performance during landing.

Made from high-strength, corrosion-resistant titanium alloy, it withstands operating temperatures from -55°C to 210°C and long-term mechanical load. Weighing 0.65kg, it allows fast inspection and lock function testing during thrust reverser MRO overhauls. FAA Part 25 certified, it is a key component for flight safety.