Size (CM): 193*135*106

Weright (KG): 250

J53003-236 is a precision-engineered aerospace engine high-pressure compressor (HPC) blade retainer clip, compliant with AS9100D quality standards and FAA/EASA regulations, optimized for CFM56 and IAE V2500 turbofan engines. It secures the HPC blades in the disk's dovetail slots, preventing blade shifting or detachment during the compressor's high-speed rotation (up to 18,000 RPM), which is critical for maintaining stable air compression, avoiding component collision, and ensuring consistent engine performance across all flight phases.

Made from a high-strength, heat-resistant nickel-chromium alloy, it withstands operating temperatures up to 720°C and intense centrifugal forces. Weighing 0.02kg with a spring-loaded locking design, it allows for quick installation and visual inspection during compressor MRO overhauls. FAA Part 25 certified, it is a safety-critical small component for HPC structural integrity.