9426M22G08 is a high-reliability aerospace engine vibration sensor, engineered to AS9100D quality standards and RTCA DO-160G specifications, optimized for narrow-body aircraft turbofan engines (e.g., CFM56-5B/7, IAE V2500). It monitors real-time vibration amplitudes and frequencies of critical rotating components (compressor/turbine rotors, gearboxes), providing early fault warnings to prevent catastrophic engine failures during flight and ground operations.

Constructed from heat-resistant nickel alloy with hermetic sealing, it operates stably across -55°C to 300°C, features ±2% measurement accuracy, and resists high-frequency mechanical shocks. Lightweight at 0.1kg with threaded mounting probes, it integrates seamlessly into engine casings. FAA/EASA compliant, it enhances predictive maintenance efficiency and upholds long-term engine operational safety for commercial fleets.