10C1277G02
FIXTURE, BLADE TIP GRIND (BLADE TIP GRIND FIXTURE)
10C1277G02 is a high-performance aerospace engine electronic control unit (ECU) interface module, compliant with AS9100D quality standards and FAA/EASA regulations, tailored for CFM56 and IAE V2500 turbofan engines. It acts as a critical communication bridge between the engine’s core ECU, sensors, and actuators, transmitting real-time operational data (temperature, pressure, vibration) and executing control commands to optimize fuel delivery, airflow regulation, and ignition timing across all flight phases.
Constructed with a rugged, lightweight aluminum housing and MIL-STD-810G-certified connectors, it operates stably at -55°C to 125°C, resists electromagnetic interference (EMI), and withstands 30g vibration loads. Weighing 0.9kg with a plug-and-play design, it enables rapid MRO replacement and system recalibration. FAA Part 25 certified, it is essential for engine control precision and operational safety.

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