
Helicopter rotor MRO testing
- Case objective: Instrument main‑rotor mast and tail‑rotor drive for real‑time torque/strain and gearbox vibration to validate lubrication changes and maintenance intervals—no drilling on flight‑critical structural hardware.
- Other information: Clamp‑on collars and protective fairings withstand rotor wash and FOD risks. Battery or inductive power depending on ground‑run vs tethered tests. Live order tracking to identify gear‑mesh anomalies before they escalate. Integrates with fleet‑maintenance analytics via Ethernet/USB exports.