Stay informed on COVID-19 updates from EASARead more

Investigation of the technical feasibility and safety benefit of an Integrated Engine / Rotor / Transmission Health Monitoring and HOMP System for Part 27 Piston Engine Small Helicopters


This study focuses on the demonstration of the technical feasibility and potential safety benefit from the retrofit of a HOMP / Health Monitoring system to an existing Part 27 small piston engine helicopters.   

An initial prototype system design shall provide flight data storage and retrieval capability. It should also provide pilot/maintenance personnel access to flight and health information and notify of operational exceedances.   

(The report was formally known under the ID  ‘EASA/2007/1’)