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’)
