A system and method for operating an aircraft. The system includes a health and usage monitoring system (HUMS) system for sensing health and usage data during flight of the aircraft, and a data transmission unit. The data transmission unit retrieves HUMS data from the HUMS system and generates a trigger signal when the retrieved HUMS data meets a selected criterion, the trigger signal being indicative of a condition of the aircraft. In response to the trigger signal, the data transmission unit transmits the retrieved HUMS data to a remote location.
REAL TIME HUMS
ECHTZEIT-HUMS
HUMS EN TEMPS RÉEL
2022-06-15
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
Tema Archive | 1998
|Emerald Group Publishing | 1996
|British Library Conference Proceedings | 1995
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