A health and monitoring system or “HUMS” mounted within a hollow structural subassembly of an aircraft landing gear assembly, the subassembly having an access port for access to the HUMS without requiring disassembly of the structural subassembly so as to require jacking up the aircraft.
AIRCRAFT LANDING GEAR ASSEMBLY INCLUDING A HEALTH AND USAGE MONITORING SYSTEM (HUMS) AND METHOD
27.04.2017
Patent
Elektronische Ressource
Englisch
Aircraft landing gear assembly including a health and usage monitoring system (HUMS) and method
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