AIRCRAFT LANDING GEAR ASSEMBLY INCLUDING A HEALTH AND USAGE MONITORING SYSTEM (HUMS) AND METHOD

摘要

A health and monitoring system or "HUMS" (20a, 20b) mounted within a hollow structural subassembly (12) of an aircraft landing gear assembly (10), the subassembly having an access port (16) for access to the HUMS without requiring disassembly of the structural subassembly so as to require jacking up the aircraft.