Browse Standards AIR6168A
Current REVISED 2019-05-23

Landing Gear Structural Health Monitoring AIR6168A

This SAE Aerospace Information Report (AIR) discusses past and present approaches for monitoring the landing gear structure and shock absorber (servicing), opportunities for corrosion detection, methods for transient overload detection, techniques for measuring the forces seen by the landing gear structure, and methods for determining the fatigue state of the landing gear structure. Landing gear tire condition and tire pressure monitoring are detailed in ARP6225, AIR4830, and ARP6137, respectively. Aircraft Brake Temperature Monitoring Systems (BTMS) are detailed in AS1145.
AIR6168A
2019-05-23
Latest
Revised
AIR6168
2012-04-12
Historical
Issued

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