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SAE AIR6168

(R) Landing Gear Structural Health Monitoring

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Organization: SAE
Publication Date: 1 May 2019
Status: active
Page Count: 16
scope:

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.

Document History

SAE AIR6168
May 1, 2019
(R) Landing Gear Structural Health Monitoring
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,...
April 1, 2012
Landing Gear Structural Health Monitoring
This SAE Aerospace Information Report (AIR) discusses past and present approaches for monitoring the landing gear structure and shock absorber, methods for transient overload detection, techniques...

References

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