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SAE AIR6168A : 2019

Landing Gear Structural Health Monitoring

Standard Details

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.

Cross Reference: AIR4830,AIR5938,ARP5908,ARP6137

General Information

Status : Revised
Standard Type: Main
Document No: SAE AIR6168A : 2019
Document Year: 2019
Pages: 16

Life Cycle

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Revised
SAE AIR6168A : 2019
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