Standard

SAE AIR6168A

May 2019 Published

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Language English

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Abstract

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.

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Standard from SAE International
Published: 23 May 2019
Document type: IS
ISBN:

Publisher SAE International
Distributor SAE International

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Refers: SAE ARP6137
Refers: SAE AIR5938
Refers: SAE ARP5908
Replaces: SAE AIR6168
Refers: SAE AIR4830

SAE AIR6168A

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SAE AIR6168A

SAE AIR6168

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SAE AIR6168A

SAE AIR6168

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