SAE AIR 6168 : 2012

SAE AIR 6168 : 2012

LANDING GEAR STRUCTURAL HEALTH MONITORING

SAE International

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Table of Contents

1. SCOPE
2. APPLICABLE DOCUMENTS
3. LANDING GEAR SHOCK ABSORBER MONITORING
4. CORROSION
5. LANDING GEAR TRANSIENT OVERLOAD DETECTION
6. LANDING GEAR FATIGUE MONITORING
7. SUMMARY
8. NOTES
APPENDIX A - ABBREVIATIONS

Abstract

Specifies past and present approaches for monitoring the landing gear structure and shock absorber, 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.

General Product Information

Document Type Standard
Status Current
Publisher SAE International
Committee A-5B

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