SAE AIR 6168 : 2012

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

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