SAE AIR6168
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
Landing Gear Structural Health Monitoring
27-05-2019
12-04-2012
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
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.
| DocumentType |
Standard
|
| PublisherName |
SAE International
|
| Status |
Superseded
|
| SupersededBy |
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 for measuring the forces seen by the landing gear structure, and methods for determining the fatigue state of the landing gear structure. This AIR covers the landing gear structure and shock absorber. It does not include the landing gear systems or landing gear wheels, tires and brakes. Landing gear tire condition and pressure monitoring are detailed in AIR4830 and ARP6137, respectively.
| SAE ARP 6137 : 2015 | TIRE PRESSURE MONITORING SYSTEMS (TPMS) FOR AIRCRAFT |
| SAE ARP5908 | Landing Gear Servicing |
| SAE AIR 4830A : 2016 | AIRCRAFT TIRE PRESSURE MONITORING SYSTEMS |
| SAE AIR5938 | Information on Hard Landings |
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