Landing Gear Structural Health Monitoring

Standard:
Issued:
  • 2012-04-12
 
  • CURRENT
Publisher:
  • SAE International
Pages:
16
Scope:

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.

Rationale:

This SAE Aerospace Information Report (AIR) has been written to provide a review of the state-of-the-art of landing gear structural health monitoring. The document is intended to augment the work of the SAE G-11SHM by extending the airframe structural health monitoring concept to the particulars of the landing gear. The purpose of this AIR is to objectively discuss and summarize historic as well as current state-of-the-art landing gear structural health monitoring technologies.

History:
Standard Published Revision Status
AIR6168 2012-04-12 Latest Issued
Access
Now
SAE MOBILUS Subscriber? You may already have access.
Buy
Select
Price
List
Download
$76.00
Add
Mail
$76.00
Members save up to 18% off list price.
Grade
If you are currently using this technical report:
Share
HTML for Linking to Page
Page URL

Related Items

Article
2016-12-08
Technical Paper / Journal Article
2010-10-19
Training / Education
2017-11-13
Training / Education
2013-02-20
Technical Paper / Journal Article
2010-10-19
Training / Education
2017-11-14
Standard
1995-03-01