Logo

SAE AIR5913 Rev A

Current Revision

Landing Gear Component Heat Damage

$103.00

$103.00

$185.40


Sub Total (1 Item(s))

$ 0.00

Estimated Shipping

$ 0.00

Total (Pre-Tax)

$ 0.00


Document Preview Not Available...

The purpose of this report is to outline types of in-service heat damage that have been observed in high strength steel landing gear components, with an emphasis on a particular type that is referred to as “Ladder Cracking” which can develop in landing gear shock struts. The report discusses how ladder cracking can be detected visually and evaluated by non-destructive inspection methods, and how it can be repaired at overhaul with the prior approval of the Original Equipment Manufacturer. This report also describes the use of a bearing material that has resolved this problem without introducing other problems. Examples of other types of service induced heat damage are also discussed.

SDO SAE: SAE International
Document Number AIR5913
Publication Date July 2, 2018
Language en - English
Page Count 15
Revision Level A
Supercedes
Committee
Publish Date Document Id Type View
July 2, 2018 AIR5913A Revision
Feb. 7, 2011 AIR5913 Revision