AIR5913A Landing Gear Component Heat Damage

Reaffirmed

11/16/2023

Features
Issuing Committee
Scope
Content
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.
Meta TagsDetails
DOI
https://doi.org/10.4271/AIR5913A
Pages
15
Citation
SAE International Information Report, Landing Gear Component Heat Damage, SAE Standard AIR5913A, Reaffirmed November 2023, Revised July 2018, Issued February 2011, https://doi.org/10.4271/AIR5913A.
Additional Details
Publisher
Published
Nov 16, 2023
Product Code
AIR5913A
Content Type
Information Report
Status
Reaffirmed
Language
English

Revisions