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SAE AIR5913

(R) Landing Gear Component Heat Damage

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Organization: SAE
Publication Date: 1 July 2018
Status: active
Page Count: 15
scope:

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 nondestructive 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.

Document History

July 1, 2018
(R) Landing Gear Component Heat Damage
A description is not available for this item.
SAE AIR5913
July 1, 2018
(R) Landing Gear Component Heat Damage
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...
June 1, 2018
(R) Landing Gear Component Heat Damage
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...
February 1, 2011
Landing Gear Shock Strut Heat Damage
INTRODUCTION The purpose of this report is to outline the type of damage referred to as "Ladder Cracking". Discuss how it is being repaired and describe the use of a bearing material that has...
February 1, 2011
Landing Gear Shock Strut Heat Damage
The purpose of this report is to outline the type of damage referred to as “Ladder Cracking”. Discuss how it is being repaired and describe the use of a bearing material that has resolved this...

References

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