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SAE AIR 5913A:2018-07-02
New product
SAE AIR 5913A:2018-07-02
Landing Gear Component Heat DamageMore info
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.
| Author | SAE |
|---|---|
| Editor | SAE |
| Document type | Standard |
| Format | File |
| ICS | 49.045 : Structure and structure elements
|
| Number of pages | 15 |
| Replace | SAE AIR 5913:2016-11-11 |
| Set | AEROPAKS10U-10 |
| Year | 2018 |
| Document history | SAE AIR 5913:2016-11-11 |
| Country | USA |
| Keyword | SAE 5913;SAE AIR5913A;SAE AIR5913A;SAE AIR 5913 |