SAE AS 6053A-2012
航空器减震器起落架的冲击试验

Tests, Impact, Shock Absorber Landing Gear, Aircraft

SAE AS 6053A-2012 发布历史

This document has been declared "Stabilized" and will no longer be subjected to periodic reviews for currency. Users are responsible for verifying references and continued suitability or technical requirements. New technology may exist. This specification covers definition of landing impact tests which are to be conducted on landing gear assemblies including shock absorbers, suggested instrumentation for the tests and required data of the resulting test report. It is intended to standardize impact test procedures on landing gear shock absorbers and to provide sufficient data to allow evaluation of the design with respect to requirements of MIL-L-8552 and MI

SAE AS 6053A-2012由美国机动车工程师协会 US-SAE 发布于 2012-10-04。

SAE AS 6053A-2012 在中国标准分类中归属于: V42 起飞着陆装置，在国际标准分类中归属于: 49.045 结构和结构元件。

SAE AS 6053A-2012的历代版本如下：

• 2012年10月04日 SAE AS 6053A-2012 航空器减震器起落架的冲击试验

SAE AS 6053A-2012 航空器减震器起落架的冲击试验 由 SAE AS 6053-2001 变更而来。

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标准号

SAE AS 6053A-2012

发布日期

2012年10月04日

实施日期

废止日期

无

中国标准分类号

V42

国际标准分类号

49.045

发布单位

US-SAE

引用标准

MIL-A-8860 MIL-A-8863 MIL-A-8868 MIL-L-8552 MIL-S-8698 MIL-S-8959 MIL-STD-831

被代替标准

SAE AS 6053-2001

适用范围

This document has been declared "Stabilized" and will no longer be subjected to periodic reviews for currency. Users are responsible for verifying references and continued suitability or technical requirements. New technology may exist. This specification covers definition of landing impact tests which are to be conducted on landing gear assemblies including shock absorbers, suggested instrumentation for the tests and required data of the resulting test report. It is intended to standardize impact test procedures on landing gear shock absorbers and to provide sufficient data to allow evaluation of the design with respect to requirements of MIL-L-8552 and MI