SAE ARP1084-1969
运行中零部件的液压外部泄漏

Hydraulic External Leakage for In-Service Components

作废

SAE ARP1084-1969 发布历史

The purpose of this document is to provide guide lines for allowable leakage for in-service aircraft hydraulic components at a nominal 100 F temperature and to outline the procedure for measuring such leakage. The limits to be applied to any specific aircraft should be adjusted before inclusion in a maintenance manual. Leakage as hereafter referred to in this document shall mean external leakage. The allowable leakage for hydraulic components has been documented in various military specifications concerning components. The leakage requirements given in the military specifications are intended in part to control the quality, assembly and proper functioning of the components. However, components that are in service sometimes develop leakage rates in excess of the specified amount. The does not necessarily imply that the components have degraded to a degree that they no longer provide reliable operation or that they would be detrimental to the system. The intent of this ARP is to establish a level of allowable leakage that will be applicable only to in-service hydraulic components. It is hoped that this will result in minimizing what is often the unnecessary removal of hydraulic components from an aircraft.

SAE ARP1084-1969由美国机动车工程师协会 US-SAE 发布于 1969-01-01。

SAE ARP1084-1969 在中国标准分类中归属于: V29 航天用液压元件与附件，在国际标准分类中归属于: 49.080 航空航天用流体系统和零部件。

SAE ARP1084-1969的历代版本如下：

• 1969年 SAE ARP1084-1969 运行中零部件的液压外部泄漏

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标准号

SAE ARP1084-1969

发布

1969年

发布单位

美国机动车工程师协会

 

 

代替标准

SAE ARP 1084A-2013

适用范围

The purpose of this document is to provide guide lines for allowable leakage for in-service aircraft hydraulic components at a nominal 100 F temperature and to outline the procedure for measuring such leakage. The limits to be applied to any specific aircraft should be adjusted before inclusion in a maintenance manual. Leakage as hereafter referred to in this document shall mean external leakage. The allowable leakage for hydraulic components has been documented in various military specifications concerning components. The leakage requirements given in the military specifications are intended in part to control the quality, assembly and proper functioning of the components. However, components that are in service sometimes develop leakage rates in excess of the specified amount. The does not necessarily imply that the components have degraded to a degree that they no longer provide reliable operation or that they would be detrimental to the system. The intent of this ARP is to establish a level of allowable leakage that will be applicable only to in-service hydraulic components. It is hoped that this will result in minimizing what is often the unnecessary removal of hydraulic components from an aircraft.

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