This aerospace recommended practice provides a framework and suggested procedures or values for requirements for the design, performance, and test of hydraulically powered servoactuators for use in aircraft flight control systems. The original version of this document was intended for military usage: consequently, the requirements still often reflect such use. However, the basic requirements of this ARP may and should be applicable to commercial usage as well, provided that appropriate considerations are given for the applicable FAR/JAR 25 regulations, hydraulic fluids, and environmental controls. This recommended practice is a guide and surrogate specification for preparing a detail specification for a particular servoactuator application.
SAE ARP 1281C-2002由美国机动车工程师协会 US-SAE 发布于 2002-09-01。
SAE ARP 1281C-2002 在中国标准分类中归属于: V37 操纵系统及其附件,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。
* 在 SAE ARP 1281C-2002 发布之后有更新,请注意新发布标准的变化。
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