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SAE ARP1281 Rev C

Current Revision

Actuators: Aircraft Flight Controls, Power Operated, Hydraulic, General Specification For

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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 conditions.

SDO SAE: SAE International
Document Number ARP1281
Publication Date Sept. 12, 2002
Language en - English
Page Count 41
Revision Level C
Supercedes
Committee
Publish Date Document Id Type View
Sept. 12, 2002 ARP1281C Revision
May 1, 1993 ARP1281B Revision
Nov. 1, 1991 ARP1281A Revision
Jan. 1, 1974 ARP1281 Revision