ARP1281C Actuators: Aircraft Flight Controls, Power Operated, Hydraulic, General Specification For

Reaffirmed

02/23/2024

Features
Issuing Committee
Scope
Content
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.
Rationale
Content
ARP1281C has been reaffirmed to comply with the SAE Five-Year Review policy.
Meta TagsDetails
DOI
https://doi.org/10.4271/ARP1281C
Pages
41
Citation
SAE International Recommended Practice, Actuators: Aircraft Flight Controls, Power Operated, Hydraulic, General Specification For, SAE Standard ARP1281C, Reaffirmed February 2024, Revised September 2002, Issued January 1974, https://doi.org/10.4271/ARP1281C.
Additional Details
Publisher
Published
Feb 23
Product Code
ARP1281C
Content Type
Recommended Practice
Status
Reaffirmed
Language
English

Revisions