AIR4922A: Primary Flight Control Hydraulic Actuation System Interface Definition - Information Report

Features

Issuing Committee: A-6A3 Flight Control and Vehicle Management Systems Cmt

Scope

Content: This SAE Aerospace Information Report (AIR) provides a description of the interfaces and their requirements for generic and specific hydraulic actuation systems used in the flight control systems of manned aircraft. Included are the basic control system characteristics and functional requirements, and the essential interfaces (structural, mechanical, hydraulic power, control input, status monitoring, and environment). Major design issues, requirements, and other considerations are presented and discussed.

Rationale

Content: This document contains information addressing aspects of technology that are not currently undergoing substantial development.

Meta Tags

Topics: Failure modes and effects analysis
Flight control actuators
Fly-by-wire control systems
Flight control systems
Control systems
Fiber optics
Electronic equipment

Details

DOI: https://doi.org/10.4271/AIR4922A

Pages: 1

Citation: SAE International Information Report, Primary Flight Control Hydraulic Actuation System Interface Definition, SAE Standard AIR4922A, Stabilized October 2015, Reaffirmed July 2008, Issued October 1996, https://doi.org/10.4271/AIR4922A.

Additional Details

Publisher: SAE International

Published: Oct 19, 2015

Product Code: AIR4922A

Content Type: Information Report

Status: Stabilized

Language: English

Historical