SAE International Primary Flight Control Hydraulic Actuation System Interface Definition AIR4922

Description
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.
Description
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.

Suppliers

Company
Product
Description
Supplier Links
Primary Flight Control Hydraulic Actuation System Interface Definition - AIR4922 - SAE International
Warrendale, PA, United States
Primary Flight Control Hydraulic Actuation System Interface Definition
AIR4922
Primary Flight Control Hydraulic Actuation System Interface Definition AIR4922
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.

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.

Supplier's Site

Technical Specifications

  SAE International
Product Category Standards and Technical Documents
Product Number AIR4922
Product Name Primary Flight Control Hydraulic Actuation System Interface Definition
Unlock Full Specs
to access all available technical data

Similar Products