SAE AIR4922 Primary Flight Control Hydraulic Actuation System Interface Definition
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Product Code:SAE AIR4922
Title:Primary Flight Control Hydraulic Actuation System Interface Definition
Issuing Committee:A-6a3 Flight Control Systems Committee
Scope:This SAE Aerospace Information Report (AIR) provides a description of the interfacesand 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.
Title:Primary Flight Control Hydraulic Actuation System Interface Definition
Issuing Committee:A-6a3 Flight Control Systems Committee
Scope:This SAE Aerospace Information Report (AIR) provides a description of the interfacesand 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.
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