SAE AIR4922A
Current
The latest, up-to-date edition.
Primary Flight Control Hydraulic Actuation System Interface Definition
Hardcopy , PDF
English
19-10-2015
FOREWORD
1. SCOPE
2. REFERENCES
3. TYPES OF INTERFACES
4. REQUIREMENTS FOR INTERFACES
5. INTERFACE DESIGN ISSUES
6. INTERFACE PROBLEMS/SOLUTIONS (LESSONS
LEARNED)
7. INTERFACE DEVELOPMENT/VALIDATION
8. APPLICATIONS OF ACTUATION SYSTEM FEATURES
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.
| DocumentType |
Standard
|
| Pages |
50
|
| ProductNote |
THIS STANDARD IS NOW STABILIZED
|
| PublisherName |
SAE International
|
| Status |
Current
|
| Supersedes |
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.
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