SAE AIR 5552 : 2015

Table of Contents

1. SCOPE
2. REFERENCES
3. APPROACH
4. REQUIREMENTS
5. DEVELOPMENT APPROACH
6. DAMAGE TOLERANCE
7. THREAT ASSESSMENT
8. MATERIAL AND PROCESS CHARACTERISATION
9. COMPONENT DESIGN
10. HYBRID ASSEMBLY
11. COMPONENT TESTING
12. CONTINUING AIRWORTHINESS

Abstract

Gives general guidance for the design considerations, qualification in endurance, strength and fatigue of landing gear using composite components as principle structural elements.

General Product Information

Published
Document Type	Standard
Status	Current
Publisher	SAE International
Pages
ISBN
Committee	A-5B