SAE AIR 5552 : 2015
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
DEVELOPMENT AND QUALIFICATION OF COMPOSITE LANDING GEARS
Hardcopy , PDF
09-21-2020
English
11-09-2015
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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
Gives general guidance for the design considerations, qualification in endurance, strength and fatigue of landing gear using composite components as principle structural elements.
| Committee |
A-5B
|
| DocumentType |
Standard
|
| Pages |
16
|
| PublisherName |
SAE International
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
| FAA AC 23-13 : 2005 | FATIGUE, FAIL-SAFE, AND DAMAGE TOLERANCE EVALUATION OF METALLIC STRUCTURE FOR NORMAL, UTILITY, ACROBATIC, AND COMMUTER CATEGORY AIRPLANES |
| SAE ARP 5644 : 2013(R2019) | LANDING GEAR SHOCK ABSORPTION TESTING OF CIVIL AIRCRAFT |
| SAE AIR 1494 : 1997 | VERIFICATION OF LANDING GEAR DESIGN STRENGTH |
| SAE ARP 1311 : 2015 | LANDING GEAR STRUCTURES AND MECHANISMS |
| FAA AC 20-107 : 2009 | COMPOSITE AIRCRAFT STRUCTURE |
| FAA AC 25.571-1 : 2011 | DAMAGE TOLERANCE AND FATIGUE EVALUATION OF STRUCTURE |
| SAE AIR 5914 : 2014 | LANDING GEAR FATIGUE SPECTRUM DEVELOPMENT FOR PART 25 AIRCRAFT |
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