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SAE AIR 5552 : 2015

Superseded

Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

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superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

DEVELOPMENT AND QUALIFICATION OF COMPOSITE LANDING GEARS

Available format(s)

Hardcopy , PDF

Superseded date

21-09-2020

Language(s)

English

Published date

09-11-2015

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Superseded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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€118.68
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