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  • SAE AIR 5552 : 2015

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    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    Superseded date:  21-09-2020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

    Publisher:  SAE International

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    Table of Contents - (Show below) - (Hide below)

    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 - (Show below) - (Hide below)

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

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    Committee A-5B
    Document Type Standard
    Publisher SAE International
    Status Superseded
    Superseded By
    Supersedes

    Standards Referencing This Book - (Show below) - (Hide below)

    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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