• SAE AIR 5914 : 2014

    Superseded A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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    LANDING GEAR FATIGUE SPECTRUM DEVELOPMENT FOR PART 25 AIRCRAFT

    Available format(s):  Hardcopy, PDF

    Superseded date:  03-02-2020

    Language(s):  English

    Published date:  01-01-2014

    Publisher:  SAE International

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

    1. SCOPE
    2. REFERENCES
    3. GENERAL
    4. SERVICE LIFE
    5. GENERAL REQUIREMENTS
    6. LANDING CONDITIONS
    7. GROUND MANEUVERING
    8. FREE EXTENSION/REBOUND (TAKEOFF TRANSITION)
    9. FLIGHT LOADINGS (GUST AND MANEUVERING LOADS)
    10. SUSTAINED ENGINE IMBALANCE CONDITIONS (IE.
        WIND MILLING ENGINE AND BLADE OUT VIBRATION
        CONDITIONS)
    11. EXTENSION, RETRACTION, AND BRAKING WHEELS
        IN AIR
    12. INTERNAL PRESSURES
    13. GROUND-AIRGROUND CYCLES
    14. NOTES

    Abstract - (Show below) - (Hide below)

    Specifies guidelines for the development of landing gear fatigue spectra for the purpose of designing and certification testing of Part 25 landing gear.

    General Product Information - (Show below) - (Hide below)

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    Status Superseded
    Superseded By

    Standards Referenced By This Book - (Show below) - (Hide below)

    SAE AIR 5552 : 2015 DEVELOPMENT AND QUALIFICATION OF COMPOSITE LANDING GEARS

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

    DEFSTAN 00-970(PT1)SEC4/2(1999) : 1999 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - DESIGN AND CONSTRUCTION
    MIL L 8552 : C LANDING GEAR, AIRCRAFT SHOCK ABSORBER [AIR OIL TYPE]
    MIL S 8812 : D STEERING SYSTEM, AIRCRAFT GENERAL REQUIREMENTS FOR
    MIL A 8866 : C AIRPLANE STRENGTH AND RIGIDITY RELIABILITY REQUIREMENTS, REPEATED LOADS, FATIGUE AND DAMAGE TOLERANCE
    SAE AIR 1489 : 2012 AEROSPACE LANDING GEAR SYSTEMS TERMINOLOGY
    SAE AS 8860 : 2012 LANDING GEAR STRUCTURAL REQUIREMENTS AS LISTED IN THE MIL-886X SERIES OF SPECIFICATIONS
    SAE ARP 1383 : 2013 AEROSPACE - IMPULSE TESTING OF HYDRAULIC COMPONENTS
    SAE ARP 5429 : 2017 LANDING GEAR FATIGUE TESTS WITH EQUIVALENT DAMAGE SPECTRA
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