• SAE AS 8860 : 2012

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    LANDING GEAR STRUCTURAL REQUIREMENTS AS LISTED IN THE MIL-886X SERIES OF SPECIFICATIONS

    Available format(s):  Hardcopy, PDF

    Language(s):  English

    Published date:  10-03-2012

    Publisher:  SAE International

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

    1. SCOPE
    2. APPLICABLE DOCUMENTS
    3. REQUIREMENTS
    4. QUALITY ASSURANCE PROVISIONS
    5. PACKAGING
    6. NOTES

    Abstract - (Show below) - (Hide below)

    Contains landing gear strength and rigidity requirements, which, in combination with other applicable specifications, define the structural design, analysis, test, and data requirements for fixed wing piloted airplanes.

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

    Committee A-5
    Document Type Standard
    Product Note This standard is now stabilized
    Publisher SAE International
    Status Current
    Supersedes

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

    SAE ARP 1311 : 2015 LANDING GEAR STRUCTURES AND MECHANISMS
    SAE AIR 5914 : 2014 LANDING GEAR FATIGUE SPECTRUM DEVELOPMENT FOR PART 25 AIRCRAFT
    SAE ARP 1595 : 2013(R2019) DESIGN AND VERIFICATION OF AIRCRAFT NOSE WHEEL STEERING SYSTEMS

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

    MIL A 8865 : B AIRPLANE STRENGTH AND RIGIDITY MISCELLANEOUS LOADS
    MIL HDBK 5 : G_VOL2 METALLIC MATERIALS AND ELEMENTS FOR AEROSPACE VEHICLE STRUCTURES
    MIL A 8863 : C AIRPLANE STRENGTH AND RIGIDITY GROUND LOADS FOR NAVY ACQUIRED AIRPLANES
    MIL STD 2066 : 0 CATAPULTING AND ARRESTING GEAR FORCING FUNCTIONS FOR AIRCRAFT STRUCTURAL DESIGN
    MIL T 81259 : B TIE DOWN, AIRFRAME DESIGN, REQUIREMENTS FOR
    MIL A 22771 : D ALUMINUM ALLOY FORGINGS, HEAT TREATED
    ANSI Y10.7 : 1954 LETTER SYMBOLS/AERONAUTICAL SCIENCES
    MIL A 8869 : B AIRPLANE STRENGTH AND RIGIDITY NUCLEAR WEAPONS EFFECTS
    MIL A 8870 : C AIRPLANE STRENGTH AND RIGIDITY VIBRATION, FLUTTER, AND DIVERGENCE
    QQ A 367 : H ALUMINUM ALLOY FORGINGS
    MIL STD 2175 : A CASTING, CLASSIFICATION AND INSPECTION OF
    MIL F 7190 : B FORGING, STEEL, FOR AIRCRAFT AND AEROSPACE EQUIPMENT AND SPECIAL ORDNANCE APPLICATIONS
    MIL L 22589 : D LAUNCHING SYSTEM, NOSE GEAR TYPE, AIRCRAFT
    MIL A 8868 : B AIRPLANE STRENGTH AND RIGIDITY DATA AND REPORTS
    MIL A 8867 : C AIRPLANE STRENGTH AND RIGIDITY GROUND TESTS
    MIL T 6053 : C TEST, IMPACT, SHOCK ABSORBER, LANDING GEAR, AIRCRAFT
    MIL A 21180 : D ALUMINUM-ALLOY CASTINGS, HIGH STRENGTH
    MIL A 8861 : B AIRPLANE STRENGTH AND RIGIDITY FLIGHT LOADS
    MIL A 8866 : C AIRPLANE STRENGTH AND RIGIDITY RELIABILITY REQUIREMENTS, REPEATED LOADS, FATIGUE AND DAMAGE TOLERANCE
    MIL A 18717 : C ARRESTING HOOK INSTALLATIONS, AIRCRAFT
    MIL D 8708 : C DEMONSTRATION REQUIREMENTS FOR AIRPLANES
    MIL F 83142 : A FORGING, TITANIUM ALLOYS, PREMIUM QUALITY
    MIL A 8860 : B AIRPLANE STRENGTH AND RIGIDITY GENERAL SPECIFICATION FOR
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