• MIL A 8866 : C

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    AIRPLANE STRENGTH AND RIGIDITY RELIABILITY REQUIREMENTS, REPEATED LOADS, FATIGUE AND DAMAGE TOLERANCE

    Available format(s):  Hardcopy, PDF

    Language(s): 

    Published date: 

    Publisher:  US Military Specs/Standards/Handbooks

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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)

    Describes strength and rigidity requirements for repeated loading condition applicable to Navy procured airplanes.

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

    Committee FSC 1510
    Development Note Partially Supersedes MIL A 008866 (B). C NOTICE 1 - Notice of Validation. (06/2004)
    Document Type Standard
    Product Note NEW CHILD NOT 2 2019 IS NOW ADDED<br>
    Publisher US Military Specs/Standards/Handbooks
    Status Current

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

    MIL A 8860 : B AIRPLANE STRENGTH AND RIGIDITY GENERAL SPECIFICATION FOR
    SAE AIR 5914 : 2014 LANDING GEAR FATIGUE SPECTRUM DEVELOPMENT FOR PART 25 AIRCRAFT
    MIL HDBK 2066 : 0 CATAPULTING AND ARRESTING GEAR FORCING FUNCTIONS FOR AIRCRAFT STRUCTURAL DESIGN
    SAE AS 8860 : 2012 LANDING GEAR STRUCTURAL REQUIREMENTS AS LISTED IN THE MIL-886X SERIES OF SPECIFICATIONS
    MIL HDBK 244 : A GUIDE TO AIRCRAFT - STORES COMPATIBILITY
    MIL A 83444 : 0 AIRPLANE DAMAGE TOLERANCE REQUIREMENTS
    MIL STD 1763 : A AIRCRAFT STORES CERTIFICATION PROCEDURES
    MIL A 8870 : C AIRPLANE STRENGTH AND RIGIDITY VIBRATION, FLUTTER, AND DIVERGENCE
    MIL A 8867 : C AIRPLANE STRENGTH AND RIGIDITY GROUND TESTS
    MIL STD 2066 : 0 CATAPULTING AND ARRESTING GEAR FORCING FUNCTIONS FOR AIRCRAFT STRUCTURAL DESIGN
    MIL A 8868 : B AIRPLANE STRENGTH AND RIGIDITY DATA AND REPORTS
    MIL DTL 9490 : E FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR
    JSSG 2006 : 0 JOINT SERVICE SPECIFICATION GUIDE - AIRCRAFT STRUCTURES
    MIL A 8861 : B AIRPLANE STRENGTH AND RIGIDITY FLIGHT LOADS
    ADS-13F-HDBK : 1997 AERONAUTICAL DESIGN STANDARD - HANDBOOK - AIR VEHICLE MATERIALS AND PROCESSES
    MIL HDBK 1763 : 0 AIRCRAFT/STORES COMPATIBILITY: SYSTEMS ENGINEERING DATA REQUIREMENTS AND TEST PROCEDURES
    MIL A 8892 : 0 AIRPLANE STRENGTH AND RIGIDITY, VIBRATION

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

    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 A 8870 : C AIRPLANE STRENGTH AND RIGIDITY VIBRATION, FLUTTER, AND DIVERGENCE
    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 A 8861 : B AIRPLANE STRENGTH AND RIGIDITY FLIGHT LOADS
    MIL D 8708 : C DEMONSTRATION REQUIREMENTS FOR AIRPLANES
    MIL A 8860 : B AIRPLANE STRENGTH AND RIGIDITY GENERAL SPECIFICATION FOR
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