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  • DEFSTAN 00-970(PT7)SEC5/2(2007) : 2007

    Withdrawn A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.
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    DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 5: AERO-ELASTICITY AND VIBRATION

    Available format(s):  Hardcopy, PDF

    Withdrawn date:  30-09-2014

    Language(s):  English

    Published date:  01-01-2007

    Publisher:  UK Ministry of Defence Standards

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

    LEAFLET 500 AERO-ELASTICITY
    LEAFLET 501 VIBRATION AND INTERNAL NOISE
    APPENDIX No 1 - Not Issued
    APPENDIX No 2 - U.S. MILITARY SPECIFICATIONS,
                    STANDARDS AND HANDBOOKS

    Abstract - (Show below) - (Hide below)

    Describes requirements concerned with: - The control of flutter, divergence, ground and air resonance and allied aero-elastic and aero-mechanical self-excited phenomena, - The restriction of structural distortion of the rotors, control systems and airframe within limits that will not dangerously impair stability and control.

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    Development Note Supersedes DEFSTAN 00-970(PT7)SEC5/1(2006). (03/2007)
    Document Type Standard
    Publisher UK Ministry of Defence Standards
    Status Withdrawn
    Supersedes

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

    ISO 2631:1978 Guide for the evaluation of human exposure to whole-body vibration
    SAE J 1013 : 1992 MEASUREMENT OF WHOLE BODY VIBRATION OF THE SEATED OPERATOR OF OFF-HIGHWAY WORK MACHINES
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