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  • SBAC TS 120 : 6

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    AGS2000 SERIES STIFFNUTS (INCLUDING CLINCH NUTS) BA & BSF THREADS FOR AIRCRAFT

    Available format(s):  Hardcopy, PDF

    Language(s):  English

    Published date:  01-05-2014

    Publisher:  SAE Industry Technologies Consortia

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

    FOREWORD
    1. BACKGROUND
    2. SCOPE
    3. ASSOCIATED DOCUMENTS
    4. LIST OF TABLES
    5. LIST OF FIGURES
    SECTION ONE: GENERAL REQUIREMENTS
    6 DEFINITIONS
    7 DESIGN AND DIMENSIONS
    8 MATERIAL AND MANUFACTURE
    9 FREEDOM FROM DEFECT
    10 PROTECTIVE COATING
    11 SCREW THREADS
    12 SQUARENESS OF FACE TO THREAD
    13 IDENTIFICATION AND MARKING
    SECTION TWO: INSPECTION AND TESTING
    14 QUALIFICATION PROCEDURE
    15 PRODUCTION BATCH ACCEPTANCE
    16 INSPECTION OF SAMPLES
    17 TESTING OF SAMPLES
    18 TEST BOLTS
    19 TORQUE TEST
    20 BOLT TOLERANCE TEST
    21 ENDURANCE TEST
    22 TORSIONAL STRENGTH TEST
    23 THRUST TEST
    24 HIGH TEMPERATURE TORQUE TEST
    25 LOW TEMPERATURE TORQUE TEST
    26 CLINCHING TEST FOR CLINCH NUTS
    APPENDIX A: EQUIPMENT FOR TESTING STIFFNUTS
    APPENDIX B: FITTING AND TESTING OF CLINCH NUTS
    APPENDIX C: MATERIALS FOR STIFFNUTS AND CLINCH NUTS

    Abstract - (Show below) - (Hide below)

    Describes the dimensions, material, finish, testing and identification of aircraft stiffnuts with BA and BSF threads.

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

    Development Note Amendment Record is available separately, see SBAC TS 120 AR. (05/2014)
    Document Type Standard
    Product Note New child AR 2014 is added
    Publisher SAE Industry Technologies Consortia
    Status Current
    Supersedes

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

    DEFSTAN 00-970(PT1)SEC4/7(2011) : 2011 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 4: DESIGN AND CONSTRUCTION
    DEFSTAN 00-970(PT1)SEC4/14(2015) : 2015 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 4: DESIGN AND CONSTRUCTION
    DEFSTAN 00-970(PT1)SEC4/12(2014) : 2014 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 4: DESIGN AND CONSTRUCTION
    DEFSTAN 00-970(PT1)SEC4/6(2010) : 2010 DESIGN AND AIRWORTHINESS REQUIREMENTS FORD SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 4: DESIGN AND CONSTRUCTION
    DEFSTAN 00-970(PT1)SEC4/13(2015) : 2015 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 4: DESIGN AND CONSTRUCTION
    DEFSTAN 00-970(PT7)SEC2/SUPP4/6(2015) : 2015 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SUPPLEMENT 4: DESIGN AND CONSTRUCTION (SUBPART D)

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

    DEFSTAN 91-114/1(2003) : 2003 LUBRICATING OIL, AIRCRAFT CONTROLS: ANTIFREEZING JOINT SERVICE DESIGNATION: OM-150
    DEFSTAN 03-25/5(2008) : 2008 SULFURIC ACID ANODIZING OF ALUMINIUM AND ALUMINIUM ALLOYS
    BS 2A 61:1962 Specification for aluminium alloy hexagonal headed bolts (B.A. and B.S.F. threads) for aircraft
    BS EN 2133:2010 Aerospace series. Cadmium plating of steels with specified tensile strength 1450 MPa, copper, copper alloys and nickel alloys
    BS 84:2007 Parallel screw threads of Whitworth form. Requirements
    BS 2A 25:1962 Specification for steel hexagonal-headed bolts (B.A. and B.S.F. threads) for aircraft
    DEFSTAN 03-19/4(2010) : 2010 ELECTRO-DEPOSITION OF CADMIUM
    DEFSTAN 80-217/1(2002) : 2002 CORROSION PREVENTIVE COMPOUND: SOFT FILM, COLD APPLICATION NATO CODE: C-614 JOINT SERVICES DESIGNATION: PX-1
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