• BS 2G 232:1987

    Current The latest, up-to-date edition.

    Specification for electric cables for general airframe or equipment interconnect use (135°C), wrapped insulation

    Available format(s):  Hardcopy, PDF

    Language(s):  English

    Published date:  30-09-1987

    Publisher:  British Standards Institution

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

    Foreword
    Committees responsible
    Specification
    1. Scope
    2. Classification
    3. Construction
    4. Designation and marking
    5. Packaging and labelling
    6. Tests
    7. Reference samples
    Tables
    1. Type 01, class 1: single-core unscreened
         interconnect cables (135 deg C)
    2. Type 02, class 1: single-core unscreened airframe
         cables (135 deg C)
    3. Type 01, classes 2, 3 and 4: multi-core unscreened,
         twisted interconnect cables without jackets
         (135 deg C)
    4. Type 02, classes 2, 3 and 4: multi-core unscreened,
         twisted airframe cables without jacket (135 deg C)
    5. Type 03, classes 2, 3 and 4: multi-core unscreened,
         twisted interconnect cables with jacket (135 deg C)
    6. Type 04, classes 2, 3 and 4: multi-core unscreened,
         twisted airframe cables with jacket (135 deg C)
    7. Type 05, classes 1, 2, 3 and 4: single-core screened
         with jacket, interconnect cables (135 deg C)
    8. Type 06, classes 1, 2, 3 and 4: single-core screened
         with jacket, and multi-core twisted and screened
         with jacket, airframe cables (135 deg C)
    9. Test application
    10. Specific test parameters
    11. Current ratings in amperes for general purpose
         135 deg C airframe cable
    Figure
    1. Variation of resistance of copper with temperature

    Abstract - (Show below) - (Hide below)

    Specifies the construction and performance requirements for a range of lightweight cables with wrapped insulation suitable for general airframe use in the size range 26 to 0000, and for equipment interconnect in the size range 26 to 18.

    Scope - (Show below) - (Hide below)

    This British Standard specifies construction and performance requirements for a range of lightweight cables with wrapped insulation suitable for general airframe use in the size range 26 to 0000, and for equipment interconnect in the size range 26 to 18. The following types of cable are specified. The cables are suitable for continuous use where the maximum stabilized conductor temperature does not exceed 135 °C. They are suitable for applications involving flexing at temperatures down to – 65 °C. The cables are suitable for use where the potential between conductors or between a conductor and screen, or the aircraft structure, does not exceed 600 V r.m.s. and the frequency does not exceed 2 000 Hz. Interconnect cables are suitable for use in areas with some physical protection, such as behind panels or bulkheads. They also have an application for the internal wiring of equipment. Airframe cables are of sufficiently robust construction to be used for open aircraft wiring. The short-term and long-term current ratings for the cables are specified in this standard. NOTE The titles of the publications referred to in this standard are listed on the inside back cover.

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

    Committee ACE/6
    Development Note Supersedes BS G232(1984) and 85/71991 DC (11/2003) Reviewed and confirmed by BSI, December 2012. (11/2012)
    Document Type Standard
    Publisher British Standards Institution
    Status Current
    Supersedes

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

    DEFSTAN 00-970(PT1)SEC6/4(2006) : 2006 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: COMBAT A/C - SECTION 6: EQUIPMENT
    DEFSTAN 00-970(PT7)SEC7/1(2006) : 2006 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 7: INSTALLATIONS
    DEFSTAN 00-970(PT1)SEC6/15(2015) : 2015 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT
    DEFSTAN 00-970(PT1)SEC6/12(2014) : 2014 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT
    DEFSTAN 00-970(PT1)SEC6/11(2013) : 2013 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT
    DEFSTAN 00-970(PT1)SEC6/9(2012) : 2012 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6 - EQUIPMENT
    DEFSTAN 00-970(PT1)SEC6/5(2007) : 2007 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: COMBAT AIRCRAFT - SECTION 6: EQUIPMENT
    DEFSTAN 00-970(PT1)SEC6/10(2013) : 2013 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT
    DEFSTAN 00-970(PT1)SEC6/8(2011) : 2011 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6 - EQUIPMENT
    DEFSTAN 00-970(PT1)SEC6/7(2011) : 2011 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT
    BS G 246:1991 Specification for cable ties for installation under controlled tension on aircraft electric cable harnesses
    DEFSTAN 00-970(PT1)SEC6/16(2016) : 2016 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT

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

    BS G 230:1984 Specification for general requirements for aircraft electrical cables (second series)
    BS G 231:1983 Specification for conductors for general purpose aircraft electrical cables and aerospace applications
    BS 3G 100-2.3.13:1973 Specification for general requirements for equipment for use in aircraft. All equipment. Environmental conditions Resistance to fire in designated fire zones
    BS G 229:1982 Schedule for environmental conditions and test procedures for airborne equipment
    BS 2011-2.1T:1981 Environmental testing. Tests Test T. Soldering
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