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  <FDSYS>
    <CFRTITLE>14</CFRTITLE>
    <CFRTITLETEXT>Aeronautics and Space</CFRTITLETEXT>
    <VOL>1</VOL>
    <DATE>1999-01-01</DATE>
    <ORIGINALDATE>1999-01-01</ORIGINALDATE>
    <COVERONLY>false</COVERONLY>
    <TITLE>Electrical system fire protection.</TITLE>
    <GRANULENUM>23.1359</GRANULENUM>
    <HEADING>Section 23.1359</HEADING>
    <ANCESTORS>
      <PARENT HEADING="" SEQ="6"/>
      <PARENT HEADING="" SEQ="5"/>
      <PARENT HEADING="SUBCHAPTER C" SEQ="4">AIRCRAFT</PARENT>
      <PARENT HEADING="PART 23" SEQ="3">AIRWORTHINESS STANDARDS: NORMAL, UTILITY, ACROBATIC, AND COMMUTER CATEGORY AIRPLANES</PARENT>
      <PARENT HEADING="" SEQ="2">Sfar No. 41</PARENT>
      <PARENT HEADING="Subpart F" SEQ="1">Equipment</PARENT>
      <PARENT HEADING="" SEQ="0">Electrical Systems and Equipment</PARENT>
    </ANCESTORS>
  </FDSYS>
  <SECTION>
    <SECTNO>§ 23.1359</SECTNO>
    <SUBJECT>Electrical system fire protection.</SUBJECT>
    <P>(a) Each component of the electrical system must meet the applicable fire protection requirements of §§ 23.863 and 23.1182.</P>
    <P>(b) Electrical cables, terminals, and equipment in designated fire zones that are used during emergency procedures must be fire-resistant.</P>

    <P>(c) Insulation on electrical wire and electrical cable must be self-extinguishing when tested at an angle of 60 degrees in accordance with the applicable portions of appendix F of this part, or other approved equivalent methods. The average burn length must not exceed 3 inches (76 mm) and the average flame time after removal of the flame source must not exceed 30 seconds. Drippings from the test specimen must <PRTPAGE P="284"/>not continue to flame for more than an average of 3 seconds after falling.</P>
    <CITA>[Doc. No. 27806, 61 FR 5169, Feb. 9, 1996]</CITA>
  </SECTION>
</CFRGRANULE>
