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  <FDSYS>
    <CFRTITLE>14</CFRTITLE>
    <CFRTITLETEXT>Aeronautics and Space</CFRTITLETEXT>
    <VOL>1</VOL>
    <DATE>2006-01-01</DATE>
    <ORIGINALDATE>2006-01-01</ORIGINALDATE>
    <COVERONLY>false</COVERONLY>
    <TITLE>Electric cables.</TITLE>
    <GRANULENUM>27.1365</GRANULENUM>
    <HEADING>Section 27.1365</HEADING>
    <ANCESTORS>
      <PARENT HEADING="Title 14" SEQ="5">Aeronautics and Space</PARENT>
      <PARENT HEADING="CHAPTER I" SEQ="4">FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION</PARENT>
      <PARENT HEADING="SUBCHAPTER C" SEQ="3">AIRCRAFT</PARENT>
      <PARENT HEADING="PART 27" SEQ="2">AIRWORTHINESS STANDARDS: NORMAL CATEGORY ROTORCRAFT</PARENT>
      <PARENT HEADING="Subpart F" SEQ="1">Equipment</PARENT>
      <PARENT HEADING="" SEQ="0">Electrical Systems and Equipment</PARENT>
    </ANCESTORS>
  </FDSYS>
  <SECTION>
    <SECTNO>§ 27.1365</SECTNO>
    <SUBJECT>Electric cables.</SUBJECT>
    <P>(a) Each electric connecting cable must be of adequate capacity.</P>
    <P>(b) Each cable that would overheat in the event of circuit overload or fault must be at least flame resistant and may not emit dangerous quantities of toxic fumes.</P>
    <P>(c) Insulation on electrical wire and cable installed in the rotorcraft must be self-extinguishing when tested in accordance with Appendix F, Part I(a)(3), of part 25 of this chapter.</P>
    <CITA>[Doc. No. 5074, 29 FR 15695, Nov. 24, 1964, as amended by Amdt. 27-35, 63 FR 43285, Aug. 12, 1998]</CITA>
  </SECTION>
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