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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>Function and installation.</TITLE>
    <GRANULENUM>23.1301</GRANULENUM>
    <HEADING>Section 23.1301</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">General</PARENT>
    </ANCESTORS>
  </FDSYS>
  <SECTION>
    <SECTNO>§ 23.1301</SECTNO>
    <SUBJECT>Function and installation.</SUBJECT>
    <P>Each item of installed equipment must—</P>
    <P>(a) Be of a kind and design appropriate to its intended function.</P>
    <P>(b) Be labeled as to its identification, function, or operating limitations, or any applicable combination of these factors;</P>
    <P>(c) Be installed according to limitations specified for that equipment; and</P>
    <P>(d) Function properly when installed.</P>
    <CITA>[Amdt. 23-20, 42 FR 36968, July 18, 1977]</CITA>
  </SECTION>
</CFRGRANULE>
