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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>General.</TITLE>
    <GRANULENUM>23.1411</GRANULENUM>
    <HEADING>Section 23.1411</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">Safety Equipment</PARENT>
    </ANCESTORS>
  </FDSYS>
  <SECTION>
    <SECTNO>§ 23.1411</SECTNO>
    <SUBJECT>General.</SUBJECT>
    <P>(a) Required safety equipment to be used by the flight crew in an emergency, such as automatic liferaft releases, must be readily accessible.</P>
    <P>(b) Stowage provisions for required safety equipment must be furnished and must—</P>
    <P>(1) Be arranged so that the equipment is directly accessible and its location is obvious; and</P>
    <P>(2) Protect the safety equipment from damage caused by being subjected to the inertia loads resulting from the ultimate static load factors specified in § 23.561(b)(3) of this part.</P>
    <CITA>[Amdt. 23-17, 41 FR 55465, Dec. 20, 1976, as amended by Amdt. 23-36, 53 FR 30815, Aug. 15, 1988]</CITA>
  </SECTION>
</CFRGRANULE>
