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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>Fuel valves.</TITLE>
    <GRANULENUM>25.995</GRANULENUM>
    <HEADING>Section 25.995</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 25" SEQ="2">AIRWORTHINESS STANDARDS: TRANSPORT CATEGORY AIRPLANES</PARENT>
      <PARENT HEADING="Subpart E" SEQ="1">Powerplant</PARENT>
      <PARENT HEADING="" SEQ="0">Fuel System Components</PARENT>
    </ANCESTORS>
  </FDSYS>
  <SECTION>
    <SECTNO>§ 25.995</SECTNO>
    <SUBJECT>Fuel valves.</SUBJECT>
    <P>In addition to the requirements of § 25.1189 for shutoff means, each fuel valve must—</P>
    <P>(a) [Reserved]</P>
    <P>(b) Be supported so that no loads resulting from their operation or from accelerated flight conditions are transmitted to the lines attached to the valve.</P>
    <CITA>[Doc. No. 5066, 29 FR 18291, Dec. 24, 1964, as amended by Amdt. 25-40, 42 FR 15043, Mar. 17, 1977]</CITA>
  </SECTION>
</CFRGRANULE>
