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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>Weight, center of gravity, and weight distribution.</TITLE>
    <GRANULENUM>25.1519</GRANULENUM>
    <HEADING>Section 25.1519</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 G" SEQ="1">Operating Limitations and Information</PARENT>
      <PARENT HEADING="" SEQ="0">Operating Limitations</PARENT>
    </ANCESTORS>
  </FDSYS>
  <SECTION>
    <SECTNO>§ 25.1519</SECTNO>
    <SUBJECT>Weight, center of gravity, and weight distribution.</SUBJECT>
    <P>The airplane weight, center of gravity, and weight distribution limitations determined under §§ 25.23 through 25.27 must be established as operating limitations.</P>
  </SECTION>
</CFRGRANULE>
