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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>Applicable requirements.</TITLE>
    <GRANULENUM>21.115</GRANULENUM>
    <HEADING>Section 21.115</HEADING>
    <ANCESTORS>
      <PARENT HEADING="Title 14" SEQ="4">Aeronautics and Space</PARENT>
      <PARENT HEADING="CHAPTER I" SEQ="3">FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION</PARENT>
      <PARENT HEADING="SUBCHAPTER C" SEQ="2">AIRCRAFT</PARENT>
      <PARENT HEADING="PART 21" SEQ="1">CERTIFICATION PROCEDURES FOR PRODUCTS AND PARTS</PARENT>
      <PARENT HEADING="Subpart E" SEQ="0">Supplemental Type Certificates</PARENT>
    </ANCESTORS>
  </FDSYS>
  <SECTION>
    <SECTNO>§ 21.115</SECTNO>
    <SUBJECT>Applicable requirements.</SUBJECT>
    <P>(a) Each applicant for a supplemental type certificate must show that the altered product meets applicable requirements specified in § 21.101 and, in the case of an acoustical change described in § 21.93(b), show compliance with the applicable noise requirements of part 36 of this chapter and, in the case of an emissions change described in § 21.93(c), show compliance with the applicable fuel venting and exhaust emissions requirements of part 34 of this chapter.</P>
    <P>(b) Each applicant for a supplemental type certificate must meet §§ 21.33 and 21.53 with respect to each change in the type design.</P>
    <CITA>[Amdt. 21-17, 32 FR 14927, Oct. 28, 1967, as amended by Amdt. 21-42, 40 FR 1033, Jan. 6, 1975; Amdt. 21-52A, 45 FR 79009, Nov. 28, 1980; Amdt. 21-61, 53 FR 3540, Feb. 5, 1988; Amdt. 21-68, 55 FR 32860, Aug. 10, 1990; Amdt. 21-71, 57 FR 42854, Sept. 16, 1992; Amdt. 21-77, 65 FR 36266, June 7, 2000]</CITA>
  </SECTION>
</CFRGRANULE>
