<?xml version="1.0" encoding="UTF-8"?><mods xmlns:xlink="http://www.w3.org/1999/xlink" xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance" xmlns="http://www.loc.gov/mods/v3" version="3.3" xsi:schemaLocation="http://www.loc.gov/mods/v3 http://www.loc.gov/standards/mods/v3/mods-3-3.xsd" ID="id-97-33142">
    <name type="corporate">
        <namePart>United States Government Publishing Office</namePart>
        <role>
            <roleTerm authority="marcrelator" type="text">publisher</roleTerm>
            <roleTerm authority="marcrelator" type="code">pbl</roleTerm>
        </role>
        <role>
            <roleTerm authority="marcrelator" type="text">distributor</roleTerm>
            <roleTerm authority="marcrelator" type="code">dst</roleTerm>
        </role>
    </name>
    <name type="corporate">
        <namePart>United States</namePart>
        <namePart>National Archives and Records Administration</namePart>
        <namePart>Office of the Federal Register</namePart>
        <role>
            <roleTerm authority="marcrelator" type="text">author</roleTerm>
            <roleTerm authority="marcrelator" type="code">aut</roleTerm>
        </role>
        <description>Government Organization</description>
    </name>
    <typeOfResource>text</typeOfResource>
    <genre authority="marcgt">government publication</genre>
    <language>
        <languageTerm type="code" authority="iso639-2b">eng</languageTerm>
    </language>
    <extension>
        <collectionCode>FR</collectionCode>
        <category>Regulatory Information</category>
        <waisDatabaseName>1997_register</waisDatabaseName>
        <branch>executive</branch>
        <dateIngested>2010-09-24</dateIngested>
    </extension>
    <genre authority="marcgt">article</genre>
    <titleInfo>
        <title>Airworthiness Directives; Teledyne Continental Motors IO-360, TSIO-360, LTSIO-360, IO-520, LIO-520, TSIO-520, LTSIO-520 Series, and Rolls-Royce plc IO-360 and TSIO-360 Series Reciprocating Engines</title>
        <partName>Rules and Regulations</partName>
    </titleInfo>
    <relatedItem type="otherFormat" xlink:href="https://www.govinfo.gov/content/pkg/FR-1997-12-19/html/97-33142.htm">
        <identifier type="FDsys Unique ID">D09002ee1be007c8b</identifier>
    </relatedItem>
    <relatedItem type="otherFormat" xlink:href="https://www.govinfo.gov/content/pkg/FR-1997-12-19/pdf/97-33142.pdf">
        <identifier type="FDsys Unique ID">D09002ee1be007d4b</identifier>
    </relatedItem>
    <name type="corporate">
        <namePart>United States</namePart>
        <namePart>Department of Transportation</namePart>
        <role>
            <roleTerm authority="marcrelator" type="text">originator</roleTerm>
            <roleTerm authority="marcrelator" type="code">org</roleTerm>
        </role>
        <description>United States Government Agency or Subagency</description>
    </name>
    <name type="corporate">
        <namePart>United States</namePart>
        <namePart>Federal Aviation Administration</namePart>
        <role>
            <roleTerm authority="marcrelator" type="text">originator</roleTerm>
            <roleTerm authority="marcrelator" type="code">org</roleTerm>
        </role>
        <description>United States Government Agency or Subagency</description>
    </name>
    <abstract>This amendment supersedes an existing airworthiness directive (AD), applicable to certain Teledyne Continental Motors (TCM) IO-520 and TSIO-520 series reciprocating engines, that currently requires ultrasonic inspection for subsurface fatigue cracks in crankshafts installed in TCM IO-520 and TSIO-520 series engines and replacement of the crankshaft if a crack is found. This amendment adds a requirement to remove crankshafts manufactured using the airmelt process and replace them with crankshafts manufactured using the vacuum arc remelt (VAR) process, incorporates new ultrasonic inspection criteria in the AD, adds engine series TCM IO-360, TSIO-360, LTSIO-360, IO-520, LIO- 520, TSIO-520, LTSIO-520 and Rolls-Royce, plc IO-360 and TSIO-360 to the applicability, and revises the economic impact analysis. This amendment is prompted by reports of crankshaft failures due to subsurface fatigue cracking on engines that had been inspected in accordance with the current AD. The actions specified by this AD are intended to prevent crankshaft failure and subsequent engine failure.</abstract>
    <identifier type="FR citation">62 FR 66502</identifier>
    <identifier type="uri">https://www.govinfo.gov/app/details/FR-1997-12-19/97-33142</identifier>
    <identifier type="FR Doc No.">97-33142</identifier>
    <identifier type="former granule identifier">fr19de97-5</identifier>
    <identifier type="Regulation ID Number">RIN 2120-AA64</identifier>
    <identifier type="billing code">4910-13-P</identifier>
    <identifier type="department code">Docket No. 93-ANE-08</identifier>
    <identifier type="department code">Amendment 39-10260</identifier>
    <identifier type="department code">AD 97-26-17</identifier>
    <location>
        <url displayLabel="Content Detail" access="object in context">https://www.govinfo.gov/app/details/FR-1997-12-19/97-33142</url>
        <url access="raw object" displayLabel="HTML rendition">https://www.govinfo.gov/content/pkg/FR-1997-12-19/html/97-33142.htm</url>
        <url access="raw object" displayLabel="PDF rendition">https://www.govinfo.gov/content/pkg/FR-1997-12-19/pdf/97-33142.pdf</url>
    </location>
    <physicalDescription>
        <extent>5 p.</extent>
    </physicalDescription>
    <part type="Rules and Regulations">
        <extent unit="pages">
            <start>66502</start>
            <end>66506</end>
        </extent>
    </part>
    <identifier type="preferred citation">62 FR 66502</identifier>
    <relatedItem type="isReferencedBy">
        <titleInfo>
            <title>Code of Federal Regulations</title>
            <partNumber>Title 14 Part 39</partNumber>
        </titleInfo>
        <identifier type="CFR citation">14 CFR Part  39</identifier>
    </relatedItem>
    <relatedItem type="isReferencedBy">
        <titleInfo>
            <title>Regulation Identification Number 2120-AA64</title>
        </titleInfo>
        <identifier type="regulation ID number">RIN 2120-AA64</identifier>
    </relatedItem>
    <extension>
        <searchTitle>Airworthiness Directives; Teledyne Continental Motors IO-360, TSIO-360, LTSIO-360, IO-520, LIO-520, TSIO-520, LTSIO-520 Series, and Rolls-Royce plc IO-360 and TSIO-360 Series Reciprocating Engines; Federal Register Vol. 62, Issue </searchTitle>
        <granuleClass>RULE</granuleClass>
        <accessId>97-33142</accessId>
        <agency order="1">DEPARTMENT OF TRANSPORTATION</agency>
        <agency order="2">Federal Aviation Administration</agency>
        <effectiveDate>1998-01-23</effectiveDate>
        <departmentDoc>Docket No. 93-ANE-08</departmentDoc>
        <departmentDoc>Amendment 39-10260</departmentDoc>
        <departmentDoc>AD 97-26-17</departmentDoc>
        <rin number="2120-AA64"/>
        <billingCode>4910-13-P</billingCode>
        <frDocNumber>97-33142</frDocNumber>
        <action>Final rule.</action>
        <summary>This amendment supersedes an existing airworthiness directive (AD), applicable to certain Teledyne Continental Motors (TCM) IO-520 and TSIO-520 series reciprocating engines, that currently requires ultrasonic inspection for subsurface fatigue cracks in crankshafts installed in TCM IO-520 and TSIO-520 series engines and replacement of the crankshaft if a crack is found. This amendment adds a requirement to remove crankshafts manufactured using the airmelt process and replace them with crankshafts manufactured using the vacuum arc remelt (VAR) process, incorporates new ultrasonic inspection criteria in the AD, adds engine series TCM IO-360, TSIO-360, LTSIO-360, IO-520, LIO- 520, TSIO-520, LTSIO-520 and Rolls-Royce, plc IO-360 and TSIO-360 to the applicability, and revises the economic impact analysis. This amendment is prompted by reports of crankshaft failures due to subsurface fatigue cracking on engines that had been inspected in accordance with the current AD. The actions specified by this AD are intended to prevent crankshaft failure and subsequent engine failure.</summary>
        <dates>Effective January 23, 1998.</dates>
        <contact>Jerry Robinette, Aerospace Engineer, Atlanta Aircraft Certification Office, FAA, Small Airplane Directorate, Campus Building, 1701 Columbia Ave., Suite 2-160, College Park, GA 30337-2748; telephone (404) 305-7371, fax (404) 305-7348.</contact>
        <cfr title="14">
                                    
            <part number="39"/>
                                
        </cfr>
    </extension>
    <relatedItem type="host" ID="P0b002ee180a413e7" xlink:href="https://www.govinfo.gov/metadata/pkg/FR-1997-12-19/mods.xml">
        <titleInfo>
            <title>Federal Register</title>
            <partNumber>Vol. 62, no. 244</partNumber>
        </titleInfo>
        <originInfo>
            <publisher>Office of the Federal Register, National Archives and Records Administration</publisher>
            <dateIssued encoding="w3cdtf">1997-12-19</dateIssued>
            <issuance>continuing</issuance>
            <frequency>daily</frequency>
        </originInfo>
        <physicalDescription>
            <note type="source content type">deposited</note>
            <digitalOrigin>born digital</digitalOrigin>
            <extent>328 p.</extent>
        </physicalDescription>
        <tableOfContents xlink:href="https://www.govinfo.gov/app/frtoc/1997-12-19">    
		  Table of Contents: 
		</tableOfContents>
        <classification authority="sudocs">AE 2.7:</classification>
        <classification authority="sudocs">GS 4.107:</classification>
        <classification authority="sudocs">AE 2.106:</classification>
        <classification authority="lcc">KF70.A2</classification>
        <identifier type="uri">https://www.govinfo.gov/app/details/FR-1997-12-19</identifier>
        <identifier type="local">P0b002ee180a413e7</identifier>
        <identifier type="issn">0097-6326</identifier>
        <identifier type="issn">0042-1219</identifier>
        <identifier type="issn">0364-1406</identifier>
        <identifier type="stock number">769-004-00000-9</identifier>
        <identifier type="ILS system id">000582072</identifier>
        <identifier type="former identifier">f:fr19de97</identifier>
        <location>
            <url displayLabel="Content Detail" access="object in context">https://www.govinfo.gov/app/details/FR-1997-12-19</url>
            <url displayLabel="PDF rendition" access="raw object">https://www.govinfo.gov/content/pkg/FR-1997-12-19/pdf/FR-1997-12-19.pdf</url>
        </location>
        <accessCondition type="GPO scope determination">fdlp</accessCondition>
        <part type="issue">
            <extent unit="pages">
                <start>66495</start>
                <end>66811</end>
            </extent>
        </part>
        <recordInfo>
            <recordContentSource authority="marcorg">DGPO</recordContentSource>
            <recordCreationDate encoding="w3cdtf">2010-09-24</recordCreationDate>
            <recordChangeDate encoding="w3cdtf">2023-05-06</recordChangeDate>
            <recordIdentifier source="DGPO">FR-1997-12-19</recordIdentifier>
            <recordOrigin>machine generated</recordOrigin>
            <languageOfCataloging>
                <languageTerm type="code" authority="iso639-2b">eng</languageTerm>
            </languageOfCataloging>
        </recordInfo>
        <extension>
            <docClass>FR</docClass>
            <accessId>FR-1997-12-19</accessId>
            <volume>62</volume>
            <issue>244</issue>
        </extension>
    </relatedItem>
</mods>
