<?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-2011-27512">
    <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>2011_register</waisDatabaseName>
        <branch>executive</branch>
        <dateIngested>2011-10-27</dateIngested>
    </extension>
    <genre authority="marcgt">article</genre>
    <titleInfo>
        <title>Airworthiness Directives; Rolls-Royce plc (RR) RB211-535 Series Turbofan Engines</title>
        <partName>Proposed Rules</partName>
    </titleInfo>
    <relatedItem type="otherFormat" xlink:href="https://www.govinfo.gov/content/pkg/FR-2011-10-25/html/2011-27512.htm">
        <identifier type="FDsys Unique ID">D09002ee1c7ff20a0</identifier>
    </relatedItem>
    <relatedItem type="otherFormat" xlink:href="https://www.govinfo.gov/content/pkg/FR-2011-10-25/pdf/2011-27512.pdf">
        <identifier type="FDsys Unique ID">D09002ee1c7ff212f</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>We propose to supersede an existing airworthiness directive (AD) that applies to all RR RB211-535E4-37, -535E4-B-37, -535E4-B-75, and -535E4-C-37 turbofan engines. The existing AD currently requires performing initial and repetitive visual and fluorescent penetrant inspections (FPI) of the low-pressure (LP) turbine stage 1, 2, and 3 discs to detect cracks in the discs. Since we issued that AD, we determined that the definition of shop visit is too restrictive in the existing AD. This proposed AD would continue to require those inspections and would change the definition of a shop visit to be less restrictive. We are proposing this AD to correct the definition of shop visit, and to detect cracks in the LP turbine stage 1, 2, and 3 discs, which could result in an uncontained release of LP turbine blades and damage to the airplane.</abstract>
    <identifier type="FR citation">76 FR 65997</identifier>
    <identifier type="uri">https://www.govinfo.gov/app/details/FR-2011-10-25/2011-27512</identifier>
    <identifier type="FR Doc No.">2011-27512</identifier>
    <identifier type="former granule identifier">fr25oc11-25</identifier>
    <identifier type="Regulation ID Number">RIN 2120-AA64</identifier>
    <identifier type="billing code">4910-13-P</identifier>
    <identifier type="department code">Docket No. FAA-2009-0994</identifier>
    <identifier type="department code">Directorate Identifier 2009-NE-39-AD</identifier>
    <location>
        <url displayLabel="Content Detail" access="object in context">https://www.govinfo.gov/app/details/FR-2011-10-25/2011-27512</url>
        <url access="raw object" displayLabel="HTML rendition">https://www.govinfo.gov/content/pkg/FR-2011-10-25/html/2011-27512.htm</url>
        <url access="raw object" displayLabel="PDF rendition">https://www.govinfo.gov/content/pkg/FR-2011-10-25/pdf/2011-27512.pdf</url>
    </location>
    <subject>
        <topic>Air Transportation</topic>
        <topic>Aircraft</topic>
        <topic>Aviation Safety</topic>
        <topic>Incorporation by Reference</topic>
        <topic>Safety</topic>
    </subject>
    <physicalDescription>
        <extent>3 p.</extent>
    </physicalDescription>
    <part type="Proposed Rules">
        <extent unit="pages">
            <start>65997</start>
            <end>65999</end>
        </extent>
    </part>
    <identifier type="preferred citation">76 FR 65997</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; Rolls-Royce plc (RR) RB211-535 Series Turbofan Engines; Federal Register Vol. 76, Issue </searchTitle>
        <granuleClass>PRORULE</granuleClass>
        <accessId>2011-27512</accessId>
        <agency order="1">DEPARTMENT OF TRANSPORTATION</agency>
        <agency order="2">Federal Aviation Administration</agency>
        <commentDate>2011-12-27</commentDate>
        <departmentDoc>Docket No. FAA-2009-0994</departmentDoc>
        <departmentDoc>Directorate Identifier 2009-NE-39-AD</departmentDoc>
        <rin number="2120-AA64"/>
        <billingCode>4910-13-P</billingCode>
        <frDocNumber>2011-27512</frDocNumber>
        <action>Notice of proposed rulemaking (NPRM).</action>
        <summary>We propose to supersede an existing airworthiness directive (AD) that applies to all RR RB211-535E4-37, -535E4-B-37, -535E4-B-75, and -535E4-C-37 turbofan engines. The existing AD currently requires performing initial and repetitive visual and fluorescent penetrant inspections (FPI) of the low-pressure (LP) turbine stage 1, 2, and 3 discs to detect cracks in the discs. Since we issued that AD, we determined that the definition of shop visit is too restrictive in the existing AD. This proposed AD would continue to require those inspections and would change the definition of a shop visit to be less restrictive. We are proposing this AD to correct the definition of shop visit, and to detect cracks in the LP turbine stage 1, 2, and 3 discs, which could result in an uncontained release of LP turbine blades and damage to the airplane.</summary>
        <dates>We must receive comments on this proposed AD by December 27, 2011.</dates>
        <contact>Alan Strom, Aerospace Engineer, Engine Certification Office, FAA, 12 New England Executive Park, Burlington, MA 01803; phone: 781-238-7143; fax: 781-238-7199; e-mail: alan.strom@faa.gov.</contact>
        <cfr title="14">
                                    
            <part number="39"/>
                                    
            <subject>Air Transportation</subject>
                                    
            <subject>Aircraft</subject>
                                    
            <subject>Aviation Safety</subject>
                                    
            <subject>Incorporation by Reference</subject>
                                    
            <subject>Safety</subject>
                                
        </cfr>
        <tocSubject1>Airworthiness Directives:</tocSubject1>
        <tocDoc>Rolls-Royce plc (RR) RB211535 Series Turbofan Engines
, </tocDoc>
        <emailRef>alan.strom@faa.gov</emailRef>
        <urlRef>http://www.regulations.gov</urlRef>
        <urlRef>http://www.rolls-royce.com/contact/civil_team.jsp</urlRef>
        <urlRef>http://www.rollsroyce.com/contact/civil_team.jsp</urlRef>
        <urlRef>https://www.aeromanager.com</urlRef>
    </extension>
    <relatedItem type="host" ID="P0b002ee180eb8184" xlink:href="https://www.govinfo.gov/metadata/pkg/FR-2011-10-25/mods.xml">
        <titleInfo>
            <title>Federal Register</title>
            <partNumber>Vol. 76, no. 206</partNumber>
        </titleInfo>
        <originInfo>
            <publisher>Office of the Federal Register, National Archives and Records Administration</publisher>
            <dateIssued encoding="w3cdtf">2011-10-25</dateIssued>
            <issuance>continuing</issuance>
            <frequency>daily</frequency>
        </originInfo>
        <physicalDescription>
            <note type="source content type">deposited</note>
            <digitalOrigin>born digital</digitalOrigin>
            <extent>250 p.</extent>
        </physicalDescription>
        <tableOfContents xlink:href="https://www.govinfo.gov/app/frtoc/2011-10-25">    
		  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-2011-10-25</identifier>
        <identifier type="local">P0b002ee180eb8184</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:fr25oc11</identifier>
        <location>
            <url displayLabel="Content Detail" access="object in context">https://www.govinfo.gov/app/details/FR-2011-10-25</url>
            <url displayLabel="PDF rendition" access="raw object">https://www.govinfo.gov/content/pkg/FR-2011-10-25/pdf/FR-2011-10-25.pdf</url>
            <url displayLabel="XML rendition" access="raw object">https://www.govinfo.gov/content/pkg/FR-2011-10-25/xml/FR-2011-10-25.xml</url>
        </location>
        <accessCondition type="GPO scope determination">fdlp</accessCondition>
        <part type="issue">
            <extent unit="pages">
                <start>65927</start>
                <end>66167</end>
            </extent>
        </part>
        <recordInfo>
            <recordContentSource authority="marcorg">DGPO</recordContentSource>
            <recordCreationDate encoding="w3cdtf">2011-10-27</recordCreationDate>
            <recordChangeDate encoding="w3cdtf">2024-06-03</recordChangeDate>
            <recordIdentifier source="DGPO">FR-2011-10-25</recordIdentifier>
            <recordOrigin>machine generated</recordOrigin>
            <languageOfCataloging>
                <languageTerm type="code" authority="iso639-2b">eng</languageTerm>
            </languageOfCataloging>
        </recordInfo>
        <extension>
            <docClass>FR</docClass>
            <accessId>FR-2011-10-25</accessId>
            <volume>76</volume>
            <issue>206</issue>
        </extension>
    </relatedItem>
</mods>
