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        <title>Airworthiness Directives; Mooney Aircraft Corporation Models M20B, M20C, M20D, M20E, M20F, M20G, M20J, M20K, M20L, M20M, and M20R Airplanes</title>
        <partName>Proposed Rules</partName>
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    <abstract>This document proposes to adopt a new airworthiness directive (AD) that would apply to certain Mooney Aircraft Corporation (Mooney) Models M20B, M20C, M20D, M20E, M20F, M20G, M20J, M20K, M20L, M20M, and M20R airplanes. The proposed AD would require repetitively inspecting the aileron control link welded area, and if cracks are found, replacing the control link with a part of improved design. Service difficulty reports (SDR's) on the aileron control link and reported failures of the aileron control link prompted the proposed action. The actions specified by the proposed AD are intended to detect and correct cracked aileron control links, which could result in loss of aileron control and loss of the airplane.</abstract>
    <identifier type="FR citation">63 FR 39254</identifier>
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    <identifier type="Regulation ID Number">RIN 2120-AA64</identifier>
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    <identifier type="department code">Docket No. 98-CE-20-AD</identifier>
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            <partNumber>Title 14 Part 39</partNumber>
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        <agency order="1">DEPARTMENT OF TRANSPORTATION</agency>
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        <commentDate>1998-09-30</commentDate>
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        <action>Notice of proposed rulemaking (NPRM).</action>
        <summary>This document proposes to adopt a new airworthiness directive (AD) that would apply to certain Mooney Aircraft Corporation (Mooney) Models M20B, M20C, M20D, M20E, M20F, M20G, M20J, M20K, M20L, M20M, and M20R airplanes. The proposed AD would require repetitively inspecting the aileron control link welded area, and if cracks are found, replacing the control link with a part of improved design. Service difficulty reports (SDR's) on the aileron control link and reported failures of the aileron control link prompted the proposed action. The actions specified by the proposed AD are intended to detect and correct cracked aileron control links, which could result in loss of aileron control and loss of the airplane.</summary>
        <dates>Comments must be received on or before September 30, 1998.</dates>
        <contact>Bob D. May, Aerospace Engineer, FAA, Airplane Certification Office, 2601 Meacham Boulevard, Fort Worth, Texas 76193-0150; telephone: (817) 222-5156; facsimile: (817) 222-5960.</contact>
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        <titleInfo>
            <title>Federal Register</title>
            <partNumber>Vol. 63, no. 140</partNumber>
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		  Table of Contents: 
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