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        <title>Airworthiness Directives; The New Piper Aircraft, Inc. Models PA-31, PA-31-300, PA-31-325, PA-31-350, PA-31P, PA-31T, PA-31T1, PA-31T2, PA-31T3, and PA-31P-350 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 all The New Piper Aircraft, Inc. (Piper) Models PA-31, PA-31-300, PA-31-325, PA-31-350, PA-31P, PA-31T, PA-31T1, PA-31T2, PA-31T3, and PA-31P-350 airplanes. This proposed AD would require you to install an inspection hole, conduct a detailed visual inspection of the rudder torque tube and associated ribs for corrosion, and, if corrosion is found, replace the rib/rudder torque tube assembly. This proposed AD is the result of reports of rudder tube corrosion. The actions specified by this proposed AD are intended to detect and correct corrosion in the rudder torque tube assembly and rudder rib, which could result in failure of the rudder torque tube. Such failure could lead to loss of rudder control.</abstract>
    <identifier type="FR citation">68 FR 33030</identifier>
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    <identifier type="FR Doc No.">03-13792</identifier>
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    <identifier type="department code">Docket No. 2003-CE-03-AD</identifier>
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    <subject>
        <topic>Air Transportation</topic>
        <topic>Aircraft</topic>
        <topic>Aviation Safety</topic>
        <topic>Safety</topic>
    </subject>
    <physicalDescription>
        <extent>3 p.</extent>
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    <identifier type="preferred citation">68 FR 33030</identifier>
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            <partNumber>Title 14 Part 39</partNumber>
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        <searchTitle>Airworthiness Directives; The New Piper Aircraft, Inc. Models PA-31, PA-31-300, PA-31-325, PA-31-350, PA-31P, PA-31T, PA-31T1, PA-31T2, PA-31T3, and PA-31P-350 Airplanes; Federal Register Vol. 68, Issue </searchTitle>
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        <agency order="1">DEPARTMENT OF TRANSPORTATION</agency>
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        <summary>This document proposes to adopt a new airworthiness directive (AD) that would apply to all The New Piper Aircraft, Inc. (Piper) Models PA-31, PA-31-300, PA-31-325, PA-31-350, PA-31P, PA-31T, PA-31T1, PA-31T2, PA-31T3, and PA-31P-350 airplanes. This proposed AD would require you to install an inspection hole, conduct a detailed visual inspection of the rudder torque tube and associated ribs for corrosion, and, if corrosion is found, replace the rib/rudder torque tube assembly. This proposed AD is the result of reports of rudder tube corrosion. The actions specified by this proposed AD are intended to detect and correct corrosion in the rudder torque tube assembly and rudder rib, which could result in failure of the rudder torque tube. Such failure could lead to loss of rudder control.</summary>
        <dates>The Federal Aviation Administration (FAA) must receive any comments on this proposed rule on or before August 11, 2003.</dates>
        <contact>William O. Herderich, Aerospace Engineer, FAA, Atlanta Aircraft Certification Office, One Crown Center, 1895 Phoenix Boulevard, Suite 450, Atlanta, Georgia 30349; telephone: (770) 703-6082; facsimile: (770) 703-6097.</contact>
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            <part number="39"/>
                                    
            <subject>Air Transportation</subject>
                                    
            <subject>Aircraft</subject>
                                    
            <subject>Aviation Safety</subject>
                                    
            <subject>Safety</subject>
                                
        </cfr>
        <tocSubject1>Airworthiness directives:</tocSubject1>
        <tocDoc>New Piper Aircraft, Inc., </tocDoc>
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            <partNumber>Vol. 68, no. 106</partNumber>
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