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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>
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    <abstract>This amendment adopts a new airworthiness directive (AD) that applies 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 AD requires you to install an inspection hole (or use for inspection the tooling hole in the rudder bottom rib), conduct a detailed visual inspection of the rudder torque tube and associated ribs for corrosion, and, if corrosion is found, replace or repair the rib/rudder torque tube assembly. This AD is the result of reports of rudder tube corrosion. The actions specified by this 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. This failure could lead to loss of rudder control.</abstract>
    <identifier type="FR citation">68 FR 67588</identifier>
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    <identifier type="FR Doc No.">03-29871</identifier>
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    <identifier type="billing code">4910-13-P</identifier>
    <identifier type="department code">Docket No. 2003-CE-03-AD</identifier>
    <identifier type="department code">Amendment 39-13376</identifier>
    <identifier type="department code">AD 2003-24-07</identifier>
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        <topic>Air Transportation</topic>
        <topic>Aircraft</topic>
        <topic>Aviation Safety</topic>
        <topic>Incorporation by Reference</topic>
        <topic>Safety</topic>
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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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        <summary>This amendment adopts a new airworthiness directive (AD) that applies 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 AD requires you to install an inspection hole (or use for inspection the tooling hole in the rudder bottom rib), conduct a detailed visual inspection of the rudder torque tube and associated ribs for corrosion, and, if corrosion is found, replace or repair the rib/rudder torque tube assembly. This AD is the result of reports of rudder tube corrosion. The actions specified by this 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. This failure could lead to loss of rudder control.</summary>
        <dates>This AD becomes effective on February 9, 2004.</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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            <subject>Air Transportation</subject>
                                    
            <subject>Aircraft</subject>
                                    
            <subject>Aviation Safety</subject>
                                    
            <subject>Incorporation by Reference</subject>
                                    
            <subject>Safety</subject>
                                
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        <tocSubject1>Airworthiness directives:</tocSubject1>
        <tocDoc>New Piper Aircraft, Inc., </tocDoc>
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            <partNumber>Vol. 68, no. 232</partNumber>
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