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        <title>Airworthiness Directives; Cessna Aircraft Company (Cessna) Models 337, 337A (USAF 02B), 337B, 337C, 337D, 337E, T337E, 337F, T337F, 337G, T337G, M337B, F 337E, FT337E, F 337F, FT337F, F 337G, and FT337GP Airplanes</title>
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    <abstract>We are adopting a new airworthiness directive (AD) for the products listed above. This AD requires inspecting the wings for internal and external damage, repairing any damage, reinforcing the wings, installing operational limitation placards in the cockpit, and adding limitations to the airplane flight manual supplement. This AD was prompted by a review of installed Flint Aero, Inc. wing tip auxiliary fuel tanks, Supplemental Type Certificate (STC) SA5090NM. We are issuing this AD to detect and correct damage in the wings and to prevent overload failure of the wing due to the installation of the STC. Damage in the wing or overload failure of the wing could result in structural failure of the wing, which could result in loss of control.</abstract>
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    <identifier type="department code">Directorate Identifier 2011-CE-010-AD</identifier>
    <identifier type="department code">Amendment 39-16758</identifier>
    <identifier type="department code">AD 2011-15-11</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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        <summary>We are adopting a new airworthiness directive (AD) for the products listed above. This AD requires inspecting the wings for internal and external damage, repairing any damage, reinforcing the wings, installing operational limitation placards in the cockpit, and adding limitations to the airplane flight manual supplement. This AD was prompted by a review of installed Flint Aero, Inc. wing tip auxiliary fuel tanks, Supplemental Type Certificate (STC) SA5090NM. We are issuing this AD to detect and correct damage in the wings and to prevent overload failure of the wing due to the installation of the STC. Damage in the wing or overload failure of the wing could result in structural failure of the wing, which could result in loss of control.</summary>
        <dates>This AD is effective September 6, 2011.</dates>
        <contact>Dara Albouyeh, Aerospace Engineer, FAA, Los Angeles Aircraft Certification Office, 3960 Paramount Blvd., Lakewood, CA 90712; phone: (562) 627-5222; fax: (562) 627-5210; e-mail: dara.albouyeh@faa.gov.</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>Cessna Aircraft Co. (Cessna) Models 337, 337A (USAF 02B), 337B, 337C, 337D, 337E, etc., Airplanes
, </tocDoc>
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