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        <title>Airworthiness Directives; Cessna Model 500, 501, 550, S550, 551, and 560 Airplanes</title>
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    <abstract>The FAA is adopting a new airworthiness directive (AD) for certain Cessna Model 500, 501, 550, S550, 551, and 560 airplanes. This AD requires revising the airplane flight manual (AFM) to prohibit use of the wing fuel boost pumps for defueling under certain conditions; installing a placard; doing other specified investigative and corrective actions as necessary; and modifying the boost pumps. This AD also requires the subsequent removal of the AFM revision and placard. This AD results from a report of a chafed electrical wiring harness, which was arcing inside the fuel tank. We are issuing this AD to prevent potential fuel vapor ignition in a fuel tank, which could result in explosion and loss of the airplane.</abstract>
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    <identifier type="department code">Docket No. FAA-2005-20970</identifier>
    <identifier type="department code">Directorate Identifier 2004-NM-53-AD</identifier>
    <identifier type="department code">Amendment 39-14511</identifier>
    <identifier type="department code">AD 2006-06-03</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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        <searchTitle>Airworthiness Directives; Cessna Model 500, 501, 550, S550, 551, and 560 Airplanes; Federal Register Vol. 71, Issue </searchTitle>
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        <summary>The FAA is adopting a new airworthiness directive (AD) for certain Cessna Model 500, 501, 550, S550, 551, and 560 airplanes. This AD requires revising the airplane flight manual (AFM) to prohibit use of the wing fuel boost pumps for defueling under certain conditions; installing a placard; doing other specified investigative and corrective actions as necessary; and modifying the boost pumps. This AD also requires the subsequent removal of the AFM revision and placard. This AD results from a report of a chafed electrical wiring harness, which was arcing inside the fuel tank. We are issuing this AD to prevent potential fuel vapor ignition in a fuel tank, which could result in explosion and loss of the airplane.</summary>
        <dates>This AD becomes effective April 20, 2006.</dates>
        <contact>Bryan Easterwood, Aerospace Engineer, Electrical Systems and Avionics Branch, ACE-119W, Wichita Aircraft Certification Office, FAA, 1801 Airport Road, room 100, Mid-Continent Airport, Wichita, Kansas 67209; telephone (316) 946-4132; fax (316) 946-4107.</contact>
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            <subject>Air Transportation</subject>
                                    
            <subject>Aircraft</subject>
                                    
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            <subject>Incorporation by Reference</subject>
                                    
            <subject>Safety</subject>
                                
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        <tocSubject1>Airworthiness directives:</tocSubject1>
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            <partNumber>Vol. 71, no. 51</partNumber>
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