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        <title>Airworthiness Directives; Cessna Aircraft Company Airplanes</title>
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    <abstract>We are revising an existing airworthiness directive (AD) for certain Cessna Aircraft Company (Cessna) Models 150F, 150G, 150H, 150J, 150K, 150L, 150M, A150K, A150L, A150M, F150F, F150G, F150H, F150J, F150K, F150L, F150M, FA150K, FA150L, FRA150L, FA150M, FRA150M, 152, A152, F152, and FA152 airplanes. That AD currently requires either installing a placard prohibiting spins and other acrobatic maneuvers in the airplane or replacing the rudder stop, the rudder stop bumper, and the attachment hardware with a rudder stop modification kit. This new AD requires a change to the modification kit and removal of a small amount of material from the rudder horn assembly for those that have not yet complied with the existing AD or for those who can not comply with the existing AD (because they were unable to obtain full rudder travel with the existing kits). This AD was prompted by operators who have reported difficulty in obtaining full rudder travel with the existing modification kit. We are issuing this AD to revise the kits to use longer rivets and allow a small amount of material to be removed from the rudder horn assembly, which allows operators to obtain full rudder travel.</abstract>
    <identifier type="FR citation">76 FR 53308</identifier>
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    <identifier type="department code">Docket No. FAA-2007-27747</identifier>
    <identifier type="department code">Directorate Identifier 2007-CE-030-AD</identifier>
    <identifier type="department code">Amendment 39-16782</identifier>
    <identifier type="department code">AD 2009-10-09 R2</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 revising an existing airworthiness directive (AD) for certain Cessna Aircraft Company (Cessna) Models 150F, 150G, 150H, 150J, 150K, 150L, 150M, A150K, A150L, A150M, F150F, F150G, F150H, F150J, F150K, F150L, F150M, FA150K, FA150L, FRA150L, FA150M, FRA150M, 152, A152, F152, and FA152 airplanes. That AD currently requires either installing a placard prohibiting spins and other acrobatic maneuvers in the airplane or replacing the rudder stop, the rudder stop bumper, and the attachment hardware with a rudder stop modification kit. This new AD requires a change to the modification kit and removal of a small amount of material from the rudder horn assembly for those that have not yet complied with the existing AD or for those who can not comply with the existing AD (because they were unable to obtain full rudder travel with the existing kits). This AD was prompted by operators who have reported difficulty in obtaining full rudder travel with the existing modification kit. We are issuing this AD to revise the kits to use longer rivets and allow a small amount of material to be removed from the rudder horn assembly, which allows operators to obtain full rudder travel.</summary>
        <dates>This AD is effective September 12, 2011.</dates>
        <contact>Ann Johnson, Aerospace Engineer, FAA, Wichita Aircraft Certification Office, 1801 Airport Road, Room 100, Wichita, Kansas 67209; telephone: (316) 946-4105; fax: (316) 946-4107; e-mail: ann.johnson@faa.gov.</contact>
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            <part number="39"/>
                                    
            <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. Airplanes
, </tocDoc>
        <emailRef>ann.johnson@faa.gov</emailRef>
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