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        <title>Airworthiness Directives; Sandel Avionics Incorporated Model ST3400 Terrain Awareness Warning System/Radio Magnetic Indicator (TAWS/RMI) Units Approved Under Technical Standard Order(s) C113, C151a, or C151b; Installed on Various Small and Transport Category Airplanes</title>
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    <abstract>The FAA is adopting a new airworthiness directive (AD). The new AD is for Sandel Avionics Incorporated Model ST3400 TAWS/RMI units as described above. This AD requires installing a warning placard on the TAWS/RMI and revising the Limitations section of the airplane flight manual (AFM). This AD also requires installing upgraded software in the TAWS/RMI. This AD results from a report that an in-flight bearing error occurred in a Model ST3400 TAWS/RMI configured to receive bearing information from a very high frequency omnidirectional range (VOR) receiver interface via a composite video signal, due to a combination of input signal fault and software error. We are issuing this AD to prevent a bearing error, which could lead to an airplane departing from its scheduled flight path, which could result in a reduction in separation from, and a possible collision with, other aircraft or terrain.</abstract>
    <identifier type="FR citation">71 FR 48461</identifier>
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    <identifier type="department code">Docket No. FAA-2006-24101</identifier>
    <identifier type="department code">Directorate Identifier 2005-NM-103-AD</identifier>
    <identifier type="department code">Amendment 39-14718</identifier>
    <identifier type="department code">AD 2006-16-18</identifier>
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        <topic>Aircraft</topic>
        <topic>Aviation Safety</topic>
        <topic>Incorporation by Reference</topic>
        <topic>Safety</topic>
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        <partNumber>I</partNumber>
        <agency order="1">DEPARTMENT OF TRANSPORTATION</agency>
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        <effectiveDate>2006-09-25</effectiveDate>
        <departmentDoc>Docket No. FAA-2006-24101</departmentDoc>
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        <summary>The FAA is adopting a new airworthiness directive (AD). The new AD is for Sandel Avionics Incorporated Model ST3400 TAWS/RMI units as described above. This AD requires installing a warning placard on the TAWS/RMI and revising the Limitations section of the airplane flight manual (AFM). This AD also requires installing upgraded software in the TAWS/RMI. This AD results from a report that an in-flight bearing error occurred in a Model ST3400 TAWS/RMI configured to receive bearing information from a very high frequency omnidirectional range (VOR) receiver interface via a composite video signal, due to a combination of input signal fault and software error. We are issuing this AD to prevent a bearing error, which could lead to an airplane departing from its scheduled flight path, which could result in a reduction in separation from, and a possible collision with, other aircraft or terrain.</summary>
        <dates>This AD becomes effective September 25, 2006.</dates>
        <contact>Ha A. Nguyen, Aerospace Engineer, Systems and Equipment Branch, ANM-130L, FAA, Los Angeles Aircraft Certification Office, 3960 Paramount Boulevard, Lakewood, California 90712-4137; telephone (562) 627-5335; fax (562) 627-5210.</contact>
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            <subject>Air Transportation</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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