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    <title>The Federal Register</title>
    <link>http://thefederalregister.com/b.p/department/DEPARTMENT_OF_TRANSPORTATION_(DOT)/2005-11-22/</link>
    <description>Daily Publications of Meetings and Rules Changes for the Federal Government</description>
    <pubDate>Mon, Dec 1 2008 11:00:00 GMT</pubDate>
    <lastBuildDate>Mon, Dec 1 2008 11:00:00 GMT</lastBuildDate>
    <webMaster>info@thefederalregister.com</webMaster>
    <item>
  <title><![CDATA[  Airworthiness Directives; Raytheon Aircraft Company Models 58P  and 58TC Airplanes]]></title>
  <link>http://thefederalregister.com/d.p/2005-11-22-05-23055</link>
  <description><![CDATA[ The FAA proposes to adopt a new airworthiness directive (AD) 
for certain Raytheon Aircraft Company (Raytheon) Models 58P and 58TC 
airplanes used as a lead airplane by the United States Forest Service. 
This proposed AD would require you to insert a new supplement into the 
Limitations Section of the Pilot's Operating Handbook and Airplane 
Flight Manual (POH/AFM) that establishes new limits for the structural 
life of the airframe (wing, fuselage, empennage, or associated 
structure); and dispose of the lifelimited airframe following 14 CFR 
43.10 when the limit of the structural life of the airframe is reached. 
This proposed AD results from Raytheon issuing a POH/AFM supplement 
that establishes the structural life limit of 4,500 hours timein
service (TIS) for the airframe (wing, fuselage, empennage, and 
associated structure) for any Models 58P and 58TC airplanes used as a 
lead airplane by the United States Forest Service; and FAA's 
determination that the structural life limit is necessary. We are 
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  <guid>http://thefederalregister.com/d.p/2005-11-22-05-23055</guid>
  <pubDate>Tue, Nov 22 2005 11:00:00 GMT</pubDate>
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