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    <title>The Federal Register</title>
    <link>http://thefederalregister.com/b.p/department/DEPARTMENT_OF_TRANSPORTATION_(DOT)/</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[DEPARTMENT OF TRANSPORTATION ]]></title>
  <link>http://thefederalregister.com/d.p/2008-11-24-E8-21238</link>
  <description><![CDATA[ The regulatory agenda is a semiannual summary of all current 
and projected rulemakings, reviews of existing regulations, and 
completed actions of the Department. The agenda provides the public 
with information about the Department of Transportation's regulatory 
activity. It is expected that this information will enable the public 
to be more aware of and allow it to more effectively participate in the 
Department's regulatory activity. The public is also invited to submit 
comments on any aspect of this agenda.
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  <guid>http://thefederalregister.com/d.p/2008-11-24-E8-21238</guid>
  <pubDate>Mon, Nov 24 2008 11:00:00 GMT</pubDate>
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<item>
  <title><![CDATA[  Airworthiness Directives; Hawker Beechcraft Corporation Model 390  Airplanes]]></title>
  <link>http://thefederalregister.com/d.p/2008-10-09-E8-23643</link>
  <description><![CDATA[ The FAA is adopting a new airworthiness directive (AD) for 
certain Hawker Beechcraft Corporation Model 390 airplanes. This AD 
requires you to modify the cabin barometric pressure switch and cabin 
altitude high switch installations and perform a functional test of the 
switches and related systems. This AD results from the possibility of 
barometric pressure switch electrical connections being incorrectly 
connected or inadvertently disconnected. We are issuing this AD to 
modify the cabin barometric pressure switch and cabin altitude high 
switch to prevent them from becoming incorrectly connected or 
inadvertently disconnected, which may result in no CABIN ALT HI 
annunciation in the cockpit and no automatic deployment of the cabin 
oxygen masks. This failure could lead to incapacitation of the crew due 
to hypoxia with possible inability to control the airplane.
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  <guid>http://thefederalregister.com/d.p/2008-10-09-E8-23643</guid>
  <pubDate>Thu, Oct 9 2008 11:00:00 GMT</pubDate>
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<item>
  <title><![CDATA[  Airworthiness Directives; Lindstrand Balloons Ltd. Models 42A,  56A, 77A, 105A, 150A, 210A, 260A, 60A, 69A, 90A, 120A,]]></title>
  <link>http://thefederalregister.com/d.p/2008-03-12-E8-4759</link>
  <description><![CDATA[ We are adopting a new airworthiness directive (AD) for the 
products listed above. This AD results from mandatory continuing 
airworthiness information (MCAI) issued by the aviation authority of 
another country to identify and correct an unsafe condition on an 
aviation product. The MCAI describes the unsafe condition as:
</p><p>    Defective burner hoses have been identified which might develop 
a leak. A significant leak, if it was ignited, could hazard the  balloon and occupants.</p><p>    Since the issue of AD G20030010 there have been occurrences of 
hose failure in batches not identified in the earlier bulletins. 
LHAB Service Bulletin (SB) No 11 supersedes the earlier SBs and  revises the applicability as required.<br/>
This AD requires actions that are intended to address the unsafe 
condition described in the MCAI.
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  <guid>http://thefederalregister.com/d.p/2008-03-12-E8-4759</guid>
  <pubDate>Wed, Mar 12 2008 11:00:00 GMT</pubDate>
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