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    <title>The Federal Register</title>
    <link>http://thefederalregister.com/b.p/department/DEPARTMENT_OF_TRANSPORTATION/2005-11-21/</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; Airbus Model A340-200 and A340-300  Series Airplanes]]></title>
  <link>http://thefederalregister.com/d.p/2005-11-21-05-22789</link>
  <description><![CDATA[ The FAA is adopting a new airworthiness directive (AD) for all 
Airbus Model A340200 and A340300 series airplanes. This AD requires 
repetitive inspections for cracking of the junction between the thrust 
reverser forward frame and the 12 o'clock and 6 o'clock beams; the 
thrust reverser common fittings; and the thrust reverser Jring 
structure at the 12 o'clock and 6 o'clock positions; and related 
investigative and corrective actions. This AD results from fatigue and 
damage tolerance testing of the engine thrust reversers which revealed 
fatigue cracking of the junction between the thrust reverser forward 
frame and the 12 o'clock beam, and of the thrust reverser Jring 
structure. We are issuing this AD to detect and correct such fatigue 
cracking, which could result in rupture of the Jring, forward frame, 
or common fittings; loss of the thrust reverser system; or inadvertent 
deployment of a thrust reverser in flight and consequent reduced 
controllability of the airplane.
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  <guid>http://thefederalregister.com/d.p/2005-11-21-05-22789</guid>
  <pubDate>Mon, Nov 21 2005 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Boeing Model 767-200 and -300 Series  Airplanes]]></title>
  <link>http://thefederalregister.com/d.p/2005-11-21-05-22791</link>
  <description><![CDATA[ The FAA is adopting a new airworthiness directive (AD) for 
certain Boeing Model 767200 and 300 series airplanes. This AD 
requires replacing hinge assemblies with new hinge assemblies in the 
outboard overhead stowage bins and reworking hinge assemblies in the 
outboard overhead stowage bins that are adjacent to curtain tracks. 
This AD results from reports of hinge assemblies of outboard overhead 
stowage bins breaking or the stowage bin doors not latching properly. 
We are issuing this AD to prevent the outboard overhead stowage bins 
opening during flight and releasing baggage, and consequently injuring 
passengers and blocking the aisles during emergency egress.
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  <guid>http://thefederalregister.com/d.p/2005-11-21-05-22791</guid>
  <pubDate>Mon, Nov 21 2005 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; British Aerospace Model HS 748  Airplanes]]></title>
  <link>http://thefederalregister.com/d.p/2005-11-21-05-22790</link>
  <description><![CDATA[ The FAA is adopting a new airworthiness directive (AD) for all 
British Aerospace Model HS 748 airplanes. This AD requires repetitive 
inspections for fatigue cracking, corrosion, and other related 
discrepancies of the rear pressure bulkhead and associated areas, and 
the fin attachment fittings, particularly the fin link beam; and 
related investigative and corrective actions. This AD results from a 
structural integrity audit of the airplane that showed the importance 
of inspecting for fatigue cracking and corrosion of these areas. We are 
issuing this AD to detect and correct cracking, corrosion, and other 
related discrepancies of the rear pressure bulkhead and associated 
areas, and the fin attachment fittings, particularly the fin link beam, 
which could result in damage to the airplane structure or injury to 
airplane occupants.
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  <guid>http://thefederalregister.com/d.p/2005-11-21-05-22790</guid>
  <pubDate>Mon, Nov 21 2005 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Empresa Brasileira de Aeronautica S.A.  (EMBRAER) Model EMB-135 Airplanes, and Model]]></title>
  <link>http://thefederalregister.com/d.p/2005-11-21-05-22792</link>
  <description><![CDATA[ The FAA is adopting a new airworthiness directive (AD) for 
certain EMBRAER Model EMB135 airplanes, and Model EMB145, 145ER, 
145MR, 145LR, 145XR, 145MP, and 145EP airplanes. This AD requires 
modification of the upper frame of the firewall for the auxiliary power 
unit (APU). This AD results from the discovery of a hole in the upper 
frame of the firewall for the APU. We are issuing this AD to ensure 
that the APU compartment is isolated from the rest of the airplane in 
the event of an APU fire. If the APU compartment is not isolated, smoke 
could enter the passenger cabin in the event of an APU fire.
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  <guid>http://thefederalregister.com/d.p/2005-11-21-05-22792</guid>
  <pubDate>Mon, Nov 21 2005 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Airbus Model A310-200 and -300 Series  Airplanes]]></title>
  <link>http://thefederalregister.com/d.p/2005-11-21-05-22971</link>
  <description><![CDATA[ The FAA proposes to adopt a new airworthiness directive (AD) 
for certain Airbus Model A310200 and 300 series airplanes. This 
proposed AD would require repetitive inspections for cracks and 
corrosion of the areas behind the scuff plates below the passenger/crew 
doors and bulk cargo door, and repair of any cracked or corroded part. 
This proposed AD also would require repetitive inspections for cracks 
of the holes of the corner doublers, the failsafe ring, and the door 
frames of the passenger/crew door structures. This proposed AD is 
prompted by reports of corrosion behind the scuff plates at passenger/
crew doors and the bulk cargo door and fatigue cracks on the corner 
doublers of the forward and aft passenger/crew door frames. We are 
proposing this AD to prevent such corrosion and fatigue cracking, which 
could result in reduced structural integrity of the door surroundings.
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  <guid>http://thefederalregister.com/d.p/2005-11-21-05-22971</guid>
  <pubDate>Mon, Nov 21 2005 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Draft Supplement Environmental Impact Statement for US 411  Connector, Bartow County, GA]]></title>
  <link>http://thefederalregister.com/d.p/2005-11-21-05-22965</link>
  <description><![CDATA[ In compliance with the National Environmental Policy Act of 
1969, the FHWA, in cooperation with the Georgia Department of 
Transportation (GDOT), have jointly prepared a Draft Supplemental 
Environmental Impact Statement (DSEIS) for proposed transportation 
improvements in the US 411 Corridor. A Notice of Availability published 
in the Federal Register on October 12, 2005 included a comment period 
through November 21, 2005. This date has been revised and extended to 
December 5, 2005, to coincide with the date listed in the EPA Federal 
Register Notice.
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  <guid>http://thefederalregister.com/d.p/2005-11-21-05-22965</guid>
  <pubDate>Mon, Nov 21 2005 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Environmental Impact Statment: Sanders and Flathead Counties, MT]]></title>
  <link>http://thefederalregister.com/d.p/2005-11-21-05-22911</link>
  <description><![CDATA[ The FHWA is issuing this notice to advise the public that the 
FHWA is rescinding the Notice of Intent (NOI) to prepare an 
environmental impact statement (EIS) for proposed improvements to the 
Thompson River Road (also known as Forest Highway 56), a county road 
located near Thompson Falls, Montana.
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  <guid>http://thefederalregister.com/d.p/2005-11-21-05-22911</guid>
  <pubDate>Mon, Nov 21 2005 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Notice of Policy Statement for Implementation of Notice and  Comment Procedures for Documents Imposing ``Binding]]></title>
  <link>http://thefederalregister.com/d.p/2005-11-21-05-22950</link>
  <description><![CDATA[ This notice establishes the Federal Transit Administration's 
(FTA, we) policy concerning notice and comment for FTA documents that 
impose binding obligations. This new policy is consistent with recent 
amendments to FTA's administrative procedures statute and provides the 
public and opportunity to comment on documents that FTA issues 
routinely.
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  <guid>http://thefederalregister.com/d.p/2005-11-21-05-22950</guid>
  <pubDate>Mon, Nov 21 2005 11:00:00 GMT</pubDate>
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