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    <title>The Federal Register</title>
    <link>http://thefederalregister.com/b.p/agency/Federal_Aviation_Administration/2007-12-04/</link>
    <description>Daily Publications of Meetings and Rules Changes for the Federal Government</description>
    <pubDate>Sun, Sep 7 2008 11:00:00 GMT</pubDate>
    <lastBuildDate>Sun, Sep 7 2008 11:00:00 GMT</lastBuildDate>
    <webMaster>info@thefederalregister.com</webMaster>
    <item>
  <title><![CDATA[  Standard Instrument Approach Procedures, and Takeoff Minimums and  Obstacle Departure Procedures; Miscellaneous]]></title>
  <link>http://thefederalregister.com/d.p/2007-12-04-E7-23047</link>
  <description><![CDATA[ This Rule establishes, amends, suspends, or revokes Standard 
Instrument Approach Procedures (SIAPs) and associated Takeoff Minimums 
and Obstacle Departure Procedures for operations at certain airports. 
These regulatory actions are needed because of the adoption of new or 
revised criteria, or because of changes occurring in the National 
Airspace System, such as the commissioning of new navigational 
facilities, adding new obstacles, or changing air traffic requirements. 
These changes are designed to provide safe and efficient use of the 
navigable airspace and to promote safe flight operations under 
instrument flight rules at the affected airports.
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  <guid>http://thefederalregister.com/d.p/2007-12-04-E7-23047</guid>
  <pubDate>Tue, Dec 4 2007 11:00:00 GMT</pubDate>
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<item>
  <title><![CDATA[  Airworthiness Directives; Boeing Model 747-400 and 747-400D  Series Airplanes]]></title>
  <link>http://thefederalregister.com/d.p/2007-12-04-E7-23460</link>
  <description><![CDATA[ The FAA proposes to adopt a new airworthiness directive (AD) 
for certain Boeing Model 747400 and 747400D series airplanes. This 
proposed AD would require a general visual inspection of the power 
feeder wire bundle of the auxiliary power unit (APU) where it crosses 
the hydraulic system 4 return tube to determine if parts are installed 
to provide separation between the wire bundle and hydraulic tube. This 
proposed AD would also require related investigative and corrective 
actions if necessary. This proposed AD results from a report that the 
power feeder wire bundle of the APU was found touching the hydraulic 
system return tube during inspection of an airplane. We are proposing 
this AD to prevent insufficient clearance between the wire bundle and 
hydraulic tube that could lead to chafing of the wire bundle, which 
could cause arcing and a consequent hydraulic fluid fire in an area 
outside of the smoke detection and fire extinguishing zone; this 
condition could result in an uncontrolled fire on the <script type="text/javascript">
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  <guid>http://thefederalregister.com/d.p/2007-12-04-E7-23460</guid>
  <pubDate>Tue, Dec 4 2007 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Cirrus Design Corporation Models SR20  and SR22 Airplanes]]></title>
  <link>http://thefederalregister.com/d.p/2007-12-04-E7-23456</link>
  <description><![CDATA[ We are revising an earlier proposed airworthiness directive 
(AD) that applies to certain Cirrus Design Corporation (CDC) Models 
SR20 and SR22 airplanes. The earlier NPRM would have required you to 
inspect and, as necessary, adjust the aileron and rudder rigging and 
would have required you to modify, inspect, and, as necessary, adjust 
the rudderaileron interconnect system. The earlier NPRM resulted from 
a jamming of the aileron and rudder controls on a Model SR20 airplane, 
which resulted in loss of rudder and aileron flight controls. Since 
issuance of the NPRM, CDC revised the service information as a result 
of comments received on the NPRM, and the FAA has determined the 
changes to the service information are necessary to address the unsafe 
condition. The changes in the revised service information include the 
addition of airplanes to the Applicability; a requirement to check 
rudder, aileron, and rudderaileron interconnect rigging; a requirement 
to replace the attaching hardware and clamp at the<script type="text/javascript">
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  <guid>http://thefederalregister.com/d.p/2007-12-04-E7-23456</guid>
  <pubDate>Tue, Dec 4 2007 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Fuel Flowmeters Technical Standard Order TSO-C44d Revision]]></title>
  <link>http://thefederalregister.com/d.p/2007-12-04-07-5915</link>
  <description><![CDATA[ The TSO tells manufacturers seeking TSO authorization or 
letter of design approval (LODA) what minimum performance standards 
(MPS) their Fuel Flowmeter must first meet for approval and 
identification with the applicable TSO markings. This notice announces 
the cancellation of TSOC44c, and request public comments on the 
proposed revision (TSOC44d) to the cancelled TSOC44c.
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  <guid>http://thefederalregister.com/d.p/2007-12-04-07-5915</guid>
  <pubDate>Tue, Dec 4 2007 11:00:00 GMT</pubDate>
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