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    <title>The Federal Register</title>
    <link>http://thefederalregister.com/b.p/agency/Federal_Aviation_Administration/2005-05-02/</link>
    <description>Daily Publications of Meetings and Rules Changes for the Federal Government</description>
    <pubDate>Fri, May 24 2013 11:00:00 GMT</pubDate>
    <lastBuildDate>Fri, May 24 2013 11:00:00 GMT</lastBuildDate>
    <webMaster>info@thefederalregister.com</webMaster>
    <item>
  <title><![CDATA[  Revision of Class E Airspace; Nome, AK ]]></title>
  <link>http://thefederalregister.com/d.p/2005-05-02-05-8723</link>
  <description><![CDATA[ This action revises Class E airspace at Nome, AK to provide 
adequate controlled airspace to contain aircraft executing new Standard 
Instrument Approach Procedures (SIAP). This Rule results in additional 
Class E surface area and Class E airspace upward from 700 feet (ft.) 
and 1,200 ft. above the surface at Nome, AK.
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  <guid>http://thefederalregister.com/d.p/2005-05-02-05-8723</guid>
  <pubDate>Mon, May 2 2005 11:00:00 GMT</pubDate>
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<item>
  <title><![CDATA[  Airworthiness Directives; BAE Systems (Operations) Limited  (Jetstream) Model 4101 Airplanes]]></title>
  <link>http://thefederalregister.com/d.p/2005-05-02-05-8656</link>
  <description><![CDATA[ The FAA proposes to supersede an existing airworthiness 
directive (AD) that applies to all BAE Systems (Operations) Limited 
(Jetstream) Model 4101 airplanes. The existing AD requires operators to 
determine the number of flight cycles accumulated on each component of 
the main landing gear (MLG) and the nose landing gear (NLG), and to 
replace each component that reaches its life limit with a serviceable 
component. The existing AD also requires operators to revise the 
Airworthiness Limitations section (ALS) of the Instructions for 
Continued Airworthiness in the aircraft maintenance manual to reflect 
the new life limits. This proposed AD would require revising the ALS to 
incorporate extended and more restrictive life limits for structurally 
significant items. This proposed AD is prompted by engineering analysis 
of fleet operations which resulted in more restrictive life limits. We 
are proposing this AD to prevent failure of certain structurally 
significant items, including the MLG and the NLG, whic<script type="text/javascript">
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  <guid>http://thefederalregister.com/d.p/2005-05-02-05-8656</guid>
  <pubDate>Mon, May 2 2005 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Boeing Model 737-600, -700, -700C, - 800, and -900 Series Airplanes]]></title>
  <link>http://thefederalregister.com/d.p/2005-05-02-05-8654</link>
  <description><![CDATA[ The FAA proposes to adopt a new airworthiness directive (AD) 
for all Boeing Model 737600, 700, 700C, 800, and 900 series 
airplanes. This proposed AD would require repetitive inspections of the 
aft pressure bulkhead web for fatigue cracks, crack indications, 
discrepant holes, and corrosion, and repair if necessary. This proposed 
AD is prompted by reports of fatigue cracks in the aft pressure 
bulkhead web. We are proposing this AD to detect and correct such 
fatigue cracks, which could result in a rapid decompression of the 
airplane.
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  <guid>http://thefederalregister.com/d.p/2005-05-02-05-8654</guid>
  <pubDate>Mon, May 2 2005 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Boeing Model 727 Airplanes ]]></title>
  <link>http://thefederalregister.com/d.p/2005-05-02-05-8655</link>
  <description><![CDATA[ The FAA proposes to adopt a new airworthiness directive (AD) 
for all Boeing Model 727 airplanes. This proposed AD would require a 
onetime inspection of the lower lobe frames of body section 43 to find 
open holes between stringers 17L and 17R; repetitive high frequency 
eddy current (HFEC) inspections for cracks of all open holes; and 
related investigative and corrective actions if necessary. The proposed 
AD also would include the optional terminating action of installing 
rivets in all open tooling holes and all unused lining holes, which 
would terminate a repetitive openhole HFEC inspection once a hole is 
plugged with a rivet. This proposed AD is prompted by reports of cracks 
at open tooling holes in the lower lobe frames of body section 43. We 
are proposing this AD to detect and correct cracks in the frames, which 
could result in cracks in the skin panels and rapid decompression of 
the airplane.
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  <guid>http://thefederalregister.com/d.p/2005-05-02-05-8655</guid>
  <pubDate>Mon, May 2 2005 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; McDonnell Douglas Model DC-9-81 (MD- 81), DC-9-82 (MD-82), DC-9-83 (MD-83), DC-9-87 (MD-87),]]></title>
  <link>http://thefederalregister.com/d.p/2005-05-02-05-8657</link>
  <description><![CDATA[ This document revises an earlier proposed airworthiness 
directive (AD), applicable to certain McDonnell Douglas airplane 
models, that would have required a onetime inspection for chafing or 
signs of arcing of the wire bundle for the auxiliary hydraulic pump, 
and other specified and corrective actions, as applicable. This new 
action revises the proposed rule by referring to revised procedures for 
performing the corrective and other specified actions. The actions 
specified by this new proposed AD are intended to prevent shorted wires 
or arcing at the auxiliary hydraulic pump, which could result in loss 
of auxiliary hydraulic power, or a fire in the wheel well of the 
airplane. This action is intended to address the identified unsafe 
condition.
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  <guid>http://thefederalregister.com/d.p/2005-05-02-05-8657</guid>
  <pubDate>Mon, May 2 2005 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Public Notice for a Change in Use of Aeronautical Property at  Millville Municipal Airport, Millville, New Jersey]]></title>
  <link>http://thefederalregister.com/d.p/2005-05-02-05-8724</link>
  <description><![CDATA[ The FAA is requesting public comment on the proposed release 
of approximately 140 acres of airport property on the south side of 
Millville Municipal Airport to permit its sale and development of a 
motorsport park. The airport land was deeded to the City of Millville 
under a quitclaim conveyance form the United States. It was later 
transferred to the Delaware River and Bay Authority (DRBA). FAA's 
action is to release the land from the deed provisions requiring 
aeronautical use of the property. The DRBA has stated that it has no 
aeronautical use for the parcel now or in the near future, according to 
the approved Airport Layout Plan. It will also be released from a 
reverter clause in the quitclaim deed. The Fair Market Value for the 
land as determined by appraisals will be paid to the DRBA for the 
maintenance, operation and capital development of the airport. [[Page 22749]]</p><p>    The motorsport park will consist of 4 racecourses, 2 paddock areas,  2 motels, 2 hotels, clubhouses, etc.</p><p>    Any comments <script type="text/javascript">
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  <guid>http://thefederalregister.com/d.p/2005-05-02-05-8724</guid>
  <pubDate>Mon, May 2 2005 11:00:00 GMT</pubDate>
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