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    <title>The Federal Register</title>
    <link>http://thefederalregister.com/b.p/agency/Federal_Aviation_Administration/2008-06-20/</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[  Miscellaneous Markings and Placards ]]></title>
  <link>http://thefederalregister.com/d.p/2008-06-20-E8-13900</link>
  <description><![CDATA[ This action corrects a typographical error that appeared in a 
final rule, which the FAA published in the Federal Register. In that 
final rule, the FAA inadvertently changed a word. The intent of this 
action is to correct the error in the regulation to ensure the 
requirement is clear and accurate.
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  <guid>http://thefederalregister.com/d.p/2008-06-20-E8-13900</guid>
  <pubDate>Fri, Jun 20 2008 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/2008-06-20-E8-13919</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 currently requires 
repetitive tests for free movement of the capsule/bearing of the nose 
landing gear (NLG), and related investigative and corrective actions. 
This proposed AD would require a modified test for free movement of the 
capsule/bearing of the NLG at reduced repeat intervals, and replacement 
of the NLG assembly with a modified assembly. This proposed AD results 
from additional reports of the NLG failing to extend fully on an 
airplane that had been inspected in accordance with AD 20041407. We 
are proposing this AD to prevent failure of the NLG to extend fully, 
which could result in reduced controllability of the airplane during 
landing.
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  <guid>http://thefederalregister.com/d.p/2008-06-20-E8-13919</guid>
  <pubDate>Fri, Jun 20 2008 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Boeing Model 707 Airplanes and Model  720 and 720B Series Airplanes]]></title>
  <link>http://thefederalregister.com/d.p/2008-06-20-E8-13925</link>
  <description><![CDATA[ We propose to adopt a new airworthiness directive (AD) for all 
Boeing Model 707 airplanes and Model 720 and 720B series airplanes. 
This proposed AD would require performing an operational test of the 
engine fuel suction feed of the fuel system, and other related testing 
if necessary. This proposed AD results from a report of inservice 
occurrences of loss of fuel system suction feed capability, followed by 
total loss of pressure of the fuel feed system. We are proposing this 
AD to detect and correct failure of the engine fuel suction feed of the 
fuel system, which could result in multiengine flameout, inability to 
restart the engines, and consequent forced landing of the airplane.
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  <guid>http://thefederalregister.com/d.p/2008-06-20-E8-13925</guid>
  <pubDate>Fri, Jun 20 2008 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Boeing Model 727 Airplanes ]]></title>
  <link>http://thefederalregister.com/d.p/2008-06-20-E8-13920</link>
  <description><![CDATA[ We propose to adopt a new airworthiness directive (AD) for 
certain Boeing Model 727 airplanes. This proposed AD would require 
performing an operational test of the engine fuel suction feed of the 
fuel system, and other related testing if necessary. This proposed AD 
results from a report of inservice occurrences of loss of fuel system 
suction feed capability, followed by total loss of pressure of the fuel 
feed system. We are proposing this AD to detect and correct failure of 
the engine fuel suction feed of the fuel system, which could result in 
multiengine flameout, inability to restart the engines, and consequent  forced landing of the airplane.<br/>
[[Page 35094]]
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  <guid>http://thefederalregister.com/d.p/2008-06-20-E8-13920</guid>
  <pubDate>Fri, Jun 20 2008 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Bombardier Model CL-600-2B19 (Regional  Jet Series 100 and 440) Airplanes]]></title>
  <link>http://thefederalregister.com/d.p/2008-06-20-E8-13922</link>
  <description><![CDATA[ We propose to adopt a new airworthiness directive (AD) for the 
products listed above that would supersede an existing AD. This 
proposed AD results from mandatory continuing airworthiness information 
(MCAI) originated by an 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>    Bombardier Aerospace has completed a system safety review of the 
aircraft fuel system against fuel tank safety standards * * *.
    [A]ssessment showed that supplemental maintenance tasks [for 
certain bonding jumpers, wiring harnesses, and hydraulic systems, 
among other items] are required to prevent potential ignition 
sources inside the fuel system, which could result in a fuel tank  explosion. * * *<br/>
The proposed AD would require actions that are intended to address the 
unsafe condition described in the MCAI.
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  <guid>http://thefederalregister.com/d.p/2008-06-20-E8-13922</guid>
  <pubDate>Fri, Jun 20 2008 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/2008-06-20-E8-13923</link>
  <description><![CDATA[ The FAA proposes to supersede an existing airworthiness 
directive (AD) that applies to all EMBRAER Model EMB135 airplanes and 
Model EMB145, 145ER, 145MR, 145LR, 145XR, 145MP, and 145EP 
airplanes. The existing AD currently requires replacing the metallic 
tubes enclosing the vent and pilot valve wires in the left and right
hand wing fuel tanks with nonconductive hoses. This proposed AD would 
add airplanes to the applicability of the existing AD. This proposed AD 
results from fuel system reviews conducted by the manufacturer. We are 
proposing this AD to prevent an ignition source inside the fuel tank 
that could ignite fuel vapor and cause a fuel tank explosion and loss 
of the airplane.
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  <guid>http://thefederalregister.com/d.p/2008-06-20-E8-13923</guid>
  <pubDate>Fri, Jun 20 2008 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Hawaii Air Tour Common Procedures Manual, FAA AWP13-136A ]]></title>
  <link>http://thefederalregister.com/d.p/2008-06-20-E8-14014</link>
  <description><![CDATA[ This notice announces the availability of and requests 
comments on the proposed draft for the Hawaii Air Tour Common 
Procedures Manual, draft AWP13136A.
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  <guid>http://thefederalregister.com/d.p/2008-06-20-E8-14014</guid>
  <pubDate>Fri, Jun 20 2008 11:00:00 GMT</pubDate>
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