<?xml version='1.0' encoding='utf-8'?>

<rss version="2.0">
  <channel>
    <title>The Federal Register</title>
    <link>http://thefederalregister.com/b.p/department/DEPARTMENT_OF_TRANSPORTATION/2007-09-04/</link>
    <description>Daily Publications of Meetings and Rules Changes for the Federal Government</description>
    <pubDate>Mon, May 20 2013 11:00:00 GMT</pubDate>
    <lastBuildDate>Mon, May 20 2013 11:00:00 GMT</lastBuildDate>
    <webMaster>info@thefederalregister.com</webMaster>
    <item>
  <title><![CDATA[  Airworthiness Standards; Aircraft Engine Standards for Engine  Life-Limited Parts]]></title>
  <link>http://thefederalregister.com/d.p/2007-09-04-E7-17369</link>
  <description><![CDATA[ The FAA is amending the certification standards for original 
and amended type certificates for aircraft engines by modifying the 
standards for engine lifelimited parts. This final rule establishes 
new and uniform standards for the design and testing of lifelimited 
parts for aircraft engines certificated by the FAA and the European 
Aviation Safety Agency (EASA). This rule retains the current lifing 
requirements, introduces damage tolerance requirements into the design  process, and strengthens cooperation between engineering, <br/>
manufacturing, and service elements of turbine engine manufacturers. 
These new requirements provide an added margin of safety and will 
reduce the number of lifelimited parts failures due to material, 
manufacturing, and service induced anomalies. Additionally, this action 
adds new standards for the design of reciprocating engine turbocharger 
rotors.
<script type="text/javascript">
<!--
google_ad_client = "pub-2051746026283201";
google_ad_width = 728;
google_ad_height = 15;
google_ad_format = "728x15_0ads_al";
//2007-08-22: federalregister-rss
google_ad_channel = "2005962856";
google_color_border = "CC0000";
google_color_bg = "FFFFFF";
google_color_link = "CC0000";
google_color_text = "000000";
google_color_url = "008000";
//-->
</script>
<script type="text/javascript"
  src="http://pagead2.googlesyndication.com/pagead/show_ads.js">
</script>
]]></description>
  <guid>http://thefederalregister.com/d.p/2007-09-04-E7-17369</guid>
  <pubDate>Tue, Sep 4 2007 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Standards: Safety Analysis ]]></title>
  <link>http://thefederalregister.com/d.p/2007-09-04-E7-17372</link>
  <description><![CDATA[ The FAA is amending the safety analysis type certification 
standard for turbine aircraft engines. This rule establishes a nearly 
uniform safety analysis standard for turbine aircraft engines certified 
in the United States under part 33 and in European countries under the 
Certification Specifications for Engines, thereby simplifying 
airworthiness approvals for import and export.
<script type="text/javascript">
<!--
google_ad_client = "pub-2051746026283201";
google_ad_width = 728;
google_ad_height = 15;
google_ad_format = "728x15_0ads_al";
//2007-08-22: federalregister-rss
google_ad_channel = "2005962856";
google_color_border = "CC0000";
google_color_bg = "FFFFFF";
google_color_link = "CC0000";
google_color_text = "000000";
google_color_url = "008000";
//-->
</script>
<script type="text/javascript"
  src="http://pagead2.googlesyndication.com/pagead/show_ads.js">
</script>
]]></description>
  <guid>http://thefederalregister.com/d.p/2007-09-04-E7-17372</guid>
  <pubDate>Tue, Sep 4 2007 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Honeywell International Inc. TFE731-2C,  -3B, -3BR, -3C, -3CR, -3D, -3DR, -4R, -5AR, -5BR,]]></title>
  <link>http://thefederalregister.com/d.p/2007-09-04-E7-17384</link>
  <description><![CDATA[ The FAA proposes to adopt a new airworthiness directive (AD) 
for Honeywell International Inc. (Honeywell) TFE7312C, 3B, 3BR, 3C, 
3CR, 3D, 3DR, 4R, 5AR, 5BR, 5R, 20R, 20AR, 20BR, 40, 40AR, 
40R, and 60 series turbofan engines. This proposed AD would require 
removal from service of certain high pressure (HP) turbine rotor 
assemblies with part numbers (P/Ns) 30757721 and 30608411 using a 
drawdown schedule, and returning them to Honeywell for curvic root 
radius inspection. This proposed AD results from the manufacturer's 
report that some HP turbine rotor discs received improperly machined 
radii in the root of the forward and aft curvic teeth during 
manufacture. We are proposing this AD to prevent uncontained failure of 
the HP turbine rotor assembly and damage to the airplane.
<script type="text/javascript">
<!--
google_ad_client = "pub-2051746026283201";
google_ad_width = 728;
google_ad_height = 15;
google_ad_format = "728x15_0ads_al";
//2007-08-22: federalregister-rss
google_ad_channel = "2005962856";
google_color_border = "CC0000";
google_color_bg = "FFFFFF";
google_color_link = "CC0000";
google_color_text = "000000";
google_color_url = "008000";
//-->
</script>
<script type="text/javascript"
  src="http://pagead2.googlesyndication.com/pagead/show_ads.js">
</script>
]]></description>
  <guid>http://thefederalregister.com/d.p/2007-09-04-E7-17384</guid>
  <pubDate>Tue, Sep 4 2007 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Environmental Impact Statement; Washoe County, NV ]]></title>
  <link>http://thefederalregister.com/d.p/2007-09-04-07-4300</link>
  <description><![CDATA[ The FHWA is issuing this notice to advise the public that an 
Environmental Impact Statement (EIS) will be prepared for a proposed 
intersection improvement project in the City of Sparks, Washoe County, 
NV.
<script type="text/javascript">
<!--
google_ad_client = "pub-2051746026283201";
google_ad_width = 728;
google_ad_height = 15;
google_ad_format = "728x15_0ads_al";
//2007-08-22: federalregister-rss
google_ad_channel = "2005962856";
google_color_border = "CC0000";
google_color_bg = "FFFFFF";
google_color_link = "CC0000";
google_color_text = "000000";
google_color_url = "008000";
//-->
</script>
<script type="text/javascript"
  src="http://pagead2.googlesyndication.com/pagead/show_ads.js">
</script>
]]></description>
  <guid>http://thefederalregister.com/d.p/2007-09-04-07-4300</guid>
  <pubDate>Tue, Sep 4 2007 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Electronically Controlled Pneumatic Brake Systems ]]></title>
  <link>http://thefederalregister.com/d.p/2007-09-04-07-4297</link>
  <description><![CDATA[ FRA proposes revisions to the regulations governing freight 
power brakes and equipment by adding a new subpart addressing 
electronically controlled pneumatic (ECP) brake systems. The proposed 
regulations are designed to provide for and encourage the safe 
implementation and use of ECP brake system technologies. The proposal 
contains specific requirements relating to design, interoperability, 
training, inspection, testing, handling defective equipment, and 
periodic maintenance related to ECP brake systems. The document also 
identifies provisions of the existing regulations and statutes where 
FRA is proposing to provide flexibility to facilitate the introduction 
of this advanced brake system technology.
<script type="text/javascript">
<!--
google_ad_client = "pub-2051746026283201";
google_ad_width = 728;
google_ad_height = 15;
google_ad_format = "728x15_0ads_al";
//2007-08-22: federalregister-rss
google_ad_channel = "2005962856";
google_color_border = "CC0000";
google_color_bg = "FFFFFF";
google_color_link = "CC0000";
google_color_text = "000000";
google_color_url = "008000";
//-->
</script>
<script type="text/javascript"
  src="http://pagead2.googlesyndication.com/pagead/show_ads.js">
</script>
]]></description>
  <guid>http://thefederalregister.com/d.p/2007-09-04-07-4297</guid>
  <pubDate>Tue, Sep 4 2007 11:00:00 GMT</pubDate>
</item>
</channel>
</rss>

