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    <title>The Federal Register</title>
    <link>http://thefederalregister.com/b.p/department/DEPARTMENT_OF_TRANSPORTATION/2007-11-29/</link>
    <description>Daily Publications of Meetings and Rules Changes for the Federal Government</description>
    <pubDate>Sun, Oct 12 2008 11:00:00 GMT</pubDate>
    <lastBuildDate>Sun, Oct 12 2008 11:00:00 GMT</lastBuildDate>
    <webMaster>info@thefederalregister.com</webMaster>
    <item>
  <title><![CDATA[  Airworthiness Directives; Cirrus Design Corporation Model SR22  Airplanes]]></title>
  <link>http://thefederalregister.com/d.p/2007-11-29-E7-23118</link>
  <description><![CDATA[ The FAA is adopting a new airworthiness directive (AD) for 
certain Cirrus Design Corporation (Cirrus) Model SR22 airplanes. This 
AD requires you to install a drain hole in the left and right outboard 
wing tips. This AD results from reports of pilots' inability to move 
the aileron control without using excessive force when flying in 
freezing conditions. Moisture from a prior rain shower entered through 
a gap at the interface of the left and right outboard wing tips and 
wing structure. The moisture traveled along the aft wing shear web, 
accumulated below the aileron control pulley, and froze at an altitude 
with an outside air temperature below freezing. When this moisture is 
exposed to freezing conditions, operation of the aileron control pulley 
is impaired. We are issuing this AD to prevent moisture from 
accumulating along the wing shear web where it may freeze in certain 
conditions. This condition could result in operational failure of the 
aileron control pulley, which could lead to loss of con<script type="text/javascript">
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  <guid>http://thefederalregister.com/d.p/2007-11-29-E7-23118</guid>
  <pubDate>Thu, Nov 29 2007 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; GROB-WERKE GMBH & CO KG Models G102  CLUB ASTIR III, G102 CLUB ASTIR IIIb, and G102 STANDARD]]></title>
  <link>http://thefederalregister.com/d.p/2007-11-29-E7-23016</link>
  <description><![CDATA[ We are adopting a new airworthiness directive (AD) for the 
products listed above. This AD results from mandatory continuing 
airworthiness information (MCAI) issued 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>    GROB received isolated difficulty reports regarding cracks on 
welded parts of the flight control system of the type G102, model 
CLUB ASTIR III & IIIb, and STANDARD ASTIR III. The cracks progress 
slowly from the welding seams periphery, and may eventually result  in rupture at a matured stage.</p><p>    We are issuing this AD to require actions to correct the unsafe 
condition on these products.
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  <guid>http://thefederalregister.com/d.p/2007-11-29-E7-23016</guid>
  <pubDate>Thu, Nov 29 2007 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Hartzell Propeller Inc. Model HC-E5N-3(  ), HC-E5N-3( )(L), and HC-E5B-5( ) Propellers]]></title>
  <link>http://thefederalregister.com/d.p/2007-11-29-E7-23119</link>
  <description><![CDATA[ The FAA is adopting a new airworthiness directive (AD) for 
Hartzell Propeller Inc. Model HCE5N3( ), HCE5N3( )(L), and HCE5B
5( ) propellers. This AD requires a onetime eddy current inspection of 
the propeller hub mounting bolt holes and replacement of the propeller 
hub if cracked. This AD results from the discovery of a fivebladed 
propeller hub with a large crack on the mounting flange of the hub. We 
are issuing this AD to prevent propeller hub failure, blade separation, 
damage to the airplane, and possible loss of airplane control.
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  <guid>http://thefederalregister.com/d.p/2007-11-29-E7-23119</guid>
  <pubDate>Thu, Nov 29 2007 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Information Collection Available for Public Comments and  Recommendations]]></title>
  <link>http://thefederalregister.com/d.p/2007-11-29-E7-23152</link>
  <description><![CDATA[ In accordance with the Paperwork Reduction Act of 1995, this 
notice announces the Maritime Administration's (MARAD's) intention to 
request extension of approval for three years of a currently approved 
information collection.
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  <guid>http://thefederalregister.com/d.p/2007-11-29-E7-23152</guid>
  <pubDate>Thu, Nov 29 2007 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Rolls-Royce plc, RB211 Trent 768-60,  772-60, and 772B-60 Turbofan Engines]]></title>
  <link>http://thefederalregister.com/d.p/2007-11-29-E7-23020</link>
  <description><![CDATA[ The FAA is superseding an existing airworthiness directive 
(AD) for RollsRoyce plc (RR) RB211 Trent 76860, 77260, and 772B60 
turbofan engines. That AD currently requires initial and repetitive on
wing or inshop inspections of the high pressure/intermediate pressure 
(HP/IP) turbine bearing oil feed tube heat shield. This AD requires the 
same actions but introduces a terminating action to the repetitive 
inspections. This AD results from RR introducing a revised HP/IP 
turbine bearing support structure as terminating action to the 
repetitive inspections of the HP/IP turbine bearing oil feed tube heat 
shield. We are issuing this AD to prevent an uncontained failure of the 
HP turbine disc and damage to the airplane.
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  <guid>http://thefederalregister.com/d.p/2007-11-29-E7-23020</guid>
  <pubDate>Thu, Nov 29 2007 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Turbomeca Arriel 2S1 and 2S2 Turboshaft  Engines]]></title>
  <link>http://thefederalregister.com/d.p/2007-11-29-E7-23031</link>
  <description><![CDATA[ We are adopting a new airworthiness directive (AD) for the 
products listed above. This AD results from mandatory continuing [[Page 67563]]<br/>
airworthiness information (MCAI) provided by the European Aviation 
Safety Agency (EASA) to identify and correct an unsafe condition on 
Turbomeca Arriel 2S1 and 2S2 turboshaft engines. The MCAI states the  following:</p><p>    During assembly of a new HP/LP fuel pump, the drain screw on the 
fuel filter unit failed when it was tightened to the torque value 
specified in the assembly schedule (12 Nm). Investigation of the 
screw showed that it was fully conformed to its specification, in 
terms of both dimensions and material. The mechanical calculations 
show, however, that a torque value of 12 Nm is too high for this 
screw, exceeding the elastic limit of the material. Failure of the 
affected screw could cause a fuel leak, resulting in an engine  flameout or engine fire.<br/>
We are issuing this AD to prevent a fuel leak as a result of a ruptured 
fuel filter drain screw that co<script type="text/javascript">
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  <guid>http://thefederalregister.com/d.p/2007-11-29-E7-23031</guid>
  <pubDate>Thu, Nov 29 2007 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  IFR Altitudes; Miscellaneous Amendments ]]></title>
  <link>http://thefederalregister.com/d.p/2007-11-29-E7-23176</link>
  <description><![CDATA[ This amendment adopts miscellaneous amendments to the required 
IFR (instrument flight rules) altitudes and changeover points for 
certain Federal airways, jet routes, or direct routes for which a 
minimum or maximum en route authorized IFR altitude is prescribed. This 
regulatory action is needed because of changes occurring in the 
National Airspace System. These changes are designed to provide for the 
safe and efficient use of the navigable airspace under instrument 
conditions in the affected areas.
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  <guid>http://thefederalregister.com/d.p/2007-11-29-E7-23176</guid>
  <pubDate>Thu, Nov 29 2007 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Proposed Modification of Class E Airspace; Hollister, CA ]]></title>
  <link>http://thefederalregister.com/d.p/2007-11-29-E7-23173</link>
  <description><![CDATA[ This action proposes to modify the Class E airspace area at 
Hollister, CA. Establishment of an Area Navigation (RNAV) Global 
Positioning System (GPS) Standard Instrument Approach Procedure (SIAP) 
at Hollister Municipal Airport, Hollister, CA, has made this proposal 
necessary. Additional controlled airspace is needed for the safety and 
management of aircraft executing the new RNAV (GPS) SIAPs at Hollister 
Municipal Airport, Hollister, CA.
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  <guid>http://thefederalregister.com/d.p/2007-11-29-E7-23173</guid>
  <pubDate>Thu, Nov 29 2007 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Proposed Establishment of Low Altitude Area Navigation Routes (T- Routes); St. Louis, MO]]></title>
  <link>http://thefederalregister.com/d.p/2007-11-29-E7-23175</link>
  <description><![CDATA[ This action proposes to establish two low altitude Area 
Navigation (RNAV) routes, designated T251 and T272, in the St. Louis, 
MO, terminal area. Troutes are low altitude Air Traffic Service 
routes, based on RNAV, for use by aircraft that have instrument flight 
rules (IFR) approved Global Positioning System (GPS)/Global Navigation 
Satellite System (GNSS) equipment. The FAA is proposing this action to 
enhance safety and improve the efficient use of the navigable airspace 
in the St. Louis, MO, terminal area.
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  <guid>http://thefederalregister.com/d.p/2007-11-29-E7-23175</guid>
  <pubDate>Thu, Nov 29 2007 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Noise Compatibility Program Notice Baton Rouge Metropolitan  Airport, Ryan Field, Baton Rouge, LA]]></title>
  <link>http://thefederalregister.com/d.p/2007-11-29-07-5873</link>
  <description><![CDATA[ The Federal Aviation Administration (FAA) announces its 
findings on the noise compatibility program submitted by the Greater 
Baton Rouge Airport District under the provisions of 49 U.S.C. (the 
Aviation Safety and Noise Abatement Act, hereinafter referred to as 
``the Act'') and 14 CFR part 150. These findings are made in  recognition of the description of Federal and nonfederal <br/>
responsibilities in Senate Report No. 9652 (1980). On July 30, 2007, 
the FAA determined that the noise exposure maps submitted by the 
Greater Baton Rouge Airport District under part 150 were in compliance 
with applicable requirements. On November 13, 2007, the FAA approved 
the Baton Rouge Metropolitan Airport, Ryan Field noise compatibility 
program. Most of the recommendations of the program were approved. No 
program elements relating to new or revised flight procedures for noise 
abatement were proposed by the airport operator.
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  <guid>http://thefederalregister.com/d.p/2007-11-29-07-5873</guid>
  <pubDate>Thu, Nov 29 2007 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Canadian Pacific Railway Company, et al.--Control--Dakota,  Minnesota & Eastern Railroad Corp., et al.]]></title>
  <link>http://thefederalregister.com/d.p/2007-11-29-E7-23146</link>
  <description><![CDATA[ The Surface Transportation Board (Board) invites public 
comments on a proposed procedural schedule for this proceeding. On 
October 5, 2007, Canadian Pacific Railway Corporation (CPRC), Soo Line 
Holding Company, a Delaware Corporation and indirect subsidiary of CPRC 
(Soo Holding), Dakota, Minnesota & Eastern Railroad Corporation (DM&E), 
and Iowa, Chicago & Eastern Railroad Corporation, a whollyowned rail 
subsidiary of DM&E (IC&E) (collectively referred to as the 
``Applicants'') submitted a filing with the Board seeking approval 
under 49 U.S.C. 1132126 of the acquisition of control of DM&E and IC&E 
by Soo Holding (and, indirectly, by CPRC). In Decision No. 2, served on 
November 2, 2007, and published in the Federal Register at 72 FR 63232
36 on November 8, 2007, the Board accepted the October 5 submission as 
a prefiling notification, thus allowing the Applicants to perfect their 
application, and provide any supplemental materials or information, on  or after December 5, 2007.\1\<br/>
    \1\ In Decision<script type="text/javascript">
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  <guid>http://thefederalregister.com/d.p/2007-11-29-E7-23146</guid>
  <pubDate>Thu, Nov 29 2007 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Canadian National Railway Company and Grand Trunk Corporation-- Control--EJ&E West Company \1\]]></title>
  <link>http://thefederalregister.com/d.p/2007-11-29-E7-23151</link>
  <description><![CDATA[ The Surface Transportation Board (Board) is accepting for 
consideration the primary application filed October 30, 2007, by 
Canadian National Railway Corporation (CNR) and Grand Trunk Corporation 
(GTC), a noncarrier holding company through which CNR controls its U.S. 
rail subsidiaries, and seven related filings. The primary application 
seeks Board approval under 49 U.S.C. 1132126 of the acquisition of 
control of EJ&E West Company (EJ&EW), a wholly owned noncarrier 
subsidiary of Elgin, Joliet and Eastern Railway Company (EJ&E), by CNR 
and GTC. This proposal is referred to as the Control Transaction, and  CNR and GTC are referred to collectively as applicants.</p><p>    The related filings are notices of exemption involving an intra
corporate family transaction and the granting of trackage rights. The 
SubNo. 1 filing provides for EJ&E to transfer property to EJ&EW, 
which, at that time, would become a rail common carrier, prior to 
applicants acquiring control of EJ&EW. The SubNos. 2 through 7 filings 
provi<script type="text/javascript">
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  <pubDate>Thu, Nov 29 2007 11:00:00 GMT</pubDate>
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