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    <title>The Federal Register</title>
    <link>http://thefederalregister.com/b.p/department/DEPARTMENT_OF_TRANSPORTATION/2006-12-07/</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[  Airworthiness Directives; Airbus Model A300 Airplanes ]]></title>
  <link>http://thefederalregister.com/d.p/2006-12-07-E6-20616</link>
  <description><![CDATA[ The FAA is superseding an existing airworthiness directive 
(AD), which applies to all Airbus Model A300 airplanes. That AD 
currently requires repetitive inspections for cracking and corrosion in 
the lower rim area of the rear pressure bulkhead and adjacent areas, 
repetitive inspections for cracking or corrosion in the service 
apertures and the upper rim area of the rear pressure bulkhead, and 
corrective actions if necessary. This new AD removes certain repetitive 
inspections and reduces the repetitive interval of one inspection. This 
new AD also requires an inspection for missing or damaged sealant in 
the area between the outer attachment angle and circumferential joint 
doubler, and corrective action if necessary. This new AD also requires 
additional inspections for corrosion of certain areas and repetitive 
inspections for airplanes on which repairs have been done. This AD 
results from reports of corrosion and cracking in the various 
components associated with the rear pressure bulkhead. We are<script type="text/javascript">
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  <guid>http://thefederalregister.com/d.p/2006-12-07-E6-20616</guid>
  <pubDate>Thu, Dec 7 2006 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Airbus Model A300 Airplanes ]]></title>
  <link>http://thefederalregister.com/d.p/2006-12-07-E6-20617</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 airworthiness authority 
of another country to identify and correct an unsafe condition on an 
aviation product. The MCAI describes the unsafe condition as failure of 
pitch trim system 2 to deflect the trimmable horizontal stabilizer at 
maximum rate, which could result in loss of highspeed trim and 
consequent reduced controllability of the airplane. 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/2006-12-07-E6-20617</guid>
  <pubDate>Thu, Dec 7 2006 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Boeing Model 747-100, 747-100B, 747- 100B SUD, 747-200B, 747-300, 747-400, 747-400D, and]]></title>
  <link>http://thefederalregister.com/d.p/2006-12-07-E6-20618</link>
  <description><![CDATA[ The FAA is revising an existing airworthiness directive (AD) 
that applies to certain Boeing Model 747100, 747100B, 747100B SUD, 
747200B, 747300, 747400, 747400D, and 747SR series airplanes. That 
AD currently requires repetitive inspections to detect cracking of 
certain lower lobe fuselage frames, and repair if necessary. This new 
AD specifies appropriate service information for certain corrective 
actions. This AD results from reports indicating that fatigue cracks 
were found in lower lobe frames on the left side of the fuselage. We 
are issuing this AD to detect and correct fatigue cracking of certain 
lower lobe fuselage frames, which could lead to fatigue cracks in the 
fuselage skin, and consequent rapid decompression of the airplane.
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  <guid>http://thefederalregister.com/d.p/2006-12-07-E6-20618</guid>
  <pubDate>Thu, Dec 7 2006 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Boeing Model 777 Airplanes ]]></title>
  <link>http://thefederalregister.com/d.p/2006-12-07-E6-20624</link>
  <description><![CDATA[ The FAA is adopting a new airworthiness directive (AD) for 
certain Boeing Model 777 airplanes. This AD requires repetitive 
inspections for corrosion or missing corrosion inhibiting compound of 
the fuselage skin under the forward and aft wingtobody fairings for 
certain airplanes, or the fuselage skin under the forward wingtobody 
fairings only for other airplanes; and corrective action if necessary. 
The AD also provides an optional preventive modification of the fairing 
areas, which terminates the repetitive inspections. This AD results 
from several reports indicating that significant levels of corrosion 
were found on the external surface of the fuselage skin under the 
forward and aft wingtobody fairings. We are issuing this AD to detect 
and correct corrosion, and prevent subsequent fatigue cracks, on the 
fuselage skin under the forward and aft wingtobody fairings, which 
could result in rapid decompression of the airplane.
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  <guid>http://thefederalregister.com/d.p/2006-12-07-E6-20624</guid>
  <pubDate>Thu, Dec 7 2006 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Gulfstream Model G-159 Airplanes]]></title>
  <link>http://thefederalregister.com/d.p/2006-12-07-E6-20620</link>
  <description><![CDATA[ This amendment adopts a new airworthiness directive (AD), 
applicable to all Gulfstream Model G159 airplanes, that requires 
repetitive nondestructive testing inspections to detect corrosion of 
the skin of certain structural assemblies, and corrective action if 
necessary. This AD also requires xray and ultrasonic inspections to 
detect corrosion and cracking of the splicing of certain structural 
assemblies, and repair if necessary. The actions specified by this AD 
are intended to detect and correct corrosion and cracking of the lower 
wing plank splices and spotwelded skins of certain structural 
assemblies, which could result in reduced controllability of the 
airplane. This action is intended to address the identified unsafe 
condition.
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  <guid>http://thefederalregister.com/d.p/2006-12-07-E6-20620</guid>
  <pubDate>Thu, Dec 7 2006 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; EADS SOCATA Model TBM 700 Airplanes]]></title>
  <link>http://thefederalregister.com/d.p/2006-12-07-E6-20760</link>
  <description><![CDATA[ We propose to adopt a new airworthiness directive (AD) for the 
products listed above. This proposed 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 the finding of an improper geometry of some pulley 
brackets, which can offset the cable in the sheave. 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/2006-12-07-E6-20760</guid>
  <pubDate>Thu, Dec 7 2006 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Proposed Modification of Class D Airspace; Luke Air Force Base,  AZ]]></title>
  <link>http://thefederalregister.com/d.p/2006-12-07-06-9563</link>
  <description><![CDATA[ This notice proposes to modify Class D airspace at Luke Air 
Force Base (LUF), AZ. This modification is necessary to contain and 
protect circling maneuvers for Category E aircraft executing these 
maneuvers in conjunction with Standard Instrument Approach Procedures 
(SIAPs) at the airport. This action would modify the existing LUF Class 
D airspace to extend upward from the surface to, but not including, 
4,000 feet mean sea level (MSL) and extend the lateral limits from 4.4 
nautical miles (NM) to 5.6 NM from the 170[deg] bearing from the 
airport clockwise to the 046[deg] bearing from the airport.
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  <guid>http://thefederalregister.com/d.p/2006-12-07-06-9563</guid>
  <pubDate>Thu, Dec 7 2006 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Proposed Amendment of Class E Airspace; Covington, GA ]]></title>
  <link>http://thefederalregister.com/d.p/2006-12-07-06-9564</link>
  <description><![CDATA[ This notice proposes to amend Class E5 airspace at Covington, 
GA. As a result of an evaluation, it has been determined a modification 
should be made to the Covington, GA, Class E5 airspace area to contain 
the Nondirectional Radio Beacon (NDB) Runway 28, Standard Instrument 
Approach Procedure (SIAP) to Covington Municipal Airport, Covington, 
GA. Additional controlled airspace extending upward from 700 feet Above 
Ground Level (AGL) is needed to contain the SIAP.
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  <guid>http://thefederalregister.com/d.p/2006-12-07-06-9564</guid>
  <pubDate>Thu, Dec 7 2006 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Reports, Forms and Recordkeeping Requirements ]]></title>
  <link>http://thefederalregister.com/d.p/2006-12-07-06-9560</link>
  <description><![CDATA[ Before a Federal agency can collect certain information from 
the public, it must receive approval from the Office of Management and 
Budget (OMB). Under procedures established by the Paperwork Reduction 
Act of 1995 (PRA), before seeking OMB approval, Federal agencies must 
solicit public comment on proposed collections of information. In this 
case, the information collection consists of a load carrying capacity  label applied to all motor homes and recreation vehicle<br/> [[Page 71025]]<br/>
(RV) trailers and a load carrying capacity modification label which 
corrects original load carrying capacity information on all RVs and 
light vehicles when significant additional weight is added between 
final vehicle certification and first retail sale. The load carrying 
capacity modification label is an alternative to current methods of 
information correction which requires the original label to be 
replaced. A PRA 60day notice was included with the published notice of 
proposed rulemaking (NPRM) on October 31, 2005 (70 F<script type="text/javascript">
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  <guid>http://thefederalregister.com/d.p/2006-12-07-06-9560</guid>
  <pubDate>Thu, Dec 7 2006 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Midtown TDR Ventures LLC--Acquisition Exemption--American Premier  Underwriters, Inc., The Owasco River Railway, Inc.,]]></title>
  <link>http://thefederalregister.com/d.p/2006-12-07-E6-20655</link>
  <description><![CDATA[
</p><p>    Midtown TDR Ventures LLC, a noncarrier, filed a notice of exemption 
under 49 CFR 1150.31 to acquire 156 miles of rail line and certain  assets related to Grand Central Terminal in New York City <br/>
(collectively, Properties) from American Premier Underwriters, Inc. 
(APU), a noncarrier, APU's wholly owned subsidiary, The Owasco River 
Railway, Inc., a noncarrier, and APU's parent, American Financial 
Group, Inc., a noncarrier, (collectively, Sellers). The acquired rail 
line, referred to as the ``HarlemHudson Line,'' extends from milepost 
0.0 at Grand Central Terminal in New York City to milepost 5.2 at Mott 
Junction, thereafter, diverging in two directions, with one line 
running north to milepost 75.7 at Poughkeepsie, NY, and a second line 
proceeding east to milepost 11.8 at Woodlawn Junction, then north to  milepost 82.0 at Wassaic, NY.</p><p>    Midtown will acquire a fee simple interest in the Properties, 
subject to an existing longterm lease to Metropolitan Transportation 
Authority (MTA), which grants<script type="text/javascript">
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  <guid>http://thefederalregister.com/d.p/2006-12-07-E6-20655</guid>
  <pubDate>Thu, Dec 7 2006 11:00:00 GMT</pubDate>
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