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    <title>The Federal Register</title>
    <link>http://thefederalregister.com/b.p/department/DEPARTMENT_OF_TRANSPORTATION/2006-12-11/</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; Columbia Aircraft Manufacturing Models  LC41-550FG and LC42-550FG Airplanes]]></title>
  <link>http://thefederalregister.com/d.p/2006-12-11-E6-20860</link>
  <description><![CDATA[ The FAA is adopting a new Airworthiness Directive (AD) for all 
Columbia Aircraft Manufacturing (previously The Lancair Company) Models 
LC41550FG and LC42550FG airplanes equipped with Kelly Aerospace 
Thermal Systems Supplemental Type Certificate (STC) SA02260CH, 
Thermawing Deice System (also known as EVade). This AD requires you to 
deactivate the deice system and install a placard in clear view of the 
pilot. This AD results from problems with the installation of the Kelly 
Aerospace Thermal Systems Thermawing Deice System following STC 
SA02260CH. We are issuing this AD to prevent a short circuit condition 
at the deice heater connector, which could result in damage to the 
wings and horizontal stabilizer. This damage could lead to reduced 
structural integrity of the airplane.
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  <guid>http://thefederalregister.com/d.p/2006-12-11-E6-20860</guid>
  <pubDate>Mon, Dec 11 2006 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Empresa Brasileira de Aeronautica S.A.  (EMBRAER) Model EMB-135ER and -135KE Airplanes; and]]></title>
  <link>http://thefederalregister.com/d.p/2006-12-11-E6-20862</link>
  <description><![CDATA[ The FAA is adopting a new airworthiness directive (AD) for all 
EMBRAER Model EMB135ER and 135KE airplanes and Model EMB145, 145ER, 
145MR, 145MP, and 145EP airplanes. This AD requires inspecting the 
fuel quantity indication system (FQIS) wire harness and the direct 
current (DC) fuel pump wire harness to determine if the harnesses are 
properly attached at their respective attachment points and properly 
separated from one another, and performing corrective actions if 
necessary. This AD results from a report that the FQIS wire harness may 
not be properly attached at its attachment points or properly separated 
from the DC fuel pump wire harness. We are issuing this AD to prevent 
chafing between those harnesses or chafing of the harnesses against 
adjacent airplane structure or components, which could present a 
potential ignition source that could result in a fire or explosion.
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  <guid>http://thefederalregister.com/d.p/2006-12-11-E6-20862</guid>
  <pubDate>Mon, Dec 11 2006 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Fokker Model F27 Mark 500 Airplanes]]></title>
  <link>http://thefederalregister.com/d.p/2006-12-11-E6-20861</link>
  <description><![CDATA[ The FAA is adopting a new airworthiness directive (AD) for all 
Fokker Model F27 Mark 500 airplanes. This AD requires an inspection to 
determine whether certain main landing gear (MLG) drag stay units 
(DSUs) are installed. This AD also requires an ultrasonic inspection to 
determine if certain tubes are installed in the affected DSUs of the 
MLG, and related investigative/corrective actions if necessary. This AD 
results from a report that, due to fatigue cracking from an improperly 
machined radius of the inner tube, a drag stay broke, and, 
consequently, led to the collapse of the MLG during landing. We are 
issuing this AD to prevent such fatigue cracking, which could result in 
reduced structural integrity or collapse of the MLG.
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  <guid>http://thefederalregister.com/d.p/2006-12-11-E6-20861</guid>
  <pubDate>Mon, Dec 11 2006 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Bombardier Model DHC-8-102, -103, and - 106 Airplanes; and Model DHC-8-200 and DHC-8-300]]></title>
  <link>http://thefederalregister.com/d.p/2006-12-11-E6-20969</link>
  <description><![CDATA[ The FAA proposes to adopt a new airworthiness directive (AD) 
for certain Bombardier Model DHC8100 (as described above), DHC8200, 
and DHC8300 series airplanes. This proposed AD would require doing a 
onetime inspection for damage of the electrical cable harness assembly 
located on the left and right wing root to fuselage aft seal, and 
repair if necessary; and reworking the fuselage aft seal assembly (left 
and right) to create a clearance between the electrical cable 
assemblies and the edge of the fairing panel. This proposed AD results 
from a report that an airplane encountered an uncommanded propeller 
feathering during climb, which resulted in an emergency landing. We are 
proposing this AD to prevent chafing or grounding of the wiring against 
the aft seal assemblies, which, if not corrected, could interrupt the 
operation of various systems, including the propeller feather control, 
alternating current (AC) electrical power, and standby hydraulic power, 
and result in reduced controllability of the<script type="text/javascript">
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  <guid>http://thefederalregister.com/d.p/2006-12-11-E6-20969</guid>
  <pubDate>Mon, Dec 11 2006 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Pacific Aerospace Corporation Ltd Model  750XL Airplanes]]></title>
  <link>http://thefederalregister.com/d.p/2006-12-11-E6-20976</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 possible undersize rivets in the fuselage roof at STN 
180.85, BL 19.67, WL 86.2. 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/2006-12-11-E6-20976</guid>
  <pubDate>Mon, Dec 11 2006 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Pilatus Aircraft Limited PC-12 and PC- 12/45 Airplanes]]></title>
  <link>http://thefederalregister.com/d.p/2006-12-11-E6-20971</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 executive seats equipped with pedestal legs that were 
produced using a material that deviates from the approved design data. 
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/2006-12-11-E6-20971</guid>
  <pubDate>Mon, Dec 11 2006 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Raytheon Aircraft Company (The Beech  Aircraft Company and BEECH Previously Held Type]]></title>
  <link>http://thefederalregister.com/d.p/2006-12-11-E6-20970</link>
  <description><![CDATA[ We propose to supersede Airworthiness Directive (AD) 72-22-01, 
which applies to certain Raytheon Aircraft Company (RAC) (The Beech 
Aircraft Company and BEECH previously held Type Certificate Nos. 3A15, 
3A16, 5A3, and A777) Models 33, 35, 36, 45, and 95 series airplanes. 
AD 722201 currently requires you to determine if each uplock roller 
is of the greasible type (one having a drilled and grooved inner race), 
replace any nongreasible uplock roller (one having a solid inner race) 
with the greasible type before further flight, install hollow zerk
ended mounting bolts on the uplock rollers, and repetitively lubricate 
the uplock mechanism. Since we issued AD 722201, there was a recent 
incident involving a RAC Model 95B55B (T42A) airplane where a seizure 
of the uplock rollers occurred. This malfunction of the uplock rollers 
is addressed in AD 722201. Thus, the FAA has determined that the 
actions of AD 722201 should also apply to certain serial numbers of 
the Model 95B55B (T42A) airplanes. Consequently,<script type="text/javascript">
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  <guid>http://thefederalregister.com/d.p/2006-12-11-E6-20970</guid>
  <pubDate>Mon, Dec 11 2006 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Notice of Final Federal Agency Actions on Proposed Highway in  California]]></title>
  <link>http://thefederalregister.com/d.p/2006-12-11-E6-20949</link>
  <description><![CDATA[ This notice announces actions taken by the FHWA and other 
Federal agencies that are final within the meaning of 23 U.S.C. 
139(l)(1). The actions relate to a proposed highway project, U.S. 
Highway 101 Prunedale Improvement Project between Kilo Posts R146.8 to 
161.6 (Post Miles R91.2 to 100.4) north of the City of Salinas in 
Monterey County, State of California. Those actions grant approvals for 
the project.
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  <guid>http://thefederalregister.com/d.p/2006-12-11-E6-20949</guid>
  <pubDate>Mon, Dec 11 2006 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Iowa Interstate Railroad, Ltd.--Trackage Rights Exemption--BNSF  Railway Company]]></title>
  <link>http://thefederalregister.com/d.p/2006-12-11-E6-20902</link>
  <description><![CDATA[
</p><p>    Pursuant to a trackage rights agreement dated November 13, 2006, 
between Iowa Interstate Railroad, Ltd. (IAIS) and BNSF Railway Company 
(BNSF), IAIS has agreed to grant BNSF overhead trackage rights on 
IAIS's main line between milepost 170.2, at Colona, IL, and milepost 
175.4, at East Moline, IL, a distance of 5.2 miles, and over various 
meeting or passing tracks connecting with IAIS's main line, as IAIS may  designate (the Joint Trackage).</p><p>    The transaction is scheduled to be consummated on or after December  22, 2006.</p><p>    The purpose of the trackage rights is to allow BNSF use of the  Joint Trackage<br/> [[Page 71609]]<br/>
only for overhead freight operations, involving trains, locomotives, 
cars and equipment operated by BNSF. Under the agreement, BNSF shall 
not perform any local freight service at or to any point or station 
located on the Joint Trackage (except for interchange with IAIS at 
Silvis, IL, which is covered by separate agreement). The overhead 
trackage rights will terminate on December 3<script type="text/javascript">
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  <guid>http://thefederalregister.com/d.p/2006-12-11-E6-20902</guid>
  <pubDate>Mon, Dec 11 2006 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Norfolk Southern Railway Company--Adverse Abandonment--St. Joseph  County, IN]]></title>
  <link>http://thefederalregister.com/d.p/2006-12-11-E6-21002</link>
  <description><![CDATA[
</p><p>    On November 21, 2006, the City of South Bend, IN (the City), the 
Brothers of Holy Cross, Inc. (the Brothers), and the Sisters of the 
Holy Cross, Inc. (the Sisters) (collectively, applicants), filed an 
application under 49 U.S.C. 10903, requesting that the Surface 
Transportation Board authorize the thirdparty or adverse abandonment 
of approximately 3.7 miles of railroad lines (the Lines) owned by 
Norfolk Southern Railway Company (NSR).\1\ The Lines are located 
between milepost UV 0.0 and milepost UV 2.8 and between milepost Z0 9.6 
and milepost Z0 10.5, and include an industrial spur that extends from 
milepost Z0 9.6 to the University of Notre Dame (the University), all 
in St. Joseph County, IN. The Lines traverse United States Postal 
Service Zip Codes 46601, 46616, 46617, 46628, 46629, and 46556 and  include no stations.<br/>
    \1\ The Chicago, Lake Shore and South Bend Railway Company 
(CLS&SB) filed a petition to reject applicants' notice of intent to 
file this adverse abandonment application o<script type="text/javascript">
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  <guid>http://thefederalregister.com/d.p/2006-12-11-E6-21002</guid>
  <pubDate>Mon, Dec 11 2006 11:00:00 GMT</pubDate>
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