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    <title>The Federal Register</title>
    <link>http://thefederalregister.com/b.p/department/DEPARTMENT_OF_TRANSPORTATION/2008-07-17/</link>
    <description>Daily Publications of Meetings and Rules Changes for the Federal Government</description>
    <pubDate>Wed, Jan 7 2009 11:00:00 GMT</pubDate>
    <lastBuildDate>Wed, Jan 7 2009 11:00:00 GMT</lastBuildDate>
    <webMaster>info@thefederalregister.com</webMaster>
    <item>
  <title><![CDATA[  Airworthiness Directives; 328 Support Services GmbH Dornier Model  328-100 and -300 Airplanes]]></title>
  <link>http://thefederalregister.com/d.p/2008-07-17-E8-15709</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) 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>    At least one incident has occurred where, immediately after 
takeoff, the passenger door of a Dornier 328 completely opened. * * 
* Substantial damage to the door, handrails, door hinge arms and  fuselage skin were found.<br/>
    * * * Although final proof could not be obtained, the most 
likely way in which the door opened was that the door handle was  inadvertently operated during the takeoff run.<br/> * * * * *<br/>
    [T]his Airworthiness Directive (AD) aims to prevent further 
incidents of inadvertent opening and possible detachment of a 
passenger door inflight, likely resulting in damage to airframe and 
systems and, under less favorable circumstances, loss of control of  the aircraft.<br/>
* <script type="text/javascript">
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  <guid>http://thefederalregister.com/d.p/2008-07-17-E8-15709</guid>
  <pubDate>Thu, Jul 17 2008 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Agusta S.p.A. Model A109E and A119  Helicopters]]></title>
  <link>http://thefederalregister.com/d.p/2008-07-17-E8-14727</link>
  <description><![CDATA[ We are adopting a new airworthiness directive (AD) for Agusta 
S.p.A. (Agusta) Model A109E and A119 helicopters. 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 European Aviation Safety Agency 
(EASA), the Technical Agent for Italy, with which we have a bilateral 
agreement, states in the MCAI: ``Some cases of interference between the 
hydraulic pipe, P/N 109076165103, and the tail rotor control [[Page 40961]]<br/>
rod assembly have been detected on Model A109E helicopters * * * The 
interference, if not corrected, could damage the hydraulic pipes and 
lead to the loss of the hydraulic system No. 1 in flight. This AD * * * 
is issued to extend the same mandatory corrective actions to A119 model  due to its design similarity with A109E.''</p><p>    This AD requires actions that are intended to address this unsafe 
condition.
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  <guid>http://thefederalregister.com/d.p/2008-07-17-E8-14727</guid>
  <pubDate>Thu, Jul 17 2008 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Airbus Model A330-200 and A340-300  Series Airplanes]]></title>
  <link>http://thefederalregister.com/d.p/2008-07-17-E8-15708</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) 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>    During fatigue tests (EF3) on the A340600, multiple damage were 
found in the upper side shell structure at skin and frame (FR) 84 & 
85 interface, from stringer 6 to 15 LH/RH. This damage occurred  between 58,341 and 72,891 simulated Flight Cycles (FC).</p><p>    Due to the higher Design Service Goal and different design (e.g. 
skin thickness) for A330200 and A340300 aircraft series, the 
damage assessment concluded on [a] potential impact on these  aircraft series.<br/> * * * * *<br/>
The unsafe condition is loss of integrity of the upper shell structure 
of the fuselage. We are issuing this AD to require actions to correct 
the unsafe condition on these products.
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]]></description>
  <guid>http://thefederalregister.com/d.p/2008-07-17-E8-15708</guid>
  <pubDate>Thu, Jul 17 2008 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Boeing Model 747-400 and 747-400D  Series Airplanes]]></title>
  <link>http://thefederalregister.com/d.p/2008-07-17-E8-15710</link>
  <description><![CDATA[ We are adopting a new airworthiness directive (AD) for certain 
Boeing Model 747400 and 747400D series airplanes. This AD requires a 
general visual inspection of the power feeder wire bundle of the 
auxiliary power unit (APU) where it crosses the hydraulic system 4 
return tube to determine if parts are installed to provide separation 
between the wire bundle and hydraulic tube. This AD also requires 
related investigative and corrective actions if necessary. This AD 
results from a report that the power feeder wire bundle of the APU was 
found touching the hydraulic system return tube during inspection of an 
airplane. We are issuing this AD to prevent insufficient clearance 
between the wire bundle and hydraulic tube that could lead to chafing 
of the wire bundle, which could cause arcing and a consequent hydraulic 
fluid fire in an area outside of the smoke detection and fire 
extinguishing zone; this condition could result in an uncontrolled fire 
on the airplane.
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]]></description>
  <guid>http://thefederalregister.com/d.p/2008-07-17-E8-15710</guid>
  <pubDate>Thu, Jul 17 2008 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Empresa Brasileira de Aeronautica S.A.  (EMBRAER) Model EMB-120, -120ER, -120FC, -120QC, and]]></title>
  <link>http://thefederalregister.com/d.p/2008-07-17-E8-15969</link>
  <description><![CDATA[ This amendment adopts a new airworthiness directive (AD), 
applicable to all EMBRAER Model EMB120 series airplanes, that requires 
revising the airplane flight manual to include operational limitations 
for use of the autopilot, installing two placards that advise the 
flight crew to check the pitch trim before descent, and modifying the 
elevator trim system, which would terminate the requirements of the AD. 
The actions specified by this AD are intended to prevent pitch trim 
upsets if the pitch trim actuators jam or freeze, which could result in 
reduced controllability of the airplane. This action is intended to 
address the identified unsafe condition.
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]]></description>
  <guid>http://thefederalregister.com/d.p/2008-07-17-E8-15969</guid>
  <pubDate>Thu, Jul 17 2008 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Fokker Model F27 Mark 050 Airplanes]]></title>
  <link>http://thefederalregister.com/d.p/2008-07-17-E8-15711</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) 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>    During scheduled Xray inspections of Fokker 50 (F27 Mark 050) 
engine mounting frames, welding defects were discovered. In two 
forward frames and one aft frame, defects were found in a total of 4 
weld locations. Investigation showed that during manufacture of the  frames, when the tubes were welded to the end fittings, <br/>
unintentional sideways movement of the electric arc resulted in some 
welds running beside the borderline for a part of the tube 
circumference. Where a weld runs beside the borderline, there is no 
connection between tube and end fitting for that part of the 
circumference, directly affecting the structural integrity of the 
engine mounting frame connections. The <script type="text/javascript">
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]]></description>
  <guid>http://thefederalregister.com/d.p/2008-07-17-E8-15711</guid>
  <pubDate>Thu, Jul 17 2008 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Pacific Aerospace Limited Model FU-24  Airplanes]]></title>
  <link>http://thefederalregister.com/d.p/2008-07-17-E8-16191</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>    To prevent the possible inflight failure of the vertical fin,  leading to loss of control of the aircraft * * *<br/>
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/2008-07-17-E8-16191</guid>
  <pubDate>Thu, Jul 17 2008 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Approval of Noise Compatibility Program; Ocala International  Airport; Ocala, FL]]></title>
  <link>http://thefederalregister.com/d.p/2008-07-17-E8-15954</link>
  <description><![CDATA[ The Federal Aviation Administration (FAA) announces its 
findings on the Noise Compatibility Program submitted by the City of 
Ocala 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 responsibilities in Senate Report No. 9652 
(1980). On December 28, 2008, the FAA determined that the noise 
exposure maps submitted by the City of Ocala under part 150 were in 
compliance with applicable requirements. On June 23, 2008, the FAA 
approved the Ocala International Airport noise compatibility program. 
All 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/2008-07-17-E8-15954</guid>
  <pubDate>Thu, Jul 17 2008 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Operating Limitations for Unscheduled Operations at John F.  Kennedy International Airport and Newark Liberty]]></title>
  <link>http://thefederalregister.com/d.p/2008-07-17-E8-15961</link>
  <description><![CDATA[ The FAA tentatively has determined that it is necessary to 
temporarily limit unscheduled aircraft operations at John F. Kennedy 
International Airport (JFK) and Newark Liberty International Airport 
(EWR). By Orders dated January 15 and May 15, 2008, the FAA restricted 
the number of scheduled operations respectively at JFK and EWR. These 
orders were a result of persistent congestion and delays at JFK and EWR 
during the peak operating hours, as well as a dramatic projected 
increase in fight delays at both airports during the summer of 2008 if 
proposed schedules were implemented as requested by carriers. The FAA 
recently published a notice of proposed rulemaking that addresses the 
operating limits of scheduled and unscheduled operations at both 
airports for the longer term. The FAA believes that in the interim it 
is necessary to limit unscheduled operations, as even the addition of a 
few operations in the critical peak hours can result in added 
congestion and delay. The intended effect of this acti<script type="text/javascript">
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  <guid>http://thefederalregister.com/d.p/2008-07-17-E8-15961</guid>
  <pubDate>Thu, Jul 17 2008 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Notice of Passenger Facility Charge (PFC) Approvals and  Disapprovals]]></title>
  <link>http://thefederalregister.com/d.p/2008-07-17-E8-15958</link>
  <description><![CDATA[ The FAA publishes a monthly notice, as appropriate, of PFC 
approvals and disapprovals under the provisions of the Aviation Safety 
and Capacity Expansion Act of 1990 (Title IX of the Omnibus Budget 
Reconciliation Act of 1990) (Pub. L. 101508) and Part 158 of the 
Federal Aviation Regulations (14 CFR Part 158). This notice is  published pursuant to paragraph (d) of Sec.  158.29.<br/> PFC Applications Approved<br/> </p><p>    Public Agency: City of Des Moines, Iowa.<br/> </p><p>    Application Number: 0811C00DSM.<br/> </p><p>    Application Type: Impose and use a PFC.<br/> </p><p>    PFC Level: $4.50.</p><p>    Total PFC Revenue Approved in This Decision: $2,525,646. </p><p>    Earliest Charge Effective Date: August 1, 2017.</p><p>    Estimated Charge Experiation Date: January 1, 2018.
</p><p>    Class of Air Carriers not Required to Collect PFC's: Part 135 air  taxi/commercial operators.</p><p>    Determination: Approved. Based on information submitted in the 
public agency's application, the FAA has determined that the proposed 
class accounts for less than 1 percent of the total annual en<script type="text/javascript">
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  <guid>http://thefederalregister.com/d.p/2008-07-17-E8-15958</guid>
  <pubDate>Thu, Jul 17 2008 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Petition for Exemption; Summary of Petition Received ]]></title>
  <link>http://thefederalregister.com/d.p/2008-07-17-E8-16248</link>
  <description><![CDATA[ This notice contains a summary of a petition seeking relief 
from specified requirements of 14 CFR. The purpose of this notice is to 
improve the public's awareness of, and participation in, this aspect of 
FAA's regulatory activities. Neither publication of this notice nor the 
inclusion or omission of information in the summary is intended to 
affect the legal status of the petition or its final disposition.
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  <guid>http://thefederalregister.com/d.p/2008-07-17-E8-16248</guid>
  <pubDate>Thu, Jul 17 2008 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Petition for Exemption; Summary of Petition Received ]]></title>
  <link>http://thefederalregister.com/d.p/2008-07-17-E8-16249</link>
  <description><![CDATA[ This notice contains a summary of a petition seeking relief 
from specified requirements of 14 CFR. The purpose of this notice is to 
improve the public's awareness of, and participation in, this aspect of 
FAA's regulatory activities. Neither publication of this notice nor the 
inclusion or omission of information in the summary is intended to 
affect the legal status of the petition or its final disposition.
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  <guid>http://thefederalregister.com/d.p/2008-07-17-E8-16249</guid>
  <pubDate>Thu, Jul 17 2008 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Environmental Impact Statement; St. Lucie County, FL ]]></title>
  <link>http://thefederalregister.com/d.p/2008-07-17-E8-16342</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 
new river crossing project in the City of Port St. Lucie, St. Lucie 
County, Florida.
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  <guid>http://thefederalregister.com/d.p/2008-07-17-E8-16342</guid>
  <pubDate>Thu, Jul 17 2008 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Environmental Impact Statement: Stone, Perry, George, and Greene  Counties, MS]]></title>
  <link>http://thefederalregister.com/d.p/2008-07-17-E8-16371</link>
  <description><![CDATA[ The Federal Highway Administration is issuing this notice to 
advise the public that an Environmental Impact Statement will be 
prepared to study improvements to State Route 15 to provide a fourlane 
facility beginning in the vicinity of Ramsey Springs, Mississippi and 
terminating on U.S. Highway 98 near Beaumont, Mississippi, a distance 
of approximately 35 miles.
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  <guid>http://thefederalregister.com/d.p/2008-07-17-E8-16371</guid>
  <pubDate>Thu, Jul 17 2008 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Notice of Final Federal Agency Actions on Proposed Highway in  Idaho]]></title>
  <link>http://thefederalregister.com/d.p/2008-07-17-E8-16052</link>
  <description><![CDATA[ This notice announces actions taken by the FHWA that are final 
within the meaning of 23 U.S.C. 139(l)(1). The actions relate to a 
proposed highway project, 184 Orchard Interchange to Gowen Interchange 
Study, in Boise, Ada County in the State of Idaho [Idaho Transportation 
Department (ITD) Key Number 6492].
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  <guid>http://thefederalregister.com/d.p/2008-07-17-E8-16052</guid>
  <pubDate>Thu, Jul 17 2008 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Notice To Rescind a Notice of Intent To Prepare an Environmental  Impact Statement (EIS), Ada and Canyon Counties, ID]]></title>
  <link>http://thefederalregister.com/d.p/2008-07-17-E8-16053</link>
  <description><![CDATA[ The FHWA is issuing this notice to advise the public that the 
Notice of Intent (NOI) published on July 17, 2007 to prepare an 
Environmental Impact Statement (EIS) for a proposed highway project in  Ada County, Idaho is being rescinded.<br/>
[[Page 41167]]
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  <guid>http://thefederalregister.com/d.p/2008-07-17-E8-16053</guid>
  <pubDate>Thu, Jul 17 2008 11:00:00 GMT</pubDate>
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<item>
  <title><![CDATA[  Railroad Workplace Safety; Adjacent-Track On-Track Safety for  Roadway Workers]]></title>
  <link>http://thefederalregister.com/d.p/2008-07-17-E8-16140</link>
  <description><![CDATA[ FRA proposes to amend its regulations on railroad workplace 
safety to reduce further the risk of serious injury or death to roadway 
workers. In particular, FRA proposes to require that railroads adopt 
specified ontrack safety procedures to protect certain roadway work 
groups from the movement of trains or other ontrack equipment on 
``adjacent track.'' FRA proposes to define ``adjacent track'' as ``any 
controlled track whose track center is 19 feet or less from the track 
center of the occupied track.'' These ontrack safety procedures would 
be required for each adjacent track when a roadway work group with at 
least one of the roadway workers on the ground, is engaged in a common 
task with an ontrack roadway maintenance machine or coupled equipment 
on an occupied track. FRA also proposes to require that railroads, 
contractors to railroads, and roadway workers comply with these 
procedures.
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]]></description>
  <guid>http://thefederalregister.com/d.p/2008-07-17-E8-16140</guid>
  <pubDate>Thu, Jul 17 2008 11:00:00 GMT</pubDate>
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