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    <title>The Federal Register</title>
    <link>http://thefederalregister.com/b.p/department/DEPARTMENT_OF_TRANSPORTATION/2007-11-26/</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 A330-200, A330-300, A340- 200, and A340-300 Series Airplanes]]></title>
  <link>http://thefederalregister.com/d.p/2007-11-26-E7-22921</link>
  <description><![CDATA[ The FAA proposes to supersede an existing airworthiness 
directive (AD) that applies to all Airbus Model A330200, A330300, 
A340200, and A340300 series airplanes. The existing AD currently 
requires a revision of the airplane flight manual to include procedures 
for a preflight elevator check before each flight, repetitive 
inspections for cracks of the attachment lugs of the mode selector 
valve position transducers on the elevator servo controls, and 
corrective actions if necessary. This proposed AD would retain the 
existing requirements, reduce the applicability of the existing AD, and 
add terminating actions. For certain airplanes, this proposed AD would 
require upgrading the flight control primary computers. This proposed 
AD results from cracks of the transducer body at its attachment lugs. 
We are proposing this AD to ensure proper functioning of the elevator 
surfaces, and to prevent cracking of the attachment lugs, which could 
result in partial loss of elevator function and consequent reduced 
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  <guid>http://thefederalregister.com/d.p/2007-11-26-E7-22921</guid>
  <pubDate>Mon, Nov 26 2007 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Airbus Model A330-200, A330-300, A340- 200, and A340-300 Series Airplanes]]></title>
  <link>http://thefederalregister.com/d.p/2007-11-26-E7-22925</link>
  <description><![CDATA[ The FAA proposes to supersede an existing airworthiness 
directive (AD) that applies to all Airbus Model A330200, A330300, 
A340200, and A340300 series airplanes. The existing AD currently 
requires an accelerated schedule of repetitive testing of the elevator 
servo control loops, and corrective actions if necessary. This proposed 
AD would retain the existing requirements, reduce the applicability of 
the existing AD, and add terminating actions. This proposed AD results 
from reports of failed elevator servo controls due to broken guides. We 
are proposing this AD to prevent failure of the elevator servo controls 
during certain phases of takeoff, which could result in an unannounced 
loss of elevator control and consequent reduced controllability of the 
airplane.
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  <guid>http://thefederalregister.com/d.p/2007-11-26-E7-22925</guid>
  <pubDate>Mon, Nov 26 2007 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Boeing Model 737-300, -400, and -500  Series Airplanes]]></title>
  <link>http://thefederalregister.com/d.p/2007-11-26-E7-22923</link>
  <description><![CDATA[ The FAA proposes to adopt a new airworthiness directive (AD) 
for certain Boeing Model 737300, 400, and 500 series airplanes. This 
proposed AD would require repetitive inspections for cracking of the 
body buttock line (BBL) 0.07 floor beam between body station (BS) 651 
and BS 676 and between BS 698 and BS 717, and related investigative and 
corrective actions if necessary. This AD also provides an optional 
terminating action for the repetitive inspections. This proposed AD 
results from reports of cracking in the BBL 0.07 floor beam. We are 
proposing this AD to prevent failure of the main deck floor beams at 
certain body stations due to fatigue cracking, which could result in 
rapid decompression of the airplane.
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  <guid>http://thefederalregister.com/d.p/2007-11-26-E7-22923</guid>
  <pubDate>Mon, Nov 26 2007 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Boeing Model 757 Airplanes Equipped  with Rolls Royce RB211-535E Engines]]></title>
  <link>http://thefederalregister.com/d.p/2007-11-26-E7-22924</link>
  <description><![CDATA[ The FAA proposes to adopt a new airworthiness directive (AD) 
for certain Boeing Model 757 airplanes equipped with Rolls Royce RB211
535E engines. This proposed AD would require repetitive inspections for 
signs of damage of the aft hinge fittings and attachment bolts of the 
thrust reversers, and related investigative and corrective actions if 
necessary. This proposed AD results from reports of several incidents 
of bolt failure at the aft hinge fittings of the thrust reversers due 
to, among other things, high operational loads. We are proposing this 
AD to prevent failure of the attachment bolts and consequent separation 
of a thrust reverser from the airplane during flight, which could 
result in structural damage to the airplane.
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  <guid>http://thefederalregister.com/d.p/2007-11-26-E7-22924</guid>
  <pubDate>Mon, Nov 26 2007 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Boeing Model 737-200 Series Airplanes]]></title>
  <link>http://thefederalregister.com/d.p/2007-11-26-E7-22926</link>
  <description><![CDATA[ The FAA proposes to adopt a new airworthiness directive (AD) 
for certain Boeing Model 737200 series airplanes. This proposed AD 
would require repetitive inspections to detect cracking of the support 
fittings of the Krueger flap actuators, and corrective actions if 
necessary. This proposed AD also would require eventual replacement of 
any existing aluminum support fitting on each wing with a steel 
fitting, and modification of the aft attachment of the actuator. Doing 
these actions would terminate the repetitive inspection requirements. 
This proposed AD results from reports of cracking due to fatigue and 
stress corrosion of the support fittings of the Krueger flap actuator. 
We are proposing this AD to prevent cracking of the support fittings, 
which could result in fracturing of the actuator attach lugs, 
separation of the actuator from the support fitting, severing of the 
hydraulic lines, resultant loss of hydraulic fluids, and consequent 
reduced controllability of the airplane.
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]]></description>
  <guid>http://thefederalregister.com/d.p/2007-11-26-E7-22926</guid>
  <pubDate>Mon, Nov 26 2007 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Boeing Model 737-100, -200, -300, -400,  and -500 Series Airplanes]]></title>
  <link>http://thefederalregister.com/d.p/2007-11-26-E7-22928</link>
  <description><![CDATA[ The FAA proposes to adopt a new airworthiness directive (AD) 
for certain Boeing Model 737100, 200, 300, 400, and 500 series 
airplanes. This proposed AD would require repetitive inspections for 
fatigue cracking in the longitudinal floor beam web, upper chord, and 
lower chord located at certain body stations, and repair if necessary. 
This proposed AD results from several reports of cracks in the center 
wing box longitudinal floor beams, upper chord, and lower chord. We are 
proposing this AD to detect and correct fatigue cracking of the upper 
and lower chords and web of the longitudinal floor beams, which could 
result in rapid loss of cabin pressure.
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  <guid>http://thefederalregister.com/d.p/2007-11-26-E7-22928</guid>
  <pubDate>Mon, Nov 26 2007 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Boeing Model 727 Airplanes ]]></title>
  <link>http://thefederalregister.com/d.p/2007-11-26-E7-22939</link>
  <description><![CDATA[ The FAA proposes to adopt a new airworthiness directive (AD) 
for all Boeing Model 727 airplanes. This proposed AD would require 
repetitive inspections for cracking or corrosion of the threaded end of 
the lower segment of the main landing gear (MLG) side strut, and 
corrective actions if necessary. This proposed AD also would require 
prior or concurrent inspection for cracking or corrosion of the threads 
and thread relief area of the lower segment, corrective action if 
necessary, and reassembly using corrosion inhibiting compound. This 
proposed AD results from reports of the threads cracking on the MLG 
side strut lower segment. We are proposing this AD to prevent a 
fractured side strut, which could result in collapse of the MLG.
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  <guid>http://thefederalregister.com/d.p/2007-11-26-E7-22939</guid>
  <pubDate>Mon, Nov 26 2007 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Seventy-Fourth Meeting: RTCA Special Committee 159: Global  Positioning System (GPS)]]></title>
  <link>http://thefederalregister.com/d.p/2007-11-26-07-5803</link>
  <description><![CDATA[ The FAA is issuing this notice to advise the public of a 
meeting of RTCA Special Committee 159: Global Positioning System.
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  <guid>http://thefederalregister.com/d.p/2007-11-26-07-5803</guid>
  <pubDate>Mon, Nov 26 2007 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  RTCA Special Committee 147 Sixty-Sixth Plenary: Minimum  Operational Performance Standards for Traffic Alert and]]></title>
  <link>http://thefederalregister.com/d.p/2007-11-26-07-5804</link>
  <description><![CDATA[ The FAA is issuing this notice to advise the public of a 
meeting of RTCA Special Committee 147: Minimum Operational Performance 
Standards for Traffic Alert and Collision Avoidance Systems Airborne 
Equipment and Working Group 75.
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  <guid>http://thefederalregister.com/d.p/2007-11-26-07-5804</guid>
  <pubDate>Mon, Nov 26 2007 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  RTCA Special Committee 205/EUROCAE Working Group 71: Software  Considerations in Aeronautical Systems Seventh Joint]]></title>
  <link>http://thefederalregister.com/d.p/2007-11-26-07-5805</link>
  <description><![CDATA[ The FAA is issuing this notice to advise the public of a 
meeting of RTCA Special Committee 205/EUROCAE Working Group 71:  Software Considerations in Aeronautical Systems.<br/>
[[Page 66019]]
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]]></description>
  <guid>http://thefederalregister.com/d.p/2007-11-26-07-5805</guid>
  <pubDate>Mon, Nov 26 2007 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Agency Information Collection Activities; Request for Comment;  Revision of an Information Collection: Hours of]]></title>
  <link>http://thefederalregister.com/d.p/2007-11-26-E7-22879</link>
  <description><![CDATA[ In accordance with the Paperwork Reduction Act of 1995, FMCSA 
announces its plans to submit the Information Collection Request 
described below to the Office of Management and Budget (OMB) for review 
and approval, and invites public comment. The FMCSA invites comments on 
its plan to request OMB approval to revise an existing information 
collection (IC) entitled, ``Hours of Service of Drivers Regulations,'' 
OMB Control Number 21260001. The Agency has updated its calculation of 
the paperwork burden of the hours of service (HOS) rules to reflect 
changes in the number of commercial motor vehicle (CMV) drivers, and to 
clarify the burden associated with supporting documents. The Agency 
requires most CMV drivers to complete and maintain a record of duty 
status (RODS), commonly referred to as a logbook, reflecting details of 
changes in duty status during each 24hour period. Drivers retain the 
RODS for a minimum period and then forward them, along with supporting 
documents (e.g., fuel receipts, road toll<script type="text/javascript">
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  <guid>http://thefederalregister.com/d.p/2007-11-26-E7-22879</guid>
  <pubDate>Mon, Nov 26 2007 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Hours of Service of Drivers: Dart Transit Company Application for  Exemption]]></title>
  <link>http://thefederalregister.com/d.p/2007-11-26-E7-22881</link>
  <description><![CDATA[ FMCSA has received from Dart Transit Company (Dart) an 
application for an exemption from certain commercial motor vehicle 
driver hoursofservice provisions of the Federal Motor Carrier Safety 
Regulations. Dart requests an exemption for 200 of its owneroperators 
from the prohibition against driving after the 14th hour of coming on
duty, following 10 consecutive hours offduty, and the requirement that 
drivers using two sleeperberth periods to accumulate the equivalent of 
10 consecutive hours offduty spend at least 8 but less than 10 
consecutive hours in the sleeperberth during one of those two periods. 
As requested by Dart, exempt drivers would be allowed to drive up to 11 
hours within a 24hour period between 3 a.m. one day and 3 a.m. the 
next day, be required to complete a minimum of 6 consecutive offduty 
or sleeperberth hours between 9 p.m. and 9 a.m., and complete 
additional periods of offduty or sleeperberth time to total at least 
10 hours of rest within any ``floating'' 24hour period. Dart wou<script type="text/javascript">
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  <guid>http://thefederalregister.com/d.p/2007-11-26-E7-22881</guid>
  <pubDate>Mon, Nov 26 2007 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Office of Analysis, Research and Technology Forum ]]></title>
  <link>http://thefederalregister.com/d.p/2007-11-26-E7-22883</link>
  <description><![CDATA[ This notice invites interested persons to participate in a 
forum titled, ``Federal Motor Carrier Safety Administration's Analysis, 
Research and Technology Programs'', sponsored by the FMCSA Office of 
Analysis, Research and Technology (ART) in conjunction with the 87th 
Annual Meeting of the Transportation Research Board (TRB). The purpose 
of the 2008 ART Forum is to provide information on various initiatives 
from FMCSA's analysis, research, and technology programs. Speaker 
topics will include the results of the OnBoard Monitoring Safety 
Study; an overview of the OnBoard Safety Technologies FMCSA has tested 
and evaluated; the results of the Violations Severity Assessment Study; 
a presentation titled, ``When Cars Collide with Trucks and Buses'', an 
update on the Employer Notification Service Pilot Project; and, a 
review of FMCSA's Wireless Roadside Inspection and Smart Roadside 
Activities. Attendees will have the opportunity to dialogue with FMCSA 
subjectmatter experts through an open question and<script type="text/javascript">
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  <guid>http://thefederalregister.com/d.p/2007-11-26-E7-22883</guid>
  <pubDate>Mon, Nov 26 2007 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Motor Carrier Safety Advisory Committee Public Meeting ]]></title>
  <link>http://thefederalregister.com/d.p/2007-11-26-E7-22915</link>
  <description><![CDATA[ FMCSA announces that the Motor Carrier Safety Advisory 
Committee (MCSAC) will hold a committee meeting. The meeting is open to 
the public.
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  <guid>http://thefederalregister.com/d.p/2007-11-26-E7-22915</guid>
  <pubDate>Mon, Nov 26 2007 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Intent To Prepare an Environmental Impact Statement for Proposed  Transit Improvements in the Draper Corridor of]]></title>
  <link>http://thefederalregister.com/d.p/2007-11-26-E7-22913</link>
  <description><![CDATA[ The Federal Transit Administration (FTA) and Utah Transit 
Authority (UTA) intend to prepare an Environmental Impact Statement 
(EIS) to evaluate proposed public transportation improvements to extend 
fixed guideway transit service through the cities of Sandy and Draper 
to the southernmost part of Salt Lake County, Utah. The Wasatch Front 
Regional Council (WFRC) has adopted a longrange transportation plan, 
which is a comprehensive system plan and includes the full buildout of 
public transportation improvements in several corridors. The general 
alignments of the corridors have been identified in the approved plan. 
The Draper Transit Corridor has been identified in the plan as a two
track extension of the existing NorthSouth Light Rail Transit (LRT) 
line from its current terminus at 10000 South in Sandy to about 14600 
South in Draper along the UTA owned rightofway. The Draper Transit 
Corridor Project, as defined in the WFRC longrange plan, was 
identified as the preferred alternative at the conclusion<script type="text/javascript">
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  <guid>http://thefederalregister.com/d.p/2007-11-26-E7-22913</guid>
  <pubDate>Mon, Nov 26 2007 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Reports, Forms, and Recordkeeping Requirements ]]></title>
  <link>http://thefederalregister.com/d.p/2007-11-26-E7-22880</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, before seeking OMB approval, Federal agencies must solicit 
public comment on proposed collections of information, including 
extensions and reinstatements of previously approved collections.
</p><p>    This document describes the collection of information for which 
NHTSA intends to seek OMB approval.
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  <guid>http://thefederalregister.com/d.p/2007-11-26-E7-22880</guid>
  <pubDate>Mon, Nov 26 2007 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Ferrari S.p.A. and Ferrari North America; Receipt of Application  for a Temporary Exemption From the Advanced Air Bag]]></title>
  <link>http://thefederalregister.com/d.p/2007-11-26-E7-22966</link>
  <description><![CDATA[ In accordance with the procedures in 49 CFR Part 555, Ferrari 
S.P.A. and Ferrari North America (collectively, ``Ferrari'') have 
petitioned the agency for a temporary exemption from certain advanced 
air bag requirements of FMVSS No. 208. The basis for the application is 
that compliance would cause substantial economic hardship to a 
manufacturer that has tried in good faith to comply with the standard.
</p><p>    This notice of receipt of an application for temporary exemption is 
published in accordance with the statutory provisions of 49 U.S.C. 
30113(b)(2). NHTSA has made no judgment on the merits of the 
application.
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  <guid>http://thefederalregister.com/d.p/2007-11-26-E7-22966</guid>
  <pubDate>Mon, Nov 26 2007 11:00:00 GMT</pubDate>
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<item>
  <title><![CDATA[  Laurinburg & Southern Railroad Co., Inc.--Discontinuance of  Service Exemption--in Hoke and Scotland Counties, NC]]></title>
  <link>http://thefederalregister.com/d.p/2007-11-26-E7-22931</link>
  <description><![CDATA[
</p><p>    Laurinburg & Southern Railroad Co., Inc. (LRS) has filed a verified 
notice of exemption under 49 CFR Part 1152 Subpart FExempt 
Abandonments and Discontinuances of Service to discontinue service over 
an approximately 17.3mile line of railroad between milepost 8.9, in or 
near Laurinburg, Scotland County, NC, and milepost 26.2, in or near 
Raeford, Hoke County, NC. The line traverses United States Postal 
Service Zip Codes 28352, 28353, 28376, 28396, and 27812, and includes  the stations of Wagram and Raeford.</p><p>    LRS has certified that: (1) No local traffic has moved over the 
line for at least 2 years; (2) that all overhead traffic, if any, can 
be or already has been rerouted over other lines; (3) no formal 
complaint filed by a user of rail service on the line (or by a state or 
local government entity acting on behalf of such user) regarding 
cessation of service over the line either is pending with the Board or 
with any U.S. District Court or has been decided in favor of 
complainant within the 2<script type="text/javascript">
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  <guid>http://thefederalregister.com/d.p/2007-11-26-E7-22931</guid>
  <pubDate>Mon, Nov 26 2007 11:00:00 GMT</pubDate>
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