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    <title>The Federal Register</title>
    <link>http://thefederalregister.com/b.p/department/DEPARTMENT_OF_TRANSPORTATION/2003-12-01/</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; Boeing Model 747-400 and -400F Series  Airplanes]]></title>
  <link>http://thefederalregister.com/d.p/2003-12-01-03-29530</link>
  <description><![CDATA[ This amendment adopts a new airworthiness directive (AD), 
applicable to certain Boeing Model 747400 and 400F series airplanes. 
This action requires replacing the rudder feel, centering, and trim 
mechanism with a new or serviceable rudder feel, centering, and trim 
mechanism. This action is necessary to prevent degradation/loss of 
rudder feel and centering, which could result in increased pilot 
workload and could lead to loss of control of the airplane. This action 
is intended to address the identified unsafe condition.
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  <guid>http://thefederalregister.com/d.p/2003-12-01-03-29530</guid>
  <pubDate>Mon, Dec 1 2003 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Boeing Model 737-100, -200, -200C, - 300, -400, and -500 Series Airplanes]]></title>
  <link>http://thefederalregister.com/d.p/2003-12-01-03-29784</link>
  <description><![CDATA[ This amendment supersedes an existing airworthiness directive 
(AD), applicable to all Boeing Model 737100, 200, 200C, 300, 400, 
and 500 series airplanes, that currently requires repetitive 
inspections to find cracks, fractures, or corrosion of each carriage 
spindle of the left and right outboard midflaps; and corrective 
action, if necessary. That AD also provides for an optional action of 
overhaul or replacement of the carriage spindles. This amendment 
requires repetitive gap checks of the inboard and outboard carriage of 
the outboard midflaps to detect fractured carriage spindles; and 
corrective actions, if necessary. This amendment also reduces the 
interval for the existing inspections and revises the overhaul 
procedures. The actions specified in this AD are intended to detect and 
correct cracked, corroded, or fractured carriage spindles and to 
prevent severe flap asymmetry, which could result in reduced control or 
loss of controllability of the airplane. This action is intended to 
address t<script type="text/javascript">
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  <guid>http://thefederalregister.com/d.p/2003-12-01-03-29784</guid>
  <pubDate>Mon, Dec 1 2003 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Dassault Model Mystere-Falcon 200  Series Airplanes]]></title>
  <link>http://thefederalregister.com/d.p/2003-12-01-03-29570</link>
  <description><![CDATA[ This amendment adopts a new airworthiness directive (AD) that 
is applicable to all Dassault Model MystereFalcon 200 series 
airplanes. This action requires a onetime inspection of the fire 
extinguishing pipe for each engine to determine whether holes for 
dispersal of fireextinguishing agent are present, and corrective 
action if necessary. This action is necessary to ensure that the 
flightcrew is able to extinguish an engine fire, should one occur. 
Inability to extinguish an engine fire could result in loss of control 
of the airplane. This action is intended to address the identified 
unsafe condition.
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  <guid>http://thefederalregister.com/d.p/2003-12-01-03-29570</guid>
  <pubDate>Mon, Dec 1 2003 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Eurocopter France Model SA-365N, N1,  AS-365N2, and AS 365 N3 Helicopters]]></title>
  <link>http://thefederalregister.com/d.p/2003-12-01-03-29223</link>
  <description><![CDATA[ This amendment adopts a new airworthiness directive (AD) for 
the specified Eurocopter France (Eurocopter) model helicopters that 
requires inspecting the fuel air vent hoses (air vent hoses) for 
chafing and fuel leakage in the interference areas, inspecting the 
length of the latch support attachment screws, installing spacers to 
prevent interference with the latch support attachment screws, and 
removing one tyrap clamp support. This amendment is prompted by a 
report of a fuel leak in the air vent hose at the 9[deg] frame on the 
pilot's side of the helicopter. The actions specified by this AD are 
intended to prevent fuel leakage, toxic fumes inside the cabin creating 
a fire hazard that could lead to a fire and smoke in the cabin, and 
subsequent loss of control of the helicopter.
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  <guid>http://thefederalregister.com/d.p/2003-12-01-03-29223</guid>
  <pubDate>Mon, Dec 1 2003 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Eurocopter France Model AS332C, L, L1,  and L2 Helicopters]]></title>
  <link>http://thefederalregister.com/d.p/2003-12-01-03-29224</link>
  <description><![CDATA[ This amendment adopts a new airworthiness directive (AD) for 
the specified Eurocopter France (Eurocopter) model helicopters that 
requires inspecting the cockpit pedal unit (pedal unit) adjustment 
lever (lever) for a crack at specified time intervals by a dye
penetrant inspection and replacing any cracked lever with an airworthy 
lever before further flight. Modifying the pedal unit is also required 
and is a terminating action for the requirements of this AD. This 
amendment is prompted by cracks detected in the lever that creates an 
unsafe condition. The actions specified by this AD are intended to 
prevent failure of the lever, loss of access to the brake pedals on the 
ground or loss of yaw control in flight, and subsequent loss of control 
of the helicopter.
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  <guid>http://thefederalregister.com/d.p/2003-12-01-03-29224</guid>
  <pubDate>Mon, Dec 1 2003 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; McDonnell Douglas Model DC-9-31 and DC- 9-32 Airplanes]]></title>
  <link>http://thefederalregister.com/d.p/2003-12-01-03-29531</link>
  <description><![CDATA[ This amendment adopts a new airworthiness directive (AD), 
applicable to certain McDonnell Douglas Model DC931 and DC932 
airplanes. This action requires installation of ceiling panels and a 
protective pad in the tailcone emergency exit passageway. The actions 
specified by this AD are intended to prevent people on board the 
airplane from striking their heads on exposed metal frames in the 
tailcone area, which could cause injury and delay or impede their 
evacuation during an emergency. This action is intended to address the 
identified unsafe condition.
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  <guid>http://thefederalregister.com/d.p/2003-12-01-03-29531</guid>
  <pubDate>Mon, Dec 1 2003 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Stage 4 Aircraft Noise Standards ]]></title>
  <link>http://thefederalregister.com/d.p/2003-12-01-03-29147</link>
  <description><![CDATA[ The FAA is proposing a new noise standard for subsonic jet 
airplanes and subsonic transport category large airplanes. This noise 
standard would ensure that the latest available noise reduction 
technology is incorporated into new aircraft designs. This noise 
standard, Stage 4, would apply to any person submitting an application 
for a new airplane type design on and after January 1, 2006. The 
standard could be chosen voluntarily prior to that date. This noise 
standard is intended to provide uniform noise certification standards 
for Stage 4 airplanes certificated in the United States and those 
airplanes that meet the new International Civil Aviation Organization 
Annex 16 Chapter 4 noise standard.
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  <guid>http://thefederalregister.com/d.p/2003-12-01-03-29147</guid>
  <pubDate>Mon, Dec 1 2003 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Notice of Intent To Rule on Request To Release Airport Property  at the Waco Regional Airport, Waco, TX]]></title>
  <link>http://thefederalregister.com/d.p/2003-12-01-03-29846</link>
  <description><![CDATA[ The FAA proposes to rule and invite public comment on the 
release of land at Waco Regional Airport under the provisions of 
Section 125 of the Wendell H. Ford Aviation Investment Reform Act for 
the 21st Century (AIR 21).
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  <guid>http://thefederalregister.com/d.p/2003-12-01-03-29846</guid>
  <pubDate>Mon, Dec 1 2003 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Random Drug and Alcohol Testing Percentage Rates of Covered  Aviation Employees for the Period of January 1, 2004,]]></title>
  <link>http://thefederalregister.com/d.p/2003-12-01-03-29848</link>
  <description><![CDATA[ The FAA has determined that the minimum random drug and 
alcohol testing percentage rates for the period January 1, 2004, 
through December 31, 2004, will remain at 25 percent of safety
sensitive aviation employees for random drug testing and 10 percent of 
safetysensitive aviation employees for random alcohol testing.
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  <guid>http://thefederalregister.com/d.p/2003-12-01-03-29848</guid>
  <pubDate>Mon, Dec 1 2003 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Notice of Intent To Rule on Application 03-05-C-00-AOO To Impose,  and Impose and Use the Revenue From a Passenger]]></title>
  <link>http://thefederalregister.com/d.p/2003-12-01-03-29845</link>
  <description><![CDATA[ This correction revises information from the previously 
published notice. In notice document 0328826 beginning on page 65342 
in the issue of Wednesday, November 19, 2003, under the SUPPLEMENTARY 
INFORMATION section, first paragraph, the substantially complete date 
should be October 3, 2003.
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  <guid>http://thefederalregister.com/d.p/2003-12-01-03-29845</guid>
  <pubDate>Mon, Dec 1 2003 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/2003-12-01-03-29847</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 Bismarck, North Dakota.<br/> </p><p>    Application Number: 0304C00BIS.<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: $5,574,555. </p><p>    Earliest Charge Effective Date: March 1, 2004.</p><p>    Estimated Charge Expiration Date: October 1, 2014.
</p><p>    Class of Air Carriers Not Required to Collect PFC's: Air taxis  filing FAA Form 180031 except commuter air carriers.</p><p>    Determination: Approved. Based on information contained in the 
public agency's application, the FAA has determined that the approved 
class accounts for less than 1 perce<script type="text/javascript">
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  <guid>http://thefederalregister.com/d.p/2003-12-01-03-29847</guid>
  <pubDate>Mon, Dec 1 2003 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Environmental Impact Statement: Kootenai and Bonner Counties,  Idaho]]></title>
  <link>http://thefederalregister.com/d.p/2003-12-01-03-29789</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 
highway project in Kootenai and Bonner Counties, Idaho.
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  <guid>http://thefederalregister.com/d.p/2003-12-01-03-29789</guid>
  <pubDate>Mon, Dec 1 2003 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Office of Research and Technology Forum ]]></title>
  <link>http://thefederalregister.com/d.p/2003-12-01-03-29851</link>
  <description><![CDATA[ This notice invites interested persons to participate in a 
forum sponsored by the FMCSA Office of Research and Technology in 
conjunction with the 83rd Annual Meeting of the Transportation Research 
Board. The purpose of the forum is to provide insights into building 
publicprivate partnerships that involve government, academia and 
industry through panel discussions and presentations highlighting such 
collaborations. On Panel I, attendees will learn about some recently 
completed and current research being managed by FMCSA staff in the 
areas of the Commercial Vehicle Information Systems & Networks, 
electronic onboard recorders, crash causation, CMV medical 
qualifications and testing, and the National Commercial Vehicle 
Roadside Testing Lab. On Panel II, industry representatives will  present firsthand accounts of how their<br/> [[Page 67259]]<br/>
organizations have worked with FMCSA to develop and promote research 
and technology designed to achieve mutual commercial motor vehicle 
safety goals and objectives.<script type="text/javascript">
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  <guid>http://thefederalregister.com/d.p/2003-12-01-03-29851</guid>
  <pubDate>Mon, Dec 1 2003 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Railroad Safety Advisory Committee (``RSAC''); Working Group  Activity Update]]></title>
  <link>http://thefederalregister.com/d.p/2003-12-01-03-29849</link>
  <description><![CDATA[ FRA is updating its announcement of RSAC's working group 
activities to reflect their current status. For additional details on 
completed activities see prior working group activity notices (68 FR 
25677).
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  <guid>http://thefederalregister.com/d.p/2003-12-01-03-29849</guid>
  <pubDate>Mon, Dec 1 2003 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Federal Motor Vehicle Safety Standards; Fuel Systems Integrity]]></title>
  <link>http://thefederalregister.com/d.p/2003-12-01-03-29805</link>
  <description><![CDATA[ In this document, NHTSA is upgrading the rear impact test in 
the Federal motor vehicle safety standard on fuel system integrity. To 
simulate being struck in the rear by another vehicle, that standard 
currently specifies that the full width of the rear of the test vehicle 
be impacted with a flat, rigid barrier at speeds up to 48 km/h (30 
mph). This final rule replaces that full rear impact test procedure 
with an offset rear impact test procedure specifying that only a 
portion of the width of the rear of the test vehicle be impacted at 80 
km/h (50 mph). Under the new rear impact procedure, a lighter, 
deformable barrier is used. The barrier is very similar to the one used 
for dynamic testing in the agency's side impact protection standard, 
except that the rear impact barrier's face is mounted slightly lower to 
simulate the diving of the front end of a vehicle during precrash 
braking. The agency has concluded that the new, more stringent rear 
impact test procedure will save lives and prevent injuri<script type="text/javascript">
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  <guid>http://thefederalregister.com/d.p/2003-12-01-03-29805</guid>
  <pubDate>Mon, Dec 1 2003 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Innovative Grants To Support Increased Safety Belt Use Rates]]></title>
  <link>http://thefederalregister.com/d.p/2003-12-01-03-29850</link>
  <description><![CDATA[ NHTSA announces the fifth year of a grant program under 
Section 1403 of the Transportation Equity Act for the 21st Century 
(TEA21) to provide funding to States for innovative projects to 
increase safety belt use rates. Consistent with prior years, the goal 
of this program is to increase safety belt use rates across the Nation 
in order to reduce the deaths, injuries, and societal costs that result 
from motor vehicle crashes. Award of funds will be based on criteria 
specified in this Notice. This Notice solicits applications from the 
States, the District of Columbia and Puerto Rico, through their 
Governors' Representatives for Highway Safety, for funds to be made 
available in fiscal year (FY) 2004. Detailed application instructions 
are provided in the Application Procedure and the Application Contents 
and Grant Criteria sections of this Notice.
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  <guid>http://thefederalregister.com/d.p/2003-12-01-03-29850</guid>
  <pubDate>Mon, Dec 1 2003 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Gas and Hazardous Liquid Gathering Lines ]]></title>
  <link>http://thefederalregister.com/d.p/2003-12-01-03-29394</link>
  <description><![CDATA[ This document announces a public meeting and an opportunity to 
submit written comments on the safety regulation of gas and hazardous 
liquid gathering lines. Congress has directed RSPA to define 
``gathering line'' for gas and hazardous liquid pipeline transportation 
and, if appropriate, define as ``regulated gathering line'' those rural 
gathering lines that, because of specific physical characteristics, 
should be regulated. The gas pipeline regulations do not clearly 
distinguish gathering lines from production facilities and transmission 
lines. This lack of clarity has caused many disputes between government 
and industry over whether the regulations cover particular pipelines. 
The current definition of hazardous liquid gathering has worked [[Page 67130]]<br/>
well. We will consider all public comments in developing future 
proposals on gathering lines.
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  <guid>http://thefederalregister.com/d.p/2003-12-01-03-29394</guid>
  <pubDate>Mon, Dec 1 2003 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Pipeline Safety: Passage of Internal Inspection Devices ]]></title>
  <link>http://thefederalregister.com/d.p/2003-12-01-03-29853</link>
  <description><![CDATA[ On April 12, 1994, RSPA issued a regulation requiring pipeline 
operators to design and construct certain new transmission lines and 
certain existing line sections that contain replaced pipe or components 
to accommodate the passage of instrumented internal inspection devices. 
Responding to petitions for reconsideration, we suspended enforcement 
on some facilities and invited comments on proposed changes to the  regulation. To help us reach a<br/> [[Page 67129]]<br/>
final decision on the petitions and issues raised by commenters, this 
notice seeks responses to the questions stated below under 
SUPPLEMENTARY INFORMATION concerning offshore gas transmission lines.
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  <guid>http://thefederalregister.com/d.p/2003-12-01-03-29853</guid>
  <pubDate>Mon, Dec 1 2003 11:00:00 GMT</pubDate>
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