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    <title>The Federal Register</title>
    <link>http://thefederalregister.com/b.p/department/DEPARTMENT_OF_TRANSPORTATION/2008-06-13/</link>
    <description>Daily Publications of Meetings and Rules Changes for the Federal Government</description>
    <pubDate>Tue, Dec 2 2008 11:00:00 GMT</pubDate>
    <lastBuildDate>Tue, Dec 2 2008 11:00:00 GMT</lastBuildDate>
    <webMaster>info@thefederalregister.com</webMaster>
    <item>
  <title><![CDATA[  Airworthiness Directives; Sandel Avionics Incorporated Model  ST3400 Terrain Awareness Warning System/Radio Magnetic]]></title>
  <link>http://thefederalregister.com/d.p/2008-06-13-E8-13165</link>
  <description><![CDATA[ The FAA is revising an existing airworthiness directive (AD) 
that applies to Sandel Avionics Incorporated Model ST3400 TAWS/RMI 
units as described above. The existing AD currently requires installing 
a warning placard on the TAWS/RMI and revising the Limitations section 
of the airplane flight manual (AFM). The existing AD also requires 
installing upgraded software in the TAWS/RMI. This new AD allows 
installing later revisions of the software described in the existing 
AD. This AD results from a report that an inflight bearing error 
occurred in a Model ST3400 TAWS/RMI configured to receive bearing 
information from a very high frequency omnidirectional range (VOR) 
receiver interface via a composite video signal, due to a combination 
of input signal fault and software error. We are issuing this AD to 
prevent a bearing error, which could lead to an airplane departing from 
its scheduled flight path, which could result in a reduction in 
separation from, and a possible collision with, other aircraft or<script type="text/javascript">
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  <guid>http://thefederalregister.com/d.p/2008-06-13-E8-13165</guid>
  <pubDate>Fri, Jun 13 2008 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Establishment of Class E Airspace; Hinton, OK ]]></title>
  <link>http://thefederalregister.com/d.p/2008-06-13-E8-12906</link>
  <description><![CDATA[ This action confirms the effective date of the direct final 
rule that establishes Class E airspace at Hinton, OK, published in the 
Federal Register March 26, 2008 (73 FR 15881), Docket No. FAA2008
0328, Airspace Docket No. 08ASW4.
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  <guid>http://thefederalregister.com/d.p/2008-06-13-E8-12906</guid>
  <pubDate>Fri, Jun 13 2008 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Revision of Legal Descriptions of Multiple Federal Airways in the  Vicinity of Farmington, NM]]></title>
  <link>http://thefederalregister.com/d.p/2008-06-13-E8-11966</link>
  <description><![CDATA[ This technical amendment corrects an error in the airspace 
description of a final rule published in the Federal Register on July 
21, 2003 (68 FR 42962), Docket No. FAA200213013, Airspace Docket No. 
02ANM10. In that rule, the description of Jet Route 10 (J10) was 
incorrect. This is an administrative correction to a published legal 
description. Additionally, the cite for J10 was incorrectly written as 
paragraph 6010(a) Domestic VOR Federal Airways: This will be corrected 
to ``paragraph 2006 Jet Routes''.
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  <guid>http://thefederalregister.com/d.p/2008-06-13-E8-11966</guid>
  <pubDate>Fri, Jun 13 2008 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[
Standard Instrument Approach Procedures, and Takeoff Minimums and  Obstacle Departure Procedures; Miscellaneous]]></title>
  <link>http://thefederalregister.com/d.p/2008-06-13-E8-12864</link>
  <description><![CDATA[ This rule establishes, amends, suspends, or revokes Standard 
Instrument Approach Procedures (SIAPs) and associated Takeoff Minimums 
and Obstacle Departure Procedures for operations at certain airports. 
These regulatory actions are needed because of the adoption of new or 
revised criteria, or because of changes occurring in the National 
Airspace System, such as the commissioning of new navigational 
facilities, adding new obstacles, or changing air traffic requirements. 
These changes are designed to provide safe and efficient use of the 
navigable airspace and to promote safe flight operations under 
instrument flight rules at the affected airports.
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  <guid>http://thefederalregister.com/d.p/2008-06-13-E8-12864</guid>
  <pubDate>Fri, Jun 13 2008 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Standard Instrument Approach Procedures, and Takeoff Minimums and  Obstacle Departure Procedures; Miscellaneous]]></title>
  <link>http://thefederalregister.com/d.p/2008-06-13-E8-12867</link>
  <description><![CDATA[ This Rule establishes, amends, suspends, or revokes STANDARD 
Instrument Approach Procedures (SIAPs) and associated Takeoff Minimums 
and Obstacle Departure Procedures for operations at certain airports. 
These regulatory actions are needed because of the adoption of new or 
revised criteria, or because of changes occurring in the National 
Airspace System, such as the commissioning of new navigational 
facilities, adding new obstacles, or changing air traffic requirements. 
These changes are designed to provide safe and efficient use of the 
navigable airspace and to promote safe flight operations under 
instrument flight rules at the affected airports.
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  <guid>http://thefederalregister.com/d.p/2008-06-13-E8-12867</guid>
  <pubDate>Fri, Jun 13 2008 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; APEX Aircraft Model CAP 10 B Airplanes]]></title>
  <link>http://thefederalregister.com/d.p/2008-06-13-E8-13319</link>
  <description><![CDATA[ We are revising an earlier NPRM for the products listed above. 
This proposed 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>    An internal review evidenced that the flight controls tie rod 
bolts currently installed on the airplane are not in accordance with 
the design data. Indeed the bolt shank length has been determined 
too short and the material properties of the spacers have been found  inadequate according to the prescribed torque value.</p><p>    Therefore, bolts' threads could be subject to excessive wear, 
which might induce play in flight controls and consequently, induce 
vibrations in the control surfaces and reduce the airplane handling.
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/2008-06-13-E8-13319</guid>
  <pubDate>Fri, Jun 13 2008 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; DG Flugzeugbau GmbH Model DG-500MB  Powered Sailplanes]]></title>
  <link>http://thefederalregister.com/d.p/2008-06-13-E8-13324</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) 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>    A DG500MB experienced, after the engine shutdown, an  uncommanded retraction of its powerplant.</p><p>    Investigations revealed that some bolts of the extension 
retraction mechanism had fractured because of fatigue stress due to 
increasing pushpull loads acting on incorrectly tightened screws.
</p><p>    This condition, if not corrected, could lead to damage of the 
propeller and the fuselage, thereby reducing the structural  integrity of the sailplane.</p><p>    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/2008-06-13-E8-13324</guid>
  <pubDate>Fri, Jun 13 2008 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Lockheed Model 382, 382B, 382E, 382F,  and 382G Series Airplanes]]></title>
  <link>http://thefederalregister.com/d.p/2008-06-13-E8-13322</link>
  <description><![CDATA[ We propose to adopt a new airworthiness directive (AD) for all 
Lockheed Model 382, 382B, 382E, 382F, and 382G series airplanes. This 
proposed AD would require revising the FAAapproved maintenance program 
by incorporating new airworthiness limitations for fuel tank systems to 
satisfy Special Federal Aviation Regulation No. 88 requirements. This 
proposed AD would also require the accomplishment of certain fuel 
system modifications, the initial inspections of certain repetitive 
fuel system limitations to phase in those inspections, and repair if 
necessary. This proposed AD results from a design review of the fuel 
tank systems. We are proposing this AD to prevent the potential for 
ignition sources inside fuel tanks caused by latent failures, 
alterations, repairs, or maintenance actions, which, in combination 
with flammable fuel vapors, could result in a fuel tank explosion and 
consequent loss of the airplane.
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  <guid>http://thefederalregister.com/d.p/2008-06-13-E8-13322</guid>
  <pubDate>Fri, Jun 13 2008 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Petition for Waiver of Compliance ]]></title>
  <link>http://thefederalregister.com/d.p/2008-06-13-E8-13376</link>
  <description><![CDATA[
</p><p>    In accordance with Part 211 of Title 49 Code of Federal Regulations 
(CFR), notice is hereby given that the Federal Railroad Administration 
(FRA) received a request for a waiver of compliance with certain 
requirements of its safety standards. The individual petition is 
described below, including the party seeking relief, the regulatory 
provisions involved, the nature of the relief being requested, and the  petitioner's arguments in favor of relief.<br/> CSX Transportation</p>
<h3>[Docket Number FRA20080039]</h3>
<p>    CSX Transportation (CSXT) seeks a waiver of compliance from certain 
provisions of 49 CFR Part 231 Safety Appliance Standards, that requires 
uncoupling levers on each end of freight cars. Specifically, this 
request is to remove uncoupling levers on CSXT owned special equipment 
cars in rail train service while loading or unloading continuous welded  rail throughout the CSXT system by CSXT forces.</p><p>    CSXT believes that these welded rail cars can be operated safely 
with the uncoupling levers removed and <script type="text/javascript">
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  <guid>http://thefederalregister.com/d.p/2008-06-13-E8-13376</guid>
  <pubDate>Fri, Jun 13 2008 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Procedures for Transportation Workplace Drug and Alcohol Testing  Programs: State Laws Requiring Drug and Alcohol Rule]]></title>
  <link>http://thefederalregister.com/d.p/2008-06-13-E8-13377</link>
  <description><![CDATA[ The Office of the Secretary (OST) is amending its drug and 
alcohol testing procedures to authorize employers to disclose to State 
commercial driver licensing (CDL) authorities the drug and alcohol 
violations of employees who hold CDLs and operate commercial motor 
vehicles (CMVs), when a State law requires such reporting. This rule 
also permits thirdparty administrators (TPAs) to provide the same 
information to State CDL licensing authorities where State law requires 
the TPAs to do so for owneroperator CMV drivers with CDLs.
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  <guid>http://thefederalregister.com/d.p/2008-06-13-E8-13377</guid>
  <pubDate>Fri, Jun 13 2008 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Notice of Applications for Certificates of Public Convenience and  Necessity and Foreign Air Carrier Permits Filed]]></title>
  <link>http://thefederalregister.com/d.p/2008-06-13-E8-13357</link>
  <description><![CDATA[
</p><p>    The following Applications for Certificates of Public Convenience 
and Necessity and Foreign Air Carrier Permits were filed under Subpart 
B (formerly Subpart Q) of the Department of Transportation's Procedural 
Regulations (See 14 CFR 301.201 et. seq.). The due date for Answers, 
Conforming Applications, or Motions to Modify Scope are set forth below 
for each application. Following the Answer period DOT may process the 
application by expedited procedures. Such procedures may consist of the 
adoption of a showcause order, a tentative order, or in appropriate  cases a final order without further proceedings.<br/> </p><p>    Docket Number: DOTOST20070084.<br/> </p><p>    Date Filed: February 25, 2008.</p><p>    Due Date for Answers, Conforming Applications, or Motion to Modify  Scope: March 17, 2008.</p><p>    Description: Application of Pinnacle Airlines, Inc., requesting a 
certificate of public convenience and necessity to engage in scheduled 
foreign air transportation of persons, property, and mail between (i) a 
point or points in th<script type="text/javascript">
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  <guid>http://thefederalregister.com/d.p/2008-06-13-E8-13357</guid>
  <pubDate>Fri, Jun 13 2008 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Aviation Proceedings, Agreements filed the Week Ending February  29, 2008]]></title>
  <link>http://thefederalregister.com/d.p/2008-06-13-E8-13359</link>
  <description><![CDATA[
</p><p>    The following Agreements were filed with the Department of 
Transportation under the provisions of 49 U.S.C. Sections 412 and 414. 
Answers may be filed within 21 days after the filing of the  application.<br/> </p><p>    Docket Number DOTOST200626409.<br/> </p><p>    Date Filed February 29, 2008.</p><p>    Parties Members of the International Air Transport Association.
</p><p>    Subject TC23 Middle East, AfricaSouth West Pacific, Flex Fares 
Package, Expedited Resolutions, (Memo 0364/0366). Intended effective  date: 1 July 2008.<br/> </p><p>    Docket Number DOTOST20080077.<br/> </p><p>    Date Filed February 29, 2008.</p><p>    Parties Members of the International Air Transport Association.
</p><p>    Subject TC23 Middle East, AfricaSouth West Pacific, Expedited 
Composite Resoultions (Memo 0367/0365), Intended effective date: 1 July  2008.<br/> </p><p>    Docket Number DOTOST20080078.<br/> </p><p>    Date Filed February 29, 2008.</p><p>    Parties Members of the International Air Transport Association,
</p><p>    Subject TC2 Within Africa, Resolutions and Specified Fares Tables [[Page 33873]]<br/>
 (Memo 0180). In<script type="text/javascript">
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  <pubDate>Fri, Jun 13 2008 11:00:00 GMT</pubDate>
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