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    <title>The Federal Register</title>
    <link>http://thefederalregister.com/b.p/department/DEPARTMENT_OF_TRANSPORTATION/2007-12-17/</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 747-200B, 747-300, and  747-400 Series Airplanes]]></title>
  <link>http://thefederalregister.com/d.p/2007-12-17-E7-24334</link>
  <description><![CDATA[ The FAA is adopting a new airworthiness directive (AD) for 
certain Boeing Model 747200B, 747300, and 747400 series airplanes. 
This AD requires an inspection to determine the manufacturer and 
manufacture date of the oxygen masks in the passenger service units of 
the outboard and center main deck, the flight attendant service units, 
flightcrew rest, upper and lower module of the door 5 overhead crew 
rest, lavatory modules, and miscellaneous ceiling panels, as 
applicable, and related investigative/corrective actions if necessary. 
This AD results from a report that several passenger masks with broken 
inline flow indicators were found following a mask deployment. We are 
issuing this AD to prevent the inline flow indicators of the passenger 
oxygen masks from fracturing and separating, which could inhibit oxygen 
flow to the masks and consequently result in exposure of the passengers 
and cabin attendants to hypoxia following a depressurization event.
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  <guid>http://thefederalregister.com/d.p/2007-12-17-E7-24334</guid>
  <pubDate>Mon, Dec 17 2007 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/2007-12-17-E7-24335</link>
  <description><![CDATA[ We are adopting a new airworthiness directive (AD) for certain  Boeing Model 737100, 200, 200C, 300, 400, and 500 series <br/>
airplanes. This AD requires repetitive detailed and highfrequency eddy 
current inspections for cracking around the heads of the fasteners on 
the forward fastener row of certain areas of the station (STA) 259.5 
circumferential butt splice, and repair if necessary. This AD also 
requires a preventive modification, which eliminates the need for the 
repetitive inspections. This AD results from a report that an operator 
found multiple cracks in the fuselage skin of a Model 737200 airplane, 
at the forward fastener row of the STA 259.5 circumferential butt 
splice between stringers 19 and 24. We are issuing this AD to prevent 
cracking of the STA 259.5 circumferential butt splice, which could 
result in loss of structural integrity of the fuselage skin and 
possible loss of cabin pressure.
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  <guid>http://thefederalregister.com/d.p/2007-12-17-E7-24335</guid>
  <pubDate>Mon, Dec 17 2007 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Boeing Model 757-200, -200CB, and -300  Series Airplanes]]></title>
  <link>http://thefederalregister.com/d.p/2007-12-17-E7-24337</link>
  <description><![CDATA[ We are adopting a new airworthiness directive (AD) for certain 
Boeing Model 757200, 200CB, and 300 series airplanes. This AD 
requires repetitive detailed inspections with a borescope for cracks of 
the intercostal tee clips; or repetitive detailed inspections for 
cracks of the intercostal tee clips and attachment fasteners at the 
number 3 and number 4 doorstops of the passenger door cutouts; and 
related investigative and corrective actions if necessary. This AD also 
provides an optional terminating action for the repetitive inspections. 
This AD results from reports of cracked intercostal tee clips at the 
number 3 and number 4 doorstops of the passenger door cutouts. We are 
issuing this AD to detect and correct cracking of the tee clips, which 
could result in additional stress on the adjacent tee clips, 
surrounding intercostals, edge frame, door structure and doorstops. 
This additional stress could cause further cracking or breaking of the 
tee clips, which could result in failure of the door to s<script type="text/javascript">
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  <guid>http://thefederalregister.com/d.p/2007-12-17-E7-24337</guid>
  <pubDate>Mon, Dec 17 2007 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Boeing Model 777-200, -200LR, -300, and  -300ER Series Airplanes]]></title>
  <link>http://thefederalregister.com/d.p/2007-12-17-E7-24338</link>
  <description><![CDATA[ The FAA is adopting a new airworthiness directive (AD) for all [[Page 71213]]<br/>
Boeing Model 777200, 200LR, 300, and 300ER series airplanes. This 
AD requires doing initial and repetitive inspections for cracking of 
the elevator actuator fittings, and replacing any cracked fitting with 
a new fitting. This AD results from a report that a cracked left 
elevator actuator fitting was found on a Model 777 airplane. We are 
issuing this AD to detect and correct a cracked actuator fitting, which 
could detach from the elevator and lead to an unrestrained elevator and 
an unacceptable flutter condition, which could result in loss of 
airplane control.
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  <guid>http://thefederalregister.com/d.p/2007-12-17-E7-24338</guid>
  <pubDate>Mon, Dec 17 2007 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Boeing Model 747-200C and -200F Series  Airplanes]]></title>
  <link>http://thefederalregister.com/d.p/2007-12-17-E7-24340</link>
  <description><![CDATA[ The FAA is adopting a new airworthiness directive (AD) for 
certain Boeing Model 747200C and 200F series airplanes. This AD 
requires, among other actions, installing mounting brackets, support 
angles, and moisture curtains in the main equipment center. This AD 
results from reports of water contamination in the electrical/
electronic units in the main equipment center. We are issuing this AD 
to prevent water contamination of the electrical/electronic units, 
which could cause the electrical/electronic units to malfunction, and 
as a consequence, could adversely affect the airplane's continued safe 
flight.
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  <guid>http://thefederalregister.com/d.p/2007-12-17-E7-24340</guid>
  <pubDate>Mon, Dec 17 2007 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; McDonnell Douglas Model DC-10-10, DC- 10-10F, DC-10-15, DC-10-30 and DC-10-30F (KC-10A and]]></title>
  <link>http://thefederalregister.com/d.p/2007-12-17-E7-23934</link>
  <description><![CDATA[ The FAA is adopting a new airworthiness directive (AD) for 
certain McDonnell Douglas Model DC1010, DC1010F, DC1015, DC1030 
and DC1030F (KC10A and KDC10) airplanes; Model DC1040 and DC10
40F airplanes; and Model MD11 and MD11F airplanes. This AD requires, 
for certain airplanes, modifying the thrust reverser command wiring of 
the number 2 engine. For certain other airplanes, this AD requires  modifying the thrust<br/> [[Page 71207]]<br/>
reverser system wiring from the flight compartment to engines 1, 2, and 
3 thrust reversers. This AD also requires installing thrust reverser 
locking systems on certain airplanes. This AD results from a 
determination that the thrust reverser systems on these McDonnell 
Douglas airplanes do not adequately preclude unwanted deployment of a 
thrust reverser. We are issuing this AD to prevent an unwanted 
deployment of a thrust reverser during flight, which could result in 
reduced controllability of the airplane.
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  <guid>http://thefederalregister.com/d.p/2007-12-17-E7-23934</guid>
  <pubDate>Mon, Dec 17 2007 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Thrush Aircraft, Inc. Model S2R Series  Airplanes]]></title>
  <link>http://thefederalregister.com/d.p/2007-12-17-E7-24218</link>
  <description><![CDATA[ We are adopting a new airworthiness directive (AD) for certain 
Thrush Aircraft, Inc. (Thrush) Model S2R series airplanes. This AD 
requires you to do repetitive visual inspections of the vertical and 
horizontal stabilizer attach fitting, attach fitting bolts, and the 
vertical fin aft spar for cracks or corrosion. This AD also requires 
immediate replacement of the vertical and horizontal stabilizer attach 
fittings and attach fitting bolts if cracked or corroded parts are 
found, and the inspection of the vertical fin aft spar with repair or 
replacement if cracks or corrosion are found. This AD requires the 
eventual replacement of the vertical and horizontal stabilizer attach 
fittings and attach fitting bolts if no corrosion or cracks are found 
as terminating action for the repetitive inspections. This AD results 
from reports of cracks in the empennage of Thrush S2R series airplanes. 
We are issuing this AD to detect and correct these cracks, which could 
cause the vertical stabilizer to lose structu<script type="text/javascript">
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  <guid>http://thefederalregister.com/d.p/2007-12-17-E7-24218</guid>
  <pubDate>Mon, Dec 17 2007 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Airbus Model A319, A320, and A321  Series Airplanes]]></title>
  <link>http://thefederalregister.com/d.p/2007-12-17-E7-24332</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>    During planned maintenance visit on two aircraft, corrosion was 
found on the upper surface of the wing lower skin panel N\o\1,  inside the Right Hand (RH) inboard dry bay.</p><p>    It was discovered that [certain] access panels * * * had been 
omitted from the access requirements of the associated AMM (airplane 
maintenance manual) task (AMM 052540) until the August 2001  revision.</p><p>    The result is that some * * * inspections may have not been 
fully accomplished due to nonremoval of [certain] panels * * *.
</p><p>    If the area has not been inspected with the correct access, and 
if AIRBUS Service Bulletin (SB) A320571121 has not been performed, 
then some aircraft could remai<script type="text/javascript">
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  <guid>http://thefederalregister.com/d.p/2007-12-17-E7-24332</guid>
  <pubDate>Mon, Dec 17 2007 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; ATR Model ATR42 and ATR72 Airplanes]]></title>
  <link>http://thefederalregister.com/d.p/2007-12-17-E7-24382</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:<br/>
    [T]he FAA has published a set of new rules related to the fuel 
tank safety, including the Special Federal Aviation Regulation 88  (SFAR 88).</p><p>    The JAA (Joint Aviation Authority) has issued an Interim Policy 
JAA INT/POL 25/12, to recommend the application of a similar 
requirement to the National Aviation Authorities (NAA) [of Europe]. * * * * *<br/>
    * * * ATR carried out a safety review on the fuel tank systems 
and zones adjacent to the fuel tanks on all ATR models * * *. * * * * *<br/>
The unsafe condition is the potential of ignition sources inside fuel 
tanks, which, in combination with flammable fuel vapors, could result 
in fuel tank explosions and consequent loss <script type="text/javascript">
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  <guid>http://thefederalregister.com/d.p/2007-12-17-E7-24382</guid>
  <pubDate>Mon, Dec 17 2007 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Boeing Model 757 Airplanes ]]></title>
  <link>http://thefederalregister.com/d.p/2007-12-17-E7-24329</link>
  <description><![CDATA[ The FAA proposes to adopt a new airworthiness directive (AD) 
for all Boeing Model 757 airplanes. This proposed AD would require 
repetitive inspections of the anchor tab of the bulkhead seal 
assemblies of the wing thermal antiice (TAI) system for cracks [[Page 71276]]<br/>
at certain outboard stations of the left and right wings, and 
corrective action if necessary. This proposed AD also provides optional 
terminating action for the repetitive inspections. This proposed AD 
results from reports of cracks found at the anchor tab of the bulkhead 
seal assemblies of the wing TAI system. In one incident the anchor tab 
and bulkhead seal assembly had separated because of the cracks. We are 
proposing this AD to prevent failure of the anchor tab of the bulkhead 
seal assembly, which in icing conditions could result in insufficient 
airflow to the wing TAI system, subsequent ice on the wings, and 
consequent reduced controllability of the airplane.
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  <guid>http://thefederalregister.com/d.p/2007-12-17-E7-24329</guid>
  <pubDate>Mon, Dec 17 2007 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Boeing Model 757-200, -200PF, and - 200CB Series Airplanes]]></title>
  <link>http://thefederalregister.com/d.p/2007-12-17-E7-24383</link>
  <description><![CDATA[ The FAA proposes to adopt a new airworthiness directive (AD) 
for certain Boeing Model 757200, 200PF, and 200CB series airplanes. 
This proposed AD would require doing an ultrasound inspection for 
disbonded tear straps not mechanically fastened to the skin, and 
related investigative and corrective actions, if necessary. This 
proposed AD results from reports indicating that bonded skin panels may 
not have been correctly anodized in phosphoric acid before the tear 
strap doubler was bonded to the skin. We are proposing this AD to 
detect and correct a weak bond between the skin and tear strap. Such 
disbonding could reduce the ability of the skin to resist cracks and 
could adversely affect the structural integrity of the airplane.
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  <guid>http://thefederalregister.com/d.p/2007-12-17-E7-24383</guid>
  <pubDate>Mon, Dec 17 2007 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Bombardier Model CL-600-2B19 (Regional  Jet Series 100 & 440) Airplanes]]></title>
  <link>http://thefederalregister.com/d.p/2007-12-17-E7-24327</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>    Bombardier Aerospace has completed a system safety review of the 
CL6002B19 aircraft fuel system against new fuel tank safety 
standards, introduced in Chapter 525 of the Airworthiness Manual 
through Notice of Proposed Amendment (NPA) 2002043. The identified 
noncompliances were assessed using Transport Canada Policy Letter 
No. 525001 to determine if mandatory corrective action is required.
</p><p>    The assessment and lightning tests showed that certain fuel tube 
selfbonded couplings do not provide sufficient lightning current 
capability. The assessment also showed that single failure of the 
integral bonding wire of the selfbonded couplings or excessive 
axial clearanc<script type="text/javascript">
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  <guid>http://thefederalregister.com/d.p/2007-12-17-E7-24327</guid>
  <pubDate>Mon, Dec 17 2007 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; EADS SOCATA Model TBM 700 Airplanes]]></title>
  <link>http://thefederalregister.com/d.p/2007-12-17-E7-24321</link>
  <description><![CDATA[ We propose to adopt a new airworthiness directive (AD) for the 
products listed above that would supersede an existing AD. 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 nonrespect of the pilot door adjustment procedure could have  damaged the stop fitting and could result in a consequent <br/> depressurization of the airplane.<br/>
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/2007-12-17-E7-24321</guid>
  <pubDate>Mon, Dec 17 2007 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Empresa Brasileira de Aeronautica S.A.  (EMBRAER) Model EMB-135BJ, -135ER, -135KE, -135KL,]]></title>
  <link>http://thefederalregister.com/d.p/2007-12-17-E7-24330</link>
  <description><![CDATA[ The FAA proposes to supersede an existing airworthiness 
directive (AD) that applies to all EMBRAER Model EMB135BJ, 135ER, 
135KE, 135KL, 135LR, 145, 145ER, 145MR, 145LR, 145XR, 145MP, 
and 145EP airplanes. The existing AD currently requires reviewing the 
airplane maintenance records for recent reports of vibration from the 
tail section or rudder pedals. The existing AD also currently requires 
repetitively inspecting the skin, attachment fittings, and control rods 
of rudder II to detect cracking, loose parts, wear, or damage; and 
related investigative/corrective actions if necessary. This proposed AD 
would require the existing repetitive inspection to be done with new 
service information. This proposed AD also would require replacing the 
locking tab washers on the control rods of the rudder II and installing 
springs on the hinge assemblies of the rudder II, which would terminate 
the repetitive inspection requirements. This proposed AD results from 
reports of rudder vibration due to wear. We are pr<script type="text/javascript">
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  <guid>http://thefederalregister.com/d.p/2007-12-17-E7-24330</guid>
  <pubDate>Mon, Dec 17 2007 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; SAAB Model SF340A and Model 340B  Airplanes]]></title>
  <link>http://thefederalregister.com/d.p/2007-12-17-E7-24326</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>    Subsequent to accidents involving Fuel Tank System explosions in 
flight * * * and on ground, the FAA has published Special Federal 
Aviation Regulation 88 (SFAR88) * * * [which] required * * *  [conducting] a design review against explosion risks.<br/>
The unsafe condition is the potential of ignition sources inside fuel 
tanks, which, in combination with flammable fuel vapors, could result 
in fuel tank explosions and consequent loss of the airplane. 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/2007-12-17-E7-24326</guid>
  <pubDate>Mon, Dec 17 2007 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Noise Exposure Map Notice for Marana Regional Airport, Marana, AZ]]></title>
  <link>http://thefederalregister.com/d.p/2007-12-17-07-6067</link>
  <description><![CDATA[ The Federal Aviation Administration (FAA) announces its 
determination that the noise exposure maps submitted by the Town of 
Marana, Arizona for Marana Regional Airport under the provisions of 49 
U.S.C. 47501, et seq. (Aviation Safety and Noise Abatement Act) and 14 
CFR part 150 are in compliance with applicable requirements.
[[Page 71475]]
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  <guid>http://thefederalregister.com/d.p/2007-12-17-07-6067</guid>
  <pubDate>Mon, Dec 17 2007 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Notice of Opportunity To Participate, Criteria Requirements and  Application Procedure for Participation in the]]></title>
  <link>http://thefederalregister.com/d.p/2007-12-17-07-6068</link>
  <description><![CDATA[ In anticipation of congress enacting an extension of the 
Airport Improvement Program (AIP) the FAA is publishing this annual 
notice. This notice announces the criteria, application procedures, and 
schedule to be applied by the Secretary of Transportation in 
designating or redesignating, and funding capital development annually 
for up to 15 current (jointuse) or former military airports seeking 
designation or redesignation to participate in the MAP. While FAA 
currently has continuing authority to designate or redesignate 
airports, FAA does not have authority to issue grants for fiscal year 
2008 MAP, and will not have authority until Congress enacts legislation  enabling FAA to issue grants.</p><p>    The MAP allows the Secretary to designate current (jointuse) or  former military airports to receive grants from<br/> [[Page 71476]]<br/>
the Airport Improvement Program (AIP). The Secretary is authorized to 
designate an airport (other than an airport designated before August  24, 1994) only if:<br/>
    (1) The airport is <script type="text/javascript">
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  <guid>http://thefederalregister.com/d.p/2007-12-17-07-6068</guid>
  <pubDate>Mon, Dec 17 2007 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[RIN-2126-AB14 ]]></title>
  <link>http://thefederalregister.com/d.p/2007-12-17-E7-24238</link>
  <description><![CDATA[ FMCSA amends the Federal Motor Carrier Safety Regulations 
effective December 27 to allow commercial motor vehicle (CMV) drivers 
up to 11 hours of driving time within a 14hour, nonextendable window 
from the start of the workday, following 10 consecutive hours off duty 
(11hour limit). This interim rule also allows motor carriers and 
drivers to restart calculations of the weekly onduty time limits after 
the driver has at least 34 consecutive hours off duty (34hour 
restart). An IFR is necessary to prevent disruption to enforcement and 
compliance with the hoursofservice (HOS) rules when the stay expires, 
as well as possible effects on the timely delivery of essential goods 
and services. This IFR will ensure that a familiar and uniform set of 
national rules governs motor carrier transportation, while FMCSA 
gathers public comments on all aspects of this interim final rule, 
conducts peer review of our analysis, and considers the appropriate 
final rule that addresses the issues identified by the Court. <script type="text/javascript">
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  <guid>http://thefederalregister.com/d.p/2007-12-17-E7-24238</guid>
  <pubDate>Mon, Dec 17 2007 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Notice of Request for a New Collection ]]></title>
  <link>http://thefederalregister.com/d.p/2007-12-17-E7-24400</link>
  <description><![CDATA[ The Federal Transit Administration invites public comments 
about our intention to request the Office of Management and Budget's 
(OMB) to approve a new collection: 49 U.S.C. 5317, New Freedom Program. 
The information to be collected will be used to accumulate mass 
transportation financial and operating information using a uniform 
system of accounts and records. The Federal Register Notice with a 60
day comment period soliciting comments was published on October 2, 
2007.
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]]></description>
  <guid>http://thefederalregister.com/d.p/2007-12-17-E7-24400</guid>
  <pubDate>Mon, Dec 17 2007 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Agency Information Collection Activity Under OMB Review ]]></title>
  <link>http://thefederalregister.com/d.p/2007-12-17-E7-24422</link>
  <description><![CDATA[ In accordance with the Paperwork Reduction Act of 1995 (44 
U.S.C. 3501 et seq.), this notice announces that the Information 
Collection Request (ICR) abstracted below has been forwarded to the 
Office of Management and Budget (OMB) for approval. The Federal 
Register Notice with a 60day comment period soliciting comments was 
published on October 1, 2007. No comments were received in response to 
that notice.
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  <guid>http://thefederalregister.com/d.p/2007-12-17-E7-24422</guid>
  <pubDate>Mon, Dec 17 2007 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Reports, Forms, and Record Keeping Requirements Agency  Information Collection Activity Under OMB Review]]></title>
  <link>http://thefederalregister.com/d.p/2007-12-17-E7-24379</link>
  <description><![CDATA[ In compliance with the Paperwork Reduction Act of 1995 (44 
U.S.C. 3501 et seq.), this notice announces that the Information 
Collection Request (ICR) abstracted below has been forwarded to the 
Office of Management and Budget (OMB) for review and comment. The ICR 
describes the nature of the information collection and the expected 
burden. The Federal Register Notice with a 60day comment period was 
published on April 27, 2007 (72 FR 2106821069).
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  <guid>http://thefederalregister.com/d.p/2007-12-17-E7-24379</guid>
  <pubDate>Mon, Dec 17 2007 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Conforming Products List of Evidential Breath Alcohol Measurement  Devices]]></title>
  <link>http://thefederalregister.com/d.p/2007-12-17-07-6040</link>
  <description><![CDATA[ This notice updates the Conforming Products List (CPL) 
published in the Federal Register on June 29, 2006 (71 FR 37159) for 
instruments that conform to the Model Specifications for Evidential 
Breath Testing Devices (58 FR 48705).
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  <guid>http://thefederalregister.com/d.p/2007-12-17-07-6040</guid>
  <pubDate>Mon, Dec 17 2007 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Mid-Michigan Railroad, Inc.--Abandonment Exemption--In Kent and  Montcalm Counties, MI]]></title>
  <link>http://thefederalregister.com/d.p/2007-12-17-E7-24311</link>
  <description><![CDATA[
</p><p>    On November 27, 2007, MidMichigan Railroad, Inc. (MMRR or 
petitioner), filed with the Surface Transportation Board a petition 
under 49 U.S.C. 10502 for exemption from the provisions of 49 U.S.C. 
10903 to permit the abandonment of a 24.70mile rail line located 
between milepost 103.20 in Lowell and milepost 78.50 in Greenville at 
the end of the line, in Kent and Montcalm Counties, MI. The line 
traverses U.S. Postal Service Zip Codes 48809, 48838, 48887, and 49331,  and<br/> [[Page 71484]]</p>
<h3>includes the stations of Lowell, Belding, and Greenville.</h3>
<p>    In addition to an exemption from 49 U.S.C. 10903, MMRR seeks an 
exemption from 49 U.S.C. 10904 [offer of financial assistance (OFA) 
procedures]. In support, MMRR states that it has entered a Memorandum 
of Understanding with the West Michigan Trails and Greenways Coalition 
(WMTGC) to sell the line to WMTGC for the public purpose of converting 
it to interim trail use/rail banking. This request will be addressed in  the final decision.</p><p>    MMRR states that, <script type="text/javascript">
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  <guid>http://thefederalregister.com/d.p/2007-12-17-E7-24311</guid>
  <pubDate>Mon, Dec 17 2007 11:00:00 GMT</pubDate>
</item>
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