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    <title>The Federal Register</title>
    <link>http://thefederalregister.com/b.p/department/DEPARTMENT_OF_TRANSPORTATION/2007-11-20/</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; Aeromot-Industria Mecanico Metalurgica  Ltda. Model AMT-100/200/200S/300 Gliders]]></title>
  <link>http://thefederalregister.com/d.p/2007-11-20-E7-22176</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>    It has been found the occurrence of incorrect use of the self
locking nuts in bolts subject to rotational loads in bolted fittings 
of some assemblies of metallic components. Such event may result in 
disconnection of those fittings, which jeopardizes the structural  integrity of the aircraft or its flight controls.</p><p>    Since this condition may occur in other airplanes of the same 
type and affects flight safety, a corrective action is required. 
Thus, sufficient reason exists to request compliance with this AD in  the indicated time limit.<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/2007-11-20-E7-22176</guid>
  <pubDate>Tue, Nov 20 2007 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Bell Helicopter Textron Canada Limited  Model 206A, 206B, 206L, 206L-1, 206L-3, 206L-4, 222,]]></title>
  <link>http://thefederalregister.com/d.p/2007-11-20-E7-22416</link>
  <description><![CDATA[ This document publishes in the Federal Register an amendment 
adopting Airworthiness Directive (AD) 20071952, which was sent 
previously to all known U.S. owners and operators of the specified Bell 
Helicopter Textron Canada Limited (BHTC) model helicopters by 
individual letters. This AD requires replacing each affected tail [[Page 65222]]<br/>
rotor blade (blade) with an airworthy blade with a serial number not 
listed in the Rotor Blades, Inc. (RBI), attachment to the BHTC Alert 
Service Bulletin (ASB), listed in the applicability section of this AD. 
This amendment is prompted by three incidents in which blade tip 
weights were slung from blades during flight causing significant 
vibration. The actions specified are intended to prevent loss of a 
blade tip weight, loss of a blade, and subsequent loss of control of 
the helicopter.
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  <guid>http://thefederalregister.com/d.p/2007-11-20-E7-22416</guid>
  <pubDate>Tue, Nov 20 2007 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Bell Helicopter Textron, Inc. Model  204B, 205A, 205A-1, 205B, 210, 212, 412, 412EP, and]]></title>
  <link>http://thefederalregister.com/d.p/2007-11-20-E7-22439</link>
  <description><![CDATA[ This document publishes in the Federal Register an amendment 
adopting Airworthiness Directive (AD) 20071953, which was sent 
previously to all known U.S. owners and operators of the specified Bell 
Helicopter Textron, Inc. (BHTI) model helicopters by individual 
letters. This AD requires replacing each affected tail rotor blade 
(blade) with an airworthy blade with a serial number not listed in the 
applicability of this AD. This AD is prompted by three incidents in 
which blade tip weights were slung from the blades during flight 
causing significant vibration. The actions specified by this AD are 
intended to prevent loss of a blade tip weight, loss of a blade, and 
subsequent loss of control of the helicopter.
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  <guid>http://thefederalregister.com/d.p/2007-11-20-E7-22439</guid>
  <pubDate>Tue, Nov 20 2007 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Cessna Aircraft Company, Model 525B  Airplanes]]></title>
  <link>http://thefederalregister.com/d.p/2007-11-20-E7-22304</link>
  <description><![CDATA[ The FAA is adopting a new airworthiness directive (AD) for 
certain Cessna Aircraft Company (Cessna) Model 525B airplanes. This AD 
requires you to incorporate electrical power relay circuit protection 
kit part number (P/N) SB525B2402. This AD results from both the need 
to protect aircraft wiring left unprotected in the original design and 
a report of a Model 525B airplane experiencing inflight loss of 
numerous systems, tripped circuit breakers, and burned wiring adjacent 
to the power distribution panel. We are issuing this AD to correct an 
incorrect wiring installation and to provide shortcircuit protection 
for all wiring from the aircraft power distribution system. This  condition could result in burned wiring<br/> [[Page 65220]]<br/>
and loss of various aircraft electrical systems.
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  <guid>http://thefederalregister.com/d.p/2007-11-20-E7-22304</guid>
  <pubDate>Tue, Nov 20 2007 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Diamond Aircraft Industries Model DA 42  Airplanes]]></title>
  <link>http://thefederalregister.com/d.p/2007-11-20-E7-22177</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>    Recently, a double inflight engine shut down incident occurred 
on a DA42 aircraft equipped with TAE12501 engines. The BFU (German 
Accident Investigation Body) found the root cause to be a violation 
of the Airplane Flight Manual procedures (takingoff with an 
insufficiently charged main aircraft battery) and momentary low 
voltage in the electrical system of the aircraft when retracting the 
main landing gear. This has been the subject of Diamond Service 
Information (SI) 42040 and a subsequent EASA Safety Information  Notice, SIN 200708, issued on 18 April 2007.</p><p>    The TAE12501 and TAE1250299 engines, approved for 
installation on the DA42, are FADEC (Full Authority Digital Engine 
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  <guid>http://thefederalregister.com/d.p/2007-11-20-E7-22177</guid>
  <pubDate>Tue, Nov 20 2007 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Airbus Model A330 Airplanes and A340- 200 and -300 Series Airplanes]]></title>
  <link>http://thefederalregister.com/d.p/2007-11-20-E7-22632</link>
  <description><![CDATA[ This document announces a reopening of the comment period for 
the abovereferenced NPRM. The NPRM proposed the adoption of a new 
airworthiness directive for certain Airbus Model A330 airplanes and 
A340200 and 300 series airplanes. That NPRM invites comments 
concerning the proposed requirements for the inspection of the fuselage 
to identify possible permanent skin repairs and permanent longitudinal 
lap joint repairs and to apply the associated corrective actions. This 
reopening of the comment period is necessary to provide additional  opportunity for public<br/> [[Page 65228]]<br/>
comment on the proposed requirements of that NPRM.
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  <guid>http://thefederalregister.com/d.p/2007-11-20-E7-22632</guid>
  <pubDate>Tue, Nov 20 2007 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Airbus Model A300, A310, and A300-600  Series Airplanes]]></title>
  <link>http://thefederalregister.com/d.p/2007-11-20-E7-22634</link>
  <description><![CDATA[ This document announces a reopening of the comment period for 
the abovereferenced NPRM. The NPRM proposed the adoption of a new 
airworthiness directive for all Airbus Model A300, A310, and A300600 
series airplanes. That NPRM invites comments concerning the proposed 
requirements for revising the Emergency Procedures sections of the 
airplane flight manuals to advise the flightcrew of new procedures for 
emergency evacuation. This reopening of the comment period is necessary 
to provide additional opportunity for public comment on the proposed 
requirements of that NPRM.
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  <guid>http://thefederalregister.com/d.p/2007-11-20-E7-22634</guid>
  <pubDate>Tue, Nov 20 2007 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; BAE Systems (Operations) Limited Model  BAe 146 and Model Avro 146-RJ Airplanes]]></title>
  <link>http://thefederalregister.com/d.p/2007-11-20-E7-22631</link>
  <description><![CDATA[ This document announces a reopening of the comment period for 
the abovereferenced NPRM. The NPRM proposed the adoption of a new 
airworthiness directive for all BAE Systems (Operations) Limited Model 
BAe 146 and Model Avro 146RJ airplanes. That NPRM invites comments 
concerning the proposed requirements for repetitive detailed visual 
inspections for corrosion, pitted fasteners, or pillowing of the APU 
heat shield and surrounding skin and, if applicable, removal of the 
heat shield and repair. This reopening of the comment period is 
necessary to provide additional opportunity for public comment on the 
proposed requirements of that NPRM.
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  <guid>http://thefederalregister.com/d.p/2007-11-20-E7-22631</guid>
  <pubDate>Tue, Nov 20 2007 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Saab Model SAAB-Fairchild SF340A (SAAB/ SF340A) and SAAB 340B Airplanes]]></title>
  <link>http://thefederalregister.com/d.p/2007-11-20-E7-22630</link>
  <description><![CDATA[ This document announces a reopening of the comment period for 
the abovereferenced NPRM. The NPRM proposed the adoption of a new 
airworthiness directive for certain Saab Model SAABFairchild SF340A 
(SAAB/SF340A) and SAAB 340B airplanes. That NPRM invited comments 
concerning the proposed requirements for doing repetitive ultrasonic 
inspections to detect cracking in the axle adaptor, replacing the axle 
adaptor if necessary, and ultimately doing the terminating action of 
inspecting and modifying the main landing gear shock strut and axle 
adaptors. This reopening of the comment period is necessary to provide 
additional opportunity for public comment on the proposed requirements 
of that NPRM.
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  <guid>http://thefederalregister.com/d.p/2007-11-20-E7-22630</guid>
  <pubDate>Tue, Nov 20 2007 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Enhancing Airline Passenger Protections ]]></title>
  <link>http://thefederalregister.com/d.p/2007-11-20-07-5760</link>
  <description><![CDATA[ The Department of Transportation (DOT or Department) is 
seeking comment on whether it should adopt a rule to enhance airline 
passenger protections in the following seven ways: require carriers to 
adopt contingency plans for lengthy tarmac delays and incorporate them 
in their contracts of carriage, require carriers to respond to consumer 
problems, deem operating a chronically delayed flight to be unfair and 
deceptive, require carriers to publish delay data, require carriers to 
publish complaint data, require ontime performance reporting for 
international flights, and require carriers to audit their compliance 
with their customer service plans. We are proposing that most of these 
measures cover certificated or commuter air carriers that operate 
domestic scheduled passenger service using any aircraft with more than 
30 passenger seats. We are proposing that one measure cover the largest 
U.S. and foreign carriers and that two other measures cover the largest 
U.S. carriers.
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  <guid>http://thefederalregister.com/d.p/2007-11-20-07-5760</guid>
  <pubDate>Tue, Nov 20 2007 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Revision of Airline Service Quality Performance Reports and  Disclosure Requirements]]></title>
  <link>http://thefederalregister.com/d.p/2007-11-20-07-5759</link>
  <description><![CDATA[ The U.S. Department of Transportation (DOT) is proposing to 
collect additional data elements when flights are cancelled, diverted, 
or experience gate returns. The additional proposed data elements would 
fill in data gaps giving the Department, the industry, and the public a 
more accurate portrayal of onground delays after flights depart the 
gate but prior to the time they take off and after flights land but 
before they reach the gate.
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  <guid>http://thefederalregister.com/d.p/2007-11-20-07-5759</guid>
  <pubDate>Tue, Nov 20 2007 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Oversales and Denied Boarding Compensation ]]></title>
  <link>http://thefederalregister.com/d.p/2007-11-20-07-5761</link>
  <description><![CDATA[ The Department of Transportation (DOT or Department) is 
proposing to amend its rules relating to oversales and denied boarding 
compensation to increase the limits on the compensation paid to 
``bumped'' passengers, to cover flights by certain U.S. and foreign air 
carriers operated with aircraft seating 30 to 60 passengers, which are 
currently exempt from the rule, and to make other changes. Such changes 
in the rule, if adopted, would be intended to maintain consumer 
protection commensurate with developments in the aviation industry.
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  <guid>http://thefederalregister.com/d.p/2007-11-20-07-5761</guid>
  <pubDate>Tue, Nov 20 2007 11:00:00 GMT</pubDate>
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