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    <title>The Federal Register</title>
    <link>http://thefederalregister.com/b.p/agency/Federal_Aviation_Administration/2008-07-01/</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; Eurocopter France Model AS 355 N  Helicopters]]></title>
  <link>http://thefederalregister.com/d.p/2008-07-01-E8-14717</link>
  <description><![CDATA[ We are adopting a new airworthiness directive (AD) for 
Eurocopter France Model AS 355 N helicopters. This 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 European Aviation Safety Agency 
(EASA), the technical agent for France, with which we have a bilateral 
agreement, states in the MCAI: ``This Airworthiness Directive (AD) is 
issued because it was found that the power drawn by the starter 
generators from the engines is above the consumption capacity at 
altitudes above 3,000 meters, declared for the engines of AS 355 N 
helicopters. Excessive power consumption of the starter generators 
reduces the engine surge margin, which can result in engine failure.''
</p><p>    After engine start, the starter generator functions as the normal 
operational electrical generator. We are issuing this AD to require 
actions that are intended to address this unsafe condition.
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  <guid>http://thefederalregister.com/d.p/2008-07-01-E8-14717</guid>
  <pubDate>Tue, Jul 1 2008 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Viking Air Limited Models DHC-6-1, DHC- 6-100, DHC-6-200, and DHC-6-300 Airplanes]]></title>
  <link>http://thefederalregister.com/d.p/2008-07-01-E8-13844</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>    There have been reports of interrivet cracking on several wing 
front spar adapter assemblies (P/N C6WM10271) on the horizontal and 
vertical flanges. It was determined that the cracking was caused by 
stress corrosion in the short transverse grain initiated by local  riveting induced stresses.<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/2008-07-01-E8-13844</guid>
  <pubDate>Tue, Jul 1 2008 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Viking Air Limited Models DHC-6-1, DHC- 6-100, DHC-6-200, and DHC-6-300 Airplanes]]></title>
  <link>http://thefederalregister.com/d.p/2008-07-01-E8-13848</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>    Service experience indicates that as aircraft become older, they  are more likely to exhibit indications of corrosion.<br/>
Additionally, the FAA has reviewed the service experience and finds 
this action to be necessary based upon that service experience. 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/2008-07-01-E8-13848</guid>
  <pubDate>Tue, Jul 1 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/2008-07-01-E8-14172</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/2008-07-01-E8-14172</guid>
  <pubDate>Tue, Jul 1 2008 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Advisory Circulars: Extended Operations (ETOPS) and Polar  Operations, AC 121-42B and Extended Operations (ETOPS) and]]></title>
  <link>http://thefederalregister.com/d.p/2008-07-01-E8-14879</link>
  <description><![CDATA[ The issuance of Advisory Circular (AC) 121-42B, Extended 
Operations (ETOPS) and Polar Operations, provides certificate holders 
with guidance for obtaining operational approval to conduct ETOPS under  14 CFR part 121.</p><p>    The issuance of AC 13542, Extended Operations (ETOPS) and 
Operations in the North Polar Area, provides certificate holders with 
guidance for obtaining operational approval to conduct Extended 
Operations (ETOPS) under 14 CFR part 135.
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  <guid>http://thefederalregister.com/d.p/2008-07-01-E8-14879</guid>
  <pubDate>Tue, Jul 1 2008 11:00:00 GMT</pubDate>
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