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    <title>The Federal Register</title>
    <link>http://thefederalregister.com/b.p/department/DEPARTMENT_OF_TRANSPORTATION/2003-12-30/</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[  Repair Stations: Service Difficulty Reporting ]]></title>
  <link>http://thefederalregister.com/d.p/2003-12-30-03-31884</link>
  <description><![CDATA[ This final rule amends the regulations governing service 
difficulty reports (SDRs) submitted to the FAA by aeronautical repair 
stations. The FAA is clarifying which type of failures, malfunctions, 
and defects repair stations must report. Finally, FAA is replacing 
certain section references with part references. This action will 
eliminate the need to revise repair station regulations if the FAA 
revises SDR rules.
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  <guid>http://thefederalregister.com/d.p/2003-12-30-03-31884</guid>
  <pubDate>Tue, Dec 30 2003 11:00:00 GMT</pubDate>
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<item>
  <title><![CDATA[  Service Difficulty Reports ]]></title>
  <link>http://thefederalregister.com/d.p/2003-12-30-03-31883</link>
  <description><![CDATA[ The Federal Aviation Administration (FAA) is further delaying 
the effective date of a final rule that amends the reporting 
requirements for air carriers and certificated domestic and foreign 
repair station operators concerning failures, malfunctions, and defects 
of aircraft, aircraft engines, systems, and components. This action is 
prompted by the FAA's decision to address industry concerns about the 
final rule. Delaying the effective date of the final rule will allow 
the agency time for consideration of industry concerns.
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  <guid>http://thefederalregister.com/d.p/2003-12-30-03-31883</guid>
  <pubDate>Tue, Dec 30 2003 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Cessna Aircraft Company Models 172R,  172S, 182S, 182T, T182T, 206H, and T206H Airplanes]]></title>
  <link>http://thefederalregister.com/d.p/2003-12-30-03-31667</link>
  <description><![CDATA[ This document makes a correction to Airworthiness Directive 
(AD) 20032413, which was published in the Federal Register on 
December 4, 2003 (68 FR 67789), and applies to certain Cessna Aircraft 
Company (Cessna) Models 172R, 172S, 182S, 182T, T182T, 206H, and T206H [[Page 75115]]<br/>
airplanes that are equipped with a Honeywell KAP 140 autopilot computer 
system installed on the center instrument control panel near the 
throttle. We inadvertently duplicated affected airplane serial numbers 
and included a serial number that should not be affected by this AD in 
the applicability section. This action corrects the applicability 
section of AD 20032413, Amendment 3913382.
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  <guid>http://thefederalregister.com/d.p/2003-12-30-03-31667</guid>
  <pubDate>Tue, Dec 30 2003 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Titeflex Corporation; Correction]]></title>
  <link>http://thefederalregister.com/d.p/2003-12-30-03-31850</link>
  <description><![CDATA[ This document makes corrections to Airworthiness Directive 
(AD) 20032305 applicable to certain Titeflex Corporation hoses 
installed on Boeing 737300, 400, 500, 600, 700, 700C, 800, 900, 
747400, 757200, 300, 767200, 300, and 300F airplanes, that was 
published in the Federal Register on November 19, 2003 (68 FR 65157). 
The AD number is incorrect in the Preamble Section and in the 
Regulatory Section five corrections are needed in Table 1. This 
document corrects these errors. In all other respects, the original 
document remains the same.
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  <guid>http://thefederalregister.com/d.p/2003-12-30-03-31850</guid>
  <pubDate>Tue, Dec 30 2003 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; GARMIN International Inc. GTX 330 Mode  S Transponders and GTX 330D Diversity Mode S]]></title>
  <link>http://thefederalregister.com/d.p/2003-12-30-03-31978</link>
  <description><![CDATA[ The FAA proposes to adopt a new airworthiness directive (AD) 
for certain GARMIN International Inc. GTX 330/GTX 330D Mode S 
transponders. This proposed AD would require you to install GTX 330/
330D Software Upgrade Version 3.03. This proposed AD is the result of 
observations that the GTX 330 and GTX 330D may detect, from other 
aircraft, the S1 (suppression) interrogating pulse below the Minimum 
Trigger Level (MTL) and, in some circumstances, not reply. The GTX 330/ 330D should still reply even if it detects<br/> [[Page 75175]]<br/>
S1 interrogating pulses below the MTL. We are issuing this proposed AD 
to prevent interrogating aircraft from possibly receiving inaccurate 
replies due to suppression from aircraft equipped with the GTX 330/330D 
Mode S Transponders when the pulses are below the MTL. The inaccurate 
replies could result in reduced vertical separation or unsafe TCAS 
resolution advisories.
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  <guid>http://thefederalregister.com/d.p/2003-12-30-03-31978</guid>
  <pubDate>Tue, Dec 30 2003 11:00:00 GMT</pubDate>
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