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    <title>The Federal Register</title>
    <link>http://thefederalregister.com/b.p/agency/Federal_Aviation_Administration/2000-08-10/</link>
    <description>Daily Publications of Meetings and Rules Changes for the Federal Government</description>
    <pubDate>Fri, May 24 2013 11:00:00 GMT</pubDate>
    <lastBuildDate>Fri, May 24 2013 11:00:00 GMT</lastBuildDate>
    <webMaster>info@thefederalregister.com</webMaster>
    <item>
  <title><![CDATA[  Special Conditions: General Electric Aircraft Engines Model CT7- 6E and CT7-8 Turboshaft Engines]]></title>
  <link>http://thefederalregister.com/d.p/2000-08-10-00-20272</link>
  <description><![CDATA[ These special conditions are issued for General Electric 
Aircraft Engines (GEAE) models CT76E and CT78 turboshaft engines. 
These engines will have a novel or unusual rated 30minute power that 
makes the issue of these special conditions necessary. The existing 
airworthiness regulations do not contain adequate or appropriate safety 
standards for this design feature. These special conditions contain the 
additional safety standards the Administrator considers to establish a 
level of safety equivalent to that established by existing 
airworthiness standards. The rated 30minute power provides necessary 
increased rotorcraft hover time to enable operators to better perform 
critical, lifesaving search and rescue missions. For this reason and 
because a delay would not be in the public interest, the FAA has 
determined that good cause exists for adopting these special conditions 
immediately upon publication.
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  <guid>http://thefederalregister.com/d.p/2000-08-10-00-20272</guid>
  <pubDate>Thu, Aug 10 2000 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Modification of Class E airspace, Wenatchee, WA ]]></title>
  <link>http://thefederalregister.com/d.p/2000-08-10-00-20273</link>
  <description><![CDATA[ This action modifies the Wenatchee, WA, Class E airspace to 
remove the Fancher field airspace exclusion at the Panghorn Memorial 
Airport, Wenatchee, WA.
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  <guid>http://thefederalregister.com/d.p/2000-08-10-00-20273</guid>
  <pubDate>Thu, Aug 10 2000 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Revision of Class E airspace, Englewood, CO ]]></title>
  <link>http://thefederalregister.com/d.p/2000-08-10-00-20274</link>
  <description><![CDATA[ This action corrects a final rule published on May 25, 2000 
that inadvertently described the Class E airspace extension as E5. 
Additionally, in the legal description text, the word ``radius'' was 
inappropriately applied. This action corrects the final rule by 
reflecting the proper airspace designation and correction of text in 
the legal description.
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  <guid>http://thefederalregister.com/d.p/2000-08-10-00-20274</guid>
  <pubDate>Thu, Aug 10 2000 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Standard Instrument Approach Procedures; Miscellaneous Amendments]]></title>
  <link>http://thefederalregister.com/d.p/2000-08-10-00-20275</link>
  <description><![CDATA[ This amendment establishes, amends, suspends, or revokes 
Standard Instrument Approach Procedures (SIAPs) 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, addition of new obstacles, or changes in 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/2000-08-10-00-20275</guid>
  <pubDate>Thu, Aug 10 2000 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Standard Instrument Approach Procedures; Miscellaneous Amendments]]></title>
  <link>http://thefederalregister.com/d.p/2000-08-10-00-20276</link>
  <description><![CDATA[ This amendment establishes, amends, suspends, or revokes 
Standard Instrument Approach Procedures (SIAPs) for operations at 
certain airports. These regulatory actions are needed because of 
changes occurring in the National Airspace System, such as the 
commissioning of new navigational facilities, addition of new 
obstacles, or changes in 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/2000-08-10-00-20276</guid>
  <pubDate>Thu, Aug 10 2000 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Standard Instrument Approach Procedures; Miscellaneous Amendments]]></title>
  <link>http://thefederalregister.com/d.p/2000-08-10-00-20277</link>
  <description><![CDATA[ This amendment establishes, amends, suspends, or revokes 
Standard Instrument Approach Procedures (SIAP's) 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, addition of new obstacles, or changes in 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/2000-08-10-00-20277</guid>
  <pubDate>Thu, Aug 10 2000 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Boeing Model 747, 757, 767, and 777  Series Airplanes]]></title>
  <link>http://thefederalregister.com/d.p/2000-08-10-00-20243</link>
  <description><![CDATA[ This document proposes the adoption of a new airworthiness 
directive (AD) that is applicable to certain Boeing Model 747, 757, 
767, and 777 series airplanes. This proposal would require modification 
of certain drip shields located on the flight deck, and followon 
actions. This action is necessary to prevent potential ignition of the 
moisture barrier cover of the drip shield, which could propagate a 
small fire that results from an otherwise harmless electrical arc, 
leading to a larger fire. This action is intended to address the 
identified unsafe condition.
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  <guid>http://thefederalregister.com/d.p/2000-08-10-00-20243</guid>
  <pubDate>Thu, Aug 10 2000 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Boeing Model 737, 747, 757, and 767  Series Airplanes]]></title>
  <link>http://thefederalregister.com/d.p/2000-08-10-00-20244</link>
  <description><![CDATA[ This document proposes the adoption of a new airworthiness 
directive (AD) that is applicable to certain Boeing Model 737, 747, 
757, and 767 series airplanes. This proposal would require rework of 
certain duct assemblies of the environmental control system (ECS) or 
replacement of the duct assemblies with new or reworked duct 
assemblies. This action is necessary to prevent potential ignition of 
fiberglass insulation material installed on the outside of the ECS 
ducts, which could propagate a small fire and lead to a larger fire. 
This action is intended to address the identified unsafe condition.
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  <guid>http://thefederalregister.com/d.p/2000-08-10-00-20244</guid>
  <pubDate>Thu, Aug 10 2000 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Boeing Model 727 Series Airplanes]]></title>
  <link>http://thefederalregister.com/d.p/2000-08-10-00-20246</link>
  <description><![CDATA[ This document proposes the adoption of a new airworthiness 
directive (AD) that is applicable to all Boeing Model 727 series 
airplanes. This proposal would require repetitive inspections of the 
bearing support fitting of the forward trunnion on the main landing 
gear (MLG) to detect corrosion and cracking; followon actions, if 
necessary; and rework of the support fitting. This action is necessary 
to prevent failure of the support fitting, which could result in 
collapse of the MLG during normal operations; consequent damage to the 
airplane structure; and injury to flight crew, passengers, or ground 
personnel. This action is intended to address the identified unsafe 
condition.
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  <guid>http://thefederalregister.com/d.p/2000-08-10-00-20246</guid>
  <pubDate>Thu, Aug 10 2000 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Boeing Model 707 and 720 Series  Airplanes]]></title>
  <link>http://thefederalregister.com/d.p/2000-08-10-00-20247</link>
  <description><![CDATA[ This document proposes the adoption of a new airworthiness 
directive (AD) that is applicable to all Boeing Model 707 and 720 
series airplanes. This proposal would require repetitive inspections of 
certain stringers and around certain fastener holes of the lower skin 
of the wings to detect fatigue cracking, and repair, if necessary. This 
action is necessary to detect and correct such cracking and consequent 
damage to adjacent structure, which could result in reduced structural 
integrity of the airplane. This action is intended to address the 
identified unsafe condition.
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  <guid>http://thefederalregister.com/d.p/2000-08-10-00-20247</guid>
  <pubDate>Thu, Aug 10 2000 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Boeing Model 737 Series Airplanes]]></title>
  <link>http://thefederalregister.com/d.p/2000-08-10-00-20248</link>
  <description><![CDATA[ This document revises an earlier proposed airworthiness 
directive (AD), applicable to certain Boeing Model 737 series 
airplanes, that would have required inspections of certain bonded skin 
panels to detect delamination of the skin doublers (tear straps) from 
the skin panels; and followon corrective actions, if necessary. That 
proposal was prompted by reports that certain skin doublers were 
delaminated from their skin panels due to improper processing of 
certain skin panels. This new action would revise the proposed rule by 
referencing new service information that incorporates new inspection 
procedures and corrective actions, and recommends new compliance times. 
This new action also would remove airplanes from the applicability. The 
actions specified by this new proposed AD are intended to prevent skin 
doublers from delaminating from their skin panels, which could result 
in fatigue cracks in the skin doublers and skin panels, and consequent 
rapid decompression of the airplane.
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  <guid>http://thefederalregister.com/d.p/2000-08-10-00-20248</guid>
  <pubDate>Thu, Aug 10 2000 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; British Aerospace HP137 Mk1, Jetstream  Series 200, and Jetstream Models 3101 and 3201]]></title>
  <link>http://thefederalregister.com/d.p/2000-08-10-00-20250</link>
  <description><![CDATA[ This document proposes to adopt a new airworthiness directive 
(AD) that would apply to certain British Aerospace HP137 Mk1, Jetstream 
series 200, and Jetstream Models 3101 and 3201 airplanes. The proposed 
AD would require you to inspect the rudder quadrant support structure 
for cracks and correct Dwasher installation; and would require you to 
replace any cracked component and replace any incorrectly installed D
washers. The proposed AD is the result of mandatory continuing 
airworthiness information (MCAI) issued by the airworthiness authority 
for the United Kingdom. The actions specified by the proposed AD are 
intended to detect, correct, and prevent further cracking in the rudder 
quadrant structure caused by incorrectly installed Dwashers. Cracks in 
this structure could result in loss of rudder control with consequent 
airplane control problems.
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  <guid>http://thefederalregister.com/d.p/2000-08-10-00-20250</guid>
  <pubDate>Thu, Aug 10 2000 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; DG Flugzeugbau GmbH Model DG-800B  Sailplanes]]></title>
  <link>http://thefederalregister.com/d.p/2000-08-10-00-20251</link>
  <description><![CDATA[ This document proposes to adopt a new airworthiness directive 
(AD) that would apply to certain DG Flugzeugbau (DG Flugzeugbau) GmbH 
Model DG 800B sailplanes. The proposed AD would require you to measure 
and correct improper propeller drive belt tension. The proposed AD is 
the result of mandatory continuing airworthiness information (MCAI) 
issued by the airworthiness authority for the Federal Republic of 
Germany. The actions specified in the proposed AD are intended to 
correct improper drive belt tension and consequent engine crankshaft or 
connecting rod bearing damage. Such damage could result in loss of 
propulsion during critical phases of flight.
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  <guid>http://thefederalregister.com/d.p/2000-08-10-00-20251</guid>
  <pubDate>Thu, Aug 10 2000 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Eurocopter France Model SA330F, G, and  J Helicopters]]></title>
  <link>http://thefederalregister.com/d.p/2000-08-10-00-20249</link>
  <description><![CDATA[ This document proposes the supersedure of an existing 
airworthiness directive (AD) for Eurocopter France Model SA330F, G, and 
J helicopters. That AD requires inspecting the tail rotor blade (blade) 
skin for cracks and replacing, as necessary, the blade. This action 
would require skin bonding and eddy current inspections of the blade 
skin for cracks and would reference a more recent service bulletin 
(SB). This proposal is prompted by improved inspection methods and by 
the manufacturer revising the SB referenced in the current AD. The 
actions specified by the proposed AD are intended to prevent fatigue 
cracking of a blade, failure of a blade, and subsequent loss of control 
of the helicopter.
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  <guid>http://thefederalregister.com/d.p/2000-08-10-00-20249</guid>
  <pubDate>Thu, Aug 10 2000 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Raytheon (Beech) Model MU-300, MU-300- 10, 400, 400A, and 400T Series Airplanes]]></title>
  <link>http://thefederalregister.com/d.p/2000-08-10-00-20245</link>
  <description><![CDATA[ This document proposes the adoption of a new airworthiness 
directive (AD) that is applicable to certain Raytheon (Beech) Model MU
300, MU30010, 400, 400A, and 400T series airplanes. This proposal 
would require a onetime inspection to detect hydraulic fluid leakage 
from the Bnut area, which attaches a hydraulic tube to the antiskid 
valve assembly, and corrective actions, if necessary; and installation 
of an additional support for the hydraulic tube. This action is 
necessary to prevent an asymmetric braking condition and a longer 
stopping distance due to sudden loss of normal braking to the left 
wheel. Such loss of normal braking could result in the airplane 
overrunning the runway surface. This action is intended to address the 
identified unsafe condition.
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  <guid>http://thefederalregister.com/d.p/2000-08-10-00-20245</guid>
  <pubDate>Thu, Aug 10 2000 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Agency Information Collection Activity Under OMB Review ]]></title>
  <link>http://thefederalregister.com/d.p/2000-08-10-00-20280</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 (IRC) abstracted below has been forwarded to the 
Office of Management and Budget (OMB) for extension of currently 
approved collection. The ICR describes the nature of the information 
collection and the expected burden. The Federal Register Notice with a 
60day comment period soliciting comments on the following collection 
of information was published on May 9, 2000 [FR 65, pages 2687126872].
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  <pubDate>Thu, Aug 10 2000 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Receipt of Noise Compatibility Program and Request for Review;  Port Columbus International Airport, Columbus, Ohio]]></title>
  <link>http://thefederalregister.com/d.p/2000-08-10-00-20278</link>
  <description><![CDATA[ The Federal Aviation Administration (FAA) announces that it is 
reviewing a proposed noise compatibility program that was submitted for 
Port Columbus International Airport under the provisions of Title I of  the Aviation Safety and Noise Abatement Act of 1979<br/> [[Page 49054]]<br/>
(Pub. L. 96193) (hereinafter referred to as ``the Act'') and 14 CFR 
part 150 of the Columbus Municipal Airport Authority. This program was 
submitted subsequent to a determination by the FAA that associated 
noise exposure maps submitted under 14 CFR part 150 for Port Columbus 
International Airport were in compliance with applicable requirements 
effective January 3, 2000. The proposed noise compatibility program 
will be approved or disapproved on or before January 10, 2001.
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]]></description>
  <guid>http://thefederalregister.com/d.p/2000-08-10-00-20278</guid>
  <pubDate>Thu, Aug 10 2000 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Notice of Intent To Rule on Application (<strong>00</strong>-06-C-<strong>00</strong>-COS) To  Impose and Use the]]></title>
  <link>http://thefederalregister.com/d.p/2000-08-10-00-20279</link>
  <description><![CDATA[ The FAA proposes to rule and invites public comment on the 
application to impose and use PFC revenue at Colorado Springs Airport 
under the provisions of 49 U.S.C. 40117 and part 158 of the Federal 
Aviation Regulations (14 CFR part 158).
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]]></description>
  <guid>http://thefederalregister.com/d.p/2000-08-10-00-20279</guid>
  <pubDate>Thu, Aug 10 2000 11:00:00 GMT</pubDate>
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