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    <title>The Federal Register</title>
    <link>http://thefederalregister.com/b.p/agency/Federal_Aviation_Administration/2002-01-07/</link>
    <description>Daily Publications of Meetings and Rules Changes for the Federal Government</description>
    <pubDate>Tue, Jun 18 2013 11:00:00 GMT</pubDate>
    <lastBuildDate>Tue, Jun 18 2013 11:00:00 GMT</lastBuildDate>
    <webMaster>info@thefederalregister.com</webMaster>
    <item>
  <title><![CDATA[  Criminal History Records Checks ]]></title>
  <link>http://thefederalregister.com/d.p/2002-01-07-02-358</link>
  <description><![CDATA[ On December 6, 2001, the FAA published a final rule with 
request for comments regarding criminal history records checks and 
invited comments. The comment period was originally scheduled to close 
on January 7, 2002; however, the FAA is extending the comment period an 
additional 10 days in response to a request from the Air Transport 
Association (ATA) and the Regional Airline Association (RAA).
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  <guid>http://thefederalregister.com/d.p/2002-01-07-02-358</guid>
  <pubDate>Mon, Jan 7 2002 11:00:00 GMT</pubDate>
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<item>
  <title><![CDATA[  Airworthiness Directives; Boeing Model 747-100, 747-200, 747-300,  and 747SR Series Airplanes Powered by General]]></title>
  <link>http://thefederalregister.com/d.p/2002-01-07-02-87</link>
  <description><![CDATA[ This amendment supersedes an existing airworthiness directive 
(AD), applicable to certain Boeing Model 747100, 747200, 747300, and 
747SR series airplanes powered by General Electric CF645/50 or Pratt & 
Whitney JT9D70 series engines, that currently requires a detailed 
visual inspection of the outboard diagonal brace for heat damage and 
cracking; and followon repetitive inspections and corrective actions, 
if necessary. This amendment requires accomplishment of the previously 
optional replacement of any existing sealant with heatresistant 
sealant as terminating action for the repetitive inspections required 
by this AD. This amendment is prompted by reports of heat damage to the 
forward end of the diagonal brace after accomplishment of a previous 
strut and wing modification. The actions specified by this AD are 
intended to prevent heat damage to the diagonal brace, which could 
cause cracking, fracture, and possible loss of the diagonal brace load 
path and consequent separation of the strut and engi<script type="text/javascript">
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  <guid>http://thefederalregister.com/d.p/2002-01-07-02-87</guid>
  <pubDate>Mon, Jan 7 2002 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Turbomeca S.A. Arrius 1A Turboshaft  Engines]]></title>
  <link>http://thefederalregister.com/d.p/2002-01-07-02-199</link>
  <description><![CDATA[ This amendment adopts a new airworthiness directive (AD) that 
is applicable to Turbomeca S.A. Arrius 1A turboshaft engines. This 
action requires replacement of the 10 main fuel injectors in Arrius 1A 
engines with new or overhauled injectors. This amendment is prompted by 
routine inspections conducted in the repair workshop demonstrating that 
some main fuel injectors were partially or totally blocked. The actions 
specified in this AD are intended to prevent blocked main fuel 
injectors that could lead to engine flameout during engine deceleration 
or that could prevent the engine from obtaining the 2\1/2\ minute one 
engine inoperative (OEI) power.
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  <guid>http://thefederalregister.com/d.p/2002-01-07-02-199</guid>
  <pubDate>Mon, Jan 7 2002 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Pratt & Whitney JT8D Series Turbofan  Engines]]></title>
  <link>http://thefederalregister.com/d.p/2002-01-07-02-303</link>
  <description><![CDATA[ This document proposes the supersedure of an existing 
airworthiness directive (AD), applicable to Pratt & Whitney JT8D series 
turbofan engines, that currently requires revisions to the Time Limits 
Section (TLS) of the manufacturer's Engine Manuals (EMs) to include 
required enhanced inspection of selected critical lifelimited parts at 
each piecepart exposure. This proposal would modify the airworthiness 
limitations section of the manufacturer's manual and an air carrier's 
approved continuous airworthiness maintenance program to incorporate 
additional inspection requirements. An FAA study of inservice events 
involving uncontained failures of critical rotating engine parts has 
indicated the need for mandatory inspections. The mandatory inspections 
are needed to identify those critical rotating parts with conditions, 
which if allowed to continue in service, could result in uncontained  failures.<br/> [[Page 698]]<br/>
The actions specified by this proposed AD are intended to prevent 
critical lifelimited rotat<script type="text/javascript">
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  <guid>http://thefederalregister.com/d.p/2002-01-07-02-303</guid>
  <pubDate>Mon, Jan 7 2002 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Pratt & Whitney JT8D-200 Series  Turbofan Engines]]></title>
  <link>http://thefederalregister.com/d.p/2002-01-07-02-304</link>
  <description><![CDATA[ This document proposes the supersedure of an existing 
airworthiness directive (AD), applicable to Pratt & Whitney JT8D200 
series turbofan engines, that currently requires revisions to the Time 
Limits Section (TLS) of the manufacturer's Engine Manuals (EMs) to 
include required enhanced inspection of selected critical lifelimited 
parts at each piecepart exposure. This proposal would modify the 
airworthiness limitations section of the manufacturer's manual and an 
air carrier's approved continuous airworthiness maintenance program to 
incorporate additional inspection requirements. An FAA study of in
service events involving uncontained failures of critical rotating 
engine parts has indicated the need for mandatory inspections. The 
mandatory inspections are needed to identify those critical rotating 
parts with conditions, which if allowed to continue in service, could 
result in uncontained failures. The actions specified by this proposed 
AD are intended to prevent critical lifelimited rotating engine<script type="text/javascript">
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  <guid>http://thefederalregister.com/d.p/2002-01-07-02-304</guid>
  <pubDate>Mon, Jan 7 2002 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Proposed Modification of Class D Airspace; Rockford, IL;  Modification of Class E Airspace; Rockford, IL]]></title>
  <link>http://thefederalregister.com/d.p/2002-01-07-02-249</link>
  <description><![CDATA[ This action proposes to modify Class D airspace at Rockford, 
IL, and modify Class E airspace at Rockford, IL. An Area Navigation 
(RNAV) Standard Instrument Approach Procedure (SIAP) to Runway (Rwy) 
01, RNAV SIAP to Rwy 7, RNAV (Y) SIAP to Rwy 19, RNAV(Z) SIAP to Rwy 
19, RNAV(Y) SIAP to Rwy 25, RNAV(Z) SIAP to Rwy 25 have been developed 
for the Greater Rockford Airport. Controlled airspace extending upward 
from the surface of the earth is needed to contain aircraft executing 
these approaches. This action would increase the radius of the existing 
Class D and Class E airspace for Greater Rockford Airport.
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  <guid>http://thefederalregister.com/d.p/2002-01-07-02-249</guid>
  <pubDate>Mon, Jan 7 2002 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Proposed Modification of Class D Airspace; Bloomington, Monroe  County Airport, IN; and Modification of Class E]]></title>
  <link>http://thefederalregister.com/d.p/2002-01-07-02-252</link>
  <description><![CDATA[ This action proposes to modify Class D airspace at 
Bloomington, Monroe County Airport, IN, and modify Class E airspace at 
Bloomington, Monroe County Airport, IN. An Area Navigation (RNAV) 
Standard Instrument Approach Procedure (SIAP) to Runway (Rwy) 06, RNAV 
SIAP to Rwy 17, RNAV SIAP to Rwy 24, and a RNAV SIAP to Rwy 35 have 
been developed for Monroe County Airport. Controlled airspace extending 
upward from the surface of the earth is needed to contain aircraft 
executing these approaches. This action would increase the radius of 
the existing Class D and Class E airspace for Monroe County Airport.
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  <guid>http://thefederalregister.com/d.p/2002-01-07-02-252</guid>
  <pubDate>Mon, Jan 7 2002 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Proposed Modification of Class E Airspace; Greenville, MI ]]></title>
  <link>http://thefederalregister.com/d.p/2002-01-07-02-248</link>
  <description><![CDATA[ This action proposes to modify Class E airspace at Greenville, 
MI. An Area Navigation (RNAV) Standard Instrument Approach Procedure 
(SIAP) to Runway (Rwy) 10, and an RNAV SIAP Rwy 28 has been developed 
for Greenville Municipal Airport. Controlled airspace extending upward 
from 700 feet or more above the surface of the earth is needed to 
contain aircraft executing this approach. This action would increase 
the radius of the existing controlled airspace for Greenville Municipal 
Airport.
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  <guid>http://thefederalregister.com/d.p/2002-01-07-02-248</guid>
  <pubDate>Mon, Jan 7 2002 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Proposed Modification of Class E Airspace; Frankfort, MI ]]></title>
  <link>http://thefederalregister.com/d.p/2002-01-07-02-250</link>
  <description><![CDATA[ This action proposes to modify Class E airspace Frankfort, MI. 
A VHF Omnidirectional RangeA (VORA) Standard Instrument Approach 
Procedure (SIAP) has been developed for Frankfort Dow Memorial Field, 
Frankfort, MI. Controlled airspace extending upward from 700 feet above 
the surface of the earth is needed to contain aircraft executing this 
approach. This action would add an extension to the existing Class E 
airspace for Frankfort Dow Memorial Field Airport.
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  <guid>http://thefederalregister.com/d.p/2002-01-07-02-250</guid>
  <pubDate>Mon, Jan 7 2002 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Proposed Modification of Class E Airspace; Manistee, MI ]]></title>
  <link>http://thefederalregister.com/d.p/2002-01-07-02-251</link>
  <description><![CDATA[ This action proposes to modify Class E airspace at Manistee, 
MI. A VHF Omnidirectional (VOR) Standard Instrument Approach Procedure 
(SIAP) Runway (Rwy) 09, and VOR SIAP Rwy 27 have been developed for 
Manistee CountyBlacker Airport. Controlled airspace extending upward 
from 700 feet above the surface of the earth is needed to contain 
aircraft executing this approach. This action would change the 
extensions to the existing Class E airspace for Manistee CountyBlacker 
Airport.
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  <guid>http://thefederalregister.com/d.p/2002-01-07-02-251</guid>
  <pubDate>Mon, Jan 7 2002 11:00:00 GMT</pubDate>
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