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    <title>The Federal Register</title>
    <link>http://thefederalregister.com/b.p/agency/Federal_Aviation_Administration/2004-02-18/</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[  Airworthiness Directives; Boeing Model 727, 727-100C, 727-200F,  and 727C Series Airplanes]]></title>
  <link>http://thefederalregister.com/d.p/2004-02-18-04-3130</link>
  <description><![CDATA[ This amendment adopts a new airworthiness directive (AD), 
applicable to certain Boeing Model 727, 727100C, 727200F, and 727C 
series airplanes, that requires repetitive openhole high frequency 
eddy current inspections for cracks in the fuselage skin, strap 
(bearstrap), and doubler at the forward and aft hinge fittings for the 
main deck cargo door, and repair of any cracks found. This action is 
necessary to detect and correct such cracks, which could reach critical 
crack length and result in rapid decompression of the airplane. This 
action is intended to address the identified unsafe condition.
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  <guid>http://thefederalregister.com/d.p/2004-02-18-04-3130</guid>
  <pubDate>Wed, Feb 18 2004 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Boeing Model 727, 727C, 727-100, and  727-100C Series Airplanes]]></title>
  <link>http://thefederalregister.com/d.p/2004-02-18-04-3131</link>
  <description><![CDATA[ This amendment adopts a new airworthiness directive (AD), 
applicable to all Boeing Model 727, 727C, 727100, and 727100C series 
airplanes, that requires repetitive detailed and special detailed 
inspections for cracks in the web, inner chord, and outer chord of the 
forward and aft frames of the aft cargo door opening; and repair of any 
crack found. This action is necessary to detect and correct such 
cracks, which could result in loss of the aft cargo door and rapid 
decompression of the airplane. This action is intended to address the 
identified unsafe condition.
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  <guid>http://thefederalregister.com/d.p/2004-02-18-04-3131</guid>
  <pubDate>Wed, Feb 18 2004 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Boeing Model 737-100, -200, -200C, - 300, -400, and -500 Series Airplanes]]></title>
  <link>http://thefederalregister.com/d.p/2004-02-18-04-3202</link>
  <description><![CDATA[ This amendment adopts a new airworthiness directive (AD), 
applicable to certain Boeing Model 737100, 200, 200C, 300, 400, 
and 500 series airplanes, that requires replacing existing screw, nut, 
and washers that attach the latch cable assembly to the latch block 
assembly of the door mounted escape slides, with new, improved screw, 
nut, and washers. This action is necessary to prevent the latch cable 
assembly from disconnecting from the latch block assembly of the door 
mounted escape slide, which could result in an escape slide not 
deploying in an emergency situation. This action is intended to address 
the identified unsafe condition.
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  <guid>http://thefederalregister.com/d.p/2004-02-18-04-3202</guid>
  <pubDate>Wed, Feb 18 2004 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Boeing Model 737-300, -400, and -500  Series Airplanes]]></title>
  <link>http://thefederalregister.com/d.p/2004-02-18-04-3348</link>
  <description><![CDATA[ This amendment supersedes an existing airworthiness directive 
(AD), applicable to certain Boeing Model 737 series airplanes, that 
currently requires a onetime general visual inspection of the seat 
locks and seat tracks of the flightcrew seats to ensure that the seats 
lock in position and to verify that lock nuts and bolts of adequate 
length are installed on the rear track lock bracket, and corrective 
action, if necessary. This amendment revises the applicability of the 
existing AD by adding airplanes. The actions specified by this AD are 
intended to prevent uncommanded movement of the flightcrew seats during 
acceleration and takeoff of the airplane, which could result in 
reduced controllability of the airplane. This action is intended to 
address the identified unsafe condition.
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  <guid>http://thefederalregister.com/d.p/2004-02-18-04-3348</guid>
  <pubDate>Wed, Feb 18 2004 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Dornier Model 328-100 Series Airplanes]]></title>
  <link>http://thefederalregister.com/d.p/2004-02-18-04-3204</link>
  <description><![CDATA[ This amendment adopts a new airworthiness directive (AD), 
applicable to certain Dornier Model 328100 series airplanes, that 
requires a onetime inspection of certain engine control cables to 
determine the batch number on the end fitting, and replacement of 
affected cables with new cables. This action is necessary to prevent 
failure of defective engine control cables, which could result in loss 
of the engine controls, and consequent reduced controllability of the 
airplane. This action is intended to address the identified unsafe 
condition.
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  <guid>http://thefederalregister.com/d.p/2004-02-18-04-3204</guid>
  <pubDate>Wed, Feb 18 2004 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Empresa Brasileira de Aeronautica S.A.  (EMBRAER) Model EMB-135 and -145 Series Airplanes]]></title>
  <link>http://thefederalregister.com/d.p/2004-02-18-04-3350</link>
  <description><![CDATA[ This document publishes in the Federal Register an amendment 
adopting airworthiness directive (AD) 20040251 that was sent 
previously to all known U.S. owners and operators of EMBRAER Model EMB
135 and 145 series airplanes by individual notices. This AD requires a 
onetime inspection of the aft rudder control rods to detect any 
discrepancy; a onetime inspection to determine if Access Panel 312AR 
is installed, and a revision to the Configuration Deviation List to 
remove any reference to Access Panel 312AR (thus prohibiting operation 
without that access panel installed); and further investigative and 
corrective actions, if necessary. The actions specified by this AD are 
intended to detect and correct failure of the control rods for the aft 
rudder, which could result in loss of control of the airplane. This 
action is intended to address the identified unsafe condition.
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  <guid>http://thefederalregister.com/d.p/2004-02-18-04-3350</guid>
  <pubDate>Wed, Feb 18 2004 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; The New Piper Aircraft, Inc. Model PA- 46-500TP Airplanes]]></title>
  <link>http://thefederalregister.com/d.p/2004-02-18-04-3050</link>
  <description><![CDATA[ The FAA adopts a new airworthiness directive (AD) for certain 
The New Piper Aircraft, Inc. (Piper) Model PA46500TP airplanes. This 
AD requires you to replace all electronic control modules in the 
airplane electrical system with newly designed modules. This AD is the 
result of smoke in the cockpit and loss of electrical systems function. 
We are issuing this AD to prevent short circuit failure and electrical 
arcing of the electronic control modules, which could result in loss of 
the electrical systems components or burning of wiring insulation and 
cause smoke in the cockpit. This condition could lead to the inability 
to properly control the airplane.
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  <guid>http://thefederalregister.com/d.p/2004-02-18-04-3050</guid>
  <pubDate>Wed, Feb 18 2004 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Pilatus Aircraft Ltd. Models PC-7, PC- 12, and PC-12/45 Airplanes]]></title>
  <link>http://thefederalregister.com/d.p/2004-02-18-04-3351</link>
  <description><![CDATA[ The FAA adopts a new airworthiness directive (AD) that 
supersedes AD 20020109, which applies to all Pilatus Aircraft Ltd. 
(Pilatus) Models PC7, PC12, and PC12/45 airplanes that incorporate a 
certain enginedriven pump. AD 20020109 currently requires you to 
inspect the joints between the enginedriven pump housing, the relief 
valve housing, and the relief valve cover for signs of fuel leakage and 
extruding gasket material; replace any enginedriven pump with any of 
the above problems; and ensure that the relief valve attachment screws  are adequately<br/> [[Page 7561]]<br/>
torqued and retorque as necessary. This AD is the result of mandatory 
continuing airworthiness information (MCAI) issued by the airworthiness 
authority for Switzerland. This AD retains the actions from AD 200201
09, adds certain enginedriven pumps to the applicability, and requires 
eventual replacement of the pump with an improved design pump to assure 
that the unsafe condition does not recur. We are issuing this AD to 
detect and correct ga<script type="text/javascript">
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  <guid>http://thefederalregister.com/d.p/2004-02-18-04-3351</guid>
  <pubDate>Wed, Feb 18 2004 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Raytheon Model Beech 400A and 400T  Series Airplanes]]></title>
  <link>http://thefederalregister.com/d.p/2004-02-18-04-3203</link>
  <description><![CDATA[ This amendment adopts a new airworthiness directive (AD), 
applicable to certain Raytheon Model Beech 400A and 400T series 
airplanes, that requires an inspection to determine the part number of 
the A194 roll trim printed circuit board (PCB), and replacement of 
certain PCBs with improved parts. This action is necessary to prevent 
intermittent sticking of the relays on the PCB in either the open or 
closed position, which could result in an outoftrim condition that 
could require using considerable control wheel force to keep the wings 
level, and consequent reduced controllability of the airplane. This 
action is intended to address the identified unsafe condition.
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  <guid>http://thefederalregister.com/d.p/2004-02-18-04-3203</guid>
  <pubDate>Wed, Feb 18 2004 11:00:00 GMT</pubDate>
</item>
<item>
  <title><![CDATA[  Airworthiness Directives; Saab Model SAAB 2000 Series Airplanes]]></title>
  <link>http://thefederalregister.com/d.p/2004-02-18-04-3349</link>
  <description><![CDATA[ This amendment adopts a new airworthiness directive (AD), 
applicable to certain Saab Model SAAB 2000 series airplanes, that 
requires replacing the dual shuttle valve in the number 2 hydraulic 
system with a new, improved valve. This action is necessary to prevent 
failure of the dual shuttle valve in the number 2 hydraulic system, [[Page 7564]]<br/>
with reduced maximum elevator rate on the left side, which could result  in pilotinduced pitch oscillation and consequent reduced <br/>
controllability of the airplane. This action is intended to address the 
identified unsafe condition.
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  <guid>http://thefederalregister.com/d.p/2004-02-18-04-3349</guid>
  <pubDate>Wed, Feb 18 2004 11:00:00 GMT</pubDate>
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