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	<title>Comments on: Air France 447</title>
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	<link>http://deepseanews.com/2009/06/air-france-447/</link>
	<description>All the news on the Earth&#039;s largest environment.</description>
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		<title>By: Amy Wagner   Fishing</title>
		<link>http://deepseanews.com/2009/06/air-france-447/comment-page-1/#comment-8512</link>
		<dc:creator>Amy Wagner   Fishing</dc:creator>
		<pubDate>Thu, 15 Oct 2009 07:39:00 +0000</pubDate>
		<guid isPermaLink="false">http://deepseanews.com/?p=4737#comment-8512</guid>
		<description>I have just stumbled by this site, I am just loving it, its great and interesting.
This was such sad news, and my heart goes out to those that lost family and friends, its funny to hear how many planes have gone down this year and it makes one feel unsafe getting on to a plane these days and you would think that with all the technology that we have there shouldn&#039;t be some many crashes.</description>
		<content:encoded><![CDATA[<p>I have just stumbled by this site, I am just loving it, its great and interesting.<br />
This was such sad news, and my heart goes out to those that lost family and friends, its funny to hear how many planes have gone down this year and it makes one feel unsafe getting on to a plane these days and you would think that with all the technology that we have there shouldn&#8217;t be some many crashes.</p>
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		<title>By: Anton</title>
		<link>http://deepseanews.com/2009/06/air-france-447/comment-page-1/#comment-7162</link>
		<dc:creator>Anton</dc:creator>
		<pubDate>Tue, 09 Jun 2009 11:08:36 +0000</pubDate>
		<guid isPermaLink="false">http://deepseanews.com/?p=4737#comment-7162</guid>
		<description>From what I&#039;ve read about the stabilizer, it&#039;s quite large compared to similar planes, and when the pilot is adjusting the stabilizer, there is no change of resistance from a &quot;slight change&quot; to &quot;major change&quot; input by the pilot... so it is easy to inadvertantly apply more stress than the pilot expects.(Electronic-Fly by wire)

If more of the plane broke up in the air than just the stabilizer, then I would expect more &quot;larger&quot; pieces to be found... but just losing the stabilizer would be enough to lose control of the plane.</description>
		<content:encoded><![CDATA[<p>From what I&#8217;ve read about the stabilizer, it&#8217;s quite large compared to similar planes, and when the pilot is adjusting the stabilizer, there is no change of resistance from a &#8220;slight change&#8221; to &#8220;major change&#8221; input by the pilot&#8230; so it is easy to inadvertantly apply more stress than the pilot expects.(Electronic-Fly by wire)</p>
<p>If more of the plane broke up in the air than just the stabilizer, then I would expect more &#8220;larger&#8221; pieces to be found&#8230; but just losing the stabilizer would be enough to lose control of the plane.</p>
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		<title>By: H Burr</title>
		<link>http://deepseanews.com/2009/06/air-france-447/comment-page-1/#comment-7154</link>
		<dc:creator>H Burr</dc:creator>
		<pubDate>Tue, 09 Jun 2009 04:26:34 +0000</pubDate>
		<guid isPermaLink="false">http://deepseanews.com/?p=4737#comment-7154</guid>
		<description>Mr.LON has made some very incorrect statements.

The A300-600 series aircraft was that of American Airlines not US Air and speed is not necessary to create excessive G forces, remember, the aircraft had many discrepancy reports prior to crash and the crew training was unprofessional which helped create an unsafe situation. The Airbus aircraft are Transports not jet fighters and no place for jocks with heavy handed maneuvers.

Tail sections and fuselage body areas are made to separate at a certain G Force during a crash sequence to allow for better chance of survival of passengers. If at any time these G Forces are exceeded in flight same will occur regardless of the aircraft manufacturer. Aircraft regardless of size entering into extremely severe storms will and can end up in tragic circumstances as it appears has happened here, the wise thing to have done was circumnavigate the storm or turn around as point of no return had been reached. The maintenance telemetry can and should not be used as a method of figuring out what happened here, without the Flight Data Recorder and/or Cockpit Voice Recorder to compare sequence of events makes this cause of crash speculative at best. I do not have a close up picture of the hookup segments and pins to see if its in tact or sheared off and did notice that there is no rudder. Tail should be composite and should float.</description>
		<content:encoded><![CDATA[<p>Mr.LON has made some very incorrect statements.</p>
<p>The A300-600 series aircraft was that of American Airlines not US Air and speed is not necessary to create excessive G forces, remember, the aircraft had many discrepancy reports prior to crash and the crew training was unprofessional which helped create an unsafe situation. The Airbus aircraft are Transports not jet fighters and no place for jocks with heavy handed maneuvers.</p>
<p>Tail sections and fuselage body areas are made to separate at a certain G Force during a crash sequence to allow for better chance of survival of passengers. If at any time these G Forces are exceeded in flight same will occur regardless of the aircraft manufacturer. Aircraft regardless of size entering into extremely severe storms will and can end up in tragic circumstances as it appears has happened here, the wise thing to have done was circumnavigate the storm or turn around as point of no return had been reached. The maintenance telemetry can and should not be used as a method of figuring out what happened here, without the Flight Data Recorder and/or Cockpit Voice Recorder to compare sequence of events makes this cause of crash speculative at best. I do not have a close up picture of the hookup segments and pins to see if its in tact or sheared off and did notice that there is no rudder. Tail should be composite and should float.</p>
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		<title>By: Tak</title>
		<link>http://deepseanews.com/2009/06/air-france-447/comment-page-1/#comment-7151</link>
		<dc:creator>Tak</dc:creator>
		<pubDate>Tue, 09 Jun 2009 02:06:38 +0000</pubDate>
		<guid isPermaLink="false">http://deepseanews.com/?p=4737#comment-7151</guid>
		<description>To Lon: &quot;Air France’s Airbus 340 vertical stabilizer section has been found more or less intact. This is an indicator that it separated in flight and not on impact.&quot;

An Airbus A320-232 registered D-AXLA operated by XL Airways (Germany) crashed during a test flight on 27 November 2008 off the coast of Canet-Plage (66-France). She has a recorded speed of 263 knots when she impacted the sea in one single piece... and her vertical fin assembly was recovered almost intact floating amongst the debris. See:
http://aviation-safety.net/database/record.php?id=20081127-0
Vertical fin:
http://www.alptraum.us/tail.jpg

But also the same happened during the crash at sea of the Boeing 757-225 operated by Alas Nacionales (Flight ALW 301 departed Puerto Plata for a charter flight to Frankfurt) on 6 February 1996: the vertical fin assembly was also found almost intact.
See:
http://aviation-safety.net/database/record.php?id=19960206-0

On the other hand, the A300-605R of American Airlines has lost his rudder, then her vertical fin assembly, before crashing.
See:
http://aviation-safety.net/database/record.php?id=20011112-0

But this is not the case in the A330-203 crash of Air France which still have her rudder and her vertical stab. It seems to me that jumping to conclusion at this stage isn&#039;t very wise.

Olivier, Toulouse, France</description>
		<content:encoded><![CDATA[<p>To Lon: &#8220;Air France’s Airbus 340 vertical stabilizer section has been found more or less intact. This is an indicator that it separated in flight and not on impact.&#8221;</p>
<p>An Airbus A320-232 registered D-AXLA operated by XL Airways (Germany) crashed during a test flight on 27 November 2008 off the coast of Canet-Plage (66-France). She has a recorded speed of 263 knots when she impacted the sea in one single piece&#8230; and her vertical fin assembly was recovered almost intact floating amongst the debris. See:<br />
<a href="http://aviation-safety.net/database/record.php?id=20081127-0" rel="nofollow">http://aviation-safety.net/database/record.php?id=20081127-0</a><br />
Vertical fin:<br />
<a href="http://www.alptraum.us/tail.jpg" rel="nofollow">http://www.alptraum.us/tail.jpg</a></p>
<p>But also the same happened during the crash at sea of the Boeing 757-225 operated by Alas Nacionales (Flight ALW 301 departed Puerto Plata for a charter flight to Frankfurt) on 6 February 1996: the vertical fin assembly was also found almost intact.<br />
See:<br />
<a href="http://aviation-safety.net/database/record.php?id=19960206-0" rel="nofollow">http://aviation-safety.net/database/record.php?id=19960206-0</a></p>
<p>On the other hand, the A300-605R of American Airlines has lost his rudder, then her vertical fin assembly, before crashing.<br />
See:<br />
<a href="http://aviation-safety.net/database/record.php?id=20011112-0" rel="nofollow">http://aviation-safety.net/database/record.php?id=20011112-0</a></p>
<p>But this is not the case in the A330-203 crash of Air France which still have her rudder and her vertical stab. It seems to me that jumping to conclusion at this stage isn&#8217;t very wise.</p>
<p>Olivier, Toulouse, France</p>
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		<title>By: lon</title>
		<link>http://deepseanews.com/2009/06/air-france-447/comment-page-1/#comment-7146</link>
		<dc:creator>lon</dc:creator>
		<pubDate>Mon, 08 Jun 2009 23:41:53 +0000</pubDate>
		<guid isPermaLink="false">http://deepseanews.com/?p=4737#comment-7146</guid>
		<description>Air France’s Airbus 340 vertical stabilizer section has been found more or less intact.  This is an indicator that it separated in flight and not on impact.  It is interesting to note that the vertical stabilizer separated from an US Airways Airbus Industries A300-605R
on take-off  in 2001 at  JFK killing all aboard.  The cause was determined to be (in part) improper rudder input by the co-pilot while dealing with wake turbulence.  As a pilot, it’s seems inconceivable that a passenger aircraft whose vertical stabilizer could separate at the connection point in turbulence would be certified as safe.  Especially when one considers that in the JFK incident the Airbus was flying under 250 knots, more or less straight and level and the pilot’s only error was excessive rudder input.  

Lon Wilmington, NC</description>
		<content:encoded><![CDATA[<p>Air France’s Airbus 340 vertical stabilizer section has been found more or less intact.  This is an indicator that it separated in flight and not on impact.  It is interesting to note that the vertical stabilizer separated from an US Airways Airbus Industries A300-605R<br />
on take-off  in 2001 at  JFK killing all aboard.  The cause was determined to be (in part) improper rudder input by the co-pilot while dealing with wake turbulence.  As a pilot, it’s seems inconceivable that a passenger aircraft whose vertical stabilizer could separate at the connection point in turbulence would be certified as safe.  Especially when one considers that in the JFK incident the Airbus was flying under 250 knots, more or less straight and level and the pilot’s only error was excessive rudder input.  </p>
<p>Lon Wilmington, NC</p>
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