<?xml version="1.0" encoding="UTF-8"?><rss version="2.0"
	xmlns:media="http://search.yahoo.com/mrss/"
	xmlns:content="http://purl.org/rss/1.0/modules/content/"
	xmlns:wfw="http://wellformedweb.org/CommentAPI/"
	xmlns:dc="http://purl.org/dc/elements/1.1/"
	xmlns:atom="http://www.w3.org/2005/Atom"
	xmlns:sy="http://purl.org/rss/1.0/modules/syndication/"
	xmlns:slash="http://purl.org/rss/1.0/modules/slash/"
	>

<channel>
	<title>EASA | George Hatcher's Air Flight Disaster</title>
	<atom:link href="https://airflightdisaster.com/tag/easa/feed/" rel="self" type="application/rss+xml" />
	<link>https://airflightdisaster.com</link>
	<description>Aviation News, Headlines &#38; Alerts</description>
	<lastBuildDate>Thu, 30 Jun 2011 17:31:30 +0000</lastBuildDate>
	<language>en-US</language>
	<sy:updatePeriod>
	hourly	</sy:updatePeriod>
	<sy:updateFrequency>
	1	</sy:updateFrequency>
	<generator>https://wordpress.org/?v=6.9.4</generator>
	<item>
		<title>A330 and A340 Landing Gear Airworthiness Directive</title>
		<link>https://airflightdisaster.com/a330-and-a340-landing-gear-airworthiness-directive/</link>
		
		<dc:creator><![CDATA[GJHatcher]]></dc:creator>
		<pubDate>Thu, 30 Jun 2011 17:31:30 +0000</pubDate>
				<category><![CDATA[Airbus]]></category>
		<category><![CDATA[EASA]]></category>
		<category><![CDATA[Landing Gear]]></category>
		<category><![CDATA[Official Report]]></category>
		<guid isPermaLink="false">http://airflightdisaster.com/?p=17562</guid>

					<description><![CDATA[<p>EASA Emergency AD No.: 2011-0122-E has been published limiting the life of A330 and A340 landing gear parts. During ground load test cycles on an A340-600 aeroplane, the MLG bogie beam prematurely fractured. The results of the investigation identified that this premature fracture was due to high tensile standing stress, resulting from dry fit axle...</p>
<p>The post <a href="https://airflightdisaster.com/a330-and-a340-landing-gear-airworthiness-directive/" data-wpel-link="internal" target="_self">A330 and A340 Landing Gear Airworthiness Directive</a> first appeared on <a href="https://airflightdisaster.com" data-wpel-link="internal" target="_self">George Hatcher's Air Flight Disaster</a>.</p>]]></description>
										<content:encoded><![CDATA[<p>EASA Emergency AD No.: 2011-0122-E  has been published limiting the life of A330 and A340 landing gear parts.</p>
<p>During ground load test cycles on an A340-600 aeroplane, the MLG bogie beam prematurely fractured.  The results of the investigation identified that this premature fracture was due to high tensile standing stress, resulting from dry fit axle assembly method. Improvement has been introduced subsequently with a grease fit axle assembly method.</p>
<p><a href="https://airflightdisaster.com/wp-content/uploads/2011/06/EASAAD20110122E.pdf" target="_blank" data-wpel-link="internal">Click to read the full pdf</a>  </p><p>The post <a href="https://airflightdisaster.com/a330-and-a340-landing-gear-airworthiness-directive/" data-wpel-link="internal" target="_self">A330 and A340 Landing Gear Airworthiness Directive</a> first appeared on <a href="https://airflightdisaster.com" data-wpel-link="internal" target="_self">George Hatcher's Air Flight Disaster</a>.</p>]]></content:encoded>
					
		
		
			</item>
	</channel>
</rss>
