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	<title>Comments on: Disc loading</title>
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	<link>http://blog.aopa.org/helicopter/?p=315</link>
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		<title>By: Sean C</title>
		<link>http://blog.aopa.org/helicopter/?p=315#comment-1180</link>
		<dc:creator>Sean C</dc:creator>
		<pubDate>Sun, 26 Sep 2010 21:59:54 +0000</pubDate>
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		<description><![CDATA[It seems axiomatic that all of the larger multi-engined helicopters will have a higher disc loading than their smaller and medium sized counterparts. To keep a similar ratio, their overall rotor blade diameter becomes impractically large, and operations outside the airport environment becomes problematical. The higher decent rates in autorotation are VERY noticable, the UH-60 for example comes down like a lead brick compared to the older UH-1.]]></description>
		<content:encoded><![CDATA[<p>It seems axiomatic that all of the larger multi-engined helicopters will have a higher disc loading than their smaller and medium sized counterparts. To keep a similar ratio, their overall rotor blade diameter becomes impractically large, and operations outside the airport environment becomes problematical. The higher decent rates in autorotation are VERY noticable, the UH-60 for example comes down like a lead brick compared to the older UH-1.</p>
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		<title>By: Brendan Fitzpatrick</title>
		<link>http://blog.aopa.org/helicopter/?p=315#comment-1036</link>
		<dc:creator>Brendan Fitzpatrick</dc:creator>
		<pubDate>Sat, 15 May 2010 23:46:13 +0000</pubDate>
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		<description><![CDATA[Good refresher - got to stand under a CH53-E - like being in a hurricane even when still 20 feet in the air.]]></description>
		<content:encoded><![CDATA[<p>Good refresher &#8211; got to stand under a CH53-E &#8211; like being in a hurricane even when still 20 feet in the air.</p>
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