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From: marv@lancair.net
Subject: Re: [LML] Re: TSIO 550  LOP
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Date: Thu, 31 May 2007 13:41:06 -0400
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<div id="_htmlarea_default_style_" style="font:10pt arial,helvetica,sans-serif"> Posted for "Colyn Case on earthlink" &lt;colyncase@earthlink.net&gt;:<br><br> thanks Lynn for the very complete information.<br> That's a good data point.<br> Please let me know if you get data from a higher altitude flight - one theory <br>is that TIT's run higher at higher pressure differential.<br><br>""<br>Here are the figures from one of my flights a few months ago:<br> 17,570' Altitude (20,090 PA)<br> IAS - 195 KTS; TAS - 265 KTS<br> Induction air temp - 84 F<br> Manifold pressure - 29.5<br> RPF - 2490<br> Fuel flow - 18.9 GPH<br> TIT # 1 - 1620 F<br> TIT # 2 - 1576 F<br> <br>  EGT           CHT<br> 1. 1456       1. 334<br> 2. 1415       1. 335<br> 3. 1451       3. 310<br> 4. 1421       4. 301<br> 5. 1425       5. 316<br> 6. 1424       6. 315<br> """<br><br>  
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