I should add the caveat that I have no cables in my elevator controls.  
Strictly a push rod configuration.

-Jeff Scott
Los Alamos,NM


> Sent: Thursday, July 31, 2014 at 12:10 PM
> From: "cruzj12--- via KRnet" <krnet at list.krnet.org>
> To: peter <jordanruthseto at aol.com>, KRnet <krnet at list.krnet.org>
> Subject: Re: KR> counter balanced elevator
>
> ?Ok Jeff I'll close up my elevator horns with no weights added. I'm thinking? 
> as long as my elevator cables are tensioned properly,I should not worry about 
> flutter.Before tail mods?top speed?was around 145 indicated. I believe 
> everything you write here, except for your gages........do you think your 
> instruments need calibration?.....just kidding.......?
> 
> Joe Cruz
> cruzj12 at frontiernet.net
> KR1.5 N3151K
> KR2S builder 
> 
> 
> On Thursday, July 31, 2014 1:31 PM, peter via KRnet <krnet at list.krnet.org> 
> wrote:
>   
> 
> 
> 
> Jeff; small correction- 190 IAS is aerodynamically equal to 190 TAS @ 
> standard conditions. Your pitot reacts to the dynamic pressure of impacting 
> air molecules, independent of density altitude,? just like your flight 
> surfaces will, so flight testing to 215 IAS has been demonstrated without 
> flutter. Congrats. Peter
> 
> 
> 
> 
> I routinely descend from 12,500' to 7000' for landing with the ASI showing 
> 190 mph IAS, which is roughly 220 mph TAS at those altitudes. 
> 
> 
> 
> 
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