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     0. 12:11 AM - Contributions Down By 17%... (Matt Dralle)
     1. 02:03 AM - Re: GSC PROP PITCH (dave)
     2. 06:17 AM - Re: 1991 AOPA Kitfox article (mikeperkins)
 
 
 
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| Subject:  | Contributions Down By 17%... | 
      
      
      Dear Listers,
      
      As of today, Contributions to the Matronics List Fund Raiser are lagging behind
      last year at this time by roughly 17%.  I have a Fund Raiser each year simply
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| Subject:  | Re: GSC PROP PITCH | 
      
      
      
      carlisle wrote:
      > Your 618 is about 10hp more than my 582.  On the 582, when I reached about 12
      deg, it overloaded the engine and had very poor performance.  11-11.5 was my
      happy spot.
      > 
      > Chris Carlisle
      > Model 2, 582, C box 2.62
      > Sioux Falls, SD
      
      
      gear box ratio comes to play as well here. 3 to 1 will have more pitch that a 2.62
      box.  I would be curious to see how the 618 exhaust was made as it is totally
      different then the 582 exhaust. 
      
      582 Exhaust on Kitfox was chopped shorter and cost 5 to 7 HP.  But the 582s seem
      to last longer on the Kitfoxes.
      
      --------
      Rotax Dealer, Ontario Canada
      http://www.cfisher.com/
      http://www.kitfoxflyer.com/
      http://rotaxaircraft.com/forum/
      Realtime Kitfox movies to separate  the internet  chatter from the truth
      http://www.youtube.com/user/kitfoxflyer
      
      
      Read this topic online here:
      
      http://forums.matronics.com/viewtopic.php?p=320488#320488
      
      
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| Subject:  | Re: 1991 AOPA Kitfox article | 
      
      
      Thanks for attaching that article. I'd not seen it before. Mark Cook is such an
      excellent writer. 
      
      Often when I run into other Kitfox builders who claim superior performance of their
      later models, I tell them with a large grin that the purchase of my Model
      I helped finance the development of their improved aircraft. 
      
      Ahh, the Model I. If it weren't for the roll axis, the Model I would not be stable
      in any axis. It wallows in yaw like a Wright Flyer. And in pitch, when left
      to its own devices, goes into ever-increasing phugoids - in the words of Buzz
      Lightyear, to infinity and beyond. The fourth axis, thrust, isn't stable either,
      thanks to the torque-peaky 532, thus requiring constant attention to RPM
      with small changes in airspeed, which varies with small changes in pitch, which
      occurs with small amounts of turbulence. This thrust-airspeed-pitch coupling
      is a sight to behold, as is the yaw-roll coupling. 
      
      My aircraft is set up correctly. I built it 16 years ago to the plans with no modifications
      whatsoever. It's CG is correct, it's controls are properly rigged.
      This is just the way a Model I performs. 
      
      Yet in smooth air, it will fly five minutes straight without touching the controls.
      It's such a light touch that I fork the stick with two fingers and just nudge
      it around, much like the touch of flying a helicopter. In turbulent air,
      however, I can't unfold a map without finding myself in unusual attitudes and
      sometimes have to use fistfulls to keep it upright. But less stability means agility,
      and it is agile to be sure. And it has a demonstrated 20-kt crosswind
      capability, and I do mean demonstrated. 
      
      That STOL airfoil gets me into trouble with the guys at the airport, especially
      when I give Young Eagles rides - some pilots absolutely insist that I'm hot-dogging
      my take-offs because of the climb attitude when in fact all I'm doing is
      simply keeping Vy. 
      
      But my Model I has taught me some stick-and-rudder skills that can't be appreciated
      in something like a 152. And it's a family member, in need of improvement
      but still loved. 
      
      Mike Perkins
      
      
      Read this topic online here:
      
      http://forums.matronics.com/viewtopic.php?p=320509#320509
      
      
 
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