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		mtherr(at)yahoo.com Guest
 
 
 
 
 
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				 Posted: Mon Apr 17, 2006 6:55 pm    Post subject: Murphy's law did not apply | 
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				Hello group! 
 
 Well, this evening, I've been lucky with some bad luck
 (or more precisely, bad design).
 
 After dinner, I decided to go flying at sunset.  I
 departed CSB3 at 19h30EAT and went to Mascouche
 (CSK3).  Then, I took position to depart from runway
 11.  Several seconds after applying full throttle, the
 engine came back to idle and the throttle lever was
 non effective.  The plane started to decelerate on the
 runway.
 
 I parked it at the end of the runway, removed the
 cowling and quickly noticed that my throttle lever was
 disassembled.  When I modified the carburetor, I cut
 down the throttle lever and made a plate what would
 accomodate the throttle push rod I'm using.  This
 plate is (or was) attached to the Carburetor throttle
 arm with two A5 Avex rivets.  
 
 The plane flew more than 200 hours before the rivets
 failed ant the plate detached from the throttle arm!
 
 Should Murphy have made this happen 10 seconds later,
 I,would have been in deep s..t (there are no good
 options for emergency landings during a moment after
 take off on that runway).  But the law did not apply
 and I simply had a good workout pulling the plane to a
 hangar I have access to (which was near the other end
 of the runway).
 
 Here are some pictures showing that plate:
 
 http://mthobby.pcperfect.com/ch601/images/DCP02135.JPG
 http://mthobby.pcperfect.com/ch601/images/DCP02158.JPG
 
 This being said, I would suggest looking at any
 situation where a couple of rivets hold a critical
 part that is subject to constant stress and vibration.
  These two rivets will be replaced with two AN3 bolts
 and lock nuts in the next few days!
 
 Michel  
 ----------------------------
 Michel Therrien CH601-HD, C-GZGQ
   http://mthobby.pcperfect.com/ch601
   http://www.zenithair.com/bldrlist/profiles/mthobby
   http://pages.infinit.net/mthobby
 
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		JohnDRead(at)aol.com Guest
 
 
 
 
 
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				 Posted: Mon Apr 17, 2006 7:15 pm    Post subject: Murphy's law did not apply | 
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				Hi Michel:
                 Were  the rivets steel or aluminum?
  
 John (soon to start building a CH710)
 
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		JohnDRead(at)AOL.COM Guest
 
 
 
 
 
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				 Posted: Mon Apr 17, 2006 7:20 pm    Post subject: Murphy's law did not apply | 
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				Hi Michel:
                 I  took look at your pictures. Why did you not weld the 
 modified bracket as opposed  to rivets?
  
 John
 
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		nfivesl(at)yahoo.com Guest
 
 
 
 
 
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				 Posted: Mon Apr 17, 2006 7:27 pm    Post subject: Murphy's law did not apply | 
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				Michel that is very timely news!  A few days ago I
 made a similar installation on my throttle where I
 installed two rivets - then, the day after I installed
 it, I drilled them out and installed AN3 bolts because
 it didn't feel right after sleeping on it!  
 
 It's good to hear you got a break on that one!
 
 Scott Laughlin
 
 --- Michel Therrien <mtherr(at)yahoo.com> wrote:
 
  	  | Quote: | 	 		   
  <mtherr(at)yahoo.com>
  
  Hello group! 
  
  Well, this evening, I've been lucky with some bad
  luck
  (or more precisely, bad design).
 
 | 	 
 
 
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		mtherr(at)yahoo.com Guest
 
 
 
 
 
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				 Posted: Tue Apr 18, 2006 2:19 am    Post subject: Murphy's law did not apply | 
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				The plate is made of 6061-t6, 0.063".  It would sure
 be a better idea to weld a 4130 plate, but at that
 time, I had no steel and no talent for welding. 
 
 I looked at my plate yesterday, no distorsion on it,
 no cracks and the hole for the pushrod is still very
 much round... I'll put it back in.
 
 do not archive.
 
 --- JohnDRead(at)aol.com wrote:
 
 
 
 ----------------------------
 Michel Therrien CH601-HD, C-GZGQ
   http://mthobby.pcperfect.com/ch601
   http://www.zenithair.com/bldrlist/profiles/mthobby
   http://pages.infinit.net/mthobby
 
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		mtherr(at)yahoo.com Guest
 
 
 
 
 
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				 Posted: Tue Apr 18, 2006 2:19 am    Post subject: Murphy's law did not apply | 
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				The rivets were the A5 Avex rivets that we use to
 build the plane....  I know one of my friend has a
 similar setup, but with AD rivets (solid rivets) and
 he has not have that situation. (yet?) Seriously, I
 don't think our soft pull rivets measure up with AD
 solid rivets in term of resistance to fatigue and
 strenght.
 
 Michel
 do not archive
 
 --- JohnDRead(at)aol.com wrote:
 
 
 
 ----------------------------
 Michel Therrien CH601-HD, C-GZGQ
   http://mthobby.pcperfect.com/ch601
   http://www.zenithair.com/bldrlist/profiles/mthobby
   http://pages.infinit.net/mthobby
 
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		bill_dom(at)yahoo.com Guest
 
 
 
 
 
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				 Posted: Tue Apr 18, 2006 4:33 am    Post subject: Murphy's law did not apply | 
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				I read or saw somewhere that throttle linkage need to
 be installed in such way that in case of failure, the
 spring should open the throttle to full position
 instead of closing it. Then you will use mixture
 control to reduce power and when in final for landing,
 you can turn off the engine and glide to the runnway.
 I thought this was common practice. Is there a reason
 why not to do this?
 
 William Dominguez
 Plansbuilt Zodiac 601XL
 
 --- Michel Therrien <mtherr(at)yahoo.com> wrote:
 
  	  | Quote: | 	 		   
  <mtherr(at)yahoo.com>
  
  Hello group! 
  
  Well, this evening, I've been lucky with some bad
  luck
  (or more precisely, bad design).
  
  After dinner, I decided to go flying at sunset.  I
  departed CSB3 at 19h30EAT and went to Mascouche
  (CSK3).  Then, I took position to depart from runway
  11.  Several seconds after applying full throttle,
  the
  engine came back to idle and the throttle lever was
  non effective.  The plane started to decelerate on
  the
  runway.
  
  I parked it at the end of the runway, removed the
  cowling and quickly noticed that my throttle lever
  was
  disassembled.  When I modified the carburetor, I cut
  down the throttle lever and made a plate what would
  accomodate the throttle push rod I'm using.  This
  plate is (or was) attached to the Carburetor
  throttle
  arm with two A5 Avex rivets.  
  
  The plane flew more than 200 hours before the rivets
  failed ant the plate detached from the throttle arm!
  
  Should Murphy have made this happen 10 seconds
  later,
  I,would have been in deep s..t (there are no good
  options for emergency landings during a moment after
  take off on that runway).  But the law did not apply
  and I simply had a good workout pulling the plane to
  a
  hangar I have access to (which was near the other
  end
  of the runway).
  
  Here are some pictures showing that plate:
  
 
 http://mthobby.pcperfect.com/ch601/images/DCP02135.JPG
 | 	  
 
 
 
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		mtherr(at)yahoo.com Guest
 
 
 
 
 
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				 Posted: Tue Apr 18, 2006 7:47 am    Post subject: Murphy's law did not apply | 
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				I had the same thought yesterday... I heard that Rotax
 engines are designed this way (full throttle in case
 of throttle failure).  I'll be looking at how to
 implement something similar on my installation.
 
 Michel
 PS: But all of this is temporary    More on that
 very soon!
 --- William Dominguez <bill_dom(at)yahoo.com> wrote:
 
  	  | Quote: | 	 		   
  <bill_dom(at)yahoo.com>
  
  I read or saw somewhere that throttle linkage need
  to
  be installed in such way that in case of failure,
  the
  spring should open the throttle to full position
  instead of closing it. Then you will use mixture
  control to reduce power and when in final for
  landing,
  you can turn off the engine and glide to the
  runnway.
  I thought this was common practice. Is there a
  reason
  why not to do this?
  
  
  
  William Dominguez
  Plansbuilt Zodiac 601XL
  
  
 
 | 	  
 ----------------------------
 Michel Therrien CH601-HD, C-GZGQ
   http://mthobby.pcperfect.com/ch601
   http://www.zenithair.com/bldrlist/profiles/mthobby
   http://pages.infinit.net/mthobby
 
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