  | 
				Matronics Email Lists Web Forum Interface to the Matronics Email Lists   
				 | 
			 
		 
		 
	
		| View previous topic :: View next topic   | 
	 
	
	
		| Author | 
		Message | 
	 
	
		jdbutterfield(at)yahoo.co Guest
 
 
 
 
 
  | 
		
			
				 Posted: Thu Oct 30, 2008 5:48 am    Post subject: how to make the wings stronger? | 
				     | 
			 
			
				
  | 
			 
			
				Hi List
 
 I actually tend to believe that most of the wing accidents were caused by pilot error/judgment.  However, not being an engineer, am wondering how one would go about making the wings stronger.  There must be a way we could modify the wing/attaching points or whatever to add a lot of strength to the wing assembly.  I have no idea or experience on how this could be done, but i am sure there are plenty of people on this list that could figure out a way.  It may be lighter and cheaper that getting a parachute system. Even a parachute won't help if a wing falls off at low altitude.  I certainly would give up a few (lot) pounds to not to ever have to worry about wing departure.
 john
 XL, corvair
 Torrance, CA
 
  |  | - The Matronics Zenith601-List Email Forum - |  |   |  Use the List Feature Navigator to browse the many List utilities available such as the Email Subscriptions page, Archive Search & Download, 7-Day Browse, Chat, FAQ, Photoshare, and much more:
 
  http://www.matronics.com/Navigator?Zenith601-List |  
  |  
 
 
 
  
 | 
			 
		  | 
	 
	
		| Back to top | 
		 | 
	 
	
		  | 
	 
	
		countzero
 
 
  Joined: 25 Oct 2007 Posts: 25
 
  | 
		
			
				 Posted: Thu Oct 30, 2008 6:03 am    Post subject: Re: how to make the wings stronger? | 
				     | 
			 
			
				
  | 
			 
			
				Hello John,
 
 You could reduce the loading on the wings by lowering your gross weight. This is not the same as improving the structure pound for pound but is far simpler for you to do.
 
 Rob
 
  |  | - The Matronics Zenith601-List Email Forum - |  |   |  Use the List Feature Navigator to browse the many List utilities available such as the Email Subscriptions page, Archive Search & Download, 7-Day Browse, Chat, FAQ, Photoshare, and much more:
 
  http://www.matronics.com/Navigator?Zenith601-List |  
  |  
 
 
 
  
 | 
			 
		  | 
	 
	
		| Back to top | 
		 | 
	 
	
		  | 
	 
	
		jaybannist(at)cs.com Guest
 
 
 
 
 
  | 
		
			
				 Posted: Thu Oct 30, 2008 6:16 am    Post subject: how to make the wings stronger? | 
				     | 
			 
			
				
  | 
			 
			
				John,
  
  This is not intended as a "flaming" response.  I just want share my thoughts on structural modifications.
  
  An aircraft structure is one of the most interdependent structural systems there is.  You can't just "beef up" one part without knowing how that effects stresses on adjacent parts and parts adjacent to those.  A building designer wouldn't dream of adding a floor to a high-rise building without checking all the existing columns, beams and foundations to see if they could take the additional weight and moments. In order to do that, he would have to have access to, and understand all the structural calculations. The same applies to an airplane.  I would not trust ANY structural modification unless I knew, without a doubt, that all the structural design calculations had been checked and that they would allow such a modification. An airplane structure is just not a good thing to "tinker" with.
  
  Jay in Dallas
  Do not archive
  
    
  
  --
 
  |  | - The Matronics Zenith601-List Email Forum - |  |   |  Use the List Feature Navigator to browse the many List utilities available such as the Email Subscriptions page, Archive Search & Download, 7-Day Browse, Chat, FAQ, Photoshare, and much more:
 
  http://www.matronics.com/Navigator?Zenith601-List |  
  |  
 
 
 
  
 | 
			 
		  | 
	 
	
		| Back to top | 
		 | 
	 
	
		  | 
	 
	
		zodierocket(at)hsfx.ca Guest
 
 
 
 
 
  | 
		
			
				 Posted: Thu Oct 30, 2008 6:37 am    Post subject: how to make the wings stronger? | 
				     | 
			 
			
				
  | 
			 
			
				When we look at the incidents, some are looked upon as pilot error, a
 thunderstorm comes to mind. But also keep in mind that mechanical errors
 can also creep in (missing bolts and cable tension are foremost in my
 thoughts). There are many flying 601XL's and quite a few have amazing
 hours accumulated. Zenair has time and time again tested the design for
 many countries standards as well as use a 3rd party to test the
 structure. 
 
 One thing I have seen in looking at some planes is that the cables are
 not to spec in tension. These may have been set properly prior to first
 flight but not stretched, which would allow slacking. We also tend not
 to own a tension meter of which I would recommend having. 
 
 We have read letters from Chris on Zenith's website and AMD's as well as
 a letter in the Zenair Newsletter about the importance of cable tension.
 Attached is a letter issued from Zenair Europe as an AD. In America we
 can only see an AD from the FAA so if we look on Zeniths website we see
 a Zenair Safety Alert at
 http://www.zenithair.com/zodiac/xl/data/ad-ze-2008-01.pdf
 
 Read this and take it to action. IF you have been flying your plane
 check it before next flight with a proper gauge. IF you're building
 remember to pre-stretch your cables and check often during initial
 flights and in a set interval during the life of the plane. 
 
 Entertaining an idea of changing a design that bears up in mathematical
 and physical structural testing seems fool hardy and ill advised.
 Ensuring that your plane is to standards as set forth by designer and
 AC43-13b would be far more prudent and well in the reach of each
 builder.
 
 My Thoughts. 
 Mark Townsend  Alma, Ontario
 Zodiac CH650 C-GOXL, CH701 Rotax 912,
 STOL CH750 Just started
 www.ch601.org / www.ch701.com
 
  |  | - The Matronics Zenith601-List Email Forum - |  |   |  Use the List Feature Navigator to browse the many List utilities available such as the Email Subscriptions page, Archive Search & Download, 7-Day Browse, Chat, FAQ, Photoshare, and much more:
 
  http://www.matronics.com/Navigator?Zenith601-List |  
  |  
 
 
 
  
	
  
	 
	
	
		
	 
	
		|  Description: | 
		
			
		 | 
		  Download | 
	 
	
		|  Filename: | 
		 AD#_ZE-2008-01.pdf | 
	 
	
		|  Filesize: | 
		 21.22 KB | 
	 
	
		|  Downloaded: | 
		 593 Time(s) | 
	 
	 
	 
 | 
			 
		  | 
	 
	
		| Back to top | 
		 | 
	 
	
		  | 
	 
	
		K Dilks
 
 
  Joined: 22 Sep 2008 Posts: 108 Location: UK
  | 
		
			
				 Posted: Thu Oct 30, 2008 6:44 am    Post subject: Re: how to make the wings stronger? | 
				     | 
			 
			
				
  | 
			 
			
				The euro plane empty weight is quoted as 265 KG
  most empty zodiacs come in at 320 to 340kg
  So besides the undercarrige where else can they save  that much weight.
  I have looked hard to day around the net but I am sure they are using ,16 skins. Maybe not on CZAW planes but on the ones from Dynaero in Portugal..    
   Not also the the data for loading . 6g is the ultimate  so operational is 4g . I wonder if guys are pulling 6 thinking there safe.
  The lower figure of 4 is somtimes give and is on the plans.Check ZAC web site.
  All in all with so many versions and makers / suppliers this is quite a mess to work out.
 
  |  | - The Matronics Zenith601-List Email Forum - |  |   |  Use the List Feature Navigator to browse the many List utilities available such as the Email Subscriptions page, Archive Search & Download, 7-Day Browse, Chat, FAQ, Photoshare, and much more:
 
  http://www.matronics.com/Navigator?Zenith601-List |  
  |  
 
 
 
  
 _________________ Back home ................. | 
			 
		  | 
	 
	
		| Back to top | 
		 | 
	 
	
		  | 
	 
	
		z601(at)anemicaardvark.co Guest
 
 
 
 
 
  | 
		
			
				 Posted: Thu Oct 30, 2008 8:16 am    Post subject: how to make the wings stronger? | 
				     | 
			 
			
				
  | 
			 
			
				On Thursday 30 October 2008 08:48, john butterfield wrote:
 
  	  | Quote: | 	 		   I actually tend to believe that most of the wing accidents were caused by
  pilot error/judgment.  However, not being an engineer, am wondering how one
  would go about making the wings stronger.  There must be a way we could
  modify the wing/attaching points or whatever to add a lot of strength to
  the wing assembly.  
 
 | 	  
  <snip> 
 
 First, let me say I agree with the caution that one cannot change one part of 
 a structure without considering the impact on the rest of the structure. We 
 can't afford to make structural changes to the design, without a lot more 
 information than is available. 
 
 Having said that, it has appeared to me (since I first looked at the design) 
 that the 6 AN5 bolts which connect the wing spar to the carry-through spar 
 are pretty small and few in number to the task. There isn't that much overlap 
 between the wing spar and the carry-through spar to transfer the wing loading 
 to the rest of the structure.
 
 The commercial designs with which I'm most familiar had more and larger bolts, 
 and in some cases, close-tolerance bolts. There is, as I recall, much more 
 overlap between the spars to allow for reasonable spacing between the extra 
 bolts.
 
 Is this the problem? Only the results of the various accident reports will 
 tell. But it could sure cause wing separation, if it is. 
 ==============================================
 Those who can, do. Those who can't, sue.
 =================================================
                Jim B. Belcher
     BS, MS Physics, math, Computer Science
                   A&P/IA
            Instrument Rated Pilot
      General Radio Telephone Certificate
 =================================================
 
  |  | - The Matronics Zenith601-List Email Forum - |  |   |  Use the List Feature Navigator to browse the many List utilities available such as the Email Subscriptions page, Archive Search & Download, 7-Day Browse, Chat, FAQ, Photoshare, and much more:
 
  http://www.matronics.com/Navigator?Zenith601-List |  
  |  
 
 
 
  
 | 
			 
		  | 
	 
	
		| Back to top | 
		 | 
	 
	
		  | 
	 
	
		Martin Pohl
 
  
  Joined: 30 Jan 2006 Posts: 118 Location: CH-8645 Jona SG, Switzerland
  | 
		
			
				 Posted: Thu Oct 30, 2008 8:17 am    Post subject: Re: how to make the wings stronger? | 
				     | 
			 
			
				
  | 
			 
			
				The average empty weight for CZAW CH601XLs seems to be around 310 - 320 kg. The new European version might be different.
 
 I checked my kit and I can assure that (on my CZAW 601XL) the wing sheet thickness is 0.025".
 
 Cheers Martin[/quote]
 
  |  | - The Matronics Zenith601-List Email Forum - |  |   |  Use the List Feature Navigator to browse the many List utilities available such as the Email Subscriptions page, Archive Search & Download, 7-Day Browse, Chat, FAQ, Photoshare, and much more:
 
  http://www.matronics.com/Navigator?Zenith601-List |  
  |  
 
 
 
  
 _________________ Martin Pohl
 
Zodiac XL QBK
 
8645 Jona, Switzerland
 
http://www.pohltec.ch/ZodiacXL/Main.html | 
			 
		  | 
	 
	
		| Back to top | 
		 | 
	 
	
		  | 
	 
	
		Joemotis(at)aol.com Guest
 
 
 
 
 
  | 
		
			
				 Posted: Thu Oct 30, 2008 4:46 pm    Post subject: how to make the wings stronger? | 
				     | 
			 
			
				
  | 
			 
			
				Maybe we should learn from this pilot!
   
  http://www.youtube.com/watch?v=XRCbkBfdBrQ&eurl=http://www.chilloutzone.de/files/08102703.html
   
  This is incredible. 
   
  Joe Motis
  Do not archive
   In a message dated 10/30/2008 9:17:07 A.M. Pacific Daylight Time,  z601(at)anemicaardvark.com writes:
   	  | Quote: | 	 		  -->    Zenith601-List message posted by: Jim Belcher    <z601(at)anemicaardvark.com>
 
 On Thursday 30 October 2008 08:48, john    butterfield wrote:
 
  	  | Quote: | 	 		   I actually tend to believe that most of the    wing accidents were caused by
  pilot error/judgment.  However, not    being an engineer, am wondering how one
  would go about making the    wings stronger.  There must be a way we could
  modify the    wing/attaching points or whatever to add a lot of strength to
  the wing    assembly.  
 
 | 	  
 <snip> 
 
 First, let me say I agree with    the caution that one cannot change one part of 
 a structure without    considering the impact on the rest of the structure. We 
 can't afford to    make structural changes to the design, without a lot more 
 information than    is available. 
 
 Having said that, it has appeared to me (since I first    looked at the design) 
 that the 6 AN5 bolts which connect the wing spar to    the carry-through spar 
 are pretty small and few in number to the task.    There isn't that much overlap 
 between the wing spar and the carry-through    spar to transfer the wing loading 
 to the rest of the structure.
 
 The    commercial designs with which I'm most familiar had more and larger bolts,    
 and in some cases, close-tolerance bolts. There is, as I recall, much more    
 overlap between the spars to allow for reasonable spacing between the    extra 
 bolts.
 
 Is this the problem? Only the results of the various    accident reports will 
 tell. But it could sure cause wing separation, if it    is. 
 ==============================================
 Those who can, do.    Those who can't,    sue.
 ========================
                   Jim B. Belcher
     BS,    MS Physics, math, Computer Science
                      A&P/IA
               Instrument Rated Pilot
      General Radio    Telephone    Certificate
 ===================e the  es  y       -->                 - MATRONICS WEB FORUMS  nbsp;               - List Contribution Web Site  ;                             =========================
 
  | 	  
 
 Plan your next getaway with AOL Travel.  Check out Today's Hot 5 Travel Deals!
   [quote][b]
 
  |  | - The Matronics Zenith601-List Email Forum - |  |   |  Use the List Feature Navigator to browse the many List utilities available such as the Email Subscriptions page, Archive Search & Download, 7-Day Browse, Chat, FAQ, Photoshare, and much more:
 
  http://www.matronics.com/Navigator?Zenith601-List |  
  |  
 
 
 
  
 | 
			 
		  | 
	 
	
		| Back to top | 
		 | 
	 
	
		  | 
	 
	
		craig(at)craigandjean.com Guest
 
 
 
 
 
  | 
		
			
				 Posted: Thu Oct 30, 2008 5:00 pm    Post subject: how to make the wings stronger? | 
				     | 
			 
			
				
  | 
			 
			
				Yeah (as previously mentioned) it is a pretty good fake:  
    
 http://www.avweb.com/blogs/insider/AVwebInsiderBlog_ViralVideo_KillaThrill_LostWingLanding_199096-1.html  
    
 -- Craig  
        
 From: owner-zenith601-list-server(at)matronics.com [mailto:owner-zenith601-list-server(at)matronics.com] On Behalf Of Joemotis(at)aol.com
  Sent: Thursday, October 30, 2008 6:45 PM
  To: zenith601-list(at)matronics.com
  Subject: Re: how to make the wings stronger?  
   
   
      
 Maybe we should learn from this pilot!  
     
    
     
 http://www.youtube.com/watch?v=XRCbkBfdBrQ&eurl=http://www.chilloutzone.de/files/08102703.html  
     
    
     
 This is incredible.   
     
    
     
 Joe Motis  
     
 Do not archive  
       
 In a message dated 10/30/2008 9:17:07 A.M. Pacific Daylight Time, z601(at)anemicaardvark.com writes:  
    	  | Quote: | 	 		    
 --> Zenith601-List message posted by: Jim Belcher <z601(at)anemicaardvark.com>
  
  On Thursday 30 October 2008 08:48, john butterfield wrote:
  
  > I actually tend to believe that most of the wing accidents were caused by
  > pilot error/judgment.  However, not being an engineer, am wondering how one
  > would go about making the wings stronger.  There must be a way we could
  > modify the wing/attaching points or whatever to add a lot of strength to
  > the wing assembly.  
  
  <snip> 
  
  First, let me say I agree with the caution that one cannot change one part of 
  a structure without considering the impact on the rest of the structure. We 
  can't afford to make structural changes to the design, without a lot more 
  information than is available. 
  
  Having said that, it has appeared to me (since I first looked at the design) 
  that the 6 AN5 bolts which connect the wing spar to the carry-through spar 
  are pretty small and few in number to the task. There isn't that much overlap 
  between the wing spar and the carry-through spar to transfer the wing loading 
  to the rest of the structure.
  
  The commercial designs with which I'm most familiar had more and larger bolts, 
  and in some cases, close-tolerance bolts. There is, as I recall, much more 
  overlap between the spars to allow for reasonable spacing between the extra 
  bolts.
  
  Is this the problem? Only the results of the various accident reports will 
  tell. But it could sure cause wing separation, if it is. 
  =====================
  Those who can, do. Those who can't, sue.
  ========================
                 Jim B. Belcher
      BS, MS Physics, math, Computer Science
                    A&P/IA
             Instrument Rated Pilot
       General Radio Telephone Certificate
  ===================e the es y   -->              - MATRONICS WEB FORUMS nbsp;            - List Contribution Web Site ;                         
  
  
     | 	    
   
 
  
          
   
 Plan your next getaway with AOL Travel. Check out Today's Hot 5 Travel Deals!  
    	  | Quote: | 	 		  |   http://www.matronics.com/Navigator?Zenith601-List  | 	  0123456789
        [quote][b]
 
  |  | - The Matronics Zenith601-List Email Forum - |  |   |  Use the List Feature Navigator to browse the many List utilities available such as the Email Subscriptions page, Archive Search & Download, 7-Day Browse, Chat, FAQ, Photoshare, and much more:
 
  http://www.matronics.com/Navigator?Zenith601-List |  
  |  
 
 
 
  
 | 
			 
		  | 
	 
	
		| Back to top | 
		 | 
	 
	
		  | 
	 
	
		Joemotis(at)aol.com Guest
 
 
 
 
 
  | 
		
			
				 Posted: Thu Oct 30, 2008 5:17 pm    Post subject: how to make the wings stronger? | 
				     | 
			 
			
				
  | 
			 
			
				It certainly faked  me out!
   
  Joe Motis
  Do Not Archive
   
   In a message dated 10/30/2008 6:01:02 P.M. Pacific Daylight Time,  craig(at)craigandjean.com writes:
   	  | Quote: | 	 		        
 Yeah    (as previously mentioned) it is a pretty good fake:   
     
 http://www.avweb.com/blogs/insider/AVwebInsiderBlog_ViralVideo_KillaThrill_LostWingLanding_199096-1.html   
     
 --    Craig   
           
 From:    owner-zenith601-list-server(at)matronics.com    [mailto:owner-zenith601-list-server(at)matronics.com] On Behalf Of    Joemotis(at)aol.com
 Sent: Thursday, October 30, 2008 6:45    PM
 To: zenith601-list(at)matronics.com
 Subject: Re:    how to make the wings    stronger?
 
    
        
 Maybe    we should learn from this pilot!
       
  
       
 http://www.youtube.com/watch?v=XRCbkBfdBrQ&eurl=http://www.chilloutzone.de/files/08102703.html
       
  
       
 This    is incredible. 
       
  
       
 Joe    Motis
       
 Do    not archive
          
 In a    message dated 10/30/2008 9:17:07 A.M. Pacific Daylight Time,    z601(at)anemicaardvark.com writes:
     	  | Quote: | 	 		       
 -->      Zenith601-List message posted by: Jim Belcher      <z601(at)anemicaardvark.com>
 
 On Thursday 30 October 2008 08:48,      john butterfield wrote:
 
  	  | Quote: | 	 		   I actually tend to believe that most of      the wing accidents were caused by
  pilot error/judgment.       However, not being an engineer, am wondering how one
  would go about      making the wings stronger.  There must be a way we could
  modify      the wing/attaching points or whatever to add a lot of strength to
       the wing assembly.  
 
 | 	  
 <snip> 
 
 First, let me say I      agree with the caution that one cannot change one part of 
 a structure      without considering the impact on the rest of the structure. We 
 can't      afford to make structural changes to the design, without a lot more      
 information than is available. 
 
 Having said that, it has appeared      to me (since I first looked at the design) 
 that the 6 AN5 bolts which      connect the wing spar to the carry-through spar 
 are pretty small and few      in number to the task. There isn't that much overlap 
 between the wing      spar and the carry-through spar to transfer the wing loading 
 to the rest      of the structure.
 
 The commercial designs with which I'm most familiar      had more and larger bolts, 
 and in some cases, close-tolerance bolts.      There is, as I recall, much more 
 overlap between the spars to allow for      reasonable spacing between the extra 
 bolts.
 
 Is this the problem?      Only the results of the various accident reports will 
 tell. But it could      sure cause wing separation, if it is. 
 =====================
 Those who      can, do. Those who can't, sue.
 ========================
                     Jim B. Belcher
     BS,      MS Physics, math, Computer Science
                        A&P/IA
                 Instrument Rated Pilot
      General Radio      Telephone Certificate
 ===================e the es y   -->                   - MATRONICS WEB FORUMS nbsp;                 - List Contribution Web Site ;                                   
  | 	  
    
             
    
 Plan    your next getaway with AOL Travel. Check    out Today's Hot 5 Travel Deals!
  	  | Quote: | 	 		  |   http://www.matronics.com/Navigator?Zenith601-List  | 	  0123456789
 0 | 	  
 
 Plan your next getaway with AOL Travel.  Check out Today's Hot 5 Travel Deals!
   [quote][b]
 
  |  | - The Matronics Zenith601-List Email Forum - |  |   |  Use the List Feature Navigator to browse the many List utilities available such as the Email Subscriptions page, Archive Search & Download, 7-Day Browse, Chat, FAQ, Photoshare, and much more:
 
  http://www.matronics.com/Navigator?Zenith601-List |  
  |  
 
 
 
  
 | 
			 
		  | 
	 
	
		| Back to top | 
		 | 
	 
	
		  | 
	 
	
		paulrod36(at)msn.com Guest
 
 
 
 
 
  | 
		
			
				 Posted: Thu Oct 30, 2008 6:55 pm    Post subject: how to make the wings stronger? | 
				     | 
			 
			
				
  | 
			 
			
				<?xml:namespace prefix="v" /><?xml:namespace prefix="o" /><![endif]-->  I'm not an engineer, and don't even play one in commercials, but I don't  recall anything surfacing in any of the failures that indicated sheared  through-bolts. 6 AN5's per wing ought to hold several thousand ponds more  then  1320 at 6G's. However, the Dutch report is the first one, I think, to  have mentioned that the spar reinforcements were twisted and bent outside the  wing/fusalage connection. If memory serves, at that point you have two (roughly)  quarter inch by one and a quarter solid aluminum bars, a web of .040 or .060  sheet, and a flange of .040, for top and bottom. All of that is held by driven  rivets (I forget the size) It would be really useful to see pictures of the  failed area. Could the rivets have not been tight? If the rivets didn't do their  job, then the individual units weren't supporting each other, and the  reinforcement bars could have given, one by one. Just a theory........
   
  Paul Rodriguez
  601XL/Corvair
  [quote]   ---
 
  |  | - The Matronics Zenith601-List Email Forum - |  |   |  Use the List Feature Navigator to browse the many List utilities available such as the Email Subscriptions page, Archive Search & Download, 7-Day Browse, Chat, FAQ, Photoshare, and much more:
 
  http://www.matronics.com/Navigator?Zenith601-List |  
  |  
 
 
 
  
 | 
			 
		  | 
	 
	
		| Back to top | 
		 | 
	 
	
		  | 
	 
	
		 | 
	 
 
  
	 
	    
	   | 
	
You cannot post new topics in this forum You cannot reply to topics in this forum You cannot edit your posts in this forum You cannot delete your posts in this forum You cannot vote in polls in this forum You cannot attach files in this forum You can download files in this forum
  | 
   
 
  
Powered by phpBB © 2001, 2005 phpBB Group
  
		 |