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601XL main spar question
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sabrina

Joined: 15 Jun 2009
Posts: 170

Posted: Tue Apr 13, 2010 12:36 pm Post subject: 601XL main spar question

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Last edited by sabrina on Fri Jun 25, 2010 9:21 pm; edited 2 times in total

sdthatcher

Joined: 13 Mar 2008
Posts: 91
Location: Port Saint Lucie

Posted: Wed Apr 14, 2010 6:27 am Post subject: Re: 601XL main spar question

Hi Sabrina,



Great to hear you are going forward with your strut idea.  Where did you say you were attaching the fuselage portion of the strut?  And did your calculations show a significant reduction in compression near the root when using the strut?  Sorry my wings are apart in NC and I'm in south Florida working on the center spar so I can't answer your question at this time.  Thanks for your input and innovative ideas.



Scott



 	  Sabrina wrote: 	
		  Hey guysâ€¦  I am about to open up my wings between nose rib 5 and nose rib 6 to install mounts for my external main spar strutsâ€¦.   As I remember, the solid rivets are pitched 40mm on center.



Could someone tell me the actual distance between the driven rivets on the forward side of their main spar? (i.e. the space available on the front spar doublers between rivets)  (As I recall, -5s are used that far outboard, so there is more space than further inboard where -6 rivets were used)



Thank you so much!



Sabrina

_________________
Scott Thatcher, Port Saint Lucie, FL
601XL with Corvair, Registered as E-LSA
N601EL, EAA203 140 hours and not flying currently.

sabrina

Joined: 15 Jun 2009
Posts: 170

Posted: Wed Apr 14, 2010 8:47 am Post subject: Re: 601XL main spar question

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Last edited by sabrina on Fri Jun 25, 2010 9:22 pm; edited 3 times in total

psm(at)att.net
Guest

Posted: Wed Apr 14, 2010 9:11 am Post subject: 601XL main spar question

Hi Sabrina,



I wonder who will do the flight testing on your new airplane design . . .



Paul

XL installing upgrade kit



--

a.f.rupp(at)att.net
Guest

Posted: Wed Apr 14, 2010 9:34 am Post subject: 601XL main spar question

Sabrina,

See attached. The spacing is 40mm along the whole wing except just inboard of rib 6 where the pitch is 20  where the front spar doubler ends 1465 from the root. One extra rivet each side of doubler end.  

Al Rupp

Lake Placid NY

N765AR 601XL



 [quote]  -------------- Original message from "Sabrina" <chicago2paris(at)msn.com>: -------------- 

 

 

 	  Quote: 	
		   --> Zenith-List message posted by: "Sabrina"  

  Hey guysâ€¦  I am about to open up my wings between nose rib 5 and nose rib 6 to  install mounts for my external main spar strutsâ€¦.   As I remember, the solid  

 rivets are pitched 40mm on center. 

  Could someone tell me the actual distance between the driven rivets on the  forward side of their main spar? (i.e. the space available on the front spar  doublers between rivets)  (As I recall, -5s are used that far outboard, so there  

 is more space than further inboard where -6 rivets were used) 

  

 Thank you so much! 

  

 Sabrina 

  

  

  

  

 Read this topic online here: 

  

 http://forums.matronics.com/viewtopic.php?p=294103#294103 

  

  

  

  

  

  

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601XL_Bottom_access_panel_001.jpg

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sabrina

Joined: 15 Jun 2009
Posts: 170

Posted: Wed Apr 14, 2010 10:14 am Post subject: Re: 601XL main spar question

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Last edited by sabrina on Fri Jun 25, 2010 9:23 pm; edited 2 times in total

sabrina

Joined: 15 Jun 2009
Posts: 170

Posted: Wed Apr 14, 2010 10:41 am Post subject: Re: 601XL main spar question

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Last edited by sabrina on Fri Jun 25, 2010 9:23 pm; edited 2 times in total

Afterfxllc(at)aol.com
Guest

Posted: Wed Apr 14, 2010 10:53 am Post subject: 601XL main spar question

The head of rivets and bolts should always be in the direction of flight  whenever possible.

  

 It is much easier to rivet if the head is forward and the bucked end is  aft.

  

 Jeff

  [quote][b]

Afterfxllc(at)aol.com
Guest

Posted: Wed Apr 14, 2010 11:04 am Post subject: 601XL main spar question

Sabrina,

  

 Instead of reinventing the wheel why don't you take a ride in an upgraded  601? I can tell you from doing 4 upgrades from sloppy builds to great  builds that I have found no abnormalities in any of the wings or center  sections. 

  

 When you taxi a upgraded 601 it just feels stronger and is quieter also.  After seeing what I have seen I am convinced we had some kind of catastrophic  failure (most likely flutter) and I think we have corrected the issue and  more.

 We haven't found any smoking guns after dozens of 601's have been torn down  other than elongated holes which would just mean the wing was stressed from over  g's.

  

 This is just my opinion and not intended to start a debate

  

 Jeff

  [quote][b]

a.f.rupp(at)att.net
Guest

Posted: Wed Apr 14, 2010 12:09 pm Post subject: 601XL main spar question

JohnDRead(at)aol.com
Guest

Posted: Wed Apr 14, 2010 12:55 pm Post subject: 601XL main spar question

It would be a good idea for you to read Chris Heintz book then you more  educated on aircraft design than you would like us to think you are  presently. But then since you think you know it all his book might be beneath  you.

  

 Regards, John  Read

 CH701 Colorado

  [quote][b]

sabrina

Joined: 15 Jun 2009
Posts: 170

Posted: Wed Apr 14, 2010 1:27 pm Post subject: Re: 601XL main spar question

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Last edited by sabrina on Fri Jun 25, 2010 9:23 pm; edited 1 time in total

sabrina

Joined: 15 Jun 2009
Posts: 170

Posted: Wed Apr 14, 2010 1:43 pm Post subject: Re: 601XL main spar question

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Last edited by sabrina on Fri Jun 25, 2010 9:24 pm; edited 2 times in total

n801bh(at)netzero.com
Guest

Posted: Wed Apr 14, 2010 2:19 pm Post subject: 601XL main spar question

I know of at least 10 people who would love to read his book........................... 

Unfortunatly they are DEAD... Killed by a CH601XL........ 

Next question please.



Ben Haas

N801BH

www.haaspowerair.com



--------

sabrina

Joined: 15 Jun 2009
Posts: 170

Posted: Wed Apr 14, 2010 2:27 pm Post subject: Re: 601XL main spar question

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Last edited by sabrina on Fri Jun 25, 2010 9:24 pm; edited 1 time in total

sabrina

Joined: 15 Jun 2009
Posts: 170

Posted: Wed Apr 14, 2010 3:04 pm Post subject: Re: 601XL main spar question

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Last edited by sabrina on Fri Jun 25, 2010 9:25 pm; edited 1 time in total

afterfxllc(at)aol.com
Guest

Posted: Wed Apr 14, 2010 4:03 pm Post subject: 601XL main spar question

Sabrina

    

   I haven't seen any hole damage in the 6 aircraft I am working on. I was referring to the people that have reported elongated holes.

    

   And I guess to know if it was + or - G's you would have to know which way the elongation is 

   either up or down.

   Jeff

 

 

   

 

 

   --

n801bh(at)netzero.com
Guest

Posted: Wed Apr 14, 2010 6:58 pm Post subject: 601XL main spar question

I will measure one tomorrow and post it for ya. 

do not archive

Ben Haas

N801BH

www.haaspowerair.com



--------

sabrina

Joined: 15 Jun 2009
Posts: 170

Posted: Wed Apr 14, 2010 7:06 pm Post subject: Re: 601XL main spar question

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Last edited by sabrina on Fri Jun 25, 2010 9:25 pm; edited 1 time in total

n801bh(at)netzero.com
Guest

Posted: Thu Apr 15, 2010 5:39 am Post subject: 601XL main spar question

No Problem ma''am.... Slow people fly slow airplanes. So , me and my 801 are a perfect match.G> 

do not archive

Ben Haas

N801BH

www.haaspowerair.com



--------

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