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  #1  
Old 03-06-2009, 08:47 PM
bobmarkert's Avatar
bobmarkert bobmarkert is offline
 
Join Date: Oct 2007
Location: Littleton, CO
Posts: 388
Default Sigh..... Another spar rib question

I’m now proficient driving 470 rivets attaching the wing ribs to the spar, but the learning curve was painful.

I needed to drill one rivet out and accidentally enlarged the hole both in the spar and rib.

Ken at Vans said to drill a new hole and add a rivet and then put pop rivet in the original hole.

I decided to add a backing plate on the back of the rib to give the pop rivet a tight hole to grip but now I wonder if that was the right decision.

Should I keep this or drill out all the rivets and get a new rib.

Someday I hope to be able to answer some questions instead of just ask them.

Bob

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Last edited by bobmarkert : 03-06-2009 at 08:53 PM.
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  #2  
Old 03-06-2009, 10:18 PM
Norman CYYJ Norman CYYJ is offline
 
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Location: Victoria B.C.
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not worry, continue on.
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  #3  
Old 03-06-2009, 11:12 PM
ignacio ignacio is offline
 
Join Date: Jun 2006
Posts: 61
Default

thats ok, its on the web and not the thick stiffners. one rivet is just fine. from what ive read these just keep the rib from buckling all ther strength is in the skins. if wrong someone please correct me.
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  #4  
Old 03-06-2009, 11:14 PM
asav8tor asav8tor is offline
 
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Location: Seattle, wa
Posts: 679
Default

Once all the skins are on I bet the torsion, shear, and axial load on the subject rivet is very close to . . . . . zero.
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  #5  
Old 03-06-2009, 11:24 PM
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airguy airguy is offline
 
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Location: Garden City, Tx
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Nice fix. Keep going.
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Built an off-plan RV9A with too much fuel and too much HP. Should drop dead any minute now.
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  #6  
Old 03-07-2009, 03:57 AM
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bobmarkert bobmarkert is offline
 
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Back to building wings!!!

Thanks Guys!
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  #7  
Old 03-07-2009, 12:07 PM
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pierre smith pierre smith is offline
 
Join Date: Jan 2005
Location: Louisville, Ga
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Default Actually.....

Quote:
Originally Posted by ignacio View Post
........ from what ive read these just keep the rib from buckling all ther strength is in the skins. if wrong someone please correct me.
The skin provides the lift and that is transferred to the ribs which in turn transfer it to the spars.....not to pick nits but the monocoque structure as a whole, lifts the airplane.

Regards,
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