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09-24-2008, 01:42 PM
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Join Date: Nov 2006
Location: Waco, Texas
Posts: 1,658
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Nutplate Question
I'm working on some inspection plates and the door is going to be held on with nutplates.
Is there a max and min distance between nutplates?
Thanks,
Phil
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09-24-2008, 01:46 PM
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Senior Curmudgeon
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Join Date: Sep 2005
Location: Dayton Airpark, NV A34
Posts: 15,408
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I dont know the answer, but I am pretty sure you need to provide more info so someone who knows these things can give you an answer.
First off, is the panel going to be structural???
What thickness material??
What size nut plates??
Good luck.
__________________
Mike Starkey
VAF 909
Rv-10, N210LM.
Flying as of 12/4/2010
Phase 1 done, 2/4/2011 
Sold after 240+ wonderful hours of flight.
"Flying the airplane is more important than radioing your plight to a person on the ground incapable of understanding or doing anything about it."
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09-24-2008, 02:04 PM
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Join Date: Nov 2006
Location: Waco, Texas
Posts: 1,658
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Thanks Mike. Here's some additional detail.
Door is .016.
Door Doubler is .032.
It's an exterior door that is exposed to airflow, but not structural.
Nutplates are K1100-06. (#6 - Accepting of dimples)
The actual door is approximately a 4 1/8" square.
Last edited by Phil : 09-24-2008 at 02:06 PM.
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09-24-2008, 03:20 PM
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Join Date: Jul 2005
Location: Hubbard Oregon
Posts: 9,027
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Quote:
Originally Posted by Phil
Thanks Mike. Here's some additional detail.
Door is .016.
Door Doubler is .032.
It's an exterior door that is exposed to airflow, but not structural.
Nutplates are K1100-06. (#6 - Accepting of dimples)
The actual door is approximately a 4 1/8" square.
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Then it is not in any main airframe skin (wing, fuselage, etc.)?
Any opening not made by Van's may have been installed in a location that would be considered structural which means the design of the cover and the fastener pattern would have to be designed to restore the skin to its orig. strength.
__________________
Opinions, information and comments are my own unless stated otherwise. They do not necessarily represent the direction/opinions of my employer.
Scott McDaniels
Van's Aircraft Engineering Prototype Shop Manager
Hubbard, Oregon
RV-6A (aka "Junkyard Special ")
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09-24-2008, 03:25 PM
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Join Date: Nov 2007
Location: Cary, N.C.
Posts: 1,216
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Check out the book "AIRCRAFT SHEET METAL". There are several pages devoted to fabricating, and installing inspection plate with nutplates.
I do not recall all the call outs, but believe that the dimensions scale very well. I think the placement of the nutplates is based on degrees (15, 30, 45,...??) around the cutout, doubler ring, and cover plate.
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09-24-2008, 03:33 PM
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Join Date: Nov 2006
Location: Waco, Texas
Posts: 1,658
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Quote:
Originally Posted by rvbuilder2002
Then it is not in any main airframe skin (wing, fuselage, etc.)?
Any opening not made by Van's may have been installed in a location that would be considered structural which means the design of the cover and the fastener pattern would have to be designed to restore the skin to its orig. strength.
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Good point, Scott.
It's actually on the underside of the elevator.
That's the reason for .016.
Phil
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09-24-2008, 05:05 PM
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Join Date: Jul 2005
Location: Hubbard Oregon
Posts: 9,027
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Quote:
Originally Posted by Phil
Good point, Scott.
It's actually on the underside of the elevator.
That's the reason for .016.
Phil
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In that case, you would probably be fine to copy what is done on the elevator trim cover.
__________________
Opinions, information and comments are my own unless stated otherwise. They do not necessarily represent the direction/opinions of my employer.
Scott McDaniels
Van's Aircraft Engineering Prototype Shop Manager
Hubbard, Oregon
RV-6A (aka "Junkyard Special ")
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