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07-17-2011, 11:07 AM
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Join Date: Jul 2005
Location: Southern California
Posts: 617
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Long bolt trick for rudder pedals
Greetings!
I almost NEVER go off-plans for anything. I'm a systems analyst, not an engineer. BUT after looking at the VAF postings about rudder pedals, I thought I would have a look.
First, spending $50 on four bolts to solve a problem that may not be a problem at all seemed pretty excessive to me.
I saw guys buying steel, aluminum and brass rod, taping it, and bolting it into place as an alternative to bolts but I also saw that as a little excessive.
So, I bought a bit of 3/16" brass rod, cut to size and drilled it for a cotter key. Here is the result.
Can anyone think of ANY reason why the shaft would need to have a nut? (by th way, i used s 5/64 drill to do the hole)
Thanx!

__________________
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David Boeshaar
RV-9A - N18TD (reserved) - Fuselage.
"My greatest fear: What if the hokey pokey really IS what its all about?"
TDAircraft.com
-July-
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07-17-2011, 11:13 AM
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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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My opinion---------looks like it should work fine, it achieves the same effect of using a long bolt, that being getting the pivot axis in line.
My only concern is in a hard braking situation, you are going to put a lot of sheering force on a piece of brass instead of steel.
__________________
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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07-17-2011, 11:41 AM
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Join Date: Oct 2005
Location: 08A
Posts: 9,476
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David,
Off topic observation....all parts get filed or sanded smooth, with rounded edges. It is a metal fatigue issue as well as pride of craftsmanship thing.
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Dan Horton
RV-8 SS
Barrett IO-390
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07-17-2011, 12:22 PM
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Join Date: Jan 2005
Location: 57AZ - NW Tucson area
Posts: 10,011
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Quote:
Originally Posted by Mike S
My opinion---------looks like it should work fine, it achieves the same effect of using a long bolt, that being getting the pivot axis in line.
My only concern is in a hard braking situation, you are going to put a lot of sheering force on a piece of brass instead of steel.
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The shear force is way higher than 500 lbs. so should not be a problem...
Wear from the brass rotating inside the steel tab might be a problem though.
__________________
Gil Alexander
EAA Technical Counselor, Airframe Mechanic
Half completed RV-10 QB purchased
RV-6A N61GX - finally flying
Grumman Tiger N12GA - flying
La Cholla Airpark (57AZ) Tucson AZ
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07-17-2011, 12:24 PM
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Join Date: Jan 2005
Location: SoCal
Posts: 2,061
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Corrosion
I seem to recall that brass and aluminum don't get along well, but I could certainly have it wrong. Engineers, what say you?
__________________
Steve Zicree
Fullerton, Ca. w/beautiful 2.5 year old son 
RV-4 99% built  and sold 
Rag and tube project well under way
paid =VAF= dues through June 2013
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07-17-2011, 12:31 PM
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Join Date: Sep 2007
Location: pittsburgh pa
Posts: 533
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Sorry guys
But I used a length of all thread, appropriately sized, from Home depot aviation stores, stop nutted appropriately.
Maybe not the most craftsman like, but effective, simple and cheap.
PS - I think the brass is fine.
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Gary Reed
RV-6 IO-360
WW 200 RV now an Al Hartzell for improved CG
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07-17-2011, 01:08 PM
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Join Date: Mar 2007
Location: Sonoma County
Posts: 3,821
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Quote:
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Originally Posted by ;559292
But I used a length of all thread, Maybe not the most craftsman like, but effective, simple and cheap.
PS - I think the brass is fine.
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Read post three.................
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07-17-2011, 01:32 PM
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Join Date: Dec 2006
Location: Paso Robles, CA
Posts: 1,177
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Good looking work Dave!
What you have done appears to have been done carefully and with skill. They look great! I can not condone or condemn your efforts from a structural basis. That would be up to a materials engineer to run the numbers and perform physical fatigue tests.
My son is starting his 3 year at Cal Poly San Luis Obispo, and guess what his Major is? Mmmm Materials engineer and and considered a senior already because of all the grades and credits that he has.
He had a great time analyzing the grain structure of some of the bolts from our business.
He wont be back in school until September and unless you are ready to fly that would timely enough to get some results, just for fun.
Just let us know if that interests you. Of course I must ask him first.
Last edited by GAHco : 07-17-2011 at 01:36 PM.
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07-17-2011, 04:35 PM
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Join Date: Jul 2005
Location: Southern California
Posts: 617
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Since this is on the rudder support, it is steel and brass. No aluminum here.
Thanx for the feedback! I love this site!
Quote:
Originally Posted by szicree
I seem to recall that brass and aluminum don't get along well, but I could certainly have it wrong. Engineers, what say you?
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__________________
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David Boeshaar
RV-9A - N18TD (reserved) - Fuselage.
"My greatest fear: What if the hokey pokey really IS what its all about?"
TDAircraft.com
-July-
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07-17-2011, 05:13 PM
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Join Date: Jan 2005
Location: SoCal
Posts: 2,061
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Quote:
Originally Posted by comfortcat
Since this is on the rudder support, it is steel and brass. No aluminum here.
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Um,...what are those angles riveted to the pedals made of? 
__________________
Steve Zicree
Fullerton, Ca. w/beautiful 2.5 year old son 
RV-4 99% built  and sold 
Rag and tube project well under way
paid =VAF= dues through June 2013
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