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11-13-2016, 04:13 PM
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Join Date: Dec 2013
Location: NOLA
Posts: 228
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Minimum Edge Distance
While finishing up section 16, I managed to smear one the last 1/8" rivet. I decided to drill it out and replace it, which went as planned. Driving the second rivet, I clinched the tail and now HAD drill out the rivet again.
As the story goes the hole became oblong in the W-1014 aileron hinge bracket assembly only and none of the other sandwhiched layers.
I then decided to upsize the hole to 5/32 to get rid of the oblong hole. Now, the problem is that I am 1/16" short on edge distance. Is 1/16" that critical or should I rebuild the hinge bracket assembly?

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Ryan
RV-14 In-Progress
Build Site
Last edited by ShortSnorter : 11-13-2016 at 04:19 PM.
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11-13-2016, 04:17 PM
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Join Date: May 2012
Location: Harrisburg, Pa
Posts: 759
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Merely my opinion, but edge distance is edge distance. Easier to correct now or once complete and you find a crack in the bracket?
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11-13-2016, 04:18 PM
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Join Date: Oct 2005
Location: Estes Park, CO
Posts: 3,931
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Edge distance
I wouldn't even ask. That's a critical part and probably not very expensive.
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Larry Larson
Estes Park, CO
http://wirejockrv7a.blogspot.com
wirejock at yahoo dot com
Donated 12/03/2019, plus a little extra.
RV-7A #73391, N511RV reserved (2,000+ hours)
HS SB, empennage, tanks, wings, fuse, working finishing kit
Disclaimer
I cannot be, nor will I be, held responsible if you try to do the same things I do and it does not work and/or causes you loss, injury, or even death in the process.
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11-13-2016, 04:40 PM
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Join Date: Dec 2013
Location: NOLA
Posts: 228
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After second thought, even if I rebuilt the hinge bracket, the bottom hole on the bracket would require 5/32" sizing since the underlying double and rear spar are already drilled to 5/32". I guess I shouldn't have been so drill happy 
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Ryan
RV-14 In-Progress
Build Site
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11-14-2016, 08:16 AM
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Join Date: Jan 2007
Location: Battleground
Posts: 4,348
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2x dia. is a rule of thumb. Check the mil specs. You get a little more tolerance than 2x, but it may not solve this issue. If it doesn't, call Van's.
https://www.vansaircraft.com/public/Specs.htm
You are allowed .281 edge margin for non flush rivets, which is a lot closer than .3125 (5/16). I assume these are non flush rivets that go here?
Measure with calipers. You might have what you need.
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Smart People do Stupid things all the time. I know, I've seen me do'em.
RV6 - Builder/Flying
Bucker Jungmann
Fiat G.46 -(restoration in progress, if I have enough life left in me)
RV1 - Proud Pilot.
Last edited by JonJay : 11-14-2016 at 08:19 AM.
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11-14-2016, 04:10 PM
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Join Date: Apr 2009
Location: Stockton, California
Posts: 294
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Are you measuring the distance from the edge of the material to the closest edge of the rivet hole - or from the edge to the center of the rivet?
Check your edge distance rules. Mil STD-403C defines Edge distance as measured from the centerline of the rivet to the edge of the sheet or joint.
For a 5/32 rivet you would need .3125 from the edge. If you have .250 from edge of sheet to edge of hole, your centerline measurement would give an edge distance of .328125"
FWIW
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11-14-2016, 04:34 PM
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Join Date: Dec 2013
Location: NOLA
Posts: 228
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I consulted with the mother ship today and came to the following conclusions:
-Since the aileron hinge brackets come pre drilled with exactly 1/4" edge distance, there would never be enough room to upsize the hole.
-Three options exist:
1) Replace the part along with the entire rear spar
2) Take the bracket off and cut the inner flange off and attempt to replace it with angle.
3) Set the single 5/32" rivet and check periodically after being service
In case anyone was wondering, I am going to opt for option 3.
I did however, order the inboard hinge bracket SB parts, so at least I'll get to drill some rivets out. One thing I learned was that the SB is not required on the outboard brackets due to the way they are mounted (spar and side of the end rib) and there haven't been any reports of issues on the outboard side.
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Ryan
RV-14 In-Progress
Build Site
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