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  #1  
Old 11-13-2016, 04:13 PM
ShortSnorter ShortSnorter is offline
 
Join Date: Dec 2013
Location: NOLA
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Default 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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Last edited by ShortSnorter : 11-13-2016 at 04:19 PM.
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  #2  
Old 11-13-2016, 04:17 PM
60av8tor 60av8tor is offline
 
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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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  #3  
Old 11-13-2016, 04:18 PM
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wirejock wirejock is offline
 
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Default Edge distance

I wouldn't even ask. That's a critical part and probably not very expensive.
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  #4  
Old 11-13-2016, 04:40 PM
ShortSnorter ShortSnorter is offline
 
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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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  #5  
Old 11-14-2016, 08:16 AM
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JonJay JonJay is offline
 
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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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Last edited by JonJay : 11-14-2016 at 08:19 AM.
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  #6  
Old 11-14-2016, 04:10 PM
Marc Bourget Marc Bourget is offline
 
Join Date: Apr 2009
Location: Stockton, California
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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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  #7  
Old 11-14-2016, 04:34 PM
ShortSnorter ShortSnorter is offline
 
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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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