TitleGarrison

No bird ever flew nonstop from New York to Tokyo, or raced 15 miles high at triple the speed of sound.                                                                                                   
  But birds do something else.
  They do not conquer the air; they romance it.
.”

  Peter Garrison

HoursAndCounting

Jur's RV7 Aircraft Factory
2917 hours
and counting
Some decisions in life are bare of any obvious logic

 

Continued workon drilling the Z-Brackets.

I decided to go the Dan Chekoway method for match drilling the Z-Brackets. The Vans manual tells you to drill all holes, mate, and later elongate the holes if the match is not perfect. I didn't like that idea too much so I have followed the positive stories from other builders on using this alternative technique where the match would be perfect from the first time.

The method is documented very well on many websites so I won't go in too much detail about it here. I found the website of Jason Beaver very helpfull. Here is the article.

First, you need to make a centerline on one side of the z-brackets. For one Z-bracket, make a hole 1/16" shifted from the centerline towards the edg. The idea here is to be able to put a wrench on this bolt head when installing.
For the other 6, shift the hold 1/16" towards the web of the Z-bracket. The idea behind this is to put the holes on the other side a little to the outside too so that you will have better access with the pop rivet tool later to attach the z-brackets to the tank baffle plate.

The picture below shows what I ended up with for the center and outboard z-brackets.
The nutplate can still go on on the other side without being interfered by the web.
Make sure that the hole is very nicely centered or you will have problems with the nutplate ears on the outer holes if you are offsetted.
I am really wondering if the offset neets to be 1/16". It seems a lot and I'm scared that the edge distance of the pop rivets that needs to be .250 on the other side won't be met. I think 1/32 should be enough and would have made me feel more comfortable.

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Important Update 7 Feb 2012:

Don't drill off center. If you do it, go 1/32" or less. In this case, you will end up with 0.200" edge distance from edge of bracket to edge of hole. Nominal would have to be 0.125 * 1.5 = 0.188"

So with 1/32" you would be fine. But I kind of go with another guys remark on the forum: this is a place where you have to modify the tool, not the airplane. Next time I would drill them all just center and see later how to rivet them).

I ended up redoing 2 of the z-brackets where I had 1/16"off leading to 0.178 edge distance. I know I am nitwitting on this, but better be safe then sorry in a piece where later on, it will be almost impossible to redo.

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I'll get back to this  when I really mate and everything is snug in place.

I preliminary layed the baffle plate on the z-brackets after installing them to the spar. I was trying to see where the holes would come out.

For the inboard bracket, the positioning of the top pop rivets looks fine. So there the outboard shift is ok.

 On the inner z-brackets, I find the hole pretty much to the edge. I measured about .230 from the red marking on the flange to the edge where the minimal edge distance for 1/8" rivets should be .250

I contacted Vans about this and here is what Scott had to say about it

Jurgen,  For the 1/8" fasteners/rivets,  your edge distance should be Ok. It's a bit under nominal  but the loads on those rivets are mainly tension and the shear loads would not be much in the direction of the shy e.d.

On the AN3 bolts he said

try to get the AN3 holes close to centerline on the flange.  The flange is narrow enough so that you won't be able to get the nominal 3/8" e.d. recommended for an AN3 bolt even when it's centered.

I'm gonna see what this gives when actually drilling the Z-Brackets to the spar once all is ready and will take a decision then to re-order or replace or not.

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Some advice on reading my log for fellow builders !

In some articles, I made corrections at later date on the original article to rectify my own stupidities or faults. Read through the entire article if you intend to use my findings/experiences on your own project !

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It’s possible (not likely) that I’m not as smart as I think I am. (Occasionally, I have moments when I know this to be true. Fortunately, the feeling passes quickly.) Although I have tried to make this information as accurate as I can, it is not only possible, but also quite likely, that erroneous and misguided information lurks within these pages. I cannot and do not warrant these pages to be error free and correct. Furthermore, I accept no liability for the use of this (mis)information. And, as many would say, your mileage may vary. If, after reading this, you are intent on proceeding, please be aware that the contents of this site are protected by copyright (copyright © 2011 and 2012). Nonetheless, you may copy this material subject to these two conditions: (1) any information used is for non-commercial purposes, and (2) the source of the material is properly credited. Of course, you may link to any page herein. At some articles, snippets of the plans from Vans are visible. These are for educational and illustrations purposes only and should never be used as plans for part construction or assembly as plans may have changed since the picture was taken and more important they are protected by Copyright by the Vans Aircraft Mothership company.

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