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

 

Today, I started solving some of the issues I encountered earlier with the matchdrilling of the aft fuselage.

When clecoing the aft fuselage back together after dimpling the holes, I realised that it was much easier this time to cleco the aft side together as it was before. Much less stress on the items as before. 

As you may remember from previous articles, I had this misdrilled hole where Sterling from Vans support advised me to dimple as is, but drill two extra #40 support holes on the stiffeners. left and right of the hole.

Here is the pre-picture as is now. the dimpled hole with the misdrill next to it is in the center of stiffener and bulkhead.
In the picture I already marked and centerlined the location for the 2 new holes.

After cleco-ing all together, drilled the extra holes, first using #45, then reaming to #40 to ensure perfect holes.  

Then I checked the rear side of the aft fuselage. Here, the idea was to drill the last row of holes on F712 to #30 because some of the holes were oval.

I contacted vans support also on this issue. After looking at my pictures, they told me that it was not this big of an issue, to leave it alone because the expansion of the rivet shaft would be sufficient to fill the few thousands on the oval hole.

I didn't really like the answer and asked if for them there would be an issue in putting #30 rivets on that location.

They told me that that would be ok, but that they are more difficult to set.

Since I can do these with the pneumatic squeezer, I don't consider this an argument.
I also measured on all sides and found that the aft flange of F712 would still provide sufficient edge distance to host #30 - AD4 rivets.

In the picture below, I started up-drilling the aft flange. First using #34 drill, then reaming with #30 reamer. 

The result was really good. as you will see some pictures below.

Then there were the 3 last holes in the fuselage side skin to aft skin.

This is how it looked like before updrilling.

This is after reaming to #30. Mucho better !

Checked to make sure the edge distance would be fine here to. this is measurement after drilling. The thin red line shows where I measured, the red arrow shows the 0.236 edge distance to the edge of the hole and the yellow arrow shows my calculation of minimum edge distance there (edge to edge of hole 1.5   * 1/8 + 0.03)

Here is an overview of all the up-drilled holes (bronze cleco's)

After the drilling, disassembled the whole thing again and started deburring and dimpling the new holes.

Here a shot of the stiffener at the new holes location.

A shot of the F712 holes after dimpling and updrilling. You can clearly see the difference in quality to the holes I had before.

A shot of the holes in the skin right side

 and left side. Notice the last row (topmost). All #30 and nicely round. This surely gives me a much better feeling.

Dimpled skin for 2 extra holes.

Next, it will be time to scuff and prime the parts.

 

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Use the kit buttons in the top ribbon bar to see a chronological overview per sub section per kit. For the full chronological article list, see chronological build link in prelude menu here below. The easiest way to lookup information is by typing in some part numbers or keywords using the search option in the ribbon bar

 

Caution !

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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Legal Mumbo-Jumbo

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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