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

 

In this session, I countersunk some remaining drilled holes.

4 of them are located in the bottom flange of the F704A. If you dimpled the skin before - which you obviously did - then the remaining undimpled ones are the ones you are looking for.
To cross check, count the holes on DWG28 (bottom left).

The holes to be countersunk are the ones where the bottom floor stiffeners meet the F704A.

I was a bit confused at first since I saw lot of different ways of doing this on builder sites. Some people countersink through bottom skin into the F704A.

The correct procedure is however described on DWG28 on the top in section B-B :

Note that the arrows only point to the centerbottom skin and the F704A flange.

It clearly states to countersink through F776 and F704A. That means that you first take the F772 forward bottom skin off before you countersink. Then you countersink the center bottom skin in assembly with F704A.

The F772 forward bottom skin must be dimpled at those locations and nest in the countersinks. (to make sure I verified with VANS support and that's what they do as well).

Here is how it looks without the bottom skin.

That was fairly easy. Next step was to countersink for the screw that goes through the side skin, bottom skin and lower longeron.

This is described in the plans on DWG38.

This is a bit confusing at first because the plans call for a rivet at this location on DWG28 so it's a bit unclear.

Called Vans support with the question if the rivet is indeed a small error on the plan and if I need to follow here the same principle as with the countersinks in the F704.
The answer was that the screw is indeed correct and that countersinking bottom skin and lower longeron, dimpling the side skin is a workable solution.

However they also stated that almost all builder countersink through all 3 parts (side skin F770, forward bottom skin and F717 lower longeron) and that that is also what they do on the quickbuilds.

A small note here: look at the plan below : machine countersink F770 and F717 for screw head). They don't mention the bottom skin here !

Make sure you install the bottom skin before you machine countersink for the screw or you are up for a surprise later.

I took the next picture before I realised something was wrong and the bottom skin needed to be on. This one is just to show you the location of the hole. The clamp will not be possible once the bottom skin is on.

Here is a shot of the left side with the countersink made.

The screw now goes in and sits flush.

 Did the same on the right side with good result

Then continued assembly of all the last parts including longerons and doublers.

Feels good to see her all together again.

Important update 9/12/2018 : This is a great point to final fit the F-7114 fuselage gussets. They are never mentioned in the manual when to install and when you realise you need them, it will be a more difficult fit.
If you read my earlier notes while mating the F-7101, you already edge deburred the F-7114 L and R and checked the fit on the mating with the F-704 wing mount holes and the F7101 gear attach webs. (I started mine when the bottom skin and side skin where already fitted on and had a lot of work getting them in good alignment). Do yourself a favor and fit them again now and matchdrill the 5 AN3 bolt holes through F-7101 and side skin.

Off course... I found some more stuff to do which I missed earlier.
This proofs that it's a good idea to take the time to put it back together again before priming.

Reminder to self:

- last 2 holes on tail cone not dimpled both sides
- check open hole in bottom of tail cone
- trim away part of seat rib at F706 bulkhead
- enlarge hole to 1 inch for fuel line pass through in gear attach doubler both sides

How to use

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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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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