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

 

Various tasks completed today.

I ended the last session with some frustration that I could not set the F-724 baggage bulkhead rivets that connect bulkhead to the F-623 corner rib and center bottom skin.

I tried two times and had to drill them out again. The reason for this is that the spacing between the corner rib and bulkhead was just to big. On the other side, there was also a small spacing and I was able to rivet them and the rivet pulled in the tab towards the corner rib. On this side, the gap was just to big.

So yesterday, I finished by making a small shim, dimpled and primed it with a brush.

It's a shitty job to do this now so do yourself a favour and make the shim while all can go appart. In my case the bulkhead was already rivetted and getting the shim in and out was kind of a difficult operation.

Installed the shim and now at least, the spacing is filled. I'll rivet it later on but now I get some help from Cindy and I want to work on the bottom skin.

First installed the center bottom skin stiffeners and squeezed them to the firewall and the F783B cover support ribs.

Only the last cover support rib attach point can not be squeezed and had to be shot with an offset rivet set.

shop heads.

More shop heads on the cover support rib side. Some small denting but nothing to worry about.

Before the bottom skin goes on, you also need to set the connection of the F-902 bulkhead with the F-717 lower longeron.

It's almost impossible to do this when the bottom skin is on so don't forget it. The other side that connects the F-902 to the F-718 upper longeron does not have to be rivetted now. There is a note on DWG23 saying to wait with the top flange until the sup panel structure is drilled.

Before the bottom skin goes on, we need to do one more thing which is sealing the firewall in place with fuel tank sealant.

Yes, black death is back !

The feul tank sealant is put in between side and bottom skin and the firewall itself. The reason for this is to keep the toxic fumes and co out of the cockpit area.

The tank sealant is also used to glue the static ports in place. These can be rivetted on the side wall or glued.

The glueing option looks nicer so decided to go that way. Unfortunatly I didn't think of this earlier so I had to scuff away the primer from the tailcone side skin in order for the sealant to attach to the bare aluminum.

Then after scuffin and cleaning, I prepared a 30gram batch of sealant mixed at 10:1 and applied a layer of sealant on both sides and top of firewall.

It doesn't have to be a thick layer as lots of it would be squeezed out when you put the clecoes in.

Dirty clecoes, shitty mess... my fuel tank building experience is suddenly very vivid again.

Eh voila, all sealed... ready to dry.

I didn't touch the inside but it looked good as it got squeezed out. The spacing is very narrow between those firewall angles and side skin and you would only make a mess if your try to clean that.

 Then glued in the static ports.

 Back view. Play safe and put some tape over the static port opening. Would be hard to get the sealant out there.

It's all ready to dry and rivetting the bottom skin on will be next point on the list.

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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