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

 

- Going through a rough ride but between the thunderstorms and lightning, I'm trying to get some more work done on the tail section. All parts were primed earlier and now it's rivetting time again. There's quite a bit of rivetting to do on the tail bulkheads, but it's all pretty straightforward and fun. 

First, I started rivetting the F-729B angle to the F-729A bellcrack rib. These days, I'm very lightly sanding my primed pieces with wet sandpaper and it gives a much smoother finish. It also keeps the accumulated gauges of material closer to the prescribed rivet lengths on the plans.

 The easiest way to rivet this was to clamp the part in the vise and squeeze the AD4 rivets with the pneumatic squeezer.

 Nice rivets.

 The F-728B angle and F-728A belcrank rib should not be rivetted yet. 

Next in line is rivetting the F-730 reinforcement plate to the F-706B fuselage bulkhead and the F-729 assembly. Again, the F-728 remains unrivetted.

First clecoed all together including the F-729C angle.

 I had to do some tuning on the opening for the electricity lines and removed a bit to give good clearance for the one-leg MS 21051-L08 nutplate. This isn't indicated on DWG-26 but you'll find it on DWG 29 section A-A and step 2 F747-L/R installation. The side of the nutplate interferes slightly with the belcrank rib F-729 rib flange.

 I did the some for the rivet head as they would be to close to the flange. Here is how it looks like after modification

 little notching also on the F-73 plate for the nutplate.

 started rivetting.

Front side

 

Finished the F-730 reinforment plate rivetting for now.

Then clecoed the whole F-706 fuselage bulkhead together.

Next up is rivetting the F-706A-R side channel to the F-706B bottom bulkhead. This is actually more tricky than it seems. It's imported that both pieces are well clamped.
Watch carefully which holes to rivet. There's only 5 that you should do now.

 Same thing on the other side.

You should not rivet the top side of the bulkhead yet. This will be done later. I knew it and still blew it, so had to remove them again. dumb dumb, but no harm done and holes are still nice.

 Next bulkhead to rivet, F-707. Very easy. Just couple of AD4's that join both sides.

 Nice heads formed with the squeezer.

 Done

 Next in row, F-708 bulkhead. More of the same joining work.

And again, nicely squeezed rivets.

The assembled the F-710. Angle F-710B is rivetted on the F-710 bulkhead.

 

view from the top

View from the front

F-711 requires some more assembly work. Here, we bring F-711 A and B together and attach the F-711 C bars with the F-711D angle.

Don't rivet the bottom 2 holes from the bars yet (will be used to drill the tailwheel fork) and also don't rivet the angle yet.

Clecoed it all together.

That's where I left off on this session. More next time.

 

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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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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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