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

 

Airplane work is a bit slow at the moment. I'm facing a first dip in the build I guess.

I have been mainly working on the tail cone bulkheads lately. There is a lot of deburring work with tons of small notches and openings that all need to be cleaned nicely. Huge work with little visible progress. In the picture below, I'm deburring one of the halfs of the F707 bulkhead.

On all these bulkheads, you need to make a 5/8" whole for cabling (bottom) and the rudder cable passthrough (sides). 

After carefull measuring, you can pilot drill the hole and then open it up with the step drill.

On the left side bulkhead, you also need to measure for a smaller snap bushing to be opened 7/16inch for a SB437-4 snap bushing. This busing will be used to pass the static air line to the front. The static ports are located around F-708 and need to pass through the tail cone and middle section to the instrument panel in the front.

 All drilled

 Static port passthrough drilled

 To see at least a little bit of progress, I decided to mount all bulkheads on the tail cone floor plate. This will also give me a better understanding of the structure.

Next is F708, same 2 part bulkhead with the same procedure of drilling bushing holes, matchdrilling and static passthrough.

The flanges on this one were so bad and "off" that I decided to already flute them a bit.

This is still very premature as you can only to the final fluting and mating on these when actually matching the skins.

The static ports (that measure static air pressure) are located on the left and right side of the F-708 bulkhead. Two flexible air hosed will lead out of these ports and join somewhere on this bulkhead using a T-connector. To guide the air tube over the bulkhead, we will use some clamps. To attach these clamps, you need to drill these 1/8inch holes on the inside border of the bulkhead equally spaced at 3" 5/16. 

I could do this later, but I figured it's more easy to drill them now than having to crawl in the tail cone to drill once the skin is installed.

 Assembly picture with F-708 in place.

 F-709 is very straightforward. It's only one piece. Just deburring and some fluting for now. This is almost the end of the turledeck.

F-710 has a bit more work to it.
The bulkhead itself only needs deburring, but the top of the bulkhead needs a custom made angle.
'Make From'... here we go again.

F710-B is very simple to make, just cut some angle to length, mark the tapering in and measure after deburring.

Then, mark a centerline on the angle and clamp it with the angle vertex flush with the web of F-710.

Backdrill throught he holes of F-710. Don't drill the top holes now ! This will be the place where the forward side of the horizontal stabilisor connects. 

The full assembly picture with F-710 in place. 

 

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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