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

 

Center fuselage is ready to be joined to the aft fuselage.

But before that, a small task needs to be completed. Notching the longerons near the end.

These notches need to be made because the longerons are in the way of the two F-711C vertical bars  which will hold the horizontal stabilizer in place later on in the project.

At first, needed to remove a small part of the end of the longeron, the details are shown on DWG18. Look carefully and measure twice. It's the longerons you are messing with. (read: expensive to replace and ship if you make a mistake)

I highlighted the important numbers for this first step on the drawing below.

first measure 1/2 inch from the inside using a caliper. Then determine the thickness of the angle (1/8") and mark that thickness. At that thickness, measure 19/32".

Be as accurate as possible. The idea of this cut is that the vertical leg of the longeron will sit between the side skin and the last F712 bulkhead. The horizontal part of the longer needs to end at the web of F712 so that the vertical stabilizer main spar can lay flat against F712.

After measuring, I measured the center  point to drill with a 1/4" drill to get a 1/8" radius.

Then, with a very small drill, drilled on the punched location.

Then I gradually opened the pilot hole using a variety of step up sizes until reached the 1/4" size.

Then I took the cutting disc to make a rough cut on the longeron. The longeron is difficult to handle size wise. That's why I decided to take the cutting disc and not use the bandsaw.

After a lot of filing with key files to smoothen things out and sanding it, it looks like he image below.

top view

Next, I needed to go for the second part of the cut that would clear for the F711 C bars.

Look again at the DWG18 details. The important numbers are highlighted in yellow.

To position the cut out, you need to use the part called "aft deck cover"

First measure the dimension shown on the right 2" 5/32 from the end of the longeron and draw a line there. This will be the basis for positioning the aft deck on the longeron.

Now lay aft deck parallel to the side of the longeron and make sure that your line you have just drawn in the middle of the last predrilled hole in the aft deck.

 clamp aft deck on longeron.

Mark the area and make sure to measure 1/8" from the side in order not to cut into the vertical leg.

Again, define the centerpoint for a 3/16" drill leading to a 3/32" radius centered in the cutout area.

Center punched and pilot hole drilled

Enlarged

After this hole was drilled I took the air cutting disc and carefully made one cut to the middle of the hole.

Filed it out until got 3/16" gap and sanded it smooth.

The finished result in the pictures below.

Close-up

That concludes the work on the longeron... now have to do it again on the pilot side longeron.

 

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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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