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

 

Another 8 hours on the counter today. Don't you just love the holidays ? I do...

I started the day with the deburring of the read spars HS603PP. Gave them a couple of wacks with the deburr tool, passed them over the scotchbrite wheel and finished them of with 400 gritt sandpaper. Real smooth. I start to have this in my fingers.

Since I could not continue rivetting the HS411 parts because of the priming requirement, I decided to move on to the next step which is the assembly of the front spar of the horizontal stabilo.re is

He is how it works. The front spar has two reinforcement bars: the HS710 and HS714, first you lay them on top of the front spar channels (HS702 flanges down!). So far all is straight and level. 

At that point, you matchdrill the inboard part of the reinforcement spars to #30 drill. The attention point here is not to drill the fuselage attachment points. You only do that when you mount the stabilo to the fuselage. And we are lightyears away from that now.
Difficulty nr 1 is that the spars come as rectangular stock angles and you have to taper them according to the measurements. To be precise, I enlarged the plans by photocopying 133% to 1/1 scale, cut them out and glued the paper template to the material.
I love that HP all-in-one inktjet printer. The picture below shows the status at that point.

Then I removed the excess material from the reinforcement bars.
Difficulty nr 2 with these parts is that once cut, they have to be bent 6° at 5inch 6/32nds from the centerline of the piece.
A lot of measuring and remeasuring is needed here. After drawing the two bend lines, the pieces went into the vise for bending. You do this by hand. Put the material between some aluminum angle pieces on the bend line, make sure the piece sits in a 90° angle and then push and 'feel' the material bend.

I read from many people that they overbend. Overbending means bending back. If you do this too many times, you weaken the material which is not so good if you hear a crack and 7000feet of thin air seperates you from mother earth.
To measure things, I created this cardboard for checking the angle.

The bending went smooth and I was able to push the material couple of degrees at a time without overdoing it to exactly 6°.
I measured it in 3 different ways and in the end I put the pieces on the plans and as you can see, they match perfectly. I was really happy with the achievement as it was one of those jobs where you can easily fuck up.

HS714:

HS710:

Here is the result flat on the table.

Then I started working on the next parts. The HS702's need to be trimmed down. The pieces delivered are measured for an RV8 and the flanges need to be cut down first to the same bend line.

Then you need to make a bend relief notch. I measured for an hour and decided to call it a day to avoid making stupid mistakes because of fatigue. I'll continue tomorrow on those.

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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Legal Mumbo-Jumbo

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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