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

 

To increase the amount of material to be primed in my next batch, I decided to move on the the next step of construction which is the preparation of the aft top skins.

Before the skins can go on, you have to cut the J-stiffeners F-786A-R and L.
These stifferens have been cut to length some time ago and now it's time to cut the sides of so that the last part of the stifferener can slide nicely in the bulkheads.
It's the same process as we needed to do some time back when we worked on the lower and upper fuselage stiffeners.

Marked distance, drilled hole, cut back the sides to the hole with the disc cutter and finished it of with the die grinder and some sanding paper.

 When both are prepared, you draw a centerlin on the top with a pen and position it in place. You don't really have to be worried about the bulkhead positions yet as the aft top skins will pull them in place once clecoed.
Now use some duct tape to fix the location of the stiffeners. (see bottom of picture). Yes, airplanes are constructed using duct tape, ackward isn't it :)

 Then slide the F-775 rear top skin in place and cleco it to the longerons and bulkheads. No need to position the F-709 bulkhead yet at this point.

 Make sure the centerline of the stiffeners is visible over the whole length through the two top lines of the aft skin. Make small adjustments if necessary but make sure the stiffener stays nicely secured in it's position.

 Drilled the intersection of stiffener and F-707 first and then moved on towards the back drilling every 3rd hole. Continuously keep checking the centerline through the holes. Drilled #40.

Check on the inside and the positioning of the holes looks good.

Drilled all the remaining "in between" holes for the stiffeners and clecoed. In the next picture, the stiffeners are drilled.

Then matchdrilled the aft top skin to the F-708 bulkhead  and to the longeron using the #40 reamer.

Do not matchdrill the F707 line yet. This will be matchdrilled when both aft and rear top skin are on.

 Another view from the top after matchdrilling.

Now it's time to position and drill the F-656 gusset plates (small triangular reinforcements) to the F-707 bulkhead. This fixes and reinforces the F-707 in it's final position.
Removed the clecoes to halfway from the bulkheads and peel the skin back so you get access to the longeron and F-707.

Cleco and clamp F-656 in place and matchdrill through the F-707. Then recheck the positioning of the longitudinal line of the F-656 and drilled using an angle drill #30.

 Clecoed the F-7112 aft top skin on to continue the matchdrilling of the forward side.

 Another shot from the side. Looks really nice.

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 !

Social Networking

Share This

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.

JSN Megazine is designed by JoomlaShine.com