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

 

Moving forward in the cabin. Next in line, the seat back rests.

It never occurred to me till now. Actually, Vans moves from the front to the back for the bottom part of the fuselage and then from the back forward for the top and interior parts.
I assembled all parts for the seatbacks and started deburring edges.
You need to cut some various angles to length. It's all pretty clear in the plans on DWG-30.

I decided to start with the F-638 seat back braces. They act like a spacer and support between the seat back and the F-705 bulkhead.

First you need to cut a triangular shape from the side flanges. Its all about weight saving.

Secondly, you cut 4 lightning holes in the web of the brace. Did this on the bench drill with the fly cutter. (God I hate that thing)

All done and ready for next step.

Decided to move on on the top of the seat backs.
Two of the F-736C angles  need to be rounded so that they fit in the top bend of the seat back. See image below.
Moving the angle with it's vertex on the 3M deburr wheel back and forward equally until you get the shape required.

For the side angles to the seat back skin, there are dimensions given on the F-637-L seat back assembly drawing. Clamp the angle to the side and measure.

As this takes a lot of time, and all hole patterns are the same, I decided to copy the holes from one angle to the other.
I drilled everything at #40 to start and will enlarge the holes later once all #40's are drilled and clecoed.

Now clamp the F-637B-L and R angles back in place and use the holes in the angle as pilots to drill the F-637A seatback skin.

For the top one, cleco the angle on the inside when you drill.

Next  is the seat back upper hinge. First you measure the hole pattern on the hinge and drill all the holes except for the two outer holes. Those will be drilled in conjuction with the angle on the side of the seat.

Draw a centerline on the back of the hinge as well. Now clamp the hinge on the seat so that the centerline is visible through the holes you already drilled in the side angles and skin. Measure equal distance left and right.
Vans dimensions don't allow for a lot of edge distance on the hinge for these two holes. I think it would be better to make them just slightly longer so the hinge would almost ready the side of the seat back skin. Now drill those two remaining holes with the side angles as drill guides.

the up-drilled all to #30. These will all be AN470 rivets so no need to dimple anything.

Back to the seat back brace and clamped the hinge parallel and centered to the edge of the seat back.
I agree. you are right, I exagerated a bit on the amount of cleco clamps.

 

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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