Hello Michael, I ended up selling my CH750 project and no longer need the engine, it is still bolted to the shipping crate Viking sent it to me on.

Hey Michael,

Thanks! I do still have it. I had to put it on hold for a bit, but will jump back in here shortly. I should be posting more in the near future.

Hi Michael,

I do have a materials list for the CH640.  I had to develop the list myself from the plans, because it did not exist when I started in 2008.  Also, I developed my own part layout drawing for the same reason.

I'm happy to share what I have.  Please contact me directly at scott_stewart@keysight.com.

-Scott

Since I haven't seen the CH640 plans, it's tough to know what kind of brake you'll need. Based on my experience with the STOL CH750, I'd strongly advise against building a Dave brake. He built a 601 with it, and it probably worked okay for that. I broke my Dave brake twice trying to form the upper firewall stiffener, which is .063" and 893mm long. I used a metal piano hinge from Home depot, and the rivet failed the first time. I repaired it with solid rivets and the second failure occurred when the piano hinge metal just stretched away. Even if you use a quality stainless steel hinge from the aircraft materials suppliers, I don't believe it will hold. Other builders have had similar experiences. I built mine 8 feet long, and that wasn't long enough to do my tail section spars (each of the 3 tail spares was almost 9 feet long). I have access to a 10' industrial brake with a modified shoe, so that it bends at a 1/8" (3.2mm) radius. I repaired and modified my Dave brake several times before I could do most of the plane, but it's still not the right brake for the job. I can't bent the thicker fuselage channels and the wing trailing edge skins.

You'll definitely want to look through your entire set of plans and determine what the longest bends are in specific thicknesses.  Around 1000mm of .063 will give you a lot of trouble on a Dave brake. If your spars/spar caps (likely in .040) require long bends, you'll need access to a brake that can handle that. Dan Hill has an excellent video series on building a HomebuiltHELP brake (free plans on their site). I'm assuming the CH640 has a lot of similarly formed components as the CH750. If so, you will have a hard time building a single brake that can do everything. The HomebuiltHELP brake (especially as Dan built it), will do probably 99% of the plane, minus the longest bends. 

The Dave brake is easy to build, but if you're going to scratch-build an airplane, building the HomebuiltHELP brake is an excellent project to start with. When my project is done (I only have a few skins and my cabin interior structures to form), I'm scrapping my entire brake. If/when I start building the CH640, I'll build up a brake similar to the HomebuiltHELP brake, but I'll also have a hydraulic press brake. In another thread, one of the builders  said the longest bends in the CH640 are the spar caps in .040, and they're almost 11 feet long (3218mm)! I am almost certain you will not be able to bend those on a Dave brake. Further, the Dave brake has no adjustable set-back, so you can run into trouble with different thicknesses and bending acute angles with it. If you have access to other brakes regularly, then a Dave brake might work for you. I would check out Dan's brake build series before you commit to a brake, though.

Sorry that was so long, but it's a complicated issue, and I'm planning on doing a video that addresses all of this. I get a lot a brake questions, so a brake video would seem prudent.

Hi Michael,

When I bought the plans, Zenair included a CD with lots of pictures. They also include a very detailed rudder assembly manual which describes the rudder skin drilling.  Did you get this CD?

The idea is that you should lay out the hole pattern on the rudder skin and drill undersize (3/32") rivet holes in the skin. The rudder skeleton should only have centerlines drawn on the spar and rib flanges. You then lay the skin around the skeleton and line up the pieces so you can see the drawn centerlines through the rivet holes. Once everything is aligned, you match drill the rivet holes into the spar and rib flanges, and then drill all holes to full size.

You use this same technique throughout the build: layout and drill undersize holes in the skins, align to center of ribs/spar, final drill assembly.

I made matching right and left blocks for my wing ribs. Every place I needed a forming block, I made two in order to firmly secure the aluminum. For those pieces, like ribs, where I needed to make left and right, I put fluting notches into both blocks. In single pieces, like the firewall, I put fluting notches into just one.

-Scott

Hi Michael,

You will want to make as smooth of a curve through all the points as looks good.  This may require you to offset from the points giving by +/- 1 mm.  The smoothness of the curve is more important than the actual measurements.  The lift performance will not change if the measurements are +/- 2 mm, but the drag will increase if the curve is not smooth.

You will notice on the wing ribs and the curved bulkheads that you will need a little artistry to achieve a good curve, using the numbers provided as only a guide.

-- Scott Stewart

Hi Michael,

Do not use the "~305" dimension they call out on your drawings.  350 +/- 20 is what you want.  I used 350 and this is how it looks completed:

Notice the position of the lightening hole relative to the rivet holes on either side.  If you used 305mm, you would overlap the rivet holes.

-Scott

Hi Michael,

It looks like Zenair revised the drawing.  On mine they showed "~405". I crossed that out and wrote 350.

For the tight Z-bend, you need to cut two matching pieces of wood to use as the forms.  For example, get two 2x4 pieces that are one foot long.  On each one, cut a 3/8-inch step down the full length into half of the long dimension.  The steps on each piece match together.  You then use a vise to smash the aluminum between the two wood form block.  The aluminum will bend around the wood step.

For smaller steps that needed to make later, I welded together two 1/8-inch steel bars shown here:

The aluminum gets pressed between them to form the bend like this:

Hi Michael,

Yes, I am still on the forum.

All in all, my plans build went fairly smoothly.  There were several parts that were dimensioned incorrectly, and I needed to remake them, but there was nothing I could have done differently about wrong dimensions on the plans.  I listed these incorrect dimensions on http://wiki.matronics.com/wiki/index.php/Complete_CH_640_Errata.  Some of the parts they call out are off, like the trim cable is the wrong length.  Also, I had to redesign the flap control a little because Zenith wanted to charge $900 for a $100 linear actuator.

As you progress through the build, keep me updated.  You will need to make or borrow several specialty tools.  For example, I made a series of hole flanging dies for the lightening holes.  You will find that many people are willing to lend out tools like this for serious builders.

Happy building,

Scott

*continued:

I haven't shown a lot of measuring and drilling in my videos. I haven't done a rudder assembly video either, because HomebuiltHelp did theirs. However, my Horizontal Stabilizer video series shows that my skins were pre-marked and drilled before drilling the skeleton underneath using the method I described. I really recommend just to get going on the rudder components and finish the rudder assembly before starting anything else (you'll need a bending brake, though). It really will teach you most of what you need to build the rest of the plane. Hope that helps!

Cheers,

Greg

Okay, we are looking at the same Construction Standards book. From your explanation, you're reading the standards correctly. The small "l" does mean length. However, it sounds like you're a little overly worried about them. In practicality, if you make a 3650mm spar to 3650.5 mm, you're within tolerance. However, it's a simple matter to file off that last .5mm so you are closer to perfect. That particular graph at the top of CS#300 is strictly for shearing and cutting raw stock to length, which says nothing about finish filing or the the width of the stock or spar webs/ribs, etc. You would never want a finished part to be 8mm off over a 1m distance. In the above spar length example, that'd mean your spar could be +/- 28mm!

The other graphs are for things like angle variation tolerances, bend radius tolerances, etc. From a practical fabrication and assembly standpoint, all of those are pretty simple. If you bend an angle to 15 degrees, and it needs to be 16 degrees, you can simply adjust it closer so that it mates properly with whatever surface it needs to mate to. If it is only off by a half a degree or less, it will probably be fine to mate to other surfaces, since most of the metal is thin enough to flex into position. Remember, we're not building rockets or fighter aircraft. In reality, these structures are much easier to build and assemble than they seem at first. I went through the same apprehension too!

For the tolerances we are most worried about as scratch-builders, check out the CH 701 construction manual, which was written with scratch-builders in mind. There really weren't any pre-fabricated kits when it was introduced. Most kits back then were just raw materials kits. At the top of Page 5, look at "Working Tolerances." Tolerances are much more critical on the formed/finished parts, and the 701 standards manual basically sums that up nicely for our needs, even on the 750 and anything else. The big Construction Standards for Zenair Light Airplanes is an awesome reference, packed with great information. However, it goes much further into depth than we really need to build a any of the Zenith airplanes. The most important things are that your mating parts match each other closely (e.g. spar height = rib height, etc.), and that they are not too undersized (weaker structure), and that they are not too oversized (too heavy).

Lastly, for the rudder skin, the way I do skins is NOT how some people like to do them. Some folks like to pre-drill their ribs first and then use strap duplicators to drill the skin holes. I only do that where I absolutely must, which is not very often. My preferred method is to test assemble the undrilled skin to the cleco'd or fully assembled skeleton to make sure it fits. Then I measure the skin for the center-line of each rib flange or spar flange (or whatever else). I take very careful measurements and determine where the rivet line will be on the skin. I then pre-drill the skin with an A3 bit. After that, I mark the center-line of the flanges and other places where the rivet lines are supposed to be on the skeletal structures. I use them line as sight lines through the pre-drilled skin holes to line everything up. Once the sight lines are aligned perfectly to the skin holes, I drill and cleco as I go, usually starting at the spar rivet line. I then go back and final drill for rivets once everything is lined up and cleco'd. This is how the older kits were assembled when you had to do a lot more drilling, but skins were pre-drilled with sight holes. It's a little extra drilling to do it that way, but it works well for me to make sure everything is square and fits together properly. This method is what works best for me, but everyone has their own approach.

I haven't shown a lot of measuring an

Michael, to which manual are you referring? Is it "Construction Standards for Zenair Light Airplanes," Draft Edition: March 22, 2011? Keep in mind, I'm not a professional airplane builder or engineer, so I'll do my best to explain:

In the Zenith 750, tolerances are not depicted in the drawings at all. All of the acceptable tolerances are listed in their construction standards guide, to be applied to the parts as you build them. In the 750 drawings, there is a number in a triangle that's adjacent to the each part number that is circled. That number denotes the revision number of the drawing.

For example, the "2" in the triangle represents the edition of the drawing for that part on the 750:

I'm not sure if I understand what you're looking at, so feel free to post a picture of the part of your plans you're referencing. In the standards book, the variation denoted by the triangle with a subscript number is just what's acceptable from a structural integrity standpoint, and does not factor in how cumulative tolerances can affect the fit of certain assemblies. I've never seen a copy of the 640 plans, so I don't know how different they are. I am planning to do a "How to interpret your blueprints" video in the very near future, and it will cover construction tolerances. Dan's channel covers a little bit about construction tolerances in this video. He and I have a little different opinion on whether or not to form your parts all at once, but his approach ensures a lower likelihood of mistakes and part fitment issues.

I try to make all my parts "perfect," but that's very tough to do. Where tolerances matter most is where parts either have to match together or nest together. An easy example is the wing spar height compared to your rib height. If your hypothetical spar is 100.25mm (within tolerance), and your ribs are 99mm tall (assuming that's within tolerance), then you'll have a height difference of 1.25mm between the two, when they should be as close to equal as possible so your wing skin doesn't wrinkle at that joint. If you have a channel with a doubler channel that nests around it, a height difference of 1mm, though it may be within tolerance, will be less than desirable for proper fitment.

Sorry for the long-winded response, just didn't want to leave anything out. Lastly, I'd call Zenith if you have any doubts about how you're interpreting the plans. They should be very willing to answer any questions you have. I'm happy to help, of course, but they are the last word on their designs.

I believe so.  The newer ch 2000 the rudder is smaller.  The ch 640 has the original size ch 2000 rudder I think... Someone else chime in if I am wrong..

to my understanding yes.