Vertical Stabilizer Tip

With the Stabilizer skin match drilled the next thing to do before priming and final riveting is to fit the fiberglass tip to the tip rib.

Having read a few articles on Sonex web sites related to the problems with this task, I expected (and found) that it was not as simple as just slipping the fiberglass tip to the end of the stabilizer and match drilling it.

First, the overall length, particularly the length of the fiberglass that is left hanging past the trailing edge of the stabilizer, should line up with the rudder trailing edge.  While this is purely an aesthetic issue, there is at least one post where the builder installed the tip only to find out after mounting the rudder that the fiberglass tip overhung considerably farther than the rudder.  It was not a “look” I wanted to copy.  The builder ultimately  removed and refit the tip by modifying  it.  His closing comment was that he spent more time fitting  the tip than constructing the vertical stabilizer.

There is a dimension on the plans that shows the trailing edge of the tip should extend 12-5/32″ beyond the edge of the vertical stab.  Not surprisingly, this is equal to the rudder tip to the center of the hinge.  This reference mark was one that I put on the fiberglass tip to avoid it as I tried to fit it.

Below I show that if I did not put the tip rib in place I could install the fiberglass tip and push it far enough forward to obtain the requisite 12-5/32″ overhang.

trailing edge mark showing that fiberglass could be press forward WITHOUT rib in place to the 12-5/32" mark

The initial fitting of the fiberglass tip would slide under the stabilizer skin without the rib in place and actually fit pretty well with regard to the leading edge of the skin fitting tightly with the fiberglass while at the same time having the tip extend the required 12-5/32″.  The fiberglass tip was a bit narrower near the leading edge than the tip rib and therefore would not slide under the skin with the rib clecoed in place.

Tip rib inside fiberglass pushed as far forward as possible. Note the leading edge of the rib corners contact the FG tip and and will slide forward no more. This puts the FG tip about 1/8 – 1/4 too far forward relative to the rib.

I was ready to either cut the fiberglass tip and reshape it to fit the tip or else consider building a narrower tip rib.  I mentioned my dilemma to a friend at work who had a hobby /  side business of building high performance rods and had experience with fiberglass fitting.  He told of a similar story of getting some ground effect fiberglass that fit on one side of the car but not the other and found that he could simple heat the parts with steam and then quickly mount them on the car while still hot and re-mold them to the proper shape.

This, of course, made perfect sense (I had read the issues with fiberglass airframes and the issue with summer heat).  So I used a hot air gun with the rib tip as a form pressing from the inside of the fiberglass tip I heated the outside and with a little care I was able to modify the fiberglass so the rib fit inside it and it fit into place between the skin and the rib.

Below is a shot of the inside of the reformed FG tip after heating with the rib pressed forward into the now wider tip.

Rib inside FG tip after heating and remolding the tip
Completed tip installation with rib in place

Top view of fiberglass without any clecos to bring the skin tight to the fiberglass.  A little pressure will easily close the gap indicating that when riveted it will be a snug fit.

After heating and molding fiberglass to rib and slipping into place under skin it can be seen that the fit is pretty good even without the aid of clecos or rivets

The end result was that it was relatively easy to heat the FG tip and mold it to accommodate the shape of the tip rib so that it could be slide between the skin and rib and still maintain the trailing edge overhang.  I can see that the normal variation in fiberglass dimensions could require more in-depth modifications but using heat to reshape the leading edge of the FG tip was an excellent tool to keep in mind.  While the FG tip needed only 1/8 to 13/16″ of manipulation at the leading edge, this small amount created a very large mounting error at the trailing edge.  The photos might not show this issue particularly well but the change was dramatic with regard to fitting the FG tip.

Return To Empennage – Vertical Stabilizer

Vertical Stablizer Skin

Well, after monkeying around for quite some time we finally resolved some issues we were having with plotting the vertical skin out on paper (1:1 scale) and actually glued it (with 3M 77 spray adhesive) to a piece of 0.025 aluminum, cut, filed and drilled it.   We used a  1″step  drill  bitto create the inside corners and tin snips to cut the sheet out.  Leaving a bit of material to be filed down to the line with a vixen file on the generally straight edges and a half moon round file on the inside corners was the way to go and made it easy to get right up to the edge of the lines the paer layout provided.

Of course the main advantage in plotting the skin out in paper first is to more easliy mark the numerous drill holes and then (as we had done in the fall) wrap the paper around the frame to verify the pilot holes were something close to the center of the ribs.  This along with obtaining a very good layout of the many irregular dimensions as well as getting the layout somewhat symetrical.

The original sheet we plotted and wrapped around the frame was a bit smaller than the design dimensions and so we went through numerous attempts to generate an accurate 1:1 scale plot.  As it turns out, the problem we were having was partly due to the inaccuracy of the plotter but there was a much larger issue to deal with.   Hygroscopic expansion (and contraction) of the paper.

Hygro-what you say?  A large sheet of paper will change by a significant amount in it’s dimensions when moved from high to low humidity environments.  What’s more, it will change with a very short time constant.  Short as in minutes, not hours or days.  We found this by measuring a plot that appeared to be nearly perfect when first generated in an office environment and then after sitting it in a cool garage in a Minnesota winter over night,  found that it had shrunk by 3/16″ over a 36″ length.  We then moved the sheet back to the warm and relatively humid office environment and watched it regain nearly all of it’s lost dimension over a 20 minute period.

We verified this dimensional change with one of the guys in our research lab that happened to have ran an experiment over the last few years to identify this precise phenomenon.  What we were observing agreed very closely with the experimental information that was previously done.

So, we dug out one of the original plots that was pretty close to the correct dimensions when left in the garage overnight and just glued it to the aluminum skin.  Once glued to the aluminim the paper was constrained to the dimension of the aluminum.

Before gluing the paper to the skin, we checked the alignment of the rib frame with the paper and found it to be close in overall dimensions but some of the ribs were slightly off from their design locations.  We marked which side of the line to drill the pilot holes to accommodate the slight misalignment and then verified these adjustments before drilling the skin.

Backlit paper layout skin over frame to show alignment of drill holes

We had previously drilled out an aluminum ruler to be used for drilling hinges and used this as a guide for edge drilling the trailing edge of the skin first.  We verified the location of the holes for the hinge and used the ruler to drill out the trailing edge that would have the hinge attached. We then match drilled the other trailing edge of the skin with the first trailing edge as a pattern.

The gluing of the paper to the aluminum and adjustment of the holes were done on February 7th, 2011 with Tim and I.  It was Superbowel Sunday and we both had places to be so we had to stop work.  I (Dan) did the remainder of the drilling and skin forming shown below the following night…..

At this point the two trailing edges are clecoed together and the skin can be carefully pressed down on the table with a 2×4 (I used a 1×6 instead) to form the leading edge.  With the trailing edges clecoed together it insures that the leading edge is formed in the center of the sheet.

Clecoed and formed skin with 1×6 in background
The above shot shows the trailing edges clecoed together and to the work bench to anchor it while forming.  You don’t have to push real hard and want to make sure you don’t kink the leading edge.  Just kind of gentle encouragement to
Formed leading edge of vertical skin
Formed vertical stabalizer skin when clecoes are released it sits with close to a 90 degree bend

I clamped the sheet to each side and used a sharpie to marke through the skin to the ribs to see how well the holes lined up with the rib centers.

Skin with sharpie dots to identify where holes will be match drilled
Red marks show where match drilled holes will land

I examined all the ribs and found that the match drill alignment was as good as I could have hoped on all ribs and on both sides.

There still is some work to do; Clamp and match drill the ribs, dimple the skin and ribs for flush rivets, prime and assemble the frame, rivet the skin to the frame.  But to a large degree these steps are “busy work” and don’t carry the concern we had prior to bending the skin.

Even though we have the horizontal stabilizer almost to the same point as well as the rudder and elevator almost ready to rivet together, this will be the first completed frame and skin assembly and it is kind of a mile stone from the fact that it represents (when assembled with the rudder) the completion of many of the procedures for scratch building.  There are still many things to do for the first time but having completed this portion is a confidence builder.

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Hoizontal Stab Assembly 2

January 2 and 3, 2010

Tim and I worked for a few hours on the afternoon of January second verifying the layout and beginning the match drilling of the stablizer. I worked a few more hours that evening and then finished a large part of the match drilling with #40 drill the following evening in about an hour (I spent almost the same amount of time documenting what I did….something is wrong with this distribution of actual work vs. documenting…..).

From here it’s updrilling, deburring, dimpling, priming and riveting and then riveting. We have to match drill the skin to the frame at some point and at this point we have not completed this step on either the vertical stablizer or this frame so we have to work this process out.

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Horizontal Stab Assembly 1

Jan 1, 2011

With the table level to provide a good platform for match drilling of the horizontal stablizer, the layout of the ribs and spars are printed on segments of 8-1/2″ x 14″ paper. Two reasons for this. I don’t have a large plotter and the one we’ve used at work for some tests does not reliably produce CAD plots in the down web direction. We understand this to be somewhat normal behavior for plotters as they wear and/or accumulate debris from use. It may be that good full size plots could be produced but that is a project all in itself and using my home laser printer to generate segments (that are very accurate in their small size) and then laying them out and anchoring to the table seems to be an easy way to achieve the same thing.

Layout sheets taped to the table in position for match drilling componentsI used AutoCad to generate the layout sheets because I am familiar with it but just about any CAD program would work. I should try Google Sketch sometime as I suspect it could easily handle a simple task such as this.
Once the table is level and the layout is put in place the piece can be held in place with blocks screwed to the table and clamps. After checking each location and alignment of ribs multiple times the components are match drilled in place.
Horizontal Stabilizer with most ribs match drilled and clecoed with # 40
Closeup of centerline from spar forming process (with brake) now used as alignment line for rib locations
Closeup of rib showing centerline again as well as layout sheet lines. Rib looks off of layout mark due to angle of photo but it is actually in very good agreement with layout.

Return To Empennage – Horizontal Stabilizer

Leveled Workshop Table

Dec 31, 2010

I took some time today to pick up some carriage bolts, nuts and washers and put our rolling 4’x12′ table on level feet so it made a better platform for assembly of the horizontal stablizer. I used scrap pieces of 2×4 and 2×6 about a foot long, drilled a 7/16″ hole in the end and screwed a 3″ long 1/2″ carriage bolt into the bottom with a washer and a stop nut.

1/2″ carriage bolt with washer and stop nut screwed into 2×6 to be anchored to side of table for leveling feet (total 10 added to 4′ x 12′ table)
One of 10 leveling feet for table anchored to side of table at floor and sitting on scrap 2×4 pad

Rudder Warp Fix

As mentioned, assembly of the rudder was moving along fine until it became apparent that the ruddder was not “square” with the world. My (Dan’s) thought is that this issue is somewhat easy to avoid but just as easy to fall into if you are not careful. The bottom line is that the rudder structure, like the wings, elevators, ailerons and flaps are thin ridgid structures that are expected to be “straight” when assembled. The geometry of the shape suggests that drilling the holes for assembly needs to be done carefully so as not to create a potato chip (warped wing) affect with the final product. A first order analysis of a 3 dimensional box shows how sensative the final shape is to the initial dimensions. If the one leg of a 2-1/2″ x 37″ rectangle is extended by 1/16″ the resulting shape (a rhombus) when coupled to a 3 dimensional assembly will be forced to satisfy the simultaneous relationship of each perspective side. If you attempt to adjust one perspective into a particular orthoganal alignment it will affect one or both of the other associated perspective views. Since the sheet dimensions are fixed (it is unlikely you will distort the sheet in its “x and y” dimensions) the sheet must accommodate the change by shifting in the “Z” dimension. How far will the part move in the Z dimension? A first order guess would be if the long side of a 2″ x 32″ rectangle is adjusted by 1/16″ the far end will raise by the ratio of 32/2 or 16 times the 1/16″ which is a full 1″.

All of this is somewhat accademic but points out what I mentioned to Tim in an E-mail that, while it is important to measure, mark and cut parts as close as possible, it is the assembly process and “rigging” of each part during assembly that defines the “trueness” of the plane. In other words, you can produce precision ribs and spars for the wings, for instance but when the skin is attached to the wing it is very easy to imagine (for me anyway) how the wing could be “warped” and just as easy to imagine how a slightly less than perfect wing structure could be properly rigged when the skin is match drilled to the ribs to obtain a straight wing.

Slight correction of rudder along the hinge which fixed the really ugly rudder

This relatively small adjustment in the match drilling, shown above, was responsible for a rudder that was close to an inch out of “plane” (no pun intended) when sitting on a flat table surface. The cause was the slightly out of square original sheet that was bent into the basic shape and then held in edge alignment through the trimming and assembly process.

The correction was not large and the slight offset in the otherwise very perfect rudder was absorbed when up-drilling to the #30 bit size. A close call and a very valuable lesson.

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Horizontal Stab Layout

December 24th. 2010:

The components for the horizontal stabilizer have been completed over the last few months and it is now time to match drill and assemble these.

Horz Stab parts laid out with elevator with small printouts on paper

Shown above are the horizontal stabilizer ribs and spars before match drilling. On the opposite side of the table are the elevator skins, ribs and root ribs with the elevator horn ready for assembly.

This step in building is one of those points where you can see things moving fast and of course, it can be the point where mistakes can be costly. I try to keep in mind that mistakes will be made and they can always be corrected, it’s just a matter of being as careful and deliberate as you can so as not to rush into anything and reduce all the previous work into a collection of aluminum scrap. By the same token, it is important not to be paralyzed by fear of making a mistake. The only way to avoid making any mistakes is to do nothing.

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Elevator Trimming

December 24th, 2010 (2 hours)

Trimming the elevators, like the rudder that they share the same control surface basic shape with (Z03-01) needs to be done with some care but after you do the first one the process should go pretty fast. Tim layed our elevators out while I was matchdrilling the rudder. As I realized the rudder was skewed after assembly all construction was halted and we found ourselves struggling to understand what went wrong. As described in the “Rudder Fix” page, the correction was straight forward as was the plan to avoid this problem is the future.

The day after I corrected the rudder I re-marked the elevators after checking them for square and cut them to size. The procedure is pretty easy.

1) Insure your table surface is flat (not necessarilly level but being level in two dimensions is an easy way to insure it is flat). and press your elvator flat to the table.

2) Trim the square end of the elevator so it is actually square. This will be the datum (reference) for the angle cut and needs to form a right angle with the bent edges of the elevator.

This small error in the elevator skin will raise heck with the final product…fix it now
After trimming for square the elevator shows square in vertical and on the table

2) Clamp the elevator with the proper 2-1/4″ height at the widest point (see SNX Z03-01). We used cleco clamps to hold the elevators in this position and found that marking the overlapped surface when the shape is in the correct spot helps, since re-measuring them every time you take the clamp off is not an efficient way to proceed.

3) Mark the angle at the root end of the elevator. You can lament over this step (like Tim did) for along time but my plan is to simple cut the part slightly long and then trim with a vixen file to the final size to correct for any errors in marking. Since Tim had the parts already marked I simply had to confirm his marks and make any adjustments.

Close up showing cleco clamp and re-marked angle end of elevator after other end was trimmed square

4) Cut the bent edges of the sheet metal with a band saw with the cleco clamps still holding it. We had a piece of wood that we slipped inside the elevator that was cut to an approximation of the final shape but I found that it was useful for the next step (file with vixen) it was not that critical during band saw cutting.

5) Finish cutting the large areas of the elevator skin with large snips and file completed cut to where they were marked with a vixen file.

One other thing to note, small variations in the root rib assembly (one of our root ribs that was clecoed to the elevator horn showed a slight curve when clecoed to the horn) will tend to create an imperfect hinge line along the back of the elevator assembly. Match drilling the root ribs assembly to the elevator skins might be best delayed until the horizontal stabilizer is ready to be mated with the elevator. This way the hinges can get properly aligned and any small adjustment in the attachment of the root ribs to the skins can be done without producing any latent (embedded) strain in the elevator / horizontal stabilizer asssembly.

Trimmed and filed elevator skins laid out with root horn

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Rudder Assembly and Warp

Match drilled rudder to ribs and hinge….found it was slightly skewed from original cutout and bend and never corrected.  OK, maybe more than slightly skewed.  About 1 inch potato chip shape.  No way to fix this easily without making it look like it was in an accident. Can salvage horn without ribs and hinge.  Can use the skin for other sheet metal parts (ribs, etc.).  If this is like the elevator spar I can make all the parts over again in a fraction of the time it took to do the first time.  Maybe one day, 8 hours from beginning to end if all goes well

Return To Empennage – Rudder