My Glasair III Construction Diary - Page 2
By
Roger Halstead
From Midland Michigan


Sunday, April 4th 2000

    Well, again it's been quite a while since I've made any entries in the Diary, but ....I've made lots of progress ... on the new Garage/Shop!
    I've badly needed more room and last fall I started a 28 X 40 foot garage/workshop

    I think my wife was so enthusiastic about the project because it meant she'd be able to get her car back in the garage.
    I had planned on being in the garage last Fall, but unfortunately things seldom go as planned.

    The contractor had planned on a vacation and the floor was to be poured while he was gone. He planned on erecting the structure when he got back  Unfortunately the mason never showed up and when the contractor came to work expecting to start building he only found a pile of sand.

As the building is to be heated with an Infrared heater I insulated the floor from the ground with 1 inch Styrofoam.
    Well, we finally got things ready and poured the concrete, but it was fall. The leaves were falling like crazy and it was getting pretty chilly at night.

    Actually we only ended up with a few "fossils", but the crew was picking up leaves like crazy.
    The Mason finished power trowelling the stuff at 1:00 AM using his pickup truck lights so he could see.

    I've managed to get most of the yard and garden tools on one end with lots of space left over.
I now have the heater, which is one of the new tube type Infrared heaters for hangers and industrial buildings.
    The heater, which is under construction is the long tube on the saw horses. Fortunately it is now hanging from the ceiling.
    The next step is to get the floor sealed and the welding bench finished.

    You can see the Salamander is doing its job and heated the room quite well, down to about 15 degrees that is.

6 hours Thursday April 26th 2000

    The welding bench is now done. Man, but that thing is heavy.
    Unfortunately, I now have to move every thing off the floor so that it can be painted.
    Two reasons for painting the floor. One, It's easier to clean and keeps it from making dust.
    And the second is that it makes it much easier to find those little parts that keep trying to hide after you drop them.

Back to Work

Well, after many projects, lots of tower work, lots of shop work, and I'm now making progress on the G-III
The floor of the shop has three coats of Epoxy paint. The "Hanger Heater" works very well, the airplane *stuff* has been moved in with the exception of the Horizontal Stabilizer which is still on the bench in the basement.

8 hours - Monday, March 26th, 2002

Cutting Bench


Click on photo for larger image

I laid out both halves of the fuselage on rubber pads, set up two shelving units to use as a bench for cutting fiberglass, received two gallons of Resin from the "New Glasair" company, created a template out of 3 mil plastic for the front wing attach point, waxed a portion of the top of my work bench, promoted one gallon of Resin, and then mixed up 100 grams of Resin and catalyst, cut two 2' square pieces of fiberglass cloth and made a practice two layer laminate.
Although I've worked with Epoxy, this is the first large piece I've done using Vinyl Ester Resin. Lots of "Air Bubbles". Time to get in a bunch of practice.

4 hours - Tuesday, March 27th, 2002

As I had a Dentist appointment, I didn't get a lot accomplished today. I cut several pieces of glass cloth to use as reinforcements for the front wing attach point, Mixed 50 grams of resin and did the first lay-up.
I had a few very small voids, but they were not in a spot to cause a problem. I filled these with resin and mixed up another 50 gram batch.
I did two more lay-ups on the reinforcements and also cut the cloth and did the first two layers of the rear wing attach point reinforcement.

6 hours - Wednesday, March 28th 2002

I finished cutting the reinforcements for the front wing attach points, finished all four layers on the right side and did all four on the left in one session. No voids in either. Using a gallon paint can as a template I marked out 12, 7 inch circles (to be used as the center of the reinforcement for the rear wing attach points) on the fiberglass cloth and cut out all 12. I also cut the two pieces to be used for the bottom of the rear attach point for the left side. I mixed the resin and did the bottom two layers for the rear attach point on the left side and 5 of the 6 round center pieces for the right side, wing rear attach point. I then laid up all 6 round pieces for the left side rear wing attach point and the last piece for the right side.

 

Left: Laminating rear attach point.

I also created a template and cut the fiberglass cloth for the Horizontal stabilizer reinforcements. I installed two of the four for each side.

Right: Fiberglass cloth pieces for Horizontal Stabilizer attach point reinforcement

4 hours - Thursday, March 29th 2002

I installed the last of the 4 horizontal stabilizer reinforcements (Total of 4 on each side) and let cure. After about an 8 hour cure, I didn't like the looks of the left side reinforcements in the tail.
I got out the heat gun and peeled all four layers off. The first two came off easy. (Relatively speaking) The second two had cured for over 24 hours and took a bit more persuasion.
I then thoroughly cleaned the area and gave the it a good sanding using coarse "Scotch Brite" (TM) pads.
After vacuuming the area, I gave it a good cleaning with Acetone and then did a single layer lay-up. The last check (3:35 AM) showed no air bubbles or voids. Now, only three more layers to go.
That area has the same look/color and feel as the factory lay-ups and they were vacuum bagged.
Two notes. Removing those layers with the heat gun would make any plastic airplane builder choose a light color paint.( the sun will heat a dark colored plane as hot as that heat gun) It's amazing what heat does to the resin between those layers. The second is that those four layers took a lot more work to remove than they did to install.

Then I had to completely redo the area to prepare it for the new lay-ups.
I had planned on jigging up the fuselage halves and starting the work to mate them on Friday, but it will be Friday evening before the tail reinforcement is finished on the left side, so that has put me back about a day...IF all goes well on Friday.

I shot plenty of pictures so should have some up in a couple of days.

8 hours total Friday, March 30th, 2002

 
Jim Powell stopped by and we mounted the fuselage halves, upside down, on saw horses, hot glued the 41 1/4 inch 2 X 4 brace between the front wing attach points.
 

Right: Installing the 41 1/4 inch brace.


We worked at getting the halves aligned, and came to the conclusion that both halves needed "block sanding" to get a true mating surface.
I remembered having a set of construction videos and decided the week end would be a good time to review them.

6 hours total Monday April 1st, 2002

Jim stopped by around 1:15 again today and we worked on fitting up the two fuselage halves.

Left:  Jim, checking the alignment.

 


 

 

Over the weekend, I studied the manuals and viewed the videotapes on assembling the fuselage. I wish I'd seen them sooner.
They used a plastic template for the lay-up areas. Then he did the lay-ups on the plastic and transferred them to the fuselage area.
They were much neater than my "glue it in place" approach, but the rest he did much the same as we have been.
The manual called for the fuselage halves to fit perfectly...It didn't say anything about the amount of "block sanding" required to make it do so.

 

Right: Fuselage edges needing block sanding.


I had also discovered (over the week end) that I forgot to prep sand the inside of the vertical stabilizer leading edge, so with the block
sanding, we just pulled the tail apart a little farther and I gave those surfaces a good going over with a coarse "ScotchBrite" pad.
When we finished today the mating surfaces look quite good and the tail is close to being straight.
Now I'm headed back out to start on a firewall substitute and clamp to hold the front of the fuselage to the proper shape.
I used the firewall template and carbon paper to transfer the outline to 1/2 inch plywood.
 

Left: Temporary Firewall.

I think I'm going to add a flange and pipe to the plywood to allow easily rotating the fuselage so we can reach some areas more easily.
There are also a lot of mold edges to be removed.

1 hour, Friday April 5th, 2002

Using the firewall template and carbon paper I traced out the firewall onto 1/2 inch plywood.
I then cut out the firewall.
The outer piece of plywood fits around the hull at the cowl flange while the temporary firewall fits just back of that point. I have a bit of trimming to do, but not much.

1 hour Tuesday April 9th, 2002

I did some more trimming on the temporary fire wall and the flange that fits around the front of the hull. Then I cut about a dozen 5" X 1" X 1.5" pieces of wood to hot glue across the back of the hull joint to keep it aligned smooth and flush.
This past week, or so has been a bit slower going, but mainly due to a couple of Dentist appointments.

3 Hours, Tuesday April 16th, 2002

I spent a lot more time sanding and trimming to get the frame to fit around the fuselage at the firewall.

2 Hours, Friday April 21st, 2002

More time block sanding and a bit of time on the books..

3 Hours, Monday April 23rd, 2002

Still more sanding .I ordered the Com antenna which fits near the leading edge of the vertical stabilizer. That is something that should have been installed while the fuselage halves were laying on the floor.

4 Hours, Thursday April 26th, 2002

 
The Com antenna arrived. I block sanded the edges of the forward belly pan and hot glued some pieces of wood at the edges of the belly pan (two on each side) These keep the belly pan from falling down into the fuselage while I work on fitting it to the fuselage.
 

Right:  Front Belly Pan, Right side detail.


3 Hours, Friday April 27th, 2002

Still more block sanding the edges of the fuselage to fit the belly pan. I also did some more trimming on the frame to hold the front of the fuselage and it ended up a bit wider with the belly pan in place. It's going to take still more to get it to fit to the point of being able to hold the fuselage together, rigidly enough to rotate the fuselage.

5 Hours, Thursday April 2nd, 2002

Jim Powell came over and helped prep sand the right, inside of the vertical stabilizer to get it ready for the Com antenna. He cleaned the area with Acetone, while I cut a single strip of cloth from scrap to seal the antenna in. Between the two of us we managed to get the foil antenna in place.

Jim cleaning com antenna area


We then put the fiberglass cloth strip on a plastic sheet and soaked it with resin. The next step was to transfer the strip from the plastic to laying over the antenna....We managed to do it, but it wasn't the neatest installation. The cloth didn't want to stay in position.
At any rate we did get it in place, then using two wood blocks, some plastic sheeting, and two big clamps we clamped the cloth down next to the coax. (The cloth kept wanting to lift around the coax to antenna joint.

Me Prepping Antenna area

Left:  Scrubbing the area where the antenna will mount using a coarse Scotch Brite (TM) pad.
Right:  Clamps and wood blocks used to hold the antenna, wet cloth, and feed line in place while the resin cured.

 

Clamping Detail

Installed Com Antenna

Left:  The antenna layout (running parallel to the leading edge of the vertical stabilizer and the temporary routing of the feed line.

The area on either side of the feed line under the cloth was filled with a medium q-cell mix.


  

Jack Yoder, EAA Tech Advisor Signing inspection sheet

This is probably one of the last photos of Jack, as he was killed in an airplane crash two days later.  Jacks friendship and expertise will sorely be missed by his friends and the homebuilding community.

I trimmed the cloth while in the green state and then mixed up some micro-spheres with resin and filled the space around the coax to give support to the antenna connection. Now it's time to complete sanding the bonding surfaces for the fuselage halves as well as finish fitting the plywood yoke around the front of the fuselage and trim the temporary fire wall to fit. THEN I can finish bonding the halves together. Sure is a lot more work than it would seem.


100 Hours to date...

7 Hours, 17 June, 2002

I cut the temporary fire wall out of a single 4' X 4' piece of 1/2 inch plywood. The outer piece, which remained intact was trimmed slightly to fit around the cowl flange and hold the fuselage in the proper shape.  The temporary firewall was trimmed to fit tightly and inserted inside and behind the cowl flange. 

2 Hours, 18 June, 2002

Both pieces were hot glued into place.

Fuselage bracket (firewall to right)

Interior of fuselage at firewall

    

               

17 Hours, June 20 through June 30, 2002

The next step was to set the fuselage right side up and the tail section on a pad at floor level.  The cabin section was clamped and held in alignment by 6 inch long by 2 inch wide wood strips, hot glued to the outer surface of the fuselage after it was aligned.  In some cases it was necessary to clamp the wood in place to force alignment.  I started at the front and worked back.  If you look carefully at the right hand picture "Underside of clamping", you will see I used two 1 X 2 boards about 8 inches long. There is a piece of 2 X 4 on top of the bottom board. That 2 X 4 fits into the recess between the shells where the 6 layer laminate will go that joins the shells.  On top, the 8 inch board clamps the piece that is hot glued in place, down tight, to hold the shells in alignment.

Behind The Windshield

Between the Doors

 Underside of clamping

The tail section had a wood block fitted between the halves at the rear of the tail.  After twisting the fuselage to align the leading edges of the vertical stabilizer the block was clamped in place. Duct tape was pulled tight around the leading edge of the tail section from both sides, aiding in keeping the two sections aligned.  The same technique was used in the aft section of the fuselage. In one spot a wood block was placed under the tape to force the one side down and into alignment.

Tail Alignment Clamp

Duct Tape holding shells together 

Note the wood block.

     Only two or three wood pieces were hot glued in place at a time. The fuselage was then given time to shift and settle.  It is amazing how the alignment just slowly shifted into place, given enough time.  It looks as if the tail will require very little alignment adjustment when the belly pan is installed. 

3 Hours July 01, 2002

Now that the fuselage has pretty much taken shape, about three more blocks along with 4 on the tail and the fuselage will be ready to invert and bond the halves together. With the heat we've had lately, I'll have to use a new batch of resin without the accelerator, just the promoter.
The current batch has enough accelerator in it that it will set in about 15 minutes with a two layer laminate. Not nearly enough time to make the multiple layer lay-ups to join the fuselage halves, or the leading edge of the vertical stabilizer

View of the alignment blocks down the back seam

Bob Winchester checking out the temporary fire wall

The over all fuselage showing vertical stab alignment blocks

3 Hours July 28, 2002

With the help of Bob Winchester and Joyce, I turned the fuselage upside down.  Leveled the fuselage laterally using the waterline 100 marks. I then used a plumb bob to make certain the tail was in alignment.  I put in one layer of fiberglass down the seam, but pulled it out before it had taken a hard set.  I wasn't happy with the bond and cleaned the whole seam with acetone, re-sanded it and wiped it down with Acetone the second time.

3 Hours July 20, 2002

More prep sanding I did one layer using the older resin that has both the promoter and accelerator.
I really had to hustle. About a 75 gram batch is the limit.  I started with a 100 gram batch, but it started to Gel about 3/4 of the way through. So.... A fast mix of a 75 gram batch did the trick and saved the lay-up.

The left and center photos show the 3 1/2 inch wide fiberglass cloth laid in place. There are already three laminations under it.   A careful examination of the right photo will show the overlap for a seam after the resin has been applied. The ends of the strips coincide with the left end of the orange mark and the dark orange spot about an inch to the right of that.  The overlaps are staggered to prevent an undue thickening of the lay-ups.

6 Hours July 21 2002

First I checked the lay-up and then trimmed the edges. Over the course of the afternoon and evening I did 3 more layers.
I promoted a new batch of resin using only the Cobalt. If I work fast and all goes correctly I can use up a 125 gram batch, but a 100 gram batch is a better compromise. Also the temperature was climbing through the evening and that made for much shorter Gel times. I did get three more layers in down the back joint, for a total of 4 and one more between the windshield and cowl flange.

 

This image shows the tail end of the lay-ups and the antenna mounted inside the vertical stabilizer.  Left is looking toward the tip of the vertical stabilizer. 
 


Just two more layers to go and then it has to set for two days to cure. Then I up-end the fuselage as far as possible and then do the lay-ups in the leading edge of the vertical stabilizer. That is supposed to be the tough one.

It's supposed to be hot and humid Sunday so I doubt I'll be able to get much done on the fuselage, but I can work on the horizontal stab which is jigged up in the basement. I think about 3 more hours and I could have the lay-ups finished. I am going to have to do a bit of trimming along the edge of the joint though.

5 Hours 21 July, 2002

I trimmed the edges of the existing layers and then finished up the last two layers in the long seam.. I also added two more layers to the space between the windshield opening and the back of the cowl.  The Temperature is running near 80 F in the shop now and that is cutting down the working time on the resin.  Even without any accelerator in the resin it still gels in about 15 minutes.  I think for tomorrow at least, I may be working on the tail in the basement. 

I plan on finishing up the last lay-up between the cowl and windshield tomorrow. (It's only 18 inches long by 3 1/2 wide.).  If the lay-ups I finished up today are cured hard enough I plan on block sanding the edges to make the look good.  I think I can do the leading edge of the vertical stabilizer where it sits now.

7 Hours 22 July, 2002

I started on the vertical stabilizer.   I prep sanded the inside of the leading edge, by wrapping a sheet of 80 grit emery cloth around a long piece of 1/2 inch thin wall conduit. and running that back-and-fourth through the channel in the leading edge of the stab.  After vacuuming and blowing out the channel, I forced a cloth soaked with Acetone down through the channel. That did an excellent job of cleaning the  channel, but made the surface far too tacky to try and slide the cloth into place.

I waited a couple of hours and slid the 2 inch wide strip of glass cloth into place.  Being cut on the bias I ended up with a one inch wide strip of cloth almost twice as long<sigh>.  However some judicious work with the half inch thin wall and a very long screw driver I was able to compress the cloth back to the proper dimensions. Using a 1 inch brush hot glued into the end of a three foot length of thin wall (with a slight bend near the end) I was able to reach all the spots in the recess at the leading edge of the vertical stabilizer.

I mixed a 100 gram batch of resin with 1 CC of  MEK.  Using the brush on the extension I was able to soak the cloth and it looked good.

9 hours 23 July, 2002

Well, I decided to try a multiple lay-up, but laying out the cloth on foil, soaking it with resin and then adding a second layer to create two layers and just put them in place. I'd work out the air bubbles from the installation after it was in place. This would allow me to get rid of all the voids between the two layers.  I had the two layers almost in place when they slid off the support and of course, slid around on each other.  I was unable to get them aligned and had to pull them. 

I cleaned up the channel with an acetone soaked cloth as in the earlier prep stages.  A couple hours later I installed the second layer in the conventional manner with little problem.  It looked good and I figured if I stayed up late enough I could get the third layer in.  I finished up on that layer around 3:00 AM.

8 Hours 24 July, 2002

Bad Day!  I went out around 2:00 PM and on inspection I found three large air bubbles/voids. that extended from the center of the seam to nearly the edge of the lay-up and about an inch and a half long.  They were all in the first 1 to 16 inches from the base of the stabilizer.  I thought about grinding off the layer in those spots and using a mill fiber mix, but it turned out that the bubbles were under the second layer.  I wasn't comfortable with that large a cut out and using mill fiber to fix it.

Using a small wood chisel and a long screw driver aided by a 16 ounce ball peen hammer I was able to remove the first foot of the three layers..  Very slow going.

7 Hours 25 July, 2002

Working slowly I was able to sand down the ends of the remaining three layers so I could get a two to three inch overlap with each of the three new layers on the previous layer without creating a large bump in the lay-up.  This was a real good workout for one of the Dremmel tools with the cable extension. I sanded the channel thoroughly with the 80 Grit and conduit as I had before. Then I vacuumed it out and cleaned with acetone.

4 Hours 26 July, 2002

After a little more sanding and a thorough cleaning I installed the first layer with about 3 inches of overlap onto the bottom three layers.

4 hours 27 July, 2002

Around noon I installed the second layer and the third layer around Midnight.  So, I'm now back to about where I was a week ago.

2 Hours 28 July, 2002

The previous work looked very good so I again prep sanded using the 80 grit on the thin wall conduit, vacuumed out and cleaned with acetone. I tried laying out the cloth strip on a piece of wax-paper that had the width lines drawn on it with a large marking pen. Holding onto both ends of the waxed paper I started sliding it down through the channel. It easily slid into place.  I slid the paper back up slightly and using two of the spring loaded clothes pins, clamped the cloth strip to the top of the stabilizer.  I then slowly slid the waxed paper out from under the cloth while keeping the cloth straight without any stretching.  I did have a small amount of repositioning, but not much.  Starting at the top of the stabilizer (the bottom of the lay-up as the fuselage is inverted.  I soaked the cloth and worked my way toward the bottom of the stabilizer.  After about 10 inches I unclipped the clothes pins and made sure that area was well coated with resin.

At 1:30 AM it still looks good, but is not yet firm enough to trim with a cutter.

3 hours 29 July, 2002

I trimmed the previous lamination, prep sanded and cleaned the surface with acetone and put the next lamination (layer #5) in place using the waxed paper.  It took less than 15 minutes for that part of the operation.  I put fans in the windows to cool the shop down during the night.

2 hours 30 July, 2002

Joyce shut the fans off before going on an early bike ride. Unfortunately I didn't get up early enough to close the windows in time to keep the shop cool and it reached near 80 F by evening. I trimmed the ends of lamination #5 and using the same method as above installed layer #6.  The high temperature made me appreciate the waxed paper method of getting the cloth in place.  I was just finishing touching up the lay-up. I was going to add one more spot and discovered the resin in the cup was gelling.  Before I could dump it out, it had hardened too much to remove all of it from the cup.  Fortunately the lay-up looks good.  It's had several hours to set and still looks good.

I had planned on running the fans again tonight, but we are supposed to get some storms, so the windows are going to have to stay closed.

I started fitting the rear belly panel and set the middle one in place for spacing and measurement.  The front one is in place, but the jig holding the front of the airplane needs a bit of sanding in one corner to give the front of the pan a little more room.

Next step will be to fit and glass in the front and rear belly pans

187 hours to date


The says you are caller

If you have comments, suggestions, or corrections email me at EAA Chapter 1093