I jumped ahead to make the clamshell so that I can turn the fuselage over earlier in my building process. I delayed putting the bottom skin on per plan because I need the access space from the bottom to install the Feather Lite leading edge. Now that the LE, ribs and bulkheads, vent lines and tank coating are in place, I can proceed to install the top and bottom skins. Since I am not too keen on the support table (per plan), I decided to turn the fuselage over to micro the bottom skin in place - IF I can turn the fuselage over easily.
I have seen many methods that were used to turn the fuselage over. Some builders used the neighborhood army while others devised a large clamshell rollover structure. The smallest clamshell, I observed, was from Jon Dembs's web site. I decided to follow his idea...
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These clamshells took me 2 evenings to complete. |
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We call it Cozy commitment, don't we? |
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Now I can proceed with the bottom skin (Section 3). |
Preparing Bottom Skin for Glassing
I did not sand the bottom skin flush with the center section spar. Instead, I smoothed out the height difference at the trailing edge of the bottom skin to the center section spar with flox. |
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This approach made the trimming of the UNI easier. However, it distracted my focus and ended up with a BIG lay up error (discussed below)! |
I cut the UNIs (3 layers) with the template for the left wing first. Then I epoxied and peel plied them in place. The UNI fits onto the bottom skin nicely with minimum pulling and tugging. No wrinkles or bubbles...I was happy how it all turned out.
The
next day, I used the right wing template and repeated the glassing and peel ply
process. Half way down the process, I kinda felt that the lay up I was doing,
was not quite the same as yesterdays' - though they should be the same
. I just got that odd feeling that the shape of the UNI pieces
are not the same shape - of course not, I thought to myself, its the left and
right wing! But the lay up schedule are the
same for both wings, I argued. After completing the second wing, I can't wait to
check on the first. ~!@#$, I had the first layer of UNI in the wrong
orientation. Instead of parallel to the leading edge, I had it perpendicular to
the leading edge
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Per Plan, the 3rd layer is a 5" strip along the OD bulkhead. Since I do not have the OD bulkhead, but an end rib. I added a 3rd layer bridging my end rib with rib (R57) with UNI running perpendicular to the fueslage.
Clear Fuel Drain Valve
Notice the 1/32" indentation along the leading edge to accommodate the overlap between the top and bottom layers? |
Fuel Sump
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I
heard many horror stories about the upcoming leak test, I decided to take a
small 'informal' leak test before the big day... At this point of my build, I
already have the bottom skin glassed, outlet piping floxed in, fuel sump glassed
in, fuel drains installed, and inner tank coated with 3 layers of E-Z Poxy. I
decided to add a bit of water in the tank to see if any leak occurs. Both sumps
took almost the same amount of water ~30 oz each. The fuel drain in the sump,
outlet piping and the sump are totally submerged. Then I lower the nose a bit
and added more water onto the fuel tank (my top is not installed yet) such that
the water level covers up the fuel drain at the leading edge. I was pleased
to see that the water pattern on both sides of the tank were quite symmetrical
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I let them sat overnight.
I returned the next morning and found a couple of drips at the temporary termination plug at the fuel line inside the fuselage (right). I realized I only hand tightened them when I installed them. I re-tightened them with a wrench and wiped dry. Then I allowed them to sit overnight again.
All was well the next day - no leak! I was surprised at the amount of fine dust/debris which floated on the top of the water surface. I used my ShopVac with a small suction tube and skimmed off the debris on the top surface. Then I opened up the fuel drain plugs and drained all the water out. I was surprised at the weight of all the water I added to the tanks for this mini test.